Started by upstream project "ESP_Beta" build number 710
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...
[WS-CLEANUP] Done
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 '2024-04-27T17:47:59.928 -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 2480
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 '2024-04-27T17:47:59.928 -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 857
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/jenkins11427990155363237133.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=7.6
++ OCCTREF=7.6
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.34.0
++ export PYTHON_VERSION=3.11.6
++ PYTHON_VERSION=3.11.6
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ macys_VM == \r\e\y\n\o\l\d\s ]]
++ [[ DARWIN64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.8/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
++ [[ 7.6 != '' ]]
++ [[ '' != '' ]]
++ [[ macys_VM == *\r\e\y\n\o\l\d\s* ]]
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
+++ [[ -r /usr/local/etc/profile.d/bash_completion.sh ]]
+++ . /usr/local/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
+++ export PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ 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-3.34.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ [[ 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 1975ms
creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv)
added seed packages: pip==24.0, setuptools==69.2.0, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/activate
++ '[' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv
++ '[' darwin20 = cygwin ']'
++ '[' darwin20 = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z '' ']'
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install f90nml
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl.metadata (61 kB)
Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl (20.6 MB)
Installing collected packages: numpy
Successfully installed numpy-1.26.4
+ pip_install openmdao
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
Using cached openmdao-3.31.1-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Requirement already satisfied: numpy in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4)
Collecting scipy (from openmdao)
Using cached scipy-1.13.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB)
Collecting requests (from openmdao)
Using cached requests-2.31.0-py3-none-any.whl.metadata (4.6 kB)
Collecting packaging (from openmdao)
Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB)
Collecting charset-normalizer<4,>=2 (from requests->openmdao)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (33 kB)
Collecting idna<4,>=2.5 (from requests->openmdao)
Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB)
Collecting urllib3<3,>=1.21.1 (from requests->openmdao)
Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached packaging-24.0-py3-none-any.whl (53 kB)
Using cached requests-2.31.0-py3-none-any.whl (62 kB)
Using cached scipy-1.13.0-cp311-cp311-macosx_10_9_x86_64.whl (39.3 MB)
Using cached certifi-2024.2.2-py3-none-any.whl (163 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl (121 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.1-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, scipy, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao
Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.31.1 packaging-24.0 requests-2.31.0 scipy-1.13.0 urllib3-2.2.1
+ [[ macys_VM == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl (13.8 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install matplotlib
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
Using cached matplotlib-3.8.4-cp311-cp311-macosx_10_12_x86_64.whl.metadata (5.8 kB)
Collecting contourpy>=1.0.1 (from matplotlib)
Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.whl.metadata (5.8 kB)
Collecting cycler>=0.10 (from matplotlib)
Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB)
Collecting fonttools>=4.22.0 (from matplotlib)
Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (159 kB)
Collecting kiwisolver>=1.3.1 (from matplotlib)
Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl.metadata (6.4 kB)
Requirement already satisfied: numpy>=1.21 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4)
Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.0)
Collecting pillow>=8 (from matplotlib)
Using cached pillow-10.3.0-cp311-cp311-macosx_10_10_x86_64.whl.metadata (9.2 kB)
Collecting pyparsing>=2.3.1 (from matplotlib)
Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB)
Collecting python-dateutil>=2.7 (from matplotlib)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB)
Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib)
Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB)
Using cached matplotlib-3.8.4-cp311-cp311-macosx_10_12_x86_64.whl (7.6 MB)
Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.whl (262 kB)
Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB)
Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_x86_64.whl (2.3 MB)
Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl (68 kB)
Using cached pillow-10.3.0-cp311-cp311-macosx_10_10_x86_64.whl (3.5 MB)
Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB)
Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.51.0 kiwisolver-1.4.5 matplotlib-3.8.4 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.0)
Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4)
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset UDUNITS2_XML_PATH
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
+ unset AFLR
+ unset AFLR_ARCH
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
--2024-04-27 17:48:53-- 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: 268487989 (256M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’
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5000K .......... .......... .......... .......... .......... 1% 1.90M 74s
5050K .......... .......... .......... .......... .......... 1% 5.96M 74s
5100K .......... .......... .......... .......... .......... 1% 5.73M 74s
5150K .......... .......... .......... .......... .......... 1% 4.67M 74s
5200K .......... .......... .......... .......... .......... 2% 4.48M 73s
5250K .......... .......... .......... .......... .......... 2% 2.30M 74s
5300K .......... .......... .......... .......... .......... 2% 2.45M 74s
5350K .......... .......... .......... .......... .......... 2% 1.53M 75s
5400K .......... .......... .......... .......... .......... 2% 1.94M 75s
5450K .......... .......... .......... .......... .......... 2% 2.02M 76s
5500K .......... .......... .......... .......... .......... 2% 11.2M 75s
5550K .......... .......... .......... .......... .......... 2% 6.23M 75s
5600K .......... .......... .......... .......... .......... 2% 8.47M 74s
5650K .......... .......... .......... .......... .......... 2% 5.83M 74s
5700K .......... .......... .......... .......... .......... 2% 3.79M 74s
5750K .......... .......... .......... .......... .......... 2% 3.73M 74s
5800K .......... .......... .......... .......... .......... 2% 3.05M 74s
5850K .......... .......... .......... .......... .......... 2% 2.65M 74s
5900K .......... .......... .......... .......... .......... 2% 2.32M 75s
5950K .......... .......... .......... .......... .......... 2% 1.66M 75s
6000K .......... .......... .......... .......... .......... 2% 2.15M 75s
6050K .......... .......... .......... .......... .......... 2% 3.66M 75s
6100K .......... .......... .......... .......... .......... 2% 4.56M 75s
6150K .......... .......... .......... .......... .......... 2% 4.08M 75s
6200K .......... .......... .......... .......... .......... 2% 2.98M 75s
6250K .......... .......... .......... .......... .......... 2% 2.29M 75s
6300K .......... .......... .......... .......... .......... 2% 1.52M 76s
6350K .......... .......... .......... .......... .......... 2% 1.19M 77s
6400K .......... .......... .......... .......... .......... 2% 1.92M 78s
6450K .......... .......... .......... .......... .......... 2% 2.27M 78s
6500K .......... .......... .......... .......... .......... 2% 3.68M 78s
6550K .......... .......... .......... .......... .......... 2% 12.2M 77s
6600K .......... .......... .......... .......... .......... 2% 4.69M 77s
6650K .......... .......... .......... .......... .......... 2% 3.99M 77s
6700K .......... .......... .......... .......... .......... 2% 3.71M 77s
6750K .......... .......... .......... .......... .......... 2% 2.30M 77s
6800K .......... .......... .......... .......... .......... 2% 2.82M 77s
6850K .......... .......... .......... .......... .......... 2% 2.63M 77s
6900K .......... .......... .......... .......... .......... 2% 3.75M 77s
6950K .......... .......... .......... .......... .......... 2% 1.87M 77s
7000K .......... .......... .......... .......... .......... 2% 3.03M 78s
7050K .......... .......... .......... .......... .......... 2% 1.68M 78s
7100K .......... .......... .......... .......... .......... 2% 1.49M 79s
7150K .......... .......... .......... .......... .......... 2% 2.85M 79s
7200K .......... .......... .......... .......... .......... 2% 3.81M 79s
7250K .......... .......... .......... .......... .......... 2% 4.70M 78s
7300K .......... .......... .......... .......... .......... 2% 4.59M 78s
7350K .......... .......... .......... .......... .......... 2% 2.88M 78s
7400K .......... .......... .......... .......... .......... 2% 4.62M 78s
7450K .......... .......... .......... .......... .......... 2% 2.65M 78s
7500K .......... .......... .......... .......... .......... 2% 3.01M 78s
7550K .......... .......... .......... .......... .......... 2% 2.57M 78s
7600K .......... .......... .......... .......... .......... 2% 1.98M 79s
7650K .......... .......... .......... .......... .......... 2% 1.46M 79s
7700K .......... .......... .......... .......... .......... 2% 1.64M 80s
7750K .......... .......... .......... .......... .......... 2% 8.57M 79s
7800K .......... .......... .......... .......... .......... 2% 6.61M 79s
7850K .......... .......... .......... .......... .......... 3% 6.36M 79s
7900K .......... .......... .......... .......... .......... 3% 7.36M 78s
7950K .......... .......... .......... .......... .......... 3% 4.01M 78s
8000K .......... .......... .......... .......... .......... 3% 4.57M 78s
8050K .......... .......... .......... .......... .......... 3% 7.69M 78s
8100K .......... .......... .......... .......... .......... 3% 4.03M 78s
8150K .......... .......... .......... .......... .......... 3% 2.55M 78s
8200K .......... .......... .......... .......... .......... 3% 3.54M 78s
8250K .......... .......... .......... .......... .......... 3% 3.00M 78s
8300K .......... .......... .......... .......... .......... 3% 5.93M 78s
8350K .......... .......... .......... .......... .......... 3% 9.55M 77s
8400K .......... .......... .......... .......... .......... 3% 9.28M 77s
8450K .......... .......... .......... .......... .......... 3% 6.00M 77s
8500K .......... .......... .......... .......... .......... 3% 3.80M 77s
8550K .......... .......... .......... .......... .......... 3% 16.5M 76s
8600K .......... .......... .......... .......... .......... 3% 4.01M 76s
8650K .......... .......... .......... .......... .......... 3% 2.64M 76s
8700K .......... .......... .......... .......... .......... 3% 2.29M 76s
8750K .......... .......... .......... .......... .......... 3% 2.05M 77s
8800K .......... .......... .......... .......... .......... 3% 3.67M 77s
8850K .......... .......... .......... .......... .......... 3% 2.30M 77s
8900K .......... .......... .......... .......... .......... 3% 2.30M 77s
8950K .......... .......... .......... .......... .......... 3% 3.06M 77s
9000K .......... .......... .......... .......... .......... 3% 2.16M 77s
9050K .......... .......... .......... .......... .......... 3% 2.63M 77s
9100K .......... .......... .......... .......... .......... 3% 2.86M 77s
9150K .......... .......... .......... .......... .......... 3% 6.84M 77s
9200K .......... .......... .......... .......... .......... 3% 2.62M 77s
9250K .......... .......... .......... .......... .......... 3% 2.93M 77s
9300K .......... .......... .......... .......... .......... 3% 2.47M 77s
9350K .......... .......... .......... .......... .......... 3% 1.52M 78s
9400K .......... .......... .......... .......... .......... 3% 2.96M 78s
9450K .......... .......... .......... .......... .......... 3% 1.13M 78s
9500K .......... .......... .......... .......... .......... 3% 2.04M 79s
9550K .......... .......... .......... .......... .......... 3% 2.77M 79s
9600K .......... .......... .......... .......... .......... 3% 3.24M 79s
9650K .......... .......... .......... .......... .......... 3% 3.42M 78s
9700K .......... .......... .......... .......... .......... 3% 2.01M 79s
9750K .......... .......... .......... .......... .......... 3% 2.46M 79s
9800K .......... .......... .......... .......... .......... 3% 1.38M 79s
9850K .......... .......... .......... .......... .......... 3% 2.16M 79s
9900K .......... .......... .......... .......... .......... 3% 1.82M 80s
9950K .......... .......... .......... .......... .......... 3% 1.74M 80s
10000K .......... .......... .......... .......... .......... 3% 8.86M 80s
10050K .......... .......... .......... .......... .......... 3% 3.29M 80s
10100K .......... .......... .......... .......... .......... 3% 3.28M 80s
10150K .......... .......... .......... .......... .......... 3% 3.77M 80s
10200K .......... .......... .......... .......... .......... 3% 2.11M 80s
10250K .......... .......... .......... .......... .......... 3% 4.34M 80s
10300K .......... .......... .......... .......... .......... 3% 3.59M 80s
10350K .......... .......... .......... .......... .......... 3% 2.28M 80s
10400K .......... .......... .......... .......... .......... 3% 2.83M 80s
10450K .......... .......... .......... .......... .......... 4% 2.98M 80s
10500K .......... .......... .......... .......... .......... 4% 1.94M 80s
10550K .......... .......... .......... .......... .......... 4% 1.50M 80s
10600K .......... .......... .......... .......... .......... 4% 1.50M 81s
10650K .......... .......... .......... .......... .......... 4% 2.47M 81s
10700K .......... .......... .......... .......... .......... 4% 5.00M 81s
10750K .......... .......... .......... .......... .......... 4% 6.18M 80s
10800K .......... .......... .......... .......... .......... 4% 4.63M 80s
10850K .......... .......... .......... .......... .......... 4% 1.98M 80s
10900K .......... .......... .......... .......... .......... 4% 2.64M 80s
10950K .......... .......... .......... .......... .......... 4% 200K 86s
11000K .......... .......... .......... .......... .......... 4% 1.67M 86s
11050K .......... .......... .......... .......... .......... 4% 2.42M 86s
11100K .......... .......... .......... .......... .......... 4% 1.95M 86s
11150K .......... .......... .......... .......... .......... 4% 2.06M 86s
11200K .......... .......... .......... .......... .......... 4% 1.53M 87s
11250K .......... .......... .......... .......... .......... 4% 2.12M 87s
11300K .......... .......... .......... .......... .......... 4% 1.95M 87s
11350K .......... .......... .......... .......... .......... 4% 1.57M 87s
11400K .......... .......... .......... .......... .......... 4% 1.11M 88s
11450K .......... .......... .......... .......... .......... 4% 1.40M 88s
11500K .......... .......... .......... .......... .......... 4% 2.34M 88s
11550K .......... .......... .......... .......... .......... 4% 6.40M 88s
11600K .......... .......... .......... .......... .......... 4% 5.70M 88s
11650K .......... .......... .......... .......... .......... 4% 6.72M 87s
11700K .......... .......... .......... .......... .......... 4% 3.65M 87s
11750K .......... .......... .......... .......... .......... 4% 4.61M 87s
11800K .......... .......... .......... .......... .......... 4% 4.04M 87s
11850K .......... .......... .......... .......... .......... 4% 2.01M 87s
11900K .......... .......... .......... .......... .......... 4% 2.72M 87s
11950K .......... .......... .......... .......... .......... 4% 2.46M 87s
12000K .......... .......... .......... .......... .......... 4% 6.85M 87s
12050K .......... .......... .......... .......... .......... 4% 3.12M 87s
12100K .......... .......... .......... .......... .......... 4% 1.96M 87s
12150K .......... .......... .......... .......... .......... 4% 1.10M 88s
12200K .......... .......... .......... .......... .......... 4% 1.18M 88s
12250K .......... .......... .......... .......... .......... 4% 2.00M 88s
12300K .......... .......... .......... .......... .......... 4% 43.3M 88s
12350K .......... .......... .......... .......... .......... 4% 41.3M 88s
12400K .......... .......... .......... .......... .......... 4% 7.96M 87s
12450K .......... .......... .......... .......... .......... 4% 3.11M 87s
12500K .......... .......... .......... .......... .......... 4% 2.36M 87s
12550K .......... .......... .......... .......... .......... 4% 2.88M 87s
12600K .......... .......... .......... .......... .......... 4% 2.65M 87s
12650K .......... .......... .......... .......... .......... 4% 3.54M 87s
12700K .......... .......... .......... .......... .......... 4% 3.83M 87s
12750K .......... .......... .......... .......... .......... 4% 4.80M 87s
12800K .......... .......... .......... .......... .......... 4% 3.96M 87s
12850K .......... .......... .......... .......... .......... 4% 3.01M 87s
12900K .......... .......... .......... .......... .......... 4% 4.04M 87s
12950K .......... .......... .......... .......... .......... 4% 2.86M 87s
13000K .......... .......... .......... .......... .......... 4% 4.03M 86s
13050K .......... .......... .......... .......... .......... 4% 1.14M 87s
13100K .......... .......... .......... .......... .......... 5% 1.52M 87s
13150K .......... .......... .......... .......... .......... 5% 2.12M 87s
13200K .......... .......... .......... .......... .......... 5% 2.21M 87s
13250K .......... .......... .......... .......... .......... 5% 3.73M 87s
13300K .......... .......... .......... .......... .......... 5% 3.04M 87s
13350K .......... .......... .......... .......... .......... 5% 2.45M 87s
13400K .......... .......... .......... .......... .......... 5% 3.91M 87s
13450K .......... .......... .......... .......... .......... 5% 1.71M 87s
13500K .......... .......... .......... .......... .......... 5% 3.31M 87s
13550K .......... .......... .......... .......... .......... 5% 464K 89s
13600K .......... .......... .......... .......... .......... 5% 35.6M 89s
13650K .......... .......... .......... .......... .......... 5% 30.5M 88s
13700K .......... .......... .......... .......... .......... 5% 2.22M 88s
13750K .......... .......... .......... .......... .......... 5% 30.6M 88s
13800K .......... .......... .......... .......... .......... 5% 1.45M 88s
13850K .......... .......... .......... .......... .......... 5% 28.4M 88s
13900K .......... .......... .......... .......... .......... 5% 36.3M 88s
13950K .......... .......... .......... .......... .......... 5% 8.21M 87s
14000K .......... .......... .......... .......... .......... 5% 5.15M 87s
14050K .......... .......... .......... .......... .......... 5% 4.09M 87s
14100K .......... .......... .......... .......... .......... 5% 1.83M 87s
14150K .......... .......... .......... .......... .......... 5% 2.60M 87s
14200K .......... .......... .......... .......... .......... 5% 1.83M 87s
14250K .......... .......... .......... .......... .......... 5% 1.88M 88s
14300K .......... .......... .......... .......... .......... 5% 2.05M 88s
14350K .......... .......... .......... .......... .......... 5% 17.8M 87s
14400K .......... .......... .......... .......... .......... 5% 5.54M 87s
14450K .......... .......... .......... .......... .......... 5% 4.62M 87s
14500K .......... .......... .......... .......... .......... 5% 5.18M 87s
14550K .......... .......... .......... .......... .......... 5% 6.10M 87s
14600K .......... .......... .......... .......... .......... 5% 9.59M 87s
14650K .......... .......... .......... .......... .......... 5% 13.5M 86s
14700K .......... .......... .......... .......... .......... 5% 6.83M 86s
14750K .......... .......... .......... .......... .......... 5% 6.48M 86s
14800K .......... .......... .......... .......... .......... 5% 16.9M 86s
14850K .......... .......... .......... .......... .......... 5% 4.64M 85s
14900K .......... .......... .......... .......... .......... 5% 7.47M 85s
14950K .......... .......... .......... .......... .......... 5% 2.30M 85s
15000K .......... .......... .......... .......... .......... 5% 2.79M 85s
15050K .......... .......... .......... .......... .......... 5% 2.75M 85s
15100K .......... .......... .......... .......... .......... 5% 3.18M 85s
15150K .......... .......... .......... .......... .......... 5% 6.17M 85s
15200K .......... .......... .......... .......... .......... 5% 5.97M 85s
15250K .......... .......... .......... .......... .......... 5% 3.66M 85s
15300K .......... .......... .......... .......... .......... 5% 3.00M 85s
15350K .......... .......... .......... .......... .......... 5% 2.22M 85s
15400K .......... .......... .......... .......... .......... 5% 2.67M 85s
15450K .......... .......... .......... .......... .......... 5% 2.59M 85s
15500K .......... .......... .......... .......... .......... 5% 4.06M 85s
15550K .......... .......... .......... .......... .......... 5% 6.02M 85s
15600K .......... .......... .......... .......... .......... 5% 4.27M 85s
15650K .......... .......... .......... .......... .......... 5% 6.10M 84s
15700K .......... .......... .......... .......... .......... 6% 3.34M 84s
15750K .......... .......... .......... .......... .......... 6% 3.62M 84s
15800K .......... .......... .......... .......... .......... 6% 2.68M 84s
15850K .......... .......... .......... .......... .......... 6% 2.08M 84s
15900K .......... .......... .......... .......... .......... 6% 2.48M 84s
15950K .......... .......... .......... .......... .......... 6% 1.95M 84s
16000K .......... .......... .......... .......... .......... 6% 3.62M 84s
16050K .......... .......... .......... .......... .......... 6% 3.39M 84s
16100K .......... .......... .......... .......... .......... 6% 3.02M 84s
16150K .......... .......... .......... .......... .......... 6% 7.56M 84s
16200K .......... .......... .......... .......... .......... 6% 4.50M 84s
16250K .......... .......... .......... .......... .......... 6% 4.19M 84s
16300K .......... .......... .......... .......... .......... 6% 3.37M 84s
16350K .......... .......... .......... .......... .......... 6% 2.82M 84s
16400K .......... .......... .......... .......... .......... 6% 3.32M 84s
16450K .......... .......... .......... .......... .......... 6% 2.31M 84s
16500K .......... .......... .......... .......... .......... 6% 1.96M 84s
16550K .......... .......... .......... .......... .......... 6% 1.83M 84s
16600K .......... .......... .......... .......... .......... 6% 1.92M 84s
16650K .......... .......... .......... .......... .......... 6% 2.84M 84s
16700K .......... .......... .......... .......... .......... 6% 1.99M 84s
16750K .......... .......... .......... .......... .......... 6% 4.63M 84s
16800K .......... .......... .......... .......... .......... 6% 3.67M 84s
16850K .......... .......... .......... .......... .......... 6% 3.54M 84s
16900K .......... .......... .......... .......... .......... 6% 10.6M 84s
16950K .......... .......... .......... .......... .......... 6% 4.80M 84s
17000K .......... .......... .......... .......... .......... 6% 4.80M 84s
17050K .......... .......... .......... .......... .......... 6% 3.71M 83s
17100K .......... .......... .......... .......... .......... 6% 3.13M 83s
17150K .......... .......... .......... .......... .......... 6% 1.89M 84s
17200K .......... .......... .......... .......... .......... 6% 988K 84s
17250K .......... .......... .......... .......... .......... 6% 465K 85s
17300K .......... .......... .......... .......... .......... 6% 62.5M 85s
17350K .......... .......... .......... .......... .......... 6% 1.77M 85s
17400K .......... .......... .......... .......... .......... 6% 976K 86s
17450K .......... .......... .......... .......... .......... 6% 2.02M 86s
17500K .......... .......... .......... .......... .......... 6% 1.87M 86s
17550K .......... .......... .......... .......... .......... 6% 3.27M 86s
17600K .......... .......... .......... .......... .......... 6% 4.81M 86s
17650K .......... .......... .......... .......... .......... 6% 10.2M 85s
17700K .......... .......... .......... .......... .......... 6% 5.85M 85s
17750K .......... .......... .......... .......... .......... 6% 7.60M 85s
17800K .......... .......... .......... .......... .......... 6% 5.08M 85s
17850K .......... .......... .......... .......... .......... 6% 3.89M 85s
17900K .......... .......... .......... .......... .......... 6% 4.59M 85s
17950K .......... .......... .......... .......... .......... 6% 4.66M 85s
18000K .......... .......... .......... .......... .......... 6% 8.55M 84s
18050K .......... .......... .......... .......... .......... 6% 9.59M 84s
18100K .......... .......... .......... .......... .......... 6% 6.23M 84s
18150K .......... .......... .......... .......... .......... 6% 8.07M 84s
18200K .......... .......... .......... .......... .......... 6% 4.06M 84s
18250K .......... .......... .......... .......... .......... 6% 6.20M 84s
18300K .......... .......... .......... .......... .......... 6% 6.12M 84s
18350K .......... .......... .......... .......... .......... 7% 3.68M 84s
18400K .......... .......... .......... .......... .......... 7% 3.09M 84s
18450K .......... .......... .......... .......... .......... 7% 9.46M 83s
18500K .......... .......... .......... .......... .......... 7% 2.45M 83s
18550K .......... .......... .......... .......... .......... 7% 2.70M 83s
18600K .......... .......... .......... .......... .......... 7% 1.86M 83s
18650K .......... .......... .......... .......... .......... 7% 2.04M 84s
18700K .......... .......... .......... .......... .......... 7% 3.69M 83s
18750K .......... .......... .......... .......... .......... 7% 7.22M 83s
18800K .......... .......... .......... .......... .......... 7% 14.2M 83s
18850K .......... .......... .......... .......... .......... 7% 5.71M 83s
18900K .......... .......... .......... .......... .......... 7% 7.20M 83s
18950K .......... .......... .......... .......... .......... 7% 5.09M 83s
19000K .......... .......... .......... .......... .......... 7% 6.48M 83s
19050K .......... .......... .......... .......... .......... 7% 7.12M 82s
19100K .......... .......... .......... .......... .......... 7% 3.92M 82s
19150K .......... .......... .......... .......... .......... 7% 3.35M 82s
19200K .......... .......... .......... .......... .......... 7% 2.36M 82s
19250K .......... .......... .......... .......... .......... 7% 3.19M 82s
19300K .......... .......... .......... .......... .......... 7% 2.23M 82s
19350K .......... .......... .......... .......... .......... 7% 1.56M 83s
19400K .......... .......... .......... .......... .......... 7% 2.05M 83s
19450K .......... .......... .......... .......... .......... 7% 1.20M 83s
19500K .......... .......... .......... .......... .......... 7% 1.48M 83s
19550K .......... .......... .......... .......... .......... 7% 2.69M 83s
19600K .......... .......... .......... .......... .......... 7% 18.1M 83s
19650K .......... .......... .......... .......... .......... 7% 2.94M 83s
19700K .......... .......... .......... .......... .......... 7% 5.41M 83s
19750K .......... .......... .......... .......... .......... 7% 6.36M 83s
19800K .......... .......... .......... .......... .......... 7% 4.56M 82s
19850K .......... .......... .......... .......... .......... 7% 3.76M 82s
19900K .......... .......... .......... .......... .......... 7% 1.79M 83s
19950K .......... .......... .......... .......... .......... 7% 8.57M 82s
20000K .......... .......... .......... .......... .......... 7% 6.09M 82s
20050K .......... .......... .......... .......... .......... 7% 5.22M 82s
20100K .......... .......... .......... .......... .......... 7% 2.50M 82s
20150K .......... .......... .......... .......... .......... 7% 3.06M 82s
20200K .......... .......... .......... .......... .......... 7% 1.93M 82s
20250K .......... .......... .......... .......... .......... 7% 2.30M 82s
20300K .......... .......... .......... .......... .......... 7% 1.42M 82s
20350K .......... .......... .......... .......... .......... 7% 2.04M 83s
20400K .......... .......... .......... .......... .......... 7% 5.17M 82s
20450K .......... .......... .......... .......... .......... 7% 2.16M 82s
20500K .......... .......... .......... .......... .......... 7% 4.66M 82s
20550K .......... .......... .......... .......... .......... 7% 3.36M 82s
20600K .......... .......... .......... .......... .......... 7% 4.60M 82s
20650K .......... .......... .......... .......... .......... 7% 4.59M 82s
20700K .......... .......... .......... .......... .......... 7% 4.63M 82s
20750K .......... .......... .......... .......... .......... 7% 4.60M 82s
20800K .......... .......... .......... .......... .......... 7% 5.43M 82s
20850K .......... .......... .......... .......... .......... 7% 4.62M 82s
20900K .......... .......... .......... .......... .......... 7% 2.00M 82s
20950K .......... .......... .......... .......... .......... 8% 2.90M 82s
21000K .......... .......... .......... .......... .......... 8% 1.25M 82s
21050K .......... .......... .......... .......... .......... 8% 2.48M 82s
21100K .......... .......... .......... .......... .......... 8% 2.46M 82s
21150K .......... .......... .......... .......... .......... 8% 3.99M 82s
21200K .......... .......... .......... .......... .......... 8% 3.40M 82s
21250K .......... .......... .......... .......... .......... 8% 3.65M 82s
21300K .......... .......... .......... .......... .......... 8% 3.79M 82s
21350K .......... .......... .......... .......... .......... 8% 2.92M 82s
21400K .......... .......... .......... .......... .......... 8% 3.61M 82s
21450K .......... .......... .......... .......... .......... 8% 4.61M 82s
21500K .......... .......... .......... .......... .......... 8% 2.85M 82s
21550K .......... .......... .......... .......... .......... 8% 29.4M 81s
21600K .......... .......... .......... .......... .......... 8% 4.82M 81s
21650K .......... .......... .......... .......... .......... 8% 4.89M 81s
21700K .......... .......... .......... .......... .......... 8% 3.41M 81s
21750K .......... .......... .......... .......... .......... 8% 3.60M 81s
21800K .......... .......... .......... .......... .......... 8% 3.46M 81s
21850K .......... .......... .......... .......... .......... 8% 6.89M 81s
21900K .......... .......... .......... .......... .......... 8% 6.41M 81s
21950K .......... .......... .......... .......... .......... 8% 3.75M 81s
22000K .......... .......... .......... .......... .......... 8% 4.65M 81s
22050K .......... .......... .......... .......... .......... 8% 2.10M 81s
22100K .......... .......... .......... .......... .......... 8% 2.46M 81s
22150K .......... .......... .......... .......... .......... 8% 5.18M 81s
22200K .......... .......... .......... .......... .......... 8% 4.76M 81s
22250K .......... .......... .......... .......... .......... 8% 5.45M 81s
22300K .......... .......... .......... .......... .......... 8% 3.52M 80s
22350K .......... .......... .......... .......... .......... 8% 4.28M 80s
22400K .......... .......... .......... .......... .......... 8% 10.6M 80s
22450K .......... .......... .......... .......... .......... 8% 5.42M 80s
22500K .......... .......... .......... .......... .......... 8% 3.49M 80s
22550K .......... .......... .......... .......... .......... 8% 17.5M 80s
22600K .......... .......... .......... .......... .......... 8% 7.03M 80s
22650K .......... .......... .......... .......... .......... 8% 9.09M 80s
22700K .......... .......... .......... .......... .......... 8% 5.32M 80s
22750K .......... .......... .......... .......... .......... 8% 11.4M 79s
22800K .......... .......... .......... .......... .......... 8% 7.05M 79s
22850K .......... .......... .......... .......... .......... 8% 3.35M 79s
22900K .......... .......... .......... .......... .......... 8% 6.06M 79s
22950K .......... .......... .......... .......... .......... 8% 4.48M 79s
23000K .......... .......... .......... .......... .......... 8% 5.30M 79s
23050K .......... .......... .......... .......... .......... 8% 5.90M 79s
23100K .......... .......... .......... .......... .......... 8% 6.97M 79s
23150K .......... .......... .......... .......... .......... 8% 4.27M 79s
23200K .......... .......... .......... .......... .......... 8% 5.44M 79s
23250K .......... .......... .......... .......... .......... 8% 5.29M 79s
23300K .......... .......... .......... .......... .......... 8% 3.94M 78s
23350K .......... .......... .......... .......... .......... 8% 2.54M 78s
23400K .......... .......... .......... .......... .......... 8% 2.11M 79s
23450K .......... .......... .......... .......... .......... 8% 1.91M 79s
23500K .......... .......... .......... .......... .......... 8% 1.74M 79s
23550K .......... .......... .......... .......... .......... 9% 1.55M 79s
23600K .......... .......... .......... .......... .......... 9% 1.85M 79s
23650K .......... .......... .......... .......... .......... 9% 3.69M 79s
23700K .......... .......... .......... .......... .......... 9% 6.58M 79s
23750K .......... .......... .......... .......... .......... 9% 8.92M 79s
23800K .......... .......... .......... .......... .......... 9% 4.28M 79s
23850K .......... .......... .......... .......... .......... 9% 3.41M 79s
23900K .......... .......... .......... .......... .......... 9% 4.56M 78s
23950K .......... .......... .......... .......... .......... 9% 3.12M 78s
24000K .......... .......... .......... .......... .......... 9% 3.32M 78s
24050K .......... .......... .......... .......... .......... 9% 18.3M 78s
24100K .......... .......... .......... .......... .......... 9% 2.47M 78s
24150K .......... .......... .......... .......... .......... 9% 5.95M 78s
24200K .......... .......... .......... .......... .......... 9% 2.47M 78s
24250K .......... .......... .......... .......... .......... 9% 2.83M 78s
24300K .......... .......... .......... .......... .......... 9% 2.42M 78s
24350K .......... .......... .......... .......... .......... 9% 5.30M 78s
24400K .......... .......... .......... .......... .......... 9% 4.44M 78s
24450K .......... .......... .......... .......... .......... 9% 2.51M 78s
24500K .......... .......... .......... .......... .......... 9% 3.10M 78s
24550K .......... .......... .......... .......... .......... 9% 2.64M 78s
24600K .......... .......... .......... .......... .......... 9% 2.11M 78s
24650K .......... .......... .......... .......... .......... 9% 1.85M 78s
24700K .......... .......... .......... .......... .......... 9% 4.42M 78s
24750K .......... .......... .......... .......... .......... 9% 3.46M 78s
24800K .......... .......... .......... .......... .......... 9% 2.44M 78s
24850K .......... .......... .......... .......... .......... 9% 2.07M 78s
24900K .......... .......... .......... .......... .......... 9% 1.87M 78s
24950K .......... .......... .......... .......... .......... 9% 1.85M 78s
25000K .......... .......... .......... .......... .......... 9% 2.65M 78s
25050K .......... .......... .......... .......... .......... 9% 5.07M 78s
25100K .......... .......... .......... .......... .......... 9% 5.41M 78s
25150K .......... .......... .......... .......... .......... 9% 5.16M 78s
25200K .......... .......... .......... .......... .......... 9% 2.87M 78s
25250K .......... .......... .......... .......... .......... 9% 3.75M 78s
25300K .......... .......... .......... .......... .......... 9% 4.76M 78s
25350K .......... .......... .......... .......... .......... 9% 5.83M 78s
25400K .......... .......... .......... .......... .......... 9% 8.06M 78s
25450K .......... .......... .......... .......... .......... 9% 3.76M 78s
25500K .......... .......... .......... .......... .......... 9% 2.79M 78s
25550K .......... .......... .......... .......... .......... 9% 3.14M 78s
25600K .......... .......... .......... .......... .......... 9% 2.95M 78s
25650K .......... .......... .......... .......... .......... 9% 2.64M 78s
25700K .......... .......... .......... .......... .......... 9% 2.30M 78s
25750K .......... .......... .......... .......... .......... 9% 4.12M 78s
25800K .......... .......... .......... .......... .......... 9% 8.49M 77s
25850K .......... .......... .......... .......... .......... 9% 5.19M 77s
25900K .......... .......... .......... .......... .......... 9% 8.78M 77s
25950K .......... .......... .......... .......... .......... 9% 4.12M 77s
26000K .......... .......... .......... .......... .......... 9% 3.42M 77s
26050K .......... .......... .......... .......... .......... 9% 3.22M 77s
26100K .......... .......... .......... .......... .......... 9% 3.30M 77s
26150K .......... .......... .......... .......... .......... 9% 7.24M 77s
26200K .......... .......... .......... .......... .......... 10% 6.35M 77s
26250K .......... .......... .......... .......... .......... 10% 4.11M 77s
26300K .......... .......... .......... .......... .......... 10% 8.76M 77s
26350K .......... .......... .......... .......... .......... 10% 5.57M 77s
26400K .......... .......... .......... .......... .......... 10% 3.77M 77s
26450K .......... .......... .......... .......... .......... 10% 5.23M 77s
26500K .......... .......... .......... .......... .......... 10% 5.57M 76s
26550K .......... .......... .......... .......... .......... 10% 4.62M 76s
26600K .......... .......... .......... .......... .......... 10% 3.09M 76s
26650K .......... .......... .......... .......... .......... 10% 8.01M 76s
26700K .......... .......... .......... .......... .......... 10% 3.60M 76s
26750K .......... .......... .......... .......... .......... 10% 4.11M 76s
26800K .......... .......... .......... .......... .......... 10% 3.03M 76s
26850K .......... .......... .......... .......... .......... 10% 2.07M 76s
26900K .......... .......... .......... .......... .......... 10% 3.39M 76s
26950K .......... .......... .......... .......... .......... 10% 6.36M 76s
27000K .......... .......... .......... .......... .......... 10% 17.8M 76s
27050K .......... .......... .......... .......... .......... 10% 10.5M 76s
27100K .......... .......... .......... .......... .......... 10% 6.05M 76s
27150K .......... .......... .......... .......... .......... 10% 32.3M 76s
27200K .......... .......... .......... .......... .......... 10% 7.24M 76s
27250K .......... .......... .......... .......... .......... 10% 6.81M 75s
27300K .......... .......... .......... .......... .......... 10% 8.30M 75s
27350K .......... .......... .......... .......... .......... 10% 6.82M 75s
27400K .......... .......... .......... .......... .......... 10% 206K 77s
27450K .......... .......... .......... .......... .......... 10% 1.80M 77s
27500K .......... .......... .......... .......... .......... 10% 20.1M 77s
27550K .......... .......... .......... .......... .......... 10% 8.49M 77s
27600K .......... .......... .......... .......... .......... 10% 3.17M 77s
27650K .......... .......... .......... .......... .......... 10% 83.8M 77s
27700K .......... .......... .......... .......... .......... 10% 4.90M 77s
27750K .......... .......... .......... .......... .......... 10% 5.15M 77s
27800K .......... .......... .......... .......... .......... 10% 3.63M 77s
27850K .......... .......... .......... .......... .......... 10% 2.90M 77s
27900K .......... .......... .......... .......... .......... 10% 2.71M 77s
27950K .......... .......... .......... .......... .......... 10% 2.05M 77s
28000K .......... .......... .......... .......... .......... 10% 1.98M 77s
28050K .......... .......... .......... .......... .......... 10% 1.72M 77s
28100K .......... .......... .......... .......... .......... 10% 1.76M 77s
28150K .......... .......... .......... .......... .......... 10% 3.12M 77s
28200K .......... .......... .......... .......... .......... 10% 6.00M 77s
28250K .......... .......... .......... .......... .......... 10% 9.18M 77s
28300K .......... .......... .......... .......... .......... 10% 8.40M 77s
28350K .......... .......... .......... .......... .......... 10% 5.62M 76s
28400K .......... .......... .......... .......... .......... 10% 6.27M 76s
28450K .......... .......... .......... .......... .......... 10% 2.65M 76s
28500K .......... .......... .......... .......... .......... 10% 2.87M 76s
28550K .......... .......... .......... .......... .......... 10% 4.01M 76s
28600K .......... .......... .......... .......... .......... 10% 1.54M 76s
28650K .......... .......... .......... .......... .......... 10% 1.74M 77s
28700K .......... .......... .......... .......... .......... 10% 5.25M 76s
28750K .......... .......... .......... .......... .......... 10% 7.82M 76s
28800K .......... .......... .......... .......... .......... 11% 6.35M 76s
28850K .......... .......... .......... .......... .......... 11% 4.48M 76s
28900K .......... .......... .......... .......... .......... 11% 2.06M 76s
28950K .......... .......... .......... .......... .......... 11% 1.76M 76s
29000K .......... .......... .......... .......... .......... 11% 1.95M 76s
29050K .......... .......... .......... .......... .......... 11% 2.00M 76s
29100K .......... .......... .......... .......... .......... 11% 1.58M 77s
29150K .......... .......... .......... .......... .......... 11% 1.38M 77s
29200K .......... .......... .......... .......... .......... 11% 1.78M 77s
29250K .......... .......... .......... .......... .......... 11% 11.4M 77s
29300K .......... .......... .......... .......... .......... 11% 4.16M 77s
29350K .......... .......... .......... .......... .......... 11% 5.41M 76s
29400K .......... .......... .......... .......... .......... 11% 3.18M 76s
29450K .......... .......... .......... .......... .......... 11% 2.91M 76s
29500K .......... .......... .......... .......... .......... 11% 1.91M 76s
29550K .......... .......... .......... .......... .......... 11% 1.95M 77s
29600K .......... .......... .......... .......... .......... 11% 1.79M 77s
29650K .......... .......... .......... .......... .......... 11% 7.39M 77s
29700K .......... .......... .......... .......... .......... 11% 4.66M 76s
29750K .......... .......... .......... .......... .......... 11% 14.6M 76s
29800K .......... .......... .......... .......... .......... 11% 4.03M 76s
29850K .......... .......... .......... .......... .......... 11% 2.68M 76s
29900K .......... .......... .......... .......... .......... 11% 5.73M 76s
29950K .......... .......... .......... .......... .......... 11% 2.85M 76s
30000K .......... .......... .......... .......... .......... 11% 2.68M 76s
30050K .......... .......... .......... .......... .......... 11% 4.02M 76s
30100K .......... .......... .......... .......... .......... 11% 4.25M 76s
30150K .......... .......... .......... .......... .......... 11% 95.6M 76s
30200K .......... .......... .......... .......... .......... 11% 5.21M 76s
30250K .......... .......... .......... .......... .......... 11% 9.31M 76s
30300K .......... .......... .......... .......... .......... 11% 3.72M 76s
30350K .......... .......... .......... .......... .......... 11% 2.61M 76s
30400K .......... .......... .......... .......... .......... 11% 5.10M 76s
30450K .......... .......... .......... .......... .......... 11% 2.68M 76s
30500K .......... .......... .......... .......... .......... 11% 4.15M 76s
30550K .......... .......... .......... .......... .......... 11% 4.08M 76s
30600K .......... .......... .......... .......... .......... 11% 11.4M 75s
30650K .......... .......... .......... .......... .......... 11% 4.09M 75s
30700K .......... .......... .......... .......... .......... 11% 3.46M 75s
30750K .......... .......... .......... .......... .......... 11% 4.98M 75s
30800K .......... .......... .......... .......... .......... 11% 3.82M 75s
30850K .......... .......... .......... .......... .......... 11% 3.76M 75s
30900K .......... .......... .......... .......... .......... 11% 5.33M 75s
30950K .......... .......... .......... .......... .......... 11% 9.61M 75s
31000K .......... .......... .......... .......... .......... 11% 5.31M 75s
31050K .......... .......... .......... .......... .......... 11% 11.2M 75s
31100K .......... .......... .......... .......... .......... 11% 7.92M 75s
31150K .......... .......... .......... .......... .......... 11% 5.00M 75s
31200K .......... .......... .......... .......... .......... 11% 2.91M 75s
31250K .......... .......... .......... .......... .......... 11% 4.02M 75s
31300K .......... .......... .......... .......... .......... 11% 4.50M 75s
31350K .......... .......... .......... .......... .......... 11% 4.80M 75s
31400K .......... .......... .......... .......... .......... 11% 17.6M 74s
31450K .......... .......... .......... .......... .......... 12% 5.16M 74s
31500K .......... .......... .......... .......... .......... 12% 8.69M 74s
31550K .......... .......... .......... .......... .......... 12% 7.40M 74s
31600K .......... .......... .......... .......... .......... 12% 4.60M 74s
31650K .......... .......... .......... .......... .......... 12% 4.05M 74s
31700K .......... .......... .......... .......... .......... 12% 2.77M 74s
31750K .......... .......... .......... .......... .......... 12% 4.01M 74s
31800K .......... .......... .......... .......... .......... 12% 1.97M 74s
31850K .......... .......... .......... .......... .......... 12% 1.15M 74s
31900K .......... .......... .......... .......... .......... 12% 1.20M 74s
31950K .......... .......... .......... .......... .......... 12% 941K 75s
32000K .......... .......... .......... .......... .......... 12% 2.82M 75s
32050K .......... .......... .......... .......... .......... 12% 5.27M 75s
32100K .......... .......... .......... .......... .......... 12% 3.34M 75s
32150K .......... .......... .......... .......... .......... 12% 8.80M 74s
32200K .......... .......... .......... .......... .......... 12% 8.26M 74s
32250K .......... .......... .......... .......... .......... 12% 9.56M 74s
32300K .......... .......... .......... .......... .......... 12% 3.81M 74s
32350K .......... .......... .......... .......... .......... 12% 4.78M 74s
32400K .......... .......... .......... .......... .......... 12% 5.29M 74s
32450K .......... .......... .......... .......... .......... 12% 3.96M 74s
32500K .......... .......... .......... .......... .......... 12% 2.78M 74s
32550K .......... .......... .......... .......... .......... 12% 3.38M 74s
32600K .......... .......... .......... .......... .......... 12% 2.85M 74s
32650K .......... .......... .......... .......... .......... 12% 2.75M 74s
32700K .......... .......... .......... .......... .......... 12% 6.14M 74s
32750K .......... .......... .......... .......... .......... 12% 3.86M 74s
32800K .......... .......... .......... .......... .......... 12% 43.6M 74s
32850K .......... .......... .......... .......... .......... 12% 2.85M 74s
32900K .......... .......... .......... .......... .......... 12% 3.42M 74s
32950K .......... .......... .......... .......... .......... 12% 2.32M 74s
33000K .......... .......... .......... .......... .......... 12% 2.93M 74s
33050K .......... .......... .......... .......... .......... 12% 4.58M 74s
33100K .......... .......... .......... .......... .......... 12% 4.22M 74s
33150K .......... .......... .......... .......... .......... 12% 5.22M 74s
33200K .......... .......... .......... .......... .......... 12% 3.20M 74s
33250K .......... .......... .......... .......... .......... 12% 3.74M 74s
33300K .......... .......... .......... .......... .......... 12% 4.56M 74s
33350K .......... .......... .......... .......... .......... 12% 2.32M 74s
33400K .......... .......... .......... .......... .......... 12% 2.54M 74s
33450K .......... .......... .......... .......... .......... 12% 1.96M 74s
33500K .......... .......... .......... .......... .......... 12% 3.96M 74s
33550K .......... .......... .......... .......... .......... 12% 2.68M 74s
33600K .......... .......... .......... .......... .......... 12% 2.08M 74s
33650K .......... .......... .......... .......... .......... 12% 1.38M 74s
33700K .......... .......... .......... .......... .......... 12% 921K 74s
33750K .......... .......... .......... .......... .......... 12% 1.27M 74s
33800K .......... .......... .......... .......... .......... 12% 1.40M 74s
33850K .......... .......... .......... .......... .......... 12% 840K 74s
33900K .......... .......... .......... .......... .......... 12% 1.61M 75s
33950K .......... .......... .......... .......... .......... 12% 1.39M 75s
34000K .......... .......... .......... .......... .......... 12% 1.26M 75s
34050K .......... .......... .......... .......... .......... 13% 1.84M 75s
34100K .......... .......... .......... .......... .......... 13% 1.35M 75s
34150K .......... .......... .......... .......... .......... 13% 10.2M 75s
34200K .......... .......... .......... .......... .......... 13% 6.22M 75s
34250K .......... .......... .......... .......... .......... 13% 4.41M 75s
34300K .......... .......... .......... .......... .......... 13% 3.37M 75s
34350K .......... .......... .......... .......... .......... 13% 2.69M 75s
34400K .......... .......... .......... .......... .......... 13% 2.05M 75s
34450K .......... .......... .......... .......... .......... 13% 1.17M 75s
34500K .......... .......... .......... .......... .......... 13% 5.75M 75s
34550K .......... .......... .......... .......... .......... 13% 5.20M 75s
34600K .......... .......... .......... .......... .......... 13% 3.14M 75s
34650K .......... .......... .......... .......... .......... 13% 2.34M 75s
34700K .......... .......... .......... .......... .......... 13% 3.63M 75s
34750K .......... .......... .......... .......... .......... 13% 8.61M 75s
34800K .......... .......... .......... .......... .......... 13% 3.65M 75s
34850K .......... .......... .......... .......... .......... 13% 53.0M 74s
34900K .......... .......... .......... .......... .......... 13% 8.12M 74s
34950K .......... .......... .......... .......... .......... 13% 5.11M 74s
35000K .......... .......... .......... .......... .......... 13% 2.92M 74s
35050K .......... .......... .......... .......... .......... 13% 3.43M 74s
35100K .......... .......... .......... .......... .......... 13% 3.29M 74s
35150K .......... .......... .......... .......... .......... 13% 5.16M 74s
35200K .......... .......... .......... .......... .......... 13% 9.64M 74s
35250K .......... .......... .......... .......... .......... 13% 4.50M 74s
35300K .......... .......... .......... .......... .......... 13% 3.69M 74s
35350K .......... .......... .......... .......... .......... 13% 3.36M 74s
35400K .......... .......... .......... .......... .......... 13% 2.27M 74s
35450K .......... .......... .......... .......... .......... 13% 2.18M 74s
35500K .......... .......... .......... .......... .......... 13% 2.89M 74s
35550K .......... .......... .......... .......... .......... 13% 1.77M 74s
35600K .......... .......... .......... .......... .......... 13% 1.45M 74s
35650K .......... .......... .......... .......... .......... 13% 3.35M 74s
35700K .......... .......... .......... .......... .......... 13% 5.91M 74s
35750K .......... .......... .......... .......... .......... 13% 5.38M 74s
35800K .......... .......... .......... .......... .......... 13% 3.15M 74s
35850K .......... .......... .......... .......... .......... 13% 30.2M 74s
35900K .......... .......... .......... .......... .......... 13% 5.72M 74s
35950K .......... .......... .......... .......... .......... 13% 19.5M 74s
36000K .......... .......... .......... .......... .......... 13% 5.77M 74s
36050K .......... .......... .......... .......... .......... 13% 5.93M 74s
36100K .......... .......... .......... .......... .......... 13% 9.03M 73s
36150K .......... .......... .......... .......... .......... 13% 4.68M 73s
36200K .......... .......... .......... .......... .......... 13% 7.07M 73s
36250K .......... .......... .......... .......... .......... 13% 4.66M 73s
36300K .......... .......... .......... .......... .......... 13% 5.00M 73s
36350K .......... .......... .......... .......... .......... 13% 3.64M 73s
36400K .......... .......... .......... .......... .......... 13% 3.32M 73s
36450K .......... .......... .......... .......... .......... 13% 1.86M 73s
36500K .......... .......... .......... .......... .......... 13% 1016K 73s
36550K .......... .......... .......... .......... .......... 13% 2.46M 73s
36600K .......... .......... .......... .......... .......... 13% 976K 74s
36650K .......... .......... .......... .......... .......... 13% 1.35M 74s
36700K .......... .......... .......... .......... .......... 14% 1.49M 74s
36750K .......... .......... .......... .......... .......... 14% 1.74M 74s
36800K .......... .......... .......... .......... .......... 14% 10.7M 74s
36850K .......... .......... .......... .......... .......... 14% 3.23M 74s
36900K .......... .......... .......... .......... .......... 14% 96.9M 74s
36950K .......... .......... .......... .......... .......... 14% 2.34M 74s
37000K .......... .......... .......... .......... .......... 14% 2.23M 74s
37050K .......... .......... .......... .......... .......... 14% 3.83M 74s
37100K .......... .......... .......... .......... .......... 14% 2.65M 74s
37150K .......... .......... .......... .......... .......... 14% 2.48M 74s
37200K .......... .......... .......... .......... .......... 14% 1.28M 74s
37250K .......... .......... .......... .......... .......... 14% 1.50M 74s
37300K .......... .......... .......... .......... .......... 14% 1.38M 74s
37350K .......... .......... .......... .......... .......... 14% 666K 74s
37400K .......... .......... .......... .......... .......... 14% 1.65M 74s
37450K .......... .......... .......... .......... .......... 14% 2.34M 74s
37500K .......... .......... .......... .......... .......... 14% 2.88M 74s
37550K .......... .......... .......... .......... .......... 14% 11.4M 74s
37600K .......... .......... .......... .......... .......... 14% 4.18M 74s
37650K .......... .......... .......... .......... .......... 14% 6.07M 74s
37700K .......... .......... .......... .......... .......... 14% 3.60M 74s
37750K .......... .......... .......... .......... .......... 14% 3.69M 74s
37800K .......... .......... .......... .......... .......... 14% 2.70M 74s
37850K .......... .......... .......... .......... .......... 14% 2.18M 74s
37900K .......... .......... .......... .......... .......... 14% 12.4M 74s
37950K .......... .......... .......... .......... .......... 14% 6.03M 74s
38000K .......... .......... .......... .......... .......... 14% 6.19M 74s
38050K .......... .......... .......... .......... .......... 14% 6.48M 74s
38100K .......... .......... .......... .......... .......... 14% 5.26M 74s
38150K .......... .......... .......... .......... .......... 14% 5.38M 74s
38200K .......... .......... .......... .......... .......... 14% 4.38M 74s
38250K .......... .......... .......... .......... .......... 14% 3.11M 74s
38300K .......... .......... .......... .......... .......... 14% 3.35M 74s
38350K .......... .......... .......... .......... .......... 14% 3.33M 74s
38400K .......... .......... .......... .......... .......... 14% 6.11M 73s
38450K .......... .......... .......... .......... .......... 14% 4.16M 73s
38500K .......... .......... .......... .......... .......... 14% 6.22M 73s
38550K .......... .......... .......... .......... .......... 14% 2.31M 73s
38600K .......... .......... .......... .......... .......... 14% 1.47M 73s
38650K .......... .......... .......... .......... .......... 14% 3.29M 73s
38700K .......... .......... .......... .......... .......... 14% 1.96M 73s
38750K .......... .......... .......... .......... .......... 14% 2.53M 73s
38800K .......... .......... .......... .......... .......... 14% 3.69M 73s
38850K .......... .......... .......... .......... .......... 14% 4.00M 73s
38900K .......... .......... .......... .......... .......... 14% 4.21M 73s
38950K .......... .......... .......... .......... .......... 14% 3.82M 73s
39000K .......... .......... .......... .......... .......... 14% 3.03M 73s
39050K .......... .......... .......... .......... .......... 14% 6.01M 73s
39100K .......... .......... .......... .......... .......... 14% 2.88M 73s
39150K .......... .......... .......... .......... .......... 14% 3.10M 73s
39200K .......... .......... .......... .......... .......... 14% 6.23M 73s
39250K .......... .......... .......... .......... .......... 14% 9.74M 73s
39300K .......... .......... .......... .......... .......... 15% 6.16M 73s
39350K .......... .......... .......... .......... .......... 15% 12.6M 73s
39400K .......... .......... .......... .......... .......... 15% 7.58M 73s
39450K .......... .......... .......... .......... .......... 15% 8.82M 73s
39500K .......... .......... .......... .......... .......... 15% 6.85M 73s
39550K .......... .......... .......... .......... .......... 15% 4.77M 73s
39600K .......... .......... .......... .......... .......... 15% 3.39M 73s
39650K .......... .......... .......... .......... .......... 15% 2.30M 73s
39700K .......... .......... .......... .......... .......... 15% 3.09M 73s
39750K .......... .......... .......... .......... .......... 15% 2.85M 73s
39800K .......... .......... .......... .......... .......... 15% 2.31M 73s
39850K .......... .......... .......... .......... .......... 15% 1.96M 73s
39900K .......... .......... .......... .......... .......... 15% 1.93M 73s
39950K .......... .......... .......... .......... .......... 15% 2.50M 73s
40000K .......... .......... .......... .......... .......... 15% 4.08M 73s
40050K .......... .......... .......... .......... .......... 15% 2.44M 73s
40100K .......... .......... .......... .......... .......... 15% 2.47M 73s
40150K .......... .......... .......... .......... .......... 15% 2.19M 73s
40200K .......... .......... .......... .......... .......... 15% 1.62M 73s
40250K .......... .......... .......... .......... .......... 15% 2.68M 73s
40300K .......... .......... .......... .......... .......... 15% 3.96M 73s
40350K .......... .......... .......... .......... .......... 15% 3.53M 73s
40400K .......... .......... .......... .......... .......... 15% 2.53M 73s
40450K .......... .......... .......... .......... .......... 15% 1.93M 73s
40500K .......... .......... .......... .......... .......... 15% 3.37M 73s
40550K .......... .......... .......... .......... .......... 15% 2.62M 73s
40600K .......... .......... .......... .......... .......... 15% 3.17M 73s
40650K .......... .......... .......... .......... .......... 15% 3.35M 73s
40700K .......... .......... .......... .......... .......... 15% 3.53M 73s
40750K .......... .......... .......... .......... .......... 15% 5.27M 72s
40800K .......... .......... .......... .......... .......... 15% 2.39M 72s
40850K .......... .......... .......... .......... .......... 15% 2.51M 72s
40900K .......... .......... .......... .......... .......... 15% 3.74M 72s
40950K .......... .......... .......... .......... .......... 15% 2.88M 72s
41000K .......... .......... .......... .......... .......... 15% 4.68M 72s
41050K .......... .......... .......... .......... .......... 15% 6.64M 72s
41100K .......... .......... .......... .......... .......... 15% 8.90M 72s
41150K .......... .......... .......... .......... .......... 15% 7.44M 72s
41200K .......... .......... .......... .......... .......... 15% 5.87M 72s
41250K .......... .......... .......... .......... .......... 15% 5.20M 72s
41300K .......... .......... .......... .......... .......... 15% 4.65M 72s
41350K .......... .......... .......... .......... .......... 15% 2.37M 72s
41400K .......... .......... .......... .......... .......... 15% 3.22M 72s
41450K .......... .......... .......... .......... .......... 15% 1.75M 72s
41500K .......... .......... .......... .......... .......... 15% 2.29M 72s
41550K .......... .......... .......... .......... .......... 15% 9.35M 72s
41600K .......... .......... .......... .......... .......... 15% 5.78M 72s
41650K .......... .......... .......... .......... .......... 15% 7.53M 72s
41700K .......... .......... .......... .......... .......... 15% 3.40M 72s
41750K .......... .......... .......... .......... .......... 15% 3.73M 72s
41800K .......... .......... .......... .......... .......... 15% 2.43M 72s
41850K .......... .......... .......... .......... .......... 15% 2.48M 72s
41900K .......... .......... .......... .......... .......... 15% 4.05M 72s
41950K .......... .......... .......... .......... .......... 16% 2.50M 72s
42000K .......... .......... .......... .......... .......... 16% 4.32M 72s
42050K .......... .......... .......... .......... .......... 16% 3.40M 72s
42100K .......... .......... .......... .......... .......... 16% 1.99M 72s
42150K .......... .......... .......... .......... .......... 16% 2.12M 72s
42200K .......... .......... .......... .......... .......... 16% 1.56M 72s
42250K .......... .......... .......... .......... .......... 16% 4.22M 72s
42300K .......... .......... .......... .......... .......... 16% 2.64M 72s
42350K .......... .......... .......... .......... .......... 16% 1.87M 72s
42400K .......... .......... .......... .......... .......... 16% 1.73M 72s
42450K .......... .......... .......... .......... .......... 16% 1.77M 72s
42500K .......... .......... .......... .......... .......... 16% 6.99M 72s
42550K .......... .......... .......... .......... .......... 16% 3.65M 72s
42600K .......... .......... .......... .......... .......... 16% 3.13M 72s
42650K .......... .......... .......... .......... .......... 16% 3.10M 72s
42700K .......... .......... .......... .......... .......... 16% 2.83M 72s
42750K .......... .......... .......... .......... .......... 16% 4.74M 72s
42800K .......... .......... .......... .......... .......... 16% 6.40M 72s
42850K .......... .......... .......... .......... .......... 16% 3.19M 72s
42900K .......... .......... .......... .......... .......... 16% 3.66M 72s
42950K .......... .......... .......... .......... .......... 16% 1.69M 72s
43000K .......... .......... .......... .......... .......... 16% 2.12M 72s
43050K .......... .......... .......... .......... .......... 16% 2.18M 72s
43100K .......... .......... .......... .......... .......... 16% 9.14M 72s
43150K .......... .......... .......... .......... .......... 16% 4.73M 72s
43200K .......... .......... .......... .......... .......... 16% 3.35M 72s
43250K .......... .......... .......... .......... .......... 16% 6.29M 71s
43300K .......... .......... .......... .......... .......... 16% 4.61M 71s
43350K .......... .......... .......... .......... .......... 16% 3.82M 71s
43400K .......... .......... .......... .......... .......... 16% 5.30M 71s
43450K .......... .......... .......... .......... .......... 16% 10.0M 71s
43500K .......... .......... .......... .......... .......... 16% 16.3M 71s
43550K .......... .......... .......... .......... .......... 16% 7.14M 71s
43600K .......... .......... .......... .......... .......... 16% 9.58M 71s
43650K .......... .......... .......... .......... .......... 16% 6.00M 71s
43700K .......... .......... .......... .......... .......... 16% 6.40M 71s
43750K .......... .......... .......... .......... .......... 16% 5.78M 71s
43800K .......... .......... .......... .......... .......... 16% 6.27M 71s
43850K .......... .......... .......... .......... .......... 16% 4.86M 71s
43900K .......... .......... .......... .......... .......... 16% 4.08M 71s
43950K .......... .......... .......... .......... .......... 16% 3.27M 71s
44000K .......... .......... .......... .......... .......... 16% 3.60M 71s
44050K .......... .......... .......... .......... .......... 16% 4.54M 71s
44100K .......... .......... .......... .......... .......... 16% 3.96M 71s
44150K .......... .......... .......... .......... .......... 16% 6.33M 71s
44200K .......... .......... .......... .......... .......... 16% 7.11M 70s
44250K .......... .......... .......... .......... .......... 16% 8.36M 70s
44300K .......... .......... .......... .......... .......... 16% 7.43M 70s
44350K .......... .......... .......... .......... .......... 16% 4.56M 70s
44400K .......... .......... .......... .......... .......... 16% 3.68M 70s
44450K .......... .......... .......... .......... .......... 16% 2.34M 70s
44500K .......... .......... .......... .......... .......... 16% 2.92M 70s
44550K .......... .......... .......... .......... .......... 17% 6.26M 70s
44600K .......... .......... .......... .......... .......... 17% 4.48M 70s
44650K .......... .......... .......... .......... .......... 17% 5.63M 70s
44700K .......... .......... .......... .......... .......... 17% 3.09M 70s
44750K .......... .......... .......... .......... .......... 17% 2.48M 70s
44800K .......... .......... .......... .......... .......... 17% 3.06M 70s
44850K .......... .......... .......... .......... .......... 17% 1.84M 70s
44900K .......... .......... .......... .......... .......... 17% 2.36M 70s
44950K .......... .......... .......... .......... .......... 17% 3.66M 70s
45000K .......... .......... .......... .......... .......... 17% 6.10M 70s
45050K .......... .......... .......... .......... .......... 17% 3.21M 70s
45100K .......... .......... .......... .......... .......... 17% 5.37M 70s
45150K .......... .......... .......... .......... .......... 17% 4.01M 70s
45200K .......... .......... .......... .......... .......... 17% 1.68M 70s
45250K .......... .......... .......... .......... .......... 17% 1.85M 70s
45300K .......... .......... .......... .......... .......... 17% 2.08M 70s
45350K .......... .......... .......... .......... .......... 17% 2.17M 70s
45400K .......... .......... .......... .......... .......... 17% 6.35M 70s
45450K .......... .......... .......... .......... .......... 17% 6.74M 70s
45500K .......... .......... .......... .......... .......... 17% 6.50M 70s
45550K .......... .......... .......... .......... .......... 17% 6.23M 70s
45600K .......... .......... .......... .......... .......... 17% 3.76M 70s
45650K .......... .......... .......... .......... .......... 17% 3.45M 70s
45700K .......... .......... .......... .......... .......... 17% 3.70M 70s
45750K .......... .......... .......... .......... .......... 17% 3.02M 70s
45800K .......... .......... .......... .......... .......... 17% 2.68M 70s
45850K .......... .......... .......... .......... .......... 17% 2.49M 70s
45900K .......... .......... .......... .......... .......... 17% 1.93M 70s
45950K .......... .......... .......... .......... .......... 17% 1.56M 70s
46000K .......... .......... .......... .......... .......... 17% 6.08M 70s
46050K .......... .......... .......... .......... .......... 17% 3.26M 70s
46100K .......... .......... .......... .......... .......... 17% 12.0M 70s
46150K .......... .......... .......... .......... .......... 17% 5.28M 70s
46200K .......... .......... .......... .......... .......... 17% 3.38M 70s
46250K .......... .......... .......... .......... .......... 17% 4.61M 70s
46300K .......... .......... .......... .......... .......... 17% 4.67M 69s
46350K .......... .......... .......... .......... .......... 17% 4.90M 69s
46400K .......... .......... .......... .......... .......... 17% 10.1M 69s
46450K .......... .......... .......... .......... .......... 17% 10.0M 69s
46500K .......... .......... .......... .......... .......... 17% 9.91M 69s
46550K .......... .......... .......... .......... .......... 17% 6.72M 69s
46600K .......... .......... .......... .......... .......... 17% 7.18M 69s
46650K .......... .......... .......... .......... .......... 17% 5.37M 69s
46700K .......... .......... .......... .......... .......... 17% 6.00M 69s
46750K .......... .......... .......... .......... .......... 17% 4.65M 69s
46800K .......... .......... .......... .......... .......... 17% 3.08M 69s
46850K .......... .......... .......... .......... .......... 17% 3.67M 69s
46900K .......... .......... .......... .......... .......... 17% 3.68M 69s
46950K .......... .......... .......... .......... .......... 17% 3.93M 69s
47000K .......... .......... .......... .......... .......... 17% 9.16M 69s
47050K .......... .......... .......... .......... .......... 17% 7.78M 69s
47100K .......... .......... .......... .......... .......... 17% 6.14M 69s
47150K .......... .......... .......... .......... .......... 18% 12.4M 69s
47200K .......... .......... .......... .......... .......... 18% 5.28M 69s
47250K .......... .......... .......... .......... .......... 18% 9.22M 68s
47300K .......... .......... .......... .......... .......... 18% 6.29M 68s
47350K .......... .......... .......... .......... .......... 18% 6.25M 68s
47400K .......... .......... .......... .......... .......... 18% 6.44M 68s
47450K .......... .......... .......... .......... .......... 18% 7.10M 68s
47500K .......... .......... .......... .......... .......... 18% 4.74M 68s
47550K .......... .......... .......... .......... .......... 18% 4.74M 68s
47600K .......... .......... .......... .......... .......... 18% 3.76M 68s
47650K .......... .......... .......... .......... .......... 18% 4.67M 68s
47700K .......... .......... .......... .......... .......... 18% 2.62M 68s
47750K .......... .......... .......... .......... .......... 18% 3.29M 68s
47800K .......... .......... .......... .......... .......... 18% 2.63M 68s
47850K .......... .......... .......... .......... .......... 18% 1.53M 68s
47900K .......... .......... .......... .......... .......... 18% 2.08M 68s
47950K .......... .......... .......... .......... .......... 18% 1.32M 68s
48000K .......... .......... .......... .......... .......... 18% 2.86M 68s
48050K .......... .......... .......... .......... .......... 18% 5.20M 68s
48100K .......... .......... .......... .......... .......... 18% 2.78M 68s
48150K .......... .......... .......... .......... .......... 18% 26.6M 68s
48200K .......... .......... .......... .......... .......... 18% 3.11M 68s
48250K .......... .......... .......... .......... .......... 18% 3.66M 68s
48300K .......... .......... .......... .......... .......... 18% 3.09M 68s
48350K .......... .......... .......... .......... .......... 18% 3.08M 68s
48400K .......... .......... .......... .......... .......... 18% 2.67M 68s
48450K .......... .......... .......... .......... .......... 18% 1.97M 68s
48500K .......... .......... .......... .......... .......... 18% 3.99M 68s
48550K .......... .......... .......... .......... .......... 18% 6.51M 68s
48600K .......... .......... .......... .......... .......... 18% 6.96M 68s
48650K .......... .......... .......... .......... .......... 18% 4.06M 68s
48700K .......... .......... .......... .......... .......... 18% 7.30M 68s
48750K .......... .......... .......... .......... .......... 18% 2.38M 68s
48800K .......... .......... .......... .......... .......... 18% 2.15M 68s
48850K .......... .......... .......... .......... .......... 18% 1.46M 68s
48900K .......... .......... .......... .......... .......... 18% 2.46M 68s
48950K .......... .......... .......... .......... .......... 18% 2.08M 68s
49000K .......... .......... .......... .......... .......... 18% 2.59M 68s
49050K .......... .......... .......... .......... .......... 18% 3.07M 68s
49100K .......... .......... .......... .......... .......... 18% 2.09M 68s
49150K .......... .......... .......... .......... .......... 18% 4.50M 68s
49200K .......... .......... .......... .......... .......... 18% 2.47M 68s
49250K .......... .......... .......... .......... .......... 18% 2.62M 68s
49300K .......... .......... .......... .......... .......... 18% 1.23M 68s
49350K .......... .......... .......... .......... .......... 18% 2.64M 68s
49400K .......... .......... .......... .......... .......... 18% 8.24M 68s
49450K .......... .......... .......... .......... .......... 18% 8.43M 68s
49500K .......... .......... .......... .......... .......... 18% 6.31M 68s
49550K .......... .......... .......... .......... .......... 18% 5.46M 68s
49600K .......... .......... .......... .......... .......... 18% 3.64M 68s
49650K .......... .......... .......... .......... .......... 18% 5.11M 68s
49700K .......... .......... .......... .......... .......... 18% 3.15M 68s
49750K .......... .......... .......... .......... .......... 18% 4.10M 68s
49800K .......... .......... .......... .......... .......... 19% 4.66M 68s
49850K .......... .......... .......... .......... .......... 19% 3.65M 68s
49900K .......... .......... .......... .......... .......... 19% 3.68M 68s
49950K .......... .......... .......... .......... .......... 19% 3.09M 68s
50000K .......... .......... .......... .......... .......... 19% 8.91M 67s
50050K .......... .......... .......... .......... .......... 19% 9.52M 67s
50100K .......... .......... .......... .......... .......... 19% 9.14M 67s
50150K .......... .......... .......... .......... .......... 19% 2.27M 67s
50200K .......... .......... .......... .......... .......... 19% 77.0M 67s
50250K .......... .......... .......... .......... .......... 19% 10.5M 67s
50300K .......... .......... .......... .......... .......... 19% 5.15M 67s
50350K .......... .......... .......... .......... .......... 19% 3.07M 67s
50400K .......... .......... .......... .......... .......... 19% 3.14M 67s
50450K .......... .......... .......... .......... .......... 19% 2.47M 67s
50500K .......... .......... .......... .......... .......... 19% 1.73M 67s
50550K .......... .......... .......... .......... .......... 19% 5.94M 67s
50600K .......... .......... .......... .......... .......... 19% 3.14M 67s
50650K .......... .......... .......... .......... .......... 19% 6.18M 67s
50700K .......... .......... .......... .......... .......... 19% 3.35M 67s
50750K .......... .......... .......... .......... .......... 19% 3.21M 67s
50800K .......... .......... .......... .......... .......... 19% 2.21M 67s
50850K .......... .......... .......... .......... .......... 19% 2.06M 67s
50900K .......... .......... .......... .......... .......... 19% 2.32M 67s
50950K .......... .......... .......... .......... .......... 19% 2.18M 67s
51000K .......... .......... .......... .......... .......... 19% 2.24M 67s
51050K .......... .......... .......... .......... .......... 19% 4.98M 67s
51100K .......... .......... .......... .......... .......... 19% 4.37M 67s
51150K .......... .......... .......... .......... .......... 19% 6.13M 67s
51200K .......... .......... .......... .......... .......... 19% 3.79M 67s
51250K .......... .......... .......... .......... .......... 19% 3.33M 67s
51300K .......... .......... .......... .......... .......... 19% 3.03M 67s
51350K .......... .......... .......... .......... .......... 19% 2.35M 67s
51400K .......... .......... .......... .......... .......... 19% 2.55M 67s
51450K .......... .......... .......... .......... .......... 19% 3.02M 67s
51500K .......... .......... .......... .......... .......... 19% 5.78M 67s
51550K .......... .......... .......... .......... .......... 19% 6.10M 67s
51600K .......... .......... .......... .......... .......... 19% 3.13M 67s
51650K .......... .......... .......... .......... .......... 19% 4.60M 67s
51700K .......... .......... .......... .......... .......... 19% 3.04M 67s
51750K .......... .......... .......... .......... .......... 19% 3.88M 67s
51800K .......... .......... .......... .......... .......... 19% 2.79M 67s
51850K .......... .......... .......... .......... .......... 19% 2.50M 67s
51900K .......... .......... .......... .......... .......... 19% 2.06M 67s
51950K .......... .......... .......... .......... .......... 19% 1.84M 67s
52000K .......... .......... .......... .......... .......... 19% 3.36M 67s
52050K .......... .......... .......... .......... .......... 19% 4.21M 67s
52100K .......... .......... .......... .......... .......... 19% 3.72M 67s
52150K .......... .......... .......... .......... .......... 19% 3.81M 67s
52200K .......... .......... .......... .......... .......... 19% 2.78M 67s
52250K .......... .......... .......... .......... .......... 19% 3.61M 67s
52300K .......... .......... .......... .......... .......... 19% 2.85M 67s
52350K .......... .......... .......... .......... .......... 19% 2.67M 67s
52400K .......... .......... .......... .......... .......... 20% 1.39M 67s
52450K .......... .......... .......... .......... .......... 20% 908K 67s
52500K .......... .......... .......... .......... .......... 20% 3.24M 67s
52550K .......... .......... .......... .......... .......... 20% 2.45M 67s
52600K .......... .......... .......... .......... .......... 20% 2.04M 67s
52650K .......... .......... .......... .......... .......... 20% 3.88M 67s
52700K .......... .......... .......... .......... .......... 20% 3.49M 67s
52750K .......... .......... .......... .......... .......... 20% 3.15M 67s
52800K .......... .......... .......... .......... .......... 20% 3.65M 67s
52850K .......... .......... .......... .......... .......... 20% 2.84M 67s
52900K .......... .......... .......... .......... .......... 20% 3.05M 67s
52950K .......... .......... .......... .......... .......... 20% 1.43M 67s
53000K .......... .......... .......... .......... .......... 20% 1.84M 67s
53050K .......... .......... .......... .......... .......... 20% 4.62M 67s
53100K .......... .......... .......... .......... .......... 20% 6.36M 67s
53150K .......... .......... .......... .......... .......... 20% 4.20M 67s
53200K .......... .......... .......... .......... .......... 20% 2.67M 67s
53250K .......... .......... .......... .......... .......... 20% 31.2M 66s
53300K .......... .......... .......... .......... .......... 20% 7.08M 66s
53350K .......... .......... .......... .......... .......... 20% 4.50M 66s
53400K .......... .......... .......... .......... .......... 20% 4.14M 66s
53450K .......... .......... .......... .......... .......... 20% 3.41M 66s
53500K .......... .......... .......... .......... .......... 20% 3.41M 66s
53550K .......... .......... .......... .......... .......... 20% 3.16M 66s
53600K .......... .......... .......... .......... .......... 20% 3.53M 66s
53650K .......... .......... .......... .......... .......... 20% 9.52M 66s
53700K .......... .......... .......... .......... .......... 20% 8.06M 66s
53750K .......... .......... .......... .......... .......... 20% 6.09M 66s
53800K .......... .......... .......... .......... .......... 20% 4.70M 66s
53850K .......... .......... .......... .......... .......... 20% 3.61M 66s
53900K .......... .......... .......... .......... .......... 20% 3.28M 66s
53950K .......... .......... .......... .......... .......... 20% 3.67M 66s
54000K .......... .......... .......... .......... .......... 20% 3.64M 66s
54050K .......... .......... .......... .......... .......... 20% 7.14M 66s
54100K .......... .......... .......... .......... .......... 20% 5.32M 66s
54150K .......... .......... .......... .......... .......... 20% 4.74M 66s
54200K .......... .......... .......... .......... .......... 20% 4.15M 66s
54250K .......... .......... .......... .......... .......... 20% 4.36M 66s
54300K .......... .......... .......... .......... .......... 20% 3.46M 66s
54350K .......... .......... .......... .......... .......... 20% 3.39M 66s
54400K .......... .......... .......... .......... .......... 20% 5.13M 66s
54450K .......... .......... .......... .......... .......... 20% 3.72M 66s
54500K .......... .......... .......... .......... .......... 20% 4.04M 66s
54550K .......... .......... .......... .......... .......... 20% 3.81M 66s
54600K .......... .......... .......... .......... .......... 20% 3.63M 66s
54650K .......... .......... .......... .......... .......... 20% 6.21M 66s
54700K .......... .......... .......... .......... .......... 20% 3.24M 66s
54750K .......... .......... .......... .......... .......... 20% 4.33M 66s
54800K .......... .......... .......... .......... .......... 20% 3.69M 65s
54850K .......... .......... .......... .......... .......... 20% 2.76M 65s
54900K .......... .......... .......... .......... .......... 20% 4.70M 65s
54950K .......... .......... .......... .......... .......... 20% 6.99M 65s
55000K .......... .......... .......... .......... .......... 20% 6.26M 65s
55050K .......... .......... .......... .......... .......... 21% 9.03M 65s
55100K .......... .......... .......... .......... .......... 21% 4.44M 65s
55150K .......... .......... .......... .......... .......... 21% 6.22M 65s
55200K .......... .......... .......... .......... .......... 21% 4.57M 65s
55250K .......... .......... .......... .......... .......... 21% 6.21M 65s
55300K .......... .......... .......... .......... .......... 21% 3.99M 65s
55350K .......... .......... .......... .......... .......... 21% 4.07M 65s
55400K .......... .......... .......... .......... .......... 21% 3.29M 65s
55450K .......... .......... .......... .......... .......... 21% 4.61M 65s
55500K .......... .......... .......... .......... .......... 21% 3.40M 65s
55550K .......... .......... .......... .......... .......... 21% 4.59M 65s
55600K .......... .......... .......... .......... .......... 21% 2.90M 65s
55650K .......... .......... .......... .......... .......... 21% 2.61M 65s
55700K .......... .......... .......... .......... .......... 21% 2.29M 65s
55750K .......... .......... .......... .......... .......... 21% 1.86M 65s
55800K .......... .......... .......... .......... .......... 21% 2.80M 65s
55850K .......... .......... .......... .......... .......... 21% 9.38M 65s
55900K .......... .......... .......... .......... .......... 21% 7.23M 65s
55950K .......... .......... .......... .......... .......... 21% 6.34M 65s
56000K .......... .......... .......... .......... .......... 21% 6.26M 65s
56050K .......... .......... .......... .......... .......... 21% 3.69M 65s
56100K .......... .......... .......... .......... .......... 21% 3.15M 65s
56150K .......... .......... .......... .......... .......... 21% 3.61M 65s
56200K .......... .......... .......... .......... .......... 21% 7.11M 65s
56250K .......... .......... .......... .......... .......... 21% 9.00M 65s
56300K .......... .......... .......... .......... .......... 21% 4.62M 65s
56350K .......... .......... .......... .......... .......... 21% 3.38M 65s
56400K .......... .......... .......... .......... .......... 21% 3.38M 65s
56450K .......... .......... .......... .......... .......... 21% 2.36M 65s
56500K .......... .......... .......... .......... .......... 21% 2.13M 65s
56550K .......... .......... .......... .......... .......... 21% 1.96M 65s
56600K .......... .......... .......... .......... .......... 21% 2.75M 65s
56650K .......... .......... .......... .......... .......... 21% 4.74M 65s
56700K .......... .......... .......... .......... .......... 21% 2.81M 65s
56750K .......... .......... .......... .......... .......... 21% 2.61M 65s
56800K .......... .......... .......... .......... .......... 21% 3.07M 64s
56850K .......... .......... .......... .......... .......... 21% 1.71M 65s
56900K .......... .......... .......... .......... .......... 21% 2.34M 65s
56950K .......... .......... .......... .......... .......... 21% 5.12M 64s
57000K .......... .......... .......... .......... .......... 21% 6.77M 64s
57050K .......... .......... .......... .......... .......... 21% 3.74M 64s
57100K .......... .......... .......... .......... .......... 21% 5.23M 64s
57150K .......... .......... .......... .......... .......... 21% 1.82M 64s
57200K .......... .......... .......... .......... .......... 21% 831K 65s
57250K .......... .......... .......... .......... .......... 21% 1.62M 65s
57300K .......... .......... .......... .......... .......... 21% 1.87M 65s
57350K .......... .......... .......... .......... .......... 21% 2.81M 65s
57400K .......... .......... .......... .......... .......... 21% 4.00M 65s
57450K .......... .......... .......... .......... .......... 21% 4.10M 65s
57500K .......... .......... .......... .......... .......... 21% 5.17M 64s
57550K .......... .......... .......... .......... .......... 21% 6.21M 64s
57600K .......... .......... .......... .......... .......... 21% 5.25M 64s
57650K .......... .......... .......... .......... .......... 22% 11.1M 64s
57700K .......... .......... .......... .......... .......... 22% 9.74M 64s
57750K .......... .......... .......... .......... .......... 22% 11.3M 64s
57800K .......... .......... .......... .......... .......... 22% 16.7M 64s
57850K .......... .......... .......... .......... .......... 22% 10.8M 64s
57900K .......... .......... .......... .......... .......... 22% 9.35M 64s
57950K .......... .......... .......... .......... .......... 22% 15.7M 64s
58000K .......... .......... .......... .......... .......... 22% 11.4M 64s
58050K .......... .......... .......... .......... .......... 22% 26.2M 64s
58100K .......... .......... .......... .......... .......... 22% 13.6M 64s
58150K .......... .......... .......... .......... .......... 22% 11.7M 64s
58200K .......... .......... .......... .......... .......... 22% 18.1M 64s
58250K .......... .......... .......... .......... .......... 22% 6.48M 64s
58300K .......... .......... .......... .......... .......... 22% 16.5M 64s
58350K .......... .......... .......... .......... .......... 22% 4.58M 64s
58400K .......... .......... .......... .......... .......... 22% 72.1M 64s
58450K .......... .......... .......... .......... .......... 22% 10.4M 63s
58500K .......... .......... .......... .......... .......... 22% 17.7M 63s
58550K .......... .......... .......... .......... .......... 22% 12.0M 63s
58600K .......... .......... .......... .......... .......... 22% 11.5M 63s
58650K .......... .......... .......... .......... .......... 22% 7.15M 63s
58700K .......... .......... .......... .......... .......... 22% 5.94M 63s
58750K .......... .......... .......... .......... .......... 22% 7.67M 63s
58800K .......... .......... .......... .......... .......... 22% 7.19M 63s
58850K .......... .......... .......... .......... .......... 22% 2.35M 63s
58900K .......... .......... .......... .......... .......... 22% 4.68M 63s
58950K .......... .......... .......... .......... .......... 22% 3.42M 63s
59000K .......... .......... .......... .......... .......... 22% 2.88M 63s
59050K .......... .......... .......... .......... .......... 22% 3.40M 63s
59100K .......... .......... .......... .......... .......... 22% 4.05M 63s
59150K .......... .......... .......... .......... .......... 22% 12.0M 63s
59200K .......... .......... .......... .......... .......... 22% 9.17M 63s
59250K .......... .......... .......... .......... .......... 22% 9.02M 63s
59300K .......... .......... .......... .......... .......... 22% 9.40M 63s
59350K .......... .......... .......... .......... .......... 22% 2.53M 63s
59400K .......... .......... .......... .......... .......... 22% 11.9M 63s
59450K .......... .......... .......... .......... .......... 22% 7.50M 63s
59500K .......... .......... .......... .......... .......... 22% 7.46M 63s
59550K .......... .......... .......... .......... .......... 22% 6.78M 63s
59600K .......... .......... .......... .......... .......... 22% 19.7M 63s
59650K .......... .......... .......... .......... .......... 22% 9.21M 63s
59700K .......... .......... .......... .......... .......... 22% 7.42M 62s
59750K .......... .......... .......... .......... .......... 22% 9.04M 62s
59800K .......... .......... .......... .......... .......... 22% 9.44M 62s
59850K .......... .......... .......... .......... .......... 22% 7.92M 62s
59900K .......... .......... .......... .......... .......... 22% 8.57M 62s
59950K .......... .......... .......... .......... .......... 22% 7.54M 62s
60000K .......... .......... .......... .......... .......... 22% 23.7M 62s
60050K .......... .......... .......... .......... .......... 22% 10.0M 62s
60100K .......... .......... .......... .......... .......... 22% 17.6M 62s
60150K .......... .......... .......... .......... .......... 22% 7.51M 62s
60200K .......... .......... .......... .......... .......... 22% 18.6M 62s
60250K .......... .......... .......... .......... .......... 22% 10.9M 62s
60300K .......... .......... .......... .......... .......... 23% 26.7M 62s
60350K .......... .......... .......... .......... .......... 23% 15.4M 62s
60400K .......... .......... .......... .......... .......... 23% 2.45M 62s
60450K .......... .......... .......... .......... .......... 23% 45.8M 62s
60500K .......... .......... .......... .......... .......... 23% 67.7M 62s
60550K .......... .......... .......... .......... .......... 23% 58.9M 62s
60600K .......... .......... .......... .......... .......... 23% 14.5M 62s
60650K .......... .......... .......... .......... .......... 23% 7.59M 61s
60700K .......... .......... .......... .......... .......... 23% 10.3M 61s
60750K .......... .......... .......... .......... .......... 23% 8.19M 61s
60800K .......... .......... .......... .......... .......... 23% 5.00M 61s
60850K .......... .......... .......... .......... .......... 23% 5.30M 61s
60900K .......... .......... .......... .......... .......... 23% 6.42M 61s
60950K .......... .......... .......... .......... .......... 23% 4.66M 61s
61000K .......... .......... .......... .......... .......... 23% 5.60M 61s
61050K .......... .......... .......... .......... .......... 23% 8.38M 61s
61100K .......... .......... .......... .......... .......... 23% 6.15M 61s
61150K .......... .......... .......... .......... .......... 23% 6.26M 61s
61200K .......... .......... .......... .......... .......... 23% 5.93M 61s
61250K .......... .......... .......... .......... .......... 23% 7.31M 61s
61300K .......... .......... .......... .......... .......... 23% 3.21M 61s
61350K .......... .......... .......... .......... .......... 23% 790K 61s
61400K .......... .......... .......... .......... .......... 23% 55.8M 61s
61450K .......... .......... .......... .......... .......... 23% 49.1M 61s
61500K .......... .......... .......... .......... .......... 23% 62.5M 61s
61550K .......... .......... .......... .......... .......... 23% 10.3M 61s
61600K .......... .......... .......... .......... .......... 23% 9.51M 61s
61650K .......... .......... .......... .......... .......... 23% 8.61M 61s
61700K .......... .......... .......... .......... .......... 23% 5.54M 61s
61750K .......... .......... .......... .......... .......... 23% 6.80M 61s
61800K .......... .......... .......... .......... .......... 23% 5.73M 61s
61850K .......... .......... .......... .......... .......... 23% 5.30M 61s
61900K .......... .......... .......... .......... .......... 23% 5.52M 61s
61950K .......... .......... .......... .......... .......... 23% 11.1M 61s
62000K .......... .......... .......... .......... .......... 23% 5.03M 61s
62050K .......... .......... .......... .......... .......... 23% 60.7M 60s
62100K .......... .......... .......... .......... .......... 23% 11.7M 60s
62150K .......... .......... .......... .......... .......... 23% 10.9M 60s
62200K .......... .......... .......... .......... .......... 23% 7.28M 60s
62250K .......... .......... .......... .......... .......... 23% 5.35M 60s
62300K .......... .......... .......... .......... .......... 23% 6.52M 60s
62350K .......... .......... .......... .......... .......... 23% 4.69M 60s
62400K .......... .......... .......... .......... .......... 23% 6.48M 60s
62450K .......... .......... .......... .......... .......... 23% 4.15M 60s
62500K .......... .......... .......... .......... .......... 23% 6.52M 60s
62550K .......... .......... .......... .......... .......... 23% 2.64M 60s
62600K .......... .......... .......... .......... .......... 23% 6.62M 60s
62650K .......... .......... .......... .......... .......... 23% 5.33M 60s
62700K .......... .......... .......... .......... .......... 23% 3.76M 60s
62750K .......... .......... .......... .......... .......... 23% 4.89M 60s
62800K .......... .......... .......... .......... .......... 23% 6.37M 60s
62850K .......... .......... .......... .......... .......... 23% 1.96M 60s
62900K .......... .......... .......... .......... .......... 24% 3.76M 60s
62950K .......... .......... .......... .......... .......... 24% 2.46M 60s
63000K .......... .......... .......... .......... .......... 24% 73.5K 62s
63050K .......... .......... .......... .......... .......... 24% 6.90M 62s
63100K .......... .......... .......... .......... .......... 24% 6.21M 62s
63150K .......... .......... .......... .......... .......... 24% 6.76M 62s
63200K .......... .......... .......... .......... .......... 24% 5.35M 62s
63250K .......... .......... .......... .......... .......... 24% 2.95M 62s
63300K .......... .......... .......... .......... .......... 24% 5.92M 62s
63350K .......... .......... .......... .......... .......... 24% 3.67M 62s
63400K .......... .......... .......... .......... .......... 24% 4.59M 62s
63450K .......... .......... .......... .......... .......... 24% 3.19M 62s
63500K .......... .......... .......... .......... .......... 24% 4.60M 62s
63550K .......... .......... .......... .......... .......... 24% 2.82M 62s
63600K .......... .......... .......... .......... .......... 24% 1.47M 62s
63650K .......... .......... .......... .......... .......... 24% 2.27M 62s
63700K .......... .......... .......... .......... .......... 24% 4.40M 62s
63750K .......... .......... .......... .......... .......... 24% 23.4M 62s
63800K .......... .......... .......... .......... .......... 24% 7.36M 62s
63850K .......... .......... .......... .......... .......... 24% 5.91M 62s
63900K .......... .......... .......... .......... .......... 24% 4.08M 62s
63950K .......... .......... .......... .......... .......... 24% 3.17M 62s
64000K .......... .......... .......... .......... .......... 24% 4.38M 62s
64050K .......... .......... .......... .......... .......... 24% 4.22M 61s
64100K .......... .......... .......... .......... .......... 24% 3.88M 61s
64150K .......... .......... .......... .......... .......... 24% 6.08M 61s
64200K .......... .......... .......... .......... .......... 24% 7.53M 61s
64250K .......... .......... .......... .......... .......... 24% 6.03M 61s
64300K .......... .......... .......... .......... .......... 24% 7.41M 61s
64350K .......... .......... .......... .......... .......... 24% 6.74M 61s
64400K .......... .......... .......... .......... .......... 24% 7.69M 61s
64450K .......... .......... .......... .......... .......... 24% 5.63M 61s
64500K .......... .......... .......... .......... .......... 24% 15.4M 61s
64550K .......... .......... .......... .......... .......... 24% 7.10M 61s
64600K .......... .......... .......... .......... .......... 24% 40.5M 61s
64650K .......... .......... .......... .......... .......... 24% 22.8M 61s
64700K .......... .......... .......... .......... .......... 24% 11.9M 61s
64750K .......... .......... .......... .......... .......... 24% 15.9M 61s
64800K .......... .......... .......... .......... .......... 24% 9.71M 61s
64850K .......... .......... .......... .......... .......... 24% 12.6M 61s
64900K .......... .......... .......... .......... .......... 24% 17.5M 61s
64950K .......... .......... .......... .......... .......... 24% 14.0M 61s
65000K .......... .......... .......... .......... .......... 24% 14.9M 61s
65050K .......... .......... .......... .......... .......... 24% 19.1M 61s
65100K .......... .......... .......... .......... .......... 24% 11.8M 61s
65150K .......... .......... .......... .......... .......... 24% 17.0M 60s
65200K .......... .......... .......... .......... .......... 24% 16.7M 60s
65250K .......... .......... .......... .......... .......... 24% 17.3M 60s
65300K .......... .......... .......... .......... .......... 24% 21.6M 60s
65350K .......... .......... .......... .......... .......... 24% 45.1M 60s
65400K .......... .......... .......... .......... .......... 24% 11.3M 60s
65450K .......... .......... .......... .......... .......... 24% 54.8M 60s
65500K .......... .......... .......... .......... .......... 25% 14.2M 60s
65550K .......... .......... .......... .......... .......... 25% 18.4M 60s
65600K .......... .......... .......... .......... .......... 25% 17.4M 60s
65650K .......... .......... .......... .......... .......... 25% 20.3M 60s
65700K .......... .......... .......... .......... .......... 25% 20.1M 60s
65750K .......... .......... .......... .......... .......... 25% 19.5M 60s
65800K .......... .......... .......... .......... .......... 25% 21.2M 60s
65850K .......... .......... .......... .......... .......... 25% 18.8M 60s
65900K .......... .......... .......... .......... .......... 25% 20.6M 60s
65950K .......... .......... .......... .......... .......... 25% 10.5M 60s
66000K .......... .......... .......... .......... .......... 25% 69.0M 60s
66050K .......... .......... .......... .......... .......... 25% 13.5M 60s
66100K .......... .......... .......... .......... .......... 25% 11.4M 59s
66150K .......... .......... .......... .......... .......... 25% 19.7M 59s
66200K .......... .......... .......... .......... .......... 25% 10.5M 59s
66250K .......... .......... .......... .......... .......... 25% 33.9M 59s
66300K .......... .......... .......... .......... .......... 25% 9.54M 59s
66350K .......... .......... .......... .......... .......... 25% 11.0M 59s
66400K .......... .......... .......... .......... .......... 25% 12.0M 59s
66450K .......... .......... .......... .......... .......... 25% 8.23M 59s
66500K .......... .......... .......... .......... .......... 25% 5.16M 59s
66550K .......... .......... .......... .......... .......... 25% 14.0M 59s
66600K .......... .......... .......... .......... .......... 25% 8.32M 59s
66650K .......... .......... .......... .......... .......... 25% 9.54M 59s
66700K .......... .......... .......... .......... .......... 25% 4.20M 59s
66750K .......... .......... .......... .......... .......... 25% 5.81M 59s
66800K .......... .......... .......... .......... .......... 25% 5.45M 59s
66850K .......... .......... .......... .......... .......... 25% 5.15M 59s
66900K .......... .......... .......... .......... .......... 25% 5.61M 59s
66950K .......... .......... .......... .......... .......... 25% 4.69M 59s
67000K .......... .......... .......... .......... .......... 25% 8.53M 59s
67050K .......... .......... .......... .......... .......... 25% 7.14M 59s
67100K .......... .......... .......... .......... .......... 25% 11.0M 59s
67150K .......... .......... .......... .......... .......... 25% 12.0M 59s
67200K .......... .......... .......... .......... .......... 25% 12.6M 59s
67250K .......... .......... .......... .......... .......... 25% 20.7M 58s
67300K .......... .......... .......... .......... .......... 25% 10.8M 58s
67350K .......... .......... .......... .......... .......... 25% 8.98M 58s
67400K .......... .......... .......... .......... .......... 25% 6.60M 58s
67450K .......... .......... .......... .......... .......... 25% 5.72M 58s
67500K .......... .......... .......... .......... .......... 25% 7.93M 58s
67550K .......... .......... .......... .......... .......... 25% 9.79M 58s
67600K .......... .......... .......... .......... .......... 25% 7.99M 58s
67650K .......... .......... .......... .......... .......... 25% 8.38M 58s
67700K .......... .......... .......... .......... .......... 25% 11.8M 58s
67750K .......... .......... .......... .......... .......... 25% 12.9M 58s
67800K .......... .......... .......... .......... .......... 25% 20.4M 58s
67850K .......... .......... .......... .......... .......... 25% 13.6M 58s
67900K .......... .......... .......... .......... .......... 25% 11.0M 58s
67950K .......... .......... .......... .......... .......... 25% 16.9M 58s
68000K .......... .......... .......... .......... .......... 25% 10.5M 58s
68050K .......... .......... .......... .......... .......... 25% 10.3M 58s
68100K .......... .......... .......... .......... .......... 25% 13.2M 58s
68150K .......... .......... .......... .......... .......... 26% 7.08M 58s
68200K .......... .......... .......... .......... .......... 26% 7.04M 58s
68250K .......... .......... .......... .......... .......... 26% 9.39M 58s
68300K .......... .......... .......... .......... .......... 26% 9.22M 58s
68350K .......... .......... .......... .......... .......... 26% 8.41M 58s
68400K .......... .......... .......... .......... .......... 26% 11.1M 58s
68450K .......... .......... .......... .......... .......... 26% 5.69M 57s
68500K .......... .......... .......... .......... .......... 26% 11.6M 57s
68550K .......... .......... .......... .......... .......... 26% 5.27M 57s
68600K .......... .......... .......... .......... .......... 26% 10.2M 57s
68650K .......... .......... .......... .......... .......... 26% 5.52M 57s
68700K .......... .......... .......... .......... .......... 26% 7.05M 57s
68750K .......... .......... .......... .......... .......... 26% 7.97M 57s
68800K .......... .......... .......... .......... .......... 26% 13.1M 57s
68850K .......... .......... .......... .......... .......... 26% 16.8M 57s
68900K .......... .......... .......... .......... .......... 26% 9.11M 57s
68950K .......... .......... .......... .......... .......... 26% 9.25M 57s
69000K .......... .......... .......... .......... .......... 26% 11.4M 57s
69050K .......... .......... .......... .......... .......... 26% 12.4M 57s
69100K .......... .......... .......... .......... .......... 26% 9.79M 57s
69150K .......... .......... .......... .......... .......... 26% 14.2M 57s
69200K .......... .......... .......... .......... .......... 26% 8.38M 57s
69250K .......... .......... .......... .......... .......... 26% 21.8M 57s
69300K .......... .......... .......... .......... .......... 26% 13.0M 57s
69350K .......... .......... .......... .......... .......... 26% 15.9M 57s
69400K .......... .......... .......... .......... .......... 26% 10.9M 57s
69450K .......... .......... .......... .......... .......... 26% 19.8M 57s
69500K .......... .......... .......... .......... .......... 26% 11.9M 57s
69550K .......... .......... .......... .......... .......... 26% 5.50M 57s
69600K .......... .......... .......... .......... .......... 26% 92.3M 56s
69650K .......... .......... .......... .......... .......... 26% 15.5M 56s
69700K .......... .......... .......... .......... .......... 26% 18.3M 56s
69750K .......... .......... .......... .......... .......... 26% 16.0M 56s
69800K .......... .......... .......... .......... .......... 26% 9.45M 56s
69850K .......... .......... .......... .......... .......... 26% 10.7M 56s
69900K .......... .......... .......... .......... .......... 26% 12.0M 56s
69950K .......... .......... .......... .......... .......... 26% 7.49M 56s
70000K .......... .......... .......... .......... .......... 26% 12.8M 56s
70050K .......... .......... .......... .......... .......... 26% 11.0M 56s
70100K .......... .......... .......... .......... .......... 26% 8.65M 56s
70150K .......... .......... .......... .......... .......... 26% 9.71M 56s
70200K .......... .......... .......... .......... .......... 26% 6.06M 56s
70250K .......... .......... .......... .......... .......... 26% 5.31M 56s
70300K .......... .......... .......... .......... .......... 26% 8.73M 56s
70350K .......... .......... .......... .......... .......... 26% 6.12M 56s
70400K .......... .......... .......... .......... .......... 26% 5.26M 56s
70450K .......... .......... .......... .......... .......... 26% 5.37M 56s
70500K .......... .......... .......... .......... .......... 26% 8.48M 56s
70550K .......... .......... .......... .......... .......... 26% 3.49M 56s
70600K .......... .......... .......... .......... .......... 26% 7.82M 56s
70650K .......... .......... .......... .......... .......... 26% 4.05M 56s
70700K .......... .......... .......... .......... .......... 26% 3.93M 56s
70750K .......... .......... .......... .......... .......... 27% 4.44M 56s
70800K .......... .......... .......... .......... .......... 27% 7.31M 56s
70850K .......... .......... .......... .......... .......... 27% 16.5M 56s
70900K .......... .......... .......... .......... .......... 27% 5.91M 56s
70950K .......... .......... .......... .......... .......... 27% 45.0M 56s
71000K .......... .......... .......... .......... .......... 27% 9.05M 55s
71050K .......... .......... .......... .......... .......... 27% 10.3M 55s
71100K .......... .......... .......... .......... .......... 27% 8.72M 55s
71150K .......... .......... .......... .......... .......... 27% 11.1M 55s
71200K .......... .......... .......... .......... .......... 27% 6.64M 55s
71250K .......... .......... .......... .......... .......... 27% 10.5M 55s
71300K .......... .......... .......... .......... .......... 27% 12.6M 55s
71350K .......... .......... .......... .......... .......... 27% 8.69M 55s
71400K .......... .......... .......... .......... .......... 27% 9.92M 55s
71450K .......... .......... .......... .......... .......... 27% 12.3M 55s
71500K .......... .......... .......... .......... .......... 27% 13.5M 55s
71550K .......... .......... .......... .......... .......... 27% 20.6M 55s
71600K .......... .......... .......... .......... .......... 27% 2.58M 55s
71650K .......... .......... .......... .......... .......... 27% 63.8M 55s
71700K .......... .......... .......... .......... .......... 27% 38.8M 55s
71750K .......... .......... .......... .......... .......... 27% 20.9M 55s
71800K .......... .......... .......... .......... .......... 27% 11.4M 55s
71850K .......... .......... .......... .......... .......... 27% 9.78M 55s
71900K .......... .......... .......... .......... .......... 27% 7.52M 55s
71950K .......... .......... .......... .......... .......... 27% 7.92M 55s
72000K .......... .......... .......... .......... .......... 27% 5.58M 55s
72050K .......... .......... .......... .......... .......... 27% 4.85M 55s
72100K .......... .......... .......... .......... .......... 27% 6.26M 55s
72150K .......... .......... .......... .......... .......... 27% 5.44M 55s
72200K .......... .......... .......... .......... .......... 27% 4.57M 55s
72250K .......... .......... .......... .......... .......... 27% 2.75M 55s
72300K .......... .......... .......... .......... .......... 27% 4.63M 55s
72350K .......... .......... .......... .......... .......... 27% 4.07M 55s
72400K .......... .......... .......... .......... .......... 27% 6.95M 54s
72450K .......... .......... .......... .......... .......... 27% 5.42M 54s
72500K .......... .......... .......... .......... .......... 27% 7.99M 54s
72550K .......... .......... .......... .......... .......... 27% 9.15M 54s
72600K .......... .......... .......... .......... .......... 27% 4.95M 54s
72650K .......... .......... .......... .......... .......... 27% 16.0M 54s
72700K .......... .......... .......... .......... .......... 27% 3.73M 54s
72750K .......... .......... .......... .......... .......... 27% 17.2M 54s
72800K .......... .......... .......... .......... .......... 27% 11.9M 54s
72850K .......... .......... .......... .......... .......... 27% 15.0M 54s
72900K .......... .......... .......... .......... .......... 27% 9.22M 54s
72950K .......... .......... .......... .......... .......... 27% 10.9M 54s
73000K .......... .......... .......... .......... .......... 27% 9.41M 54s
73050K .......... .......... .......... .......... .......... 27% 9.03M 54s
73100K .......... .......... .......... .......... .......... 27% 11.1M 54s
73150K .......... .......... .......... .......... .......... 27% 9.64M 54s
73200K .......... .......... .......... .......... .......... 27% 7.41M 54s
73250K .......... .......... .......... .......... .......... 27% 5.21M 54s
73300K .......... .......... .......... .......... .......... 27% 5.20M 54s
73350K .......... .......... .......... .......... .......... 27% 5.98M 54s
73400K .......... .......... .......... .......... .......... 28% 7.40M 54s
73450K .......... .......... .......... .......... .......... 28% 11.8M 54s
73500K .......... .......... .......... .......... .......... 28% 17.6M 54s
73550K .......... .......... .......... .......... .......... 28% 12.2M 54s
73600K .......... .......... .......... .......... .......... 28% 12.4M 54s
73650K .......... .......... .......... .......... .......... 28% 4.19M 54s
73700K .......... .......... .......... .......... .......... 28% 57.9M 54s
73750K .......... .......... .......... .......... .......... 28% 7.45M 54s
73800K .......... .......... .......... .......... .......... 28% 6.21M 53s
73850K .......... .......... .......... .......... .......... 28% 4.82M 53s
73900K .......... .......... .......... .......... .......... 28% 5.17M 53s
73950K .......... .......... .......... .......... .......... 28% 3.27M 53s
74000K .......... .......... .......... .......... .......... 28% 4.74M 53s
74050K .......... .......... .......... .......... .......... 28% 7.20M 53s
74100K .......... .......... .......... .......... .......... 28% 15.8M 53s
74150K .......... .......... .......... .......... .......... 28% 8.90M 53s
74200K .......... .......... .......... .......... .......... 28% 8.14M 53s
74250K .......... .......... .......... .......... .......... 28% 9.52M 53s
74300K .......... .......... .......... .......... .......... 28% 12.5M 53s
74350K .......... .......... .......... .......... .......... 28% 8.11M 53s
74400K .......... .......... .......... .......... .......... 28% 17.6M 53s
74450K .......... .......... .......... .......... .......... 28% 12.3M 53s
74500K .......... .......... .......... .......... .......... 28% 11.2M 53s
74550K .......... .......... .......... .......... .......... 28% 24.6M 53s
74600K .......... .......... .......... .......... .......... 28% 12.6M 53s
74650K .......... .......... .......... .......... .......... 28% 3.73M 53s
74700K .......... .......... .......... .......... .......... 28% 43.9M 53s
74750K .......... .......... .......... .......... .......... 28% 28.5M 53s
74800K .......... .......... .......... .......... .......... 28% 7.32M 53s
74850K .......... .......... .......... .......... .......... 28% 12.1M 53s
74900K .......... .......... .......... .......... .......... 28% 7.45M 53s
74950K .......... .......... .......... .......... .......... 28% 8.71M 53s
75000K .......... .......... .......... .......... .......... 28% 8.81M 53s
75050K .......... .......... .......... .......... .......... 28% 8.33M 53s
75100K .......... .......... .......... .......... .......... 28% 7.16M 53s
75150K .......... .......... .......... .......... .......... 28% 6.81M 53s
75200K .......... .......... .......... .......... .......... 28% 51.0M 53s
75250K .......... .......... .......... .......... .......... 28% 16.4M 52s
75300K .......... .......... .......... .......... .......... 28% 14.3M 52s
75350K .......... .......... .......... .......... .......... 28% 12.1M 52s
75400K .......... .......... .......... .......... .......... 28% 11.9M 52s
75450K .......... .......... .......... .......... .......... 28% 11.8M 52s
75500K .......... .......... .......... .......... .......... 28% 11.1M 52s
75550K .......... .......... .......... .......... .......... 28% 9.76M 52s
75600K .......... .......... .......... .......... .......... 28% 14.7M 52s
75650K .......... .......... .......... .......... .......... 28% 11.8M 52s
75700K .......... .......... .......... .......... .......... 28% 2.81M 52s
75750K .......... .......... .......... .......... .......... 28% 53.4M 52s
75800K .......... .......... .......... .......... .......... 28% 72.8M 52s
75850K .......... .......... .......... .......... .......... 28% 12.6M 52s
75900K .......... .......... .......... .......... .......... 28% 5.20M 52s
75950K .......... .......... .......... .......... .......... 28% 3.76M 52s
76000K .......... .......... .......... .......... .......... 29% 5.63M 52s
76050K .......... .......... .......... .......... .......... 29% 4.94M 52s
76100K .......... .......... .......... .......... .......... 29% 3.25M 52s
76150K .......... .......... .......... .......... .......... 29% 5.09M 52s
76200K .......... .......... .......... .......... .......... 29% 4.38M 52s
76250K .......... .......... .......... .......... .......... 29% 5.98M 52s
76300K .......... .......... .......... .......... .......... 29% 6.10M 52s
76350K .......... .......... .......... .......... .......... 29% 9.12M 52s
76400K .......... .......... .......... .......... .......... 29% 14.8M 52s
76450K .......... .......... .......... .......... .......... 29% 8.80M 52s
76500K .......... .......... .......... .......... .......... 29% 17.0M 52s
76550K .......... .......... .......... .......... .......... 29% 10.7M 52s
76600K .......... .......... .......... .......... .......... 29% 15.1M 52s
76650K .......... .......... .......... .......... .......... 29% 11.7M 52s
76700K .......... .......... .......... .......... .......... 29% 4.66M 52s
76750K .......... .......... .......... .......... .......... 29% 24.8M 51s
76800K .......... .......... .......... .......... .......... 29% 9.38M 51s
76850K .......... .......... .......... .......... .......... 29% 5.24M 51s
76900K .......... .......... .......... .......... .......... 29% 5.98M 51s
76950K .......... .......... .......... .......... .......... 29% 7.07M 51s
77000K .......... .......... .......... .......... .......... 29% 5.22M 51s
77050K .......... .......... .......... .......... .......... 29% 4.80M 51s
77100K .......... .......... .......... .......... .......... 29% 5.20M 51s
77150K .......... .......... .......... .......... .......... 29% 4.31M 51s
77200K .......... .......... .......... .......... .......... 29% 2.58M 51s
77250K .......... .......... .......... .......... .......... 29% 3.41M 51s
77300K .......... .......... .......... .......... .......... 29% 3.62M 51s
77350K .......... .......... .......... .......... .......... 29% 4.04M 51s
77400K .......... .......... .......... .......... .......... 29% 6.96M 51s
77450K .......... .......... .......... .......... .......... 29% 5.90M 51s
77500K .......... .......... .......... .......... .......... 29% 7.20M 51s
77550K .......... .......... .......... .......... .......... 29% 7.54M 51s
77600K .......... .......... .......... .......... .......... 29% 5.46M 51s
77650K .......... .......... .......... .......... .......... 29% 5.08M 51s
77700K .......... .......... .......... .......... .......... 29% 2.13M 51s
77750K .......... .......... .......... .......... .......... 29% 29.4M 51s
77800K .......... .......... .......... .......... .......... 29% 32.6M 51s
77850K .......... .......... .......... .......... .......... 29% 12.1M 51s
77900K .......... .......... .......... .......... .......... 29% 8.43M 51s
77950K .......... .......... .......... .......... .......... 29% 5.82M 51s
78000K .......... .......... .......... .......... .......... 29% 5.45M 51s
78050K .......... .......... .......... .......... .......... 29% 7.66M 51s
78100K .......... .......... .......... .......... .......... 29% 4.66M 51s
78150K .......... .......... .......... .......... .......... 29% 6.29M 51s
78200K .......... .......... .......... .......... .......... 29% 3.13M 51s
78250K .......... .......... .......... .......... .......... 29% 4.55M 51s
78300K .......... .......... .......... .......... .......... 29% 4.87M 51s
78350K .......... .......... .......... .......... .......... 29% 5.82M 51s
78400K .......... .......... .......... .......... .......... 29% 6.97M 51s
78450K .......... .......... .......... .......... .......... 29% 2.61M 51s
78500K .......... .......... .......... .......... .......... 29% 4.07M 51s
78550K .......... .......... .......... .......... .......... 29% 4.72M 51s
78600K .......... .......... .......... .......... .......... 29% 5.26M 51s
78650K .......... .......... .......... .......... .......... 30% 12.4M 51s
78700K .......... .......... .......... .......... .......... 30% 7.83M 51s
78750K .......... .......... .......... .......... .......... 30% 2.72M 51s
78800K .......... .......... .......... .......... .......... 30% 4.84M 51s
78850K .......... .......... .......... .......... .......... 30% 2.97M 51s
78900K .......... .......... .......... .......... .......... 30% 3.14M 51s
78950K .......... .......... .......... .......... .......... 30% 5.73M 50s
79000K .......... .......... .......... .......... .......... 30% 7.16M 50s
79050K .......... .......... .......... .......... .......... 30% 6.00M 50s
79100K .......... .......... .......... .......... .......... 30% 6.11M 50s
79150K .......... .......... .......... .......... .......... 30% 6.87M 50s
79200K .......... .......... .......... .......... .......... 30% 11.3M 50s
79250K .......... .......... .......... .......... .......... 30% 22.0M 50s
79300K .......... .......... .......... .......... .......... 30% 10.6M 50s
79350K .......... .......... .......... .......... .......... 30% 11.6M 50s
79400K .......... .......... .......... .......... .......... 30% 18.8M 50s
79450K .......... .......... .......... .......... .......... 30% 9.13M 50s
79500K .......... .......... .......... .......... .......... 30% 10.9M 50s
79550K .......... .......... .......... .......... .......... 30% 13.9M 50s
79600K .......... .......... .......... .......... .......... 30% 7.72M 50s
79650K .......... .......... .......... .......... .......... 30% 13.4M 50s
79700K .......... .......... .......... .......... .......... 30% 6.78M 50s
79750K .......... .......... .......... .......... .......... 30% 1.98M 50s
79800K .......... .......... .......... .......... .......... 30% 70.8M 50s
79850K .......... .......... .......... .......... .......... 30% 42.6M 50s
79900K .......... .......... .......... .......... .......... 30% 14.8M 50s
79950K .......... .......... .......... .......... .......... 30% 6.38M 50s
80000K .......... .......... .......... .......... .......... 30% 5.79M 50s
80050K .......... .......... .......... .......... .......... 30% 6.57M 50s
80100K .......... .......... .......... .......... .......... 30% 4.56M 50s
80150K .......... .......... .......... .......... .......... 30% 8.27M 50s
80200K .......... .......... .......... .......... .......... 30% 5.06M 50s
80250K .......... .......... .......... .......... .......... 30% 6.03M 50s
80300K .......... .......... .......... .......... .......... 30% 4.82M 50s
80350K .......... .......... .......... .......... .......... 30% 9.35M 50s
80400K .......... .......... .......... .......... .......... 30% 6.08M 50s
80450K .......... .......... .......... .......... .......... 30% 6.20M 50s
80500K .......... .......... .......... .......... .......... 30% 8.31M 50s
80550K .......... .......... .......... .......... .......... 30% 8.87M 50s
80600K .......... .......... .......... .......... .......... 30% 4.62M 49s
80650K .......... .......... .......... .......... .......... 30% 5.50M 49s
80700K .......... .......... .......... .......... .......... 30% 4.41M 49s
80750K .......... .......... .......... .......... .......... 30% 5.31M 49s
80800K .......... .......... .......... .......... .......... 30% 3.27M 49s
80850K .......... .......... .......... .......... .......... 30% 11.0M 49s
80900K .......... .......... .......... .......... .......... 30% 4.60M 49s
80950K .......... .......... .......... .......... .......... 30% 6.10M 49s
81000K .......... .......... .......... .......... .......... 30% 15.1M 49s
81050K .......... .......... .......... .......... .......... 30% 10.7M 49s
81100K .......... .......... .......... .......... .......... 30% 10.2M 49s
81150K .......... .......... .......... .......... .......... 30% 10.2M 49s
81200K .......... .......... .......... .......... .......... 30% 10.9M 49s
81250K .......... .......... .......... .......... .......... 31% 7.38M 49s
81300K .......... .......... .......... .......... .......... 31% 6.23M 49s
81350K .......... .......... .......... .......... .......... 31% 6.24M 49s
81400K .......... .......... .......... .......... .......... 31% 6.64M 49s
81450K .......... .......... .......... .......... .......... 31% 4.34M 49s
81500K .......... .......... .......... .......... .......... 31% 5.40M 49s
81550K .......... .......... .......... .......... .......... 31% 4.81M 49s
81600K .......... .......... .......... .......... .......... 31% 2.02M 49s
81650K .......... .......... .......... .......... .......... 31% 3.94M 49s
81700K .......... .......... .......... .......... .......... 31% 2.43M 49s
81750K .......... .......... .......... .......... .......... 31% 2.66M 49s
81800K .......... .......... .......... .......... .......... 31% 4.01M 49s
81850K .......... .......... .......... .......... .......... 31% 2.81M 49s
81900K .......... .......... .......... .......... .......... 31% 5.18M 49s
81950K .......... .......... .......... .......... .......... 31% 7.68M 49s
82000K .......... .......... .......... .......... .......... 31% 9.40M 49s
82050K .......... .......... .......... .......... .......... 31% 10.1M 49s
82100K .......... .......... .......... .......... .......... 31% 9.76M 49s
82150K .......... .......... .......... .......... .......... 31% 8.60M 49s
82200K .......... .......... .......... .......... .......... 31% 6.30M 49s
82250K .......... .......... .......... .......... .......... 31% 22.6M 49s
82300K .......... .......... .......... .......... .......... 31% 15.0M 49s
82350K .......... .......... .......... .......... .......... 31% 9.56M 49s
82400K .......... .......... .......... .......... .......... 31% 17.0M 49s
82450K .......... .......... .......... .......... .......... 31% 17.3M 49s
82500K .......... .......... .......... .......... .......... 31% 16.8M 49s
82550K .......... .......... .......... .......... .......... 31% 6.10M 49s
82600K .......... .......... .......... .......... .......... 31% 52.4M 48s
82650K .......... .......... .......... .......... .......... 31% 108M 48s
82700K .......... .......... .......... .......... .......... 31% 13.1M 48s
82750K .......... .......... .......... .......... .......... 31% 13.0M 48s
82800K .......... .......... .......... .......... .......... 31% 10.7M 48s
82850K .......... .......... .......... .......... .......... 31% 1.89M 48s
82900K .......... .......... .......... .......... .......... 31% 44.7M 48s
82950K .......... .......... .......... .......... .......... 31% 43.4M 48s
83000K .......... .......... .......... .......... .......... 31% 20.2M 48s
83050K .......... .......... .......... .......... .......... 31% 4.31M 48s
83100K .......... .......... .......... .......... .......... 31% 5.86M 48s
83150K .......... .......... .......... .......... .......... 31% 4.98M 48s
83200K .......... .......... .......... .......... .......... 31% 4.58M 48s
83250K .......... .......... .......... .......... .......... 31% 7.16M 48s
83300K .......... .......... .......... .......... .......... 31% 14.3M 48s
83350K .......... .......... .......... .......... .......... 31% 11.6M 48s
83400K .......... .......... .......... .......... .......... 31% 17.1M 48s
83450K .......... .......... .......... .......... .......... 31% 11.5M 48s
83500K .......... .......... .......... .......... .......... 31% 24.9M 48s
83550K .......... .......... .......... .......... .......... 31% 16.0M 48s
83600K .......... .......... .......... .......... .......... 31% 6.88M 48s
83650K .......... .......... .......... .......... .......... 31% 28.5M 48s
83700K .......... .......... .......... .......... .......... 31% 5.51M 48s
83750K .......... .......... .......... .......... .......... 31% 20.5M 48s
83800K .......... .......... .......... .......... .......... 31% 10.9M 48s
83850K .......... .......... .......... .......... .......... 31% 2.59M 48s
83900K .......... .......... .......... .......... .......... 32% 52.3M 48s
83950K .......... .......... .......... .......... .......... 32% 17.1M 48s
84000K .......... .......... .......... .......... .......... 32% 4.73M 48s
84050K .......... .......... .......... .......... .......... 32% 6.09M 48s
84100K .......... .......... .......... .......... .......... 32% 7.88M 48s
84150K .......... .......... .......... .......... .......... 32% 8.93M 48s
84200K .......... .......... .......... .......... .......... 32% 6.38M 48s
84250K .......... .......... .......... .......... .......... 32% 50.0M 47s
84300K .......... .......... .......... .......... .......... 32% 9.11M 47s
84350K .......... .......... .......... .......... .......... 32% 9.42M 47s
84400K .......... .......... .......... .......... .......... 32% 9.26M 47s
84450K .......... .......... .......... .......... .......... 32% 5.52M 47s
84500K .......... .......... .......... .......... .......... 32% 7.75M 47s
84550K .......... .......... .......... .......... .......... 32% 8.41M 47s
84600K .......... .......... .......... .......... .......... 32% 3.09M 47s
84650K .......... .......... .......... .......... .......... 32% 4.08M 47s
84700K .......... .......... .......... .......... .......... 32% 2.44M 47s
84750K .......... .......... .......... .......... .......... 32% 3.47M 47s
84800K .......... .......... .......... .......... .......... 32% 4.08M 47s
84850K .......... .......... .......... .......... .......... 32% 4.36M 47s
84900K .......... .......... .......... .......... .......... 32% 2.79M 47s
84950K .......... .......... .......... .......... .......... 32% 40.6M 47s
85000K .......... .......... .......... .......... .......... 32% 58.2M 47s
85050K .......... .......... .......... .......... .......... 32% 9.68M 47s
85100K .......... .......... .......... .......... .......... 32% 6.54M 47s
85150K .......... .......... .......... .......... .......... 32% 11.7M 47s
85200K .......... .......... .......... .......... .......... 32% 5.27M 47s
85250K .......... .......... .......... .......... .......... 32% 9.12M 47s
85300K .......... .......... .......... .......... .......... 32% 7.18M 47s
85350K .......... .......... .......... .......... .......... 32% 10.5M 47s
85400K .......... .......... .......... .......... .......... 32% 15.9M 47s
85450K .......... .......... .......... .......... .......... 32% 6.10M 47s
85500K .......... .......... .......... .......... .......... 32% 18.6M 47s
85550K .......... .......... .......... .......... .......... 32% 4.64M 47s
85600K .......... .......... .......... .......... .......... 32% 3.38M 47s
85650K .......... .......... .......... .......... .......... 32% 3.50M 47s
85700K .......... .......... .......... .......... .......... 32% 3.97M 47s
85750K .......... .......... .......... .......... .......... 32% 3.56M 47s
85800K .......... .......... .......... .......... .......... 32% 3.07M 47s
85850K .......... .......... .......... .......... .......... 32% 2.01M 47s
85900K .......... .......... .......... .......... .......... 32% 1.91M 47s
85950K .......... .......... .......... .......... .......... 32% 17.4M 47s
86000K .......... .......... .......... .......... .......... 32% 10.6M 47s
86050K .......... .......... .......... .......... .......... 32% 27.7M 47s
86100K .......... .......... .......... .......... .......... 32% 13.5M 47s
86150K .......... .......... .......... .......... .......... 32% 14.6M 47s
86200K .......... .......... .......... .......... .......... 32% 10.8M 47s
86250K .......... .......... .......... .......... .......... 32% 12.7M 47s
86300K .......... .......... .......... .......... .......... 32% 15.1M 47s
86350K .......... .......... .......... .......... .......... 32% 12.1M 47s
86400K .......... .......... .......... .......... .......... 32% 7.40M 47s
86450K .......... .......... .......... .......... .......... 32% 12.7M 46s
86500K .......... .......... .......... .......... .......... 33% 11.5M 46s
86550K .......... .......... .......... .......... .......... 33% 16.2M 46s
86600K .......... .......... .......... .......... .......... 33% 6.80M 46s
86650K .......... .......... .......... .......... .......... 33% 12.4M 46s
86700K .......... .......... .......... .......... .......... 33% 6.43M 46s
86750K .......... .......... .......... .......... .......... 33% 8.42M 46s
86800K .......... .......... .......... .......... .......... 33% 9.36M 46s
86850K .......... .......... .......... .......... .......... 33% 6.42M 46s
86900K .......... .......... .......... .......... .......... 33% 4.29M 46s
86950K .......... .......... .......... .......... .......... 33% 3.96M 46s
87000K .......... .......... .......... .......... .......... 33% 73.8M 46s
87050K .......... .......... .......... .......... .......... 33% 8.86M 46s
87100K .......... .......... .......... .......... .......... 33% 8.07M 46s
87150K .......... .......... .......... .......... .......... 33% 5.67M 46s
87200K .......... .......... .......... .......... .......... 33% 4.63M 46s
87250K .......... .......... .......... .......... .......... 33% 6.81M 46s
87300K .......... .......... .......... .......... .......... 33% 7.47M 46s
87350K .......... .......... .......... .......... .......... 33% 7.39M 46s
87400K .......... .......... .......... .......... .......... 33% 12.0M 46s
87450K .......... .......... .......... .......... .......... 33% 7.02M 46s
87500K .......... .......... .......... .......... .......... 33% 7.06M 46s
87550K .......... .......... .......... .......... .......... 33% 8.72M 46s
87600K .......... .......... .......... .......... .......... 33% 6.51M 46s
87650K .......... .......... .......... .......... .......... 33% 6.21M 46s
87700K .......... .......... .......... .......... .......... 33% 3.78M 46s
87750K .......... .......... .......... .......... .......... 33% 4.76M 46s
87800K .......... .......... .......... .......... .......... 33% 6.32M 46s
87850K .......... .......... .......... .......... .......... 33% 4.82M 46s
87900K .......... .......... .......... .......... .......... 33% 3.67M 46s
87950K .......... .......... .......... .......... .......... 33% 3.66M 46s
88000K .......... .......... .......... .......... .......... 33% 63.5M 46s
88050K .......... .......... .......... .......... .......... 33% 47.3M 46s
88100K .......... .......... .......... .......... .......... 33% 16.2M 46s
88150K .......... .......... .......... .......... .......... 33% 9.50M 46s
88200K .......... .......... .......... .......... .......... 33% 8.24M 46s
88250K .......... .......... .......... .......... .......... 33% 7.35M 46s
88300K .......... .......... .......... .......... .......... 33% 11.6M 46s
88350K .......... .......... .......... .......... .......... 33% 10.5M 45s
88400K .......... .......... .......... .......... .......... 33% 17.4M 45s
88450K .......... .......... .......... .......... .......... 33% 9.57M 45s
88500K .......... .......... .......... .......... .......... 33% 18.4M 45s
88550K .......... .......... .......... .......... .......... 33% 17.4M 45s
88600K .......... .......... .......... .......... .......... 33% 12.5M 45s
88650K .......... .......... .......... .......... .......... 33% 26.0M 45s
88700K .......... .......... .......... .......... .......... 33% 19.3M 45s
88750K .......... .......... .......... .......... .......... 33% 16.8M 45s
88800K .......... .......... .......... .......... .......... 33% 16.4M 45s
88850K .......... .......... .......... .......... .......... 33% 13.0M 45s
88900K .......... .......... .......... .......... .......... 33% 14.6M 45s
88950K .......... .......... .......... .......... .......... 33% 12.1M 45s
89000K .......... .......... .......... .......... .......... 33% 2.48M 45s
89050K .......... .......... .......... .......... .......... 33% 48.7M 45s
89100K .......... .......... .......... .......... .......... 34% 60.3M 45s
89150K .......... .......... .......... .......... .......... 34% 47.6M 45s
89200K .......... .......... .......... .......... .......... 34% 23.1M 45s
89250K .......... .......... .......... .......... .......... 34% 6.32M 45s
89300K .......... .......... .......... .......... .......... 34% 54.0M 45s
89350K .......... .......... .......... .......... .......... 34% 13.0M 45s
89400K .......... .......... .......... .......... .......... 34% 12.4M 45s
89450K .......... .......... .......... .......... .......... 34% 12.4M 45s
89500K .......... .......... .......... .......... .......... 34% 13.5M 45s
89550K .......... .......... .......... .......... .......... 34% 13.6M 45s
89600K .......... .......... .......... .......... .......... 34% 11.8M 45s
89650K .......... .......... .......... .......... .......... 34% 13.1M 45s
89700K .......... .......... .......... .......... .......... 34% 10.6M 45s
89750K .......... .......... .......... .......... .......... 34% 9.96M 45s
89800K .......... .......... .......... .......... .......... 34% 16.3M 45s
89850K .......... .......... .......... .......... .......... 34% 8.52M 45s
89900K .......... .......... .......... .......... .......... 34% 21.7M 45s
89950K .......... .......... .......... .......... .......... 34% 42.5M 44s
90000K .......... .......... .......... .......... .......... 34% 2.71M 44s
90050K .......... .......... .......... .......... .......... 34% 80.4M 44s
90100K .......... .......... .......... .......... .......... 34% 56.5M 44s
90150K .......... .......... .......... .......... .......... 34% 58.2M 44s
90200K .......... .......... .......... .......... .......... 34% 43.5M 44s
90250K .......... .......... .......... .......... .......... 34% 14.4M 44s
90300K .......... .......... .......... .......... .......... 34% 10.9M 44s
90350K .......... .......... .......... .......... .......... 34% 14.3M 44s
90400K .......... .......... .......... .......... .......... 34% 9.39M 44s
90450K .......... .......... .......... .......... .......... 34% 9.97M 44s
90500K .......... .......... .......... .......... .......... 34% 7.64M 44s
90550K .......... .......... .......... .......... .......... 34% 22.9M 44s
90600K .......... .......... .......... .......... .......... 34% 8.72M 44s
90650K .......... .......... .......... .......... .......... 34% 18.7M 44s
90700K .......... .......... .......... .......... .......... 34% 9.60M 44s
90750K .......... .......... .......... .......... .......... 34% 15.4M 44s
90800K .......... .......... .......... .......... .......... 34% 18.3M 44s
90850K .......... .......... .......... .......... .......... 34% 10.1M 44s
90900K .......... .......... .......... .......... .......... 34% 15.1M 44s
90950K .......... .......... .......... .......... .......... 34% 9.55M 44s
91000K .......... .......... .......... .......... .......... 34% 10.5M 44s
91050K .......... .......... .......... .......... .......... 34% 3.98M 44s
91100K .......... .......... .......... .......... .......... 34% 36.6M 44s
91150K .......... .......... .......... .......... .......... 34% 85.2M 44s
91200K .......... .......... .......... .......... .......... 34% 14.4M 44s
91250K .......... .......... .......... .......... .......... 34% 9.86M 44s
91300K .......... .......... .......... .......... .......... 34% 10.4M 44s
91350K .......... .......... .......... .......... .......... 34% 4.65M 44s
91400K .......... .......... .......... .......... .......... 34% 20.5M 44s
91450K .......... .......... .......... .......... .......... 34% 5.60M 44s
91500K .......... .......... .......... .......... .......... 34% 51.0M 44s
91550K .......... .......... .......... .......... .......... 34% 9.46M 44s
91600K .......... .......... .......... .......... .......... 34% 8.47M 44s
91650K .......... .......... .......... .......... .......... 34% 8.20M 44s
91700K .......... .......... .......... .......... .......... 34% 10.3M 44s
91750K .......... .......... .......... .......... .......... 35% 8.64M 43s
91800K .......... .......... .......... .......... .......... 35% 8.38M 43s
91850K .......... .......... .......... .......... .......... 35% 5.84M 43s
91900K .......... .......... .......... .......... .......... 35% 8.25M 43s
91950K .......... .......... .......... .......... .......... 35% 6.43M 43s
92000K .......... .......... .......... .......... .......... 35% 8.95M 43s
92050K .......... .......... .......... .......... .......... 35% 3.00M 43s
92100K .......... .......... .......... .......... .......... 35% 66.6M 43s
92150K .......... .......... .......... .......... .......... 35% 7.56M 43s
92200K .......... .......... .......... .......... .......... 35% 7.13M 43s
92250K .......... .......... .......... .......... .......... 35% 3.79M 43s
92300K .......... .......... .......... .......... .......... 35% 6.40M 43s
92350K .......... .......... .......... .......... .......... 35% 4.91M 43s
92400K .......... .......... .......... .......... .......... 35% 5.87M 43s
92450K .......... .......... .......... .......... .......... 35% 5.00M 43s
92500K .......... .......... .......... .......... .......... 35% 7.42M 43s
92550K .......... .......... .......... .......... .......... 35% 10.9M 43s
92600K .......... .......... .......... .......... .......... 35% 7.64M 43s
92650K .......... .......... .......... .......... .......... 35% 11.1M 43s
92700K .......... .......... .......... .......... .......... 35% 6.91M 43s
92750K .......... .......... .......... .......... .......... 35% 8.82M 43s
92800K .......... .......... .......... .......... .......... 35% 6.23M 43s
92850K .......... .......... .......... .......... .......... 35% 6.38M 43s
92900K .......... .......... .......... .......... .......... 35% 5.96M 43s
92950K .......... .......... .......... .......... .......... 35% 8.08M 43s
93000K .......... .......... .......... .......... .......... 35% 5.20M 43s
93050K .......... .......... .......... .......... .......... 35% 11.6M 43s
93100K .......... .......... .......... .......... .......... 35% 3.18M 43s
93150K .......... .......... .......... .......... .......... 35% 67.0M 43s
93200K .......... .......... .......... .......... .......... 35% 15.9M 43s
93250K .......... .......... .......... .......... .......... 35% 21.6M 43s
93300K .......... .......... .......... .......... .......... 35% 11.1M 43s
93350K .......... .......... .......... .......... .......... 35% 7.46M 43s
93400K .......... .......... .......... .......... .......... 35% 10.4M 43s
93450K .......... .......... .......... .......... .......... 35% 7.85M 43s
93500K .......... .......... .......... .......... .......... 35% 6.85M 43s
93550K .......... .......... .......... .......... .......... 35% 11.4M 43s
93600K .......... .......... .......... .......... .......... 35% 4.79M 43s
93650K .......... .......... .......... .......... .......... 35% 9.46M 43s
93700K .......... .......... .......... .......... .......... 35% 6.98M 43s
93750K .......... .......... .......... .......... .......... 35% 9.03M 43s
93800K .......... .......... .......... .......... .......... 35% 6.58M 43s
93850K .......... .......... .......... .......... .......... 35% 6.27M 42s
93900K .......... .......... .......... .......... .......... 35% 6.17M 42s
93950K .......... .......... .......... .......... .......... 35% 6.92M 42s
94000K .......... .......... .......... .......... .......... 35% 4.65M 42s
94050K .......... .......... .......... .......... .......... 35% 11.8M 42s
94100K .......... .......... .......... .......... .......... 35% 2.65M 42s
94150K .......... .......... .......... .......... .......... 35% 88.8M 42s
94200K .......... .......... .......... .......... .......... 35% 85.5M 42s
94250K .......... .......... .......... .......... .......... 35% 73.9M 42s
94300K .......... .......... .......... .......... .......... 35% 1.35M 42s
94350K .......... .......... .......... .......... .......... 36% 4.77M 42s
94400K .......... .......... .......... .......... .......... 36% 7.36M 42s
94450K .......... .......... .......... .......... .......... 36% 4.11M 42s
94500K .......... .......... .......... .......... .......... 36% 5.53M 42s
94550K .......... .......... .......... .......... .......... 36% 4.05M 42s
94600K .......... .......... .......... .......... .......... 36% 3.70M 42s
94650K .......... .......... .......... .......... .......... 36% 3.88M 42s
94700K .......... .......... .......... .......... .......... 36% 4.11M 42s
94750K .......... .......... .......... .......... .......... 36% 3.49M 42s
94800K .......... .......... .......... .......... .......... 36% 2.27M 42s
94850K .......... .......... .......... .......... .......... 36% 2.69M 42s
94900K .......... .......... .......... .......... .......... 36% 5.03M 42s
94950K .......... .......... .......... .......... .......... 36% 3.52M 42s
95000K .......... .......... .......... .......... .......... 36% 5.23M 42s
95050K .......... .......... .......... .......... .......... 36% 3.07M 42s
95100K .......... .......... .......... .......... .......... 36% 4.62M 42s
95150K .......... .......... .......... .......... .......... 36% 2.98M 42s
95200K .......... .......... .......... .......... .......... 36% 8.60M 42s
95250K .......... .......... .......... .......... .......... 36% 18.8M 42s
95300K .......... .......... .......... .......... .......... 36% 9.70M 42s
95350K .......... .......... .......... .......... .......... 36% 4.92M 42s
95400K .......... .......... .......... .......... .......... 36% 13.9M 42s
95450K .......... .......... .......... .......... .......... 36% 7.61M 42s
95500K .......... .......... .......... .......... .......... 36% 10.1M 42s
95550K .......... .......... .......... .......... .......... 36% 9.66M 42s
95600K .......... .......... .......... .......... .......... 36% 6.01M 42s
95650K .......... .......... .......... .......... .......... 36% 7.42M 42s
95700K .......... .......... .......... .......... .......... 36% 7.33M 42s
95750K .......... .......... .......... .......... .......... 36% 5.99M 42s
95800K .......... .......... .......... .......... .......... 36% 8.66M 42s
95850K .......... .......... .......... .......... .......... 36% 5.41M 42s
95900K .......... .......... .......... .......... .......... 36% 7.15M 42s
95950K .......... .......... .......... .......... .......... 36% 3.30M 42s
96000K .......... .......... .......... .......... .......... 36% 3.68M 42s
96050K .......... .......... .......... .......... .......... 36% 3.66M 42s
96100K .......... .......... .......... .......... .......... 36% 4.96M 42s
96150K .......... .......... .......... .......... .......... 36% 216K 42s
96200K .......... .......... .......... .......... .......... 36% 3.69M 42s
96250K .......... .......... .......... .......... .......... 36% 6.10M 42s
96300K .......... .......... .......... .......... .......... 36% 4.55M 42s
96350K .......... .......... .......... .......... .......... 36% 3.78M 42s
96400K .......... .......... .......... .......... .......... 36% 5.18M 42s
96450K .......... .......... .......... .......... .......... 36% 3.12M 42s
96500K .......... .......... .......... .......... .......... 36% 4.32M 42s
96550K .......... .......... .......... .......... .......... 36% 3.51M 42s
96600K .......... .......... .......... .......... .......... 36% 2.72M 42s
96650K .......... .......... .......... .......... .......... 36% 6.64M 42s
96700K .......... .......... .......... .......... .......... 36% 7.36M 42s
96750K .......... .......... .......... .......... .......... 36% 12.3M 42s
96800K .......... .......... .......... .......... .......... 36% 11.9M 42s
96850K .......... .......... .......... .......... .......... 36% 11.0M 42s
96900K .......... .......... .......... .......... .......... 36% 7.43M 42s
96950K .......... .......... .......... .......... .......... 36% 6.13M 42s
97000K .......... .......... .......... .......... .......... 37% 9.23M 42s
97050K .......... .......... .......... .......... .......... 37% 9.47M 42s
97100K .......... .......... .......... .......... .......... 37% 6.15M 42s
97150K .......... .......... .......... .......... .......... 37% 7.24M 42s
97200K .......... .......... .......... .......... .......... 37% 3.10M 42s
97250K .......... .......... .......... .......... .......... 37% 12.1M 42s
97300K .......... .......... .......... .......... .......... 37% 3.99M 42s
97350K .......... .......... .......... .......... .......... 37% 3.44M 42s
97400K .......... .......... .......... .......... .......... 37% 2.39M 42s
97450K .......... .......... .......... .......... .......... 37% 2.93M 42s
97500K .......... .......... .......... .......... .......... 37% 3.71M 42s
97550K .......... .......... .......... .......... .......... 37% 11.1M 42s
97600K .......... .......... .......... .......... .......... 37% 10.2M 42s
97650K .......... .......... .......... .......... .......... 37% 15.9M 42s
97700K .......... .......... .......... .......... .......... 37% 7.96M 42s
97750K .......... .......... .......... .......... .......... 37% 9.80M 41s
97800K .......... .......... .......... .......... .......... 37% 12.2M 41s
97850K .......... .......... .......... .......... .......... 37% 11.6M 41s
97900K .......... .......... .......... .......... .......... 37% 12.3M 41s
97950K .......... .......... .......... .......... .......... 37% 10.8M 41s
98000K .......... .......... .......... .......... .......... 37% 12.1M 41s
98050K .......... .......... .......... .......... .......... 37% 16.3M 41s
98100K .......... .......... .......... .......... .......... 37% 12.1M 41s
98150K .......... .......... .......... .......... .......... 37% 11.8M 41s
98200K .......... .......... .......... .......... .......... 37% 3.74M 41s
98250K .......... .......... .......... .......... .......... 37% 54.8M 41s
98300K .......... .......... .......... .......... .......... 37% 48.6M 41s
98350K .......... .......... .......... .......... .......... 37% 35.8M 41s
98400K .......... .......... .......... .......... .......... 37% 7.41M 41s
98450K .......... .......... .......... .......... .......... 37% 9.76M 41s
98500K .......... .......... .......... .......... .......... 37% 7.62M 41s
98550K .......... .......... .......... .......... .......... 37% 10.2M 41s
98600K .......... .......... .......... .......... .......... 37% 9.45M 41s
98650K .......... .......... .......... .......... .......... 37% 10.5M 41s
98700K .......... .......... .......... .......... .......... 37% 6.38M 41s
98750K .......... .......... .......... .......... .......... 37% 8.45M 41s
98800K .......... .......... .......... .......... .......... 37% 6.98M 41s
98850K .......... .......... .......... .......... .......... 37% 6.13M 41s
98900K .......... .......... .......... .......... .......... 37% 9.14M 41s
98950K .......... .......... .......... .......... .......... 37% 6.83M 41s
99000K .......... .......... .......... .......... .......... 37% 8.40M 41s
99050K .......... .......... .......... .......... .......... 37% 6.34M 41s
99100K .......... .......... .......... .......... .......... 37% 4.13M 41s
99150K .......... .......... .......... .......... .......... 37% 16.5M 41s
99200K .......... .......... .......... .......... .......... 37% 5.82M 41s
99250K .......... .......... .......... .......... .......... 37% 4.64M 41s
99300K .......... .......... .......... .......... .......... 37% 6.29M 41s
99350K .......... .......... .......... .......... .......... 37% 6.51M 41s
99400K .......... .......... .......... .......... .......... 37% 17.3M 41s
99450K .......... .......... .......... .......... .......... 37% 6.48M 41s
99500K .......... .......... .......... .......... .......... 37% 10.9M 41s
99550K .......... .......... .......... .......... .......... 37% 10.8M 41s
99600K .......... .......... .......... .......... .......... 38% 7.63M 41s
99650K .......... .......... .......... .......... .......... 38% 15.9M 41s
99700K .......... .......... .......... .......... .......... 38% 13.4M 41s
99750K .......... .......... .......... .......... .......... 38% 8.62M 41s
99800K .......... .......... .......... .......... .......... 38% 6.88M 41s
99850K .......... .......... .......... .......... .......... 38% 9.84M 40s
99900K .......... .......... .......... .......... .......... 38% 10.1M 40s
99950K .......... .......... .......... .......... .......... 38% 18.8M 40s
100000K .......... .......... .......... .......... .......... 38% 6.10M 40s
100050K .......... .......... .......... .......... .......... 38% 39.4M 40s
100100K .......... .......... .......... .......... .......... 38% 6.07M 40s
100150K .......... .......... .......... .......... .......... 38% 6.78M 40s
100200K .......... .......... .......... .......... .......... 38% 9.76M 40s
100250K .......... .......... .......... .......... .......... 38% 1.71M 40s
100300K .......... .......... .......... .......... .......... 38% 52.5M 40s
100350K .......... .......... .......... .......... .......... 38% 54.3M 40s
100400K .......... .......... .......... .......... .......... 38% 44.7M 40s
100450K .......... .......... .......... .......... .......... 38% 26.8M 40s
100500K .......... .......... .......... .......... .......... 38% 11.1M 40s
100550K .......... .......... .......... .......... .......... 38% 14.7M 40s
100600K .......... .......... .......... .......... .......... 38% 7.84M 40s
100650K .......... .......... .......... .......... .......... 38% 6.96M 40s
100700K .......... .......... .......... .......... .......... 38% 10.3M 40s
100750K .......... .......... .......... .......... .......... 38% 5.90M 40s
100800K .......... .......... .......... .......... .......... 38% 5.66M 40s
100850K .......... .......... .......... .......... .......... 38% 7.26M 40s
100900K .......... .......... .......... .......... .......... 38% 7.46M 40s
100950K .......... .......... .......... .......... .......... 38% 4.95M 40s
101000K .......... .......... .......... .......... .......... 38% 8.72M 40s
101050K .......... .......... .......... .......... .......... 38% 6.18M 40s
101100K .......... .......... .......... .......... .......... 38% 16.5M 40s
101150K .......... .......... .......... .......... .......... 38% 10.9M 40s
101200K .......... .......... .......... .......... .......... 38% 8.92M 40s
101250K .......... .......... .......... .......... .......... 38% 10.9M 40s
101300K .......... .......... .......... .......... .......... 38% 2.45M 40s
101350K .......... .......... .......... .......... .......... 38% 60.3M 40s
101400K .......... .......... .......... .......... .......... 38% 60.2M 40s
101450K .......... .......... .......... .......... .......... 38% 25.1M 40s
101500K .......... .......... .......... .......... .......... 38% 17.2M 40s
101550K .......... .......... .......... .......... .......... 38% 18.2M 40s
101600K .......... .......... .......... .......... .......... 38% 11.0M 40s
101650K .......... .......... .......... .......... .......... 38% 16.7M 40s
101700K .......... .......... .......... .......... .......... 38% 9.18M 40s
101750K .......... .......... .......... .......... .......... 38% 15.9M 40s
101800K .......... .......... .......... .......... .......... 38% 9.21M 40s
101850K .......... .......... .......... .......... .......... 38% 16.3M 40s
101900K .......... .......... .......... .......... .......... 38% 10.5M 40s
101950K .......... .......... .......... .......... .......... 38% 14.3M 39s
102000K .......... .......... .......... .......... .......... 38% 16.6M 39s
102050K .......... .......... .......... .......... .......... 38% 17.0M 39s
102100K .......... .......... .......... .......... .......... 38% 16.8M 39s
102150K .......... .......... .......... .......... .......... 38% 19.7M 39s
102200K .......... .......... .......... .......... .......... 38% 17.6M 39s
102250K .......... .......... .......... .......... .......... 39% 9.13M 39s
102300K .......... .......... .......... .......... .......... 39% 1.77M 39s
102350K .......... .......... .......... .......... .......... 39% 46.3M 39s
102400K .......... .......... .......... .......... .......... 39% 67.9M 39s
102450K .......... .......... .......... .......... .......... 39% 66.9M 39s
102500K .......... .......... .......... .......... .......... 39% 20.1M 39s
102550K .......... .......... .......... .......... .......... 39% 10.4M 39s
102600K .......... .......... .......... .......... .......... 39% 9.64M 39s
102650K .......... .......... .......... .......... .......... 39% 20.4M 39s
102700K .......... .......... .......... .......... .......... 39% 9.50M 39s
102750K .......... .......... .......... .......... .......... 39% 11.6M 39s
102800K .......... .......... .......... .......... .......... 39% 21.1M 39s
102850K .......... .......... .......... .......... .......... 39% 9.08M 39s
102900K .......... .......... .......... .......... .......... 39% 14.0M 39s
102950K .......... .......... .......... .......... .......... 39% 10.0M 39s
103000K .......... .......... .......... .......... .......... 39% 16.4M 39s
103050K .......... .......... .......... .......... .......... 39% 11.9M 39s
103100K .......... .......... .......... .......... .......... 39% 9.86M 39s
103150K .......... .......... .......... .......... .......... 39% 18.2M 39s
103200K .......... .......... .......... .......... .......... 39% 12.1M 39s
103250K .......... .......... .......... .......... .......... 39% 21.0M 39s
103300K .......... .......... .......... .......... .......... 39% 6.45M 39s
103350K .......... .......... .......... .......... .......... 39% 4.28M 39s
103400K .......... .......... .......... .......... .......... 39% 51.2M 39s
103450K .......... .......... .......... .......... .......... 39% 52.2M 39s
103500K .......... .......... .......... .......... .......... 39% 5.48M 39s
103550K .......... .......... .......... .......... .......... 39% 6.57M 39s
103600K .......... .......... .......... .......... .......... 39% 6.73M 39s
103650K .......... .......... .......... .......... .......... 39% 7.69M 39s
103700K .......... .......... .......... .......... .......... 39% 5.14M 39s
103750K .......... .......... .......... .......... .......... 39% 9.28M 39s
103800K .......... .......... .......... .......... .......... 39% 10.4M 39s
103850K .......... .......... .......... .......... .......... 39% 9.71M 39s
103900K .......... .......... .......... .......... .......... 39% 12.2M 39s
103950K .......... .......... .......... .......... .......... 39% 7.91M 39s
104000K .......... .......... .......... .......... .......... 39% 12.9M 39s
104050K .......... .......... .......... .......... .......... 39% 9.05M 39s
104100K .......... .......... .......... .......... .......... 39% 8.91M 38s
104150K .......... .......... .......... .......... .......... 39% 12.6M 38s
104200K .......... .......... .......... .......... .......... 39% 7.17M 38s
104250K .......... .......... .......... .......... .......... 39% 7.82M 38s
104300K .......... .......... .......... .......... .......... 39% 22.2M 38s
104350K .......... .......... .......... .......... .......... 39% 2.98M 38s
104400K .......... .......... .......... .......... .......... 39% 60.1M 38s
104450K .......... .......... .......... .......... .......... 39% 60.8M 38s
104500K .......... .......... .......... .......... .......... 39% 14.0M 38s
104550K .......... .......... .......... .......... .......... 39% 9.40M 38s
104600K .......... .......... .......... .......... .......... 39% 9.83M 38s
104650K .......... .......... .......... .......... .......... 39% 8.71M 38s
104700K .......... .......... .......... .......... .......... 39% 7.16M 38s
104750K .......... .......... .......... .......... .......... 39% 8.70M 38s
104800K .......... .......... .......... .......... .......... 39% 9.10M 38s
104850K .......... .......... .......... .......... .......... 40% 6.83M 38s
104900K .......... .......... .......... .......... .......... 40% 5.45M 38s
104950K .......... .......... .......... .......... .......... 40% 3.41M 38s
105000K .......... .......... .......... .......... .......... 40% 8.48M 38s
105050K .......... .......... .......... .......... .......... 40% 4.41M 38s
105100K .......... .......... .......... .......... .......... 40% 4.69M 38s
105150K .......... .......... .......... .......... .......... 40% 5.05M 38s
105200K .......... .......... .......... .......... .......... 40% 4.24M 38s
105250K .......... .......... .......... .......... .......... 40% 5.25M 38s
105300K .......... .......... .......... .......... .......... 40% 11.1M 38s
105350K .......... .......... .......... .......... .......... 40% 2.59M 38s
105400K .......... .......... .......... .......... .......... 40% 33.7M 38s
105450K .......... .......... .......... .......... .......... 40% 16.1M 38s
105500K .......... .......... .......... .......... .......... 40% 6.28M 38s
105550K .......... .......... .......... .......... .......... 40% 5.67M 38s
105600K .......... .......... .......... .......... .......... 40% 6.24M 38s
105650K .......... .......... .......... .......... .......... 40% 2.43M 38s
105700K .......... .......... .......... .......... .......... 40% 3.14M 38s
105750K .......... .......... .......... .......... .......... 40% 3.81M 38s
105800K .......... .......... .......... .......... .......... 40% 6.88M 38s
105850K .......... .......... .......... .......... .......... 40% 11.0M 38s
105900K .......... .......... .......... .......... .......... 40% 17.9M 38s
105950K .......... .......... .......... .......... .......... 40% 17.4M 38s
106000K .......... .......... .......... .......... .......... 40% 17.0M 38s
106050K .......... .......... .......... .......... .......... 40% 17.4M 38s
106100K .......... .......... .......... .......... .......... 40% 8.10M 38s
106150K .......... .......... .......... .......... .......... 40% 11.3M 38s
106200K .......... .......... .......... .......... .......... 40% 11.0M 38s
106250K .......... .......... .......... .......... .......... 40% 16.3M 38s
106300K .......... .......... .......... .......... .......... 40% 10.6M 38s
106350K .......... .......... .......... .......... .......... 40% 7.23M 38s
106400K .......... .......... .......... .......... .......... 40% 2.55M 38s
106450K .......... .......... .......... .......... .......... 40% 40.7M 38s
106500K .......... .......... .......... .......... .......... 40% 45.4M 38s
106550K .......... .......... .......... .......... .......... 40% 12.7M 38s
106600K .......... .......... .......... .......... .......... 40% 4.08M 38s
106650K .......... .......... .......... .......... .......... 40% 5.25M 37s
106700K .......... .......... .......... .......... .......... 40% 5.09M 37s
106750K .......... .......... .......... .......... .......... 40% 3.77M 37s
106800K .......... .......... .......... .......... .......... 40% 5.15M 37s
106850K .......... .......... .......... .......... .......... 40% 5.25M 37s
106900K .......... .......... .......... .......... .......... 40% 6.21M 37s
106950K .......... .......... .......... .......... .......... 40% 5.00M 37s
107000K .......... .......... .......... .......... .......... 40% 12.2M 37s
107050K .......... .......... .......... .......... .......... 40% 22.1M 37s
107100K .......... .......... .......... .......... .......... 40% 9.48M 37s
107150K .......... .......... .......... .......... .......... 40% 35.5M 37s
107200K .......... .......... .......... .......... .......... 40% 19.6M 37s
107250K .......... .......... .......... .......... .......... 40% 12.6M 37s
107300K .......... .......... .......... .......... .......... 40% 21.7M 37s
107350K .......... .......... .......... .......... .......... 40% 8.53M 37s
107400K .......... .......... .......... .......... .......... 40% 3.77M 37s
107450K .......... .......... .......... .......... .......... 40% 53.4M 37s
107500K .......... .......... .......... .......... .......... 41% 55.6M 37s
107550K .......... .......... .......... .......... .......... 41% 67.1M 37s
107600K .......... .......... .......... .......... .......... 41% 8.57M 37s
107650K .......... .......... .......... .......... .......... 41% 14.8M 37s
107700K .......... .......... .......... .......... .......... 41% 10.2M 37s
107750K .......... .......... .......... .......... .......... 41% 10.9M 37s
107800K .......... .......... .......... .......... .......... 41% 4.99M 37s
107850K .......... .......... .......... .......... .......... 41% 11.9M 37s
107900K .......... .......... .......... .......... .......... 41% 8.05M 37s
107950K .......... .......... .......... .......... .......... 41% 7.73M 37s
108000K .......... .......... .......... .......... .......... 41% 8.52M 37s
108050K .......... .......... .......... .......... .......... 41% 7.35M 37s
108100K .......... .......... .......... .......... .......... 41% 7.77M 37s
108150K .......... .......... .......... .......... .......... 41% 11.6M 37s
108200K .......... .......... .......... .......... .......... 41% 9.49M 37s
108250K .......... .......... .......... .......... .......... 41% 7.10M 37s
108300K .......... .......... .......... .......... .......... 41% 15.2M 37s
108350K .......... .......... .......... .......... .......... 41% 12.3M 37s
108400K .......... .......... .......... .......... .......... 41% 11.9M 37s
108450K .......... .......... .......... .......... .......... 41% 2.40M 37s
108500K .......... .......... .......... .......... .......... 41% 58.1M 37s
108550K .......... .......... .......... .......... .......... 41% 55.6M 37s
108600K .......... .......... .......... .......... .......... 41% 37.4M 37s
108650K .......... .......... .......... .......... .......... 41% 10.7M 37s
108700K .......... .......... .......... .......... .......... 41% 3.89M 37s
108750K .......... .......... .......... .......... .......... 41% 6.12M 37s
108800K .......... .......... .......... .......... .......... 41% 5.19M 37s
108850K .......... .......... .......... .......... .......... 41% 5.22M 37s
108900K .......... .......... .......... .......... .......... 41% 4.97M 37s
108950K .......... .......... .......... .......... .......... 41% 7.02M 37s
109000K .......... .......... .......... .......... .......... 41% 4.66M 37s
109050K .......... .......... .......... .......... .......... 41% 35.4M 36s
109100K .......... .......... .......... .......... .......... 41% 6.88M 36s
109150K .......... .......... .......... .......... .......... 41% 10.4M 36s
109200K .......... .......... .......... .......... .......... 41% 4.72M 36s
109250K .......... .......... .......... .......... .......... 41% 6.02M 36s
109300K .......... .......... .......... .......... .......... 41% 6.98M 36s
109350K .......... .......... .......... .......... .......... 41% 5.03M 36s
109400K .......... .......... .......... .......... .......... 41% 6.41M 36s
109450K .......... .......... .......... .......... .......... 41% 2.05M 36s
109500K .......... .......... .......... .......... .......... 41% 55.9M 36s
109550K .......... .......... .......... .......... .......... 41% 39.9M 36s
109600K .......... .......... .......... .......... .......... 41% 40.3M 36s
109650K .......... .......... .......... .......... .......... 41% 19.1M 36s
109700K .......... .......... .......... .......... .......... 41% 11.1M 36s
109750K .......... .......... .......... .......... .......... 41% 13.8M 36s
109800K .......... .......... .......... .......... .......... 41% 11.7M 36s
109850K .......... .......... .......... .......... .......... 41% 8.77M 36s
109900K .......... .......... .......... .......... .......... 41% 6.96M 36s
109950K .......... .......... .......... .......... .......... 41% 8.62M 36s
110000K .......... .......... .......... .......... .......... 41% 9.25M 36s
110050K .......... .......... .......... .......... .......... 41% 11.4M 36s
110100K .......... .......... .......... .......... .......... 42% 6.74M 36s
110150K .......... .......... .......... .......... .......... 42% 10.9M 36s
110200K .......... .......... .......... .......... .......... 42% 5.33M 36s
110250K .......... .......... .......... .......... .......... 42% 9.86M 36s
110300K .......... .......... .......... .......... .......... 42% 10.5M 36s
110350K .......... .......... .......... .......... .......... 42% 5.90M 36s
110400K .......... .......... .......... .......... .......... 42% 6.16M 36s
110450K .......... .......... .......... .......... .......... 42% 5.98M 36s
110500K .......... .......... .......... .......... .......... 42% 3.01M 36s
110550K .......... .......... .......... .......... .......... 42% 19.9M 36s
110600K .......... .......... .......... .......... .......... 42% 5.71M 36s
110650K .......... .......... .......... .......... .......... 42% 5.37M 36s
110700K .......... .......... .......... .......... .......... 42% 16.0M 36s
110750K .......... .......... .......... .......... .......... 42% 14.8M 36s
110800K .......... .......... .......... .......... .......... 42% 6.58M 36s
110850K .......... .......... .......... .......... .......... 42% 8.17M 36s
110900K .......... .......... .......... .......... .......... 42% 7.86M 36s
110950K .......... .......... .......... .......... .......... 42% 5.94M 36s
111000K .......... .......... .......... .......... .......... 42% 9.28M 36s
111050K .......... .......... .......... .......... .......... 42% 6.62M 36s
111100K .......... .......... .......... .......... .......... 42% 5.16M 36s
111150K .......... .......... .......... .......... .......... 42% 12.2M 36s
111200K .......... .......... .......... .......... .......... 42% 5.52M 36s
111250K .......... .......... .......... .......... .......... 42% 18.2M 36s
111300K .......... .......... .......... .......... .......... 42% 6.01M 36s
111350K .......... .......... .......... .......... .......... 42% 4.81M 36s
111400K .......... .......... .......... .......... .......... 42% 9.00M 36s
111450K .......... .......... .......... .......... .......... 42% 4.10M 36s
111500K .......... .......... .......... .......... .......... 42% 1.49M 36s
111550K .......... .......... .......... .......... .......... 42% 47.4M 36s
111600K .......... .......... .......... .......... .......... 42% 35.3M 36s
111650K .......... .......... .......... .......... .......... 42% 41.2M 36s
111700K .......... .......... .......... .......... .......... 42% 11.0M 36s
111750K .......... .......... .......... .......... .......... 42% 5.06M 35s
111800K .......... .......... .......... .......... .......... 42% 5.57M 35s
111850K .......... .......... .......... .......... .......... 42% 5.43M 35s
111900K .......... .......... .......... .......... .......... 42% 8.27M 35s
111950K .......... .......... .......... .......... .......... 42% 6.72M 35s
112000K .......... .......... .......... .......... .......... 42% 5.92M 35s
112050K .......... .......... .......... .......... .......... 42% 13.8M 35s
112100K .......... .......... .......... .......... .......... 42% 8.66M 35s
112150K .......... .......... .......... .......... .......... 42% 49.7M 35s
112200K .......... .......... .......... .......... .......... 42% 12.2M 35s
112250K .......... .......... .......... .......... .......... 42% 12.8M 35s
112300K .......... .......... .......... .......... .......... 42% 14.8M 35s
112350K .......... .......... .......... .......... .......... 42% 11.2M 35s
112400K .......... .......... .......... .......... .......... 42% 14.7M 35s
112450K .......... .......... .......... .......... .......... 42% 13.6M 35s
112500K .......... .......... .......... .......... .......... 42% 11.8M 35s
112550K .......... .......... .......... .......... .......... 42% 3.03M 35s
112600K .......... .......... .......... .......... .......... 42% 43.4M 35s
112650K .......... .......... .......... .......... .......... 42% 67.1M 35s
112700K .......... .......... .......... .......... .......... 43% 22.8M 35s
112750K .......... .......... .......... .......... .......... 43% 36.2M 35s
112800K .......... .......... .......... .......... .......... 43% 8.62M 35s
112850K .......... .......... .......... .......... .......... 43% 9.36M 35s
112900K .......... .......... .......... .......... .......... 43% 46.9M 35s
112950K .......... .......... .......... .......... .......... 43% 12.5M 35s
113000K .......... .......... .......... .......... .......... 43% 11.4M 35s
113050K .......... .......... .......... .......... .......... 43% 7.91M 35s
113100K .......... .......... .......... .......... .......... 43% 10.9M 35s
113150K .......... .......... .......... .......... .......... 43% 11.4M 35s
113200K .......... .......... .......... .......... .......... 43% 7.63M 35s
113250K .......... .......... .......... .......... .......... 43% 10.3M 35s
113300K .......... .......... .......... .......... .......... 43% 5.15M 35s
113350K .......... .......... .......... .......... .......... 43% 6.30M 35s
113400K .......... .......... .......... .......... .......... 43% 7.10M 35s
113450K .......... .......... .......... .......... .......... 43% 4.37M 35s
113500K .......... .......... .......... .......... .......... 43% 5.37M 35s
113550K .......... .......... .......... .......... .......... 43% 1.55M 35s
113600K .......... .......... .......... .......... .......... 43% 32.7M 35s
113650K .......... .......... .......... .......... .......... 43% 58.1M 35s
113700K .......... .......... .......... .......... .......... 43% 3.32M 35s
113750K .......... .......... .......... .......... .......... 43% 2.91M 35s
113800K .......... .......... .......... .......... .......... 43% 3.29M 35s
113850K .......... .......... .......... .......... .......... 43% 3.56M 35s
113900K .......... .......... .......... .......... .......... 43% 6.78M 35s
113950K .......... .......... .......... .......... .......... 43% 4.32M 35s
114000K .......... .......... .......... .......... .......... 43% 6.92M 35s
114050K .......... .......... .......... .......... .......... 43% 7.54M 35s
114100K .......... .......... .......... .......... .......... 43% 4.68M 35s
114150K .......... .......... .......... .......... .......... 43% 12.4M 35s
114200K .......... .......... .......... .......... .......... 43% 8.40M 35s
114250K .......... .......... .......... .......... .......... 43% 10.7M 35s
114300K .......... .......... .......... .......... .......... 43% 16.9M 35s
114350K .......... .......... .......... .......... .......... 43% 9.46M 35s
114400K .......... .......... .......... .......... .......... 43% 6.21M 35s
114450K .......... .......... .......... .......... .......... 43% 8.47M 34s
114500K .......... .......... .......... .......... .......... 43% 6.54M 34s
114550K .......... .......... .......... .......... .......... 43% 6.50M 34s
114600K .......... .......... .......... .......... .......... 43% 1.67M 34s
114650K .......... .......... .......... .......... .......... 43% 59.3M 34s
114700K .......... .......... .......... .......... .......... 43% 36.0M 34s
114750K .......... .......... .......... .......... .......... 43% 44.3M 34s
114800K .......... .......... .......... .......... .......... 43% 6.85M 34s
114850K .......... .......... .......... .......... .......... 43% 9.44M 34s
114900K .......... .......... .......... .......... .......... 43% 6.50M 34s
114950K .......... .......... .......... .......... .......... 43% 11.1M 34s
115000K .......... .......... .......... .......... .......... 43% 7.96M 34s
115050K .......... .......... .......... .......... .......... 43% 13.1M 34s
115100K .......... .......... .......... .......... .......... 43% 7.46M 34s
115150K .......... .......... .......... .......... .......... 43% 12.1M 34s
115200K .......... .......... .......... .......... .......... 43% 8.54M 34s
115250K .......... .......... .......... .......... .......... 43% 7.85M 34s
115300K .......... .......... .......... .......... .......... 43% 12.9M 34s
115350K .......... .......... .......... .......... .......... 44% 15.9M 34s
115400K .......... .......... .......... .......... .......... 44% 10.8M 34s
115450K .......... .......... .......... .......... .......... 44% 9.02M 34s
115500K .......... .......... .......... .......... .......... 44% 8.53M 34s
115550K .......... .......... .......... .......... .......... 44% 9.30M 34s
115600K .......... .......... .......... .......... .......... 44% 2.05M 34s
115650K .......... .......... .......... .......... .......... 44% 66.2M 34s
115700K .......... .......... .......... .......... .......... 44% 39.4M 34s
115750K .......... .......... .......... .......... .......... 44% 46.6M 34s
115800K .......... .......... .......... .......... .......... 44% 47.4M 34s
115850K .......... .......... .......... .......... .......... 44% 6.46M 34s
115900K .......... .......... .......... .......... .......... 44% 13.1M 34s
115950K .......... .......... .......... .......... .......... 44% 7.24M 34s
116000K .......... .......... .......... .......... .......... 44% 12.3M 34s
116050K .......... .......... .......... .......... .......... 44% 13.2M 34s
116100K .......... .......... .......... .......... .......... 44% 10.8M 34s
116150K .......... .......... .......... .......... .......... 44% 19.4M 34s
116200K .......... .......... .......... .......... .......... 44% 9.94M 34s
116250K .......... .......... .......... .......... .......... 44% 18.3M 34s
116300K .......... .......... .......... .......... .......... 44% 18.4M 34s
116350K .......... .......... .......... .......... .......... 44% 16.8M 34s
116400K .......... .......... .......... .......... .......... 44% 19.5M 34s
116450K .......... .......... .......... .......... .......... 44% 18.9M 34s
116500K .......... .......... .......... .......... .......... 44% 18.6M 34s
116550K .......... .......... .......... .......... .......... 44% 19.7M 34s
116600K .......... .......... .......... .......... .......... 44% 21.0M 34s
116650K .......... .......... .......... .......... .......... 44% 2.35M 34s
116700K .......... .......... .......... .......... .......... 44% 37.9M 34s
116750K .......... .......... .......... .......... .......... 44% 42.8M 34s
116800K .......... .......... .......... .......... .......... 44% 55.1M 34s
116850K .......... .......... .......... .......... .......... 44% 8.64M 34s
116900K .......... .......... .......... .......... .......... 44% 68.6M 34s
116950K .......... .......... .......... .......... .......... 44% 11.2M 34s
117000K .......... .......... .......... .......... .......... 44% 15.6M 33s
117050K .......... .......... .......... .......... .......... 44% 10.6M 33s
117100K .......... .......... .......... .......... .......... 44% 12.5M 33s
117150K .......... .......... .......... .......... .......... 44% 14.7M 33s
117200K .......... .......... .......... .......... .......... 44% 8.30M 33s
117250K .......... .......... .......... .......... .......... 44% 16.6M 33s
117300K .......... .......... .......... .......... .......... 44% 11.4M 33s
117350K .......... .......... .......... .......... .......... 44% 15.4M 33s
117400K .......... .......... .......... .......... .......... 44% 18.0M 33s
117450K .......... .......... .......... .......... .......... 44% 15.5M 33s
117500K .......... .......... .......... .......... .......... 44% 14.9M 33s
117550K .......... .......... .......... .......... .......... 44% 8.14M 33s
117600K .......... .......... .......... .......... .......... 44% 19.3M 33s
117650K .......... .......... .......... .......... .......... 44% 2.82M 33s
117700K .......... .......... .......... .......... .......... 44% 44.6M 33s
117750K .......... .......... .......... .......... .......... 44% 61.3M 33s
117800K .......... .......... .......... .......... .......... 44% 52.1M 33s
117850K .......... .......... .......... .......... .......... 44% 27.7M 33s
117900K .......... .......... .......... .......... .......... 44% 10.7M 33s
117950K .......... .......... .......... .......... .......... 45% 11.6M 33s
118000K .......... .......... .......... .......... .......... 45% 9.09M 33s
118050K .......... .......... .......... .......... .......... 45% 14.4M 33s
118100K .......... .......... .......... .......... .......... 45% 7.67M 33s
118150K .......... .......... .......... .......... .......... 45% 13.4M 33s
118200K .......... .......... .......... .......... .......... 45% 7.40M 33s
118250K .......... .......... .......... .......... .......... 45% 21.8M 33s
118300K .......... .......... .......... .......... .......... 45% 15.2M 33s
118350K .......... .......... .......... .......... .......... 45% 8.82M 33s
118400K .......... .......... .......... .......... .......... 45% 11.0M 33s
118450K .......... .......... .......... .......... .......... 45% 10.0M 33s
118500K .......... .......... .......... .......... .......... 45% 19.2M 33s
118550K .......... .......... .......... .......... .......... 45% 11.1M 33s
118600K .......... .......... .......... .......... .......... 45% 10.5M 33s
118650K .......... .......... .......... .......... .......... 45% 10.3M 33s
118700K .......... .......... .......... .......... .......... 45% 2.17M 33s
118750K .......... .......... .......... .......... .......... 45% 63.8M 33s
118800K .......... .......... .......... .......... .......... 45% 43.9M 33s
118850K .......... .......... .......... .......... .......... 45% 52.6M 33s
118900K .......... .......... .......... .......... .......... 45% 12.5M 33s
118950K .......... .......... .......... .......... .......... 45% 22.1M 33s
119000K .......... .......... .......... .......... .......... 45% 6.22M 33s
119050K .......... .......... .......... .......... .......... 45% 49.2M 33s
119100K .......... .......... .......... .......... .......... 45% 11.1M 33s
119150K .......... .......... .......... .......... .......... 45% 12.0M 33s
119200K .......... .......... .......... .......... .......... 45% 8.65M 33s
119250K .......... .......... .......... .......... .......... 45% 10.3M 33s
119300K .......... .......... .......... .......... .......... 45% 12.6M 33s
119350K .......... .......... .......... .......... .......... 45% 7.90M 33s
119400K .......... .......... .......... .......... .......... 45% 16.7M 33s
119450K .......... .......... .......... .......... .......... 45% 9.53M 32s
119500K .......... .......... .......... .......... .......... 45% 14.2M 32s
119550K .......... .......... .......... .......... .......... 45% 16.0M 32s
119600K .......... .......... .......... .......... .......... 45% 15.1M 32s
119650K .......... .......... .......... .......... .......... 45% 17.7M 32s
119700K .......... .......... .......... .......... .......... 45% 2.30M 32s
119750K .......... .......... .......... .......... .......... 45% 63.7M 32s
119800K .......... .......... .......... .......... .......... 45% 28.6M 32s
119850K .......... .......... .......... .......... .......... 45% 48.1M 32s
119900K .......... .......... .......... .......... .......... 45% 54.3M 32s
119950K .......... .......... .......... .......... .......... 45% 16.0M 32s
120000K .......... .......... .......... .......... .......... 45% 19.4M 32s
120050K .......... .......... .......... .......... .......... 45% 23.3M 32s
120100K .......... .......... .......... .......... .......... 45% 20.2M 32s
120150K .......... .......... .......... .......... .......... 45% 18.3M 32s
120200K .......... .......... .......... .......... .......... 45% 6.51M 32s
120250K .......... .......... .......... .......... .......... 45% 19.3M 32s
120300K .......... .......... .......... .......... .......... 45% 9.97M 32s
120350K .......... .......... .......... .......... .......... 45% 7.50M 32s
120400K .......... .......... .......... .......... .......... 45% 18.3M 32s
120450K .......... .......... .......... .......... .......... 45% 9.20M 32s
120500K .......... .......... .......... .......... .......... 45% 14.4M 32s
120550K .......... .......... .......... .......... .......... 45% 11.4M 32s
120600K .......... .......... .......... .......... .......... 46% 7.60M 32s
120650K .......... .......... .......... .......... .......... 46% 27.1M 32s
120700K .......... .......... .......... .......... .......... 46% 8.92M 32s
120750K .......... .......... .......... .......... .......... 46% 1.61M 32s
120800K .......... .......... .......... .......... .......... 46% 39.8M 32s
120850K .......... .......... .......... .......... .......... 46% 34.2M 32s
120900K .......... .......... .......... .......... .......... 46% 63.2M 32s
120950K .......... .......... .......... .......... .......... 46% 6.92M 32s
121000K .......... .......... .......... .......... .......... 46% 7.09M 32s
121050K .......... .......... .......... .......... .......... 46% 15.1M 32s
121100K .......... .......... .......... .......... .......... 46% 4.47M 32s
121150K .......... .......... .......... .......... .......... 46% 49.3M 32s
121200K .......... .......... .......... .......... .......... 46% 7.27M 32s
121250K .......... .......... .......... .......... .......... 46% 7.42M 32s
121300K .......... .......... .......... .......... .......... 46% 6.92M 32s
121350K .......... .......... .......... .......... .......... 46% 8.41M 32s
121400K .......... .......... .......... .......... .......... 46% 5.66M 32s
121450K .......... .......... .......... .......... .......... 46% 12.8M 32s
121500K .......... .......... .......... .......... .......... 46% 7.80M 32s
121550K .......... .......... .......... .......... .......... 46% 7.20M 32s
121600K .......... .......... .......... .......... .......... 46% 10.9M 32s
121650K .......... .......... .......... .......... .......... 46% 10.1M 32s
121700K .......... .......... .......... .......... .......... 46% 7.87M 32s
121750K .......... .......... .......... .......... .......... 46% 2.41M 32s
121800K .......... .......... .......... .......... .......... 46% 44.8M 32s
121850K .......... .......... .......... .......... .......... 46% 38.8M 32s
121900K .......... .......... .......... .......... .......... 46% 84.6M 32s
121950K .......... .......... .......... .......... .......... 46% 32.9M 32s
122000K .......... .......... .......... .......... .......... 46% 10.4M 32s
122050K .......... .......... .......... .......... .......... 46% 18.1M 32s
122100K .......... .......... .......... .......... .......... 46% 13.5M 32s
122150K .......... .......... .......... .......... .......... 46% 10.4M 31s
122200K .......... .......... .......... .......... .......... 46% 8.86M 31s
122250K .......... .......... .......... .......... .......... 46% 22.0M 31s
122300K .......... .......... .......... .......... .......... 46% 10.8M 31s
122350K .......... .......... .......... .......... .......... 46% 10.2M 31s
122400K .......... .......... .......... .......... .......... 46% 17.9M 31s
122450K .......... .......... .......... .......... .......... 46% 12.0M 31s
122500K .......... .......... .......... .......... .......... 46% 11.1M 31s
122550K .......... .......... .......... .......... .......... 46% 13.8M 31s
122600K .......... .......... .......... .......... .......... 46% 15.9M 31s
122650K .......... .......... .......... .......... .......... 46% 10.7M 31s
122700K .......... .......... .......... .......... .......... 46% 5.83M 31s
122750K .......... .......... .......... .......... .......... 46% 56.6M 31s
122800K .......... .......... .......... .......... .......... 46% 2.53M 31s
122850K .......... .......... .......... .......... .......... 46% 30.8M 31s
122900K .......... .......... .......... .......... .......... 46% 56.1M 31s
122950K .......... .......... .......... .......... .......... 46% 40.0M 31s
123000K .......... .......... .......... .......... .......... 46% 11.9M 31s
123050K .......... .......... .......... .......... .......... 46% 7.96M 31s
123100K .......... .......... .......... .......... .......... 46% 9.53M 31s
123150K .......... .......... .......... .......... .......... 46% 4.35M 31s
123200K .......... .......... .......... .......... .......... 47% 11.9M 31s
123250K .......... .......... .......... .......... .......... 47% 7.54M 31s
123300K .......... .......... .......... .......... .......... 47% 7.83M 31s
123350K .......... .......... .......... .......... .......... 47% 8.99M 31s
123400K .......... .......... .......... .......... .......... 47% 12.6M 31s
123450K .......... .......... .......... .......... .......... 47% 7.93M 31s
123500K .......... .......... .......... .......... .......... 47% 6.42M 31s
123550K .......... .......... .......... .......... .......... 47% 7.76M 31s
123600K .......... .......... .......... .......... .......... 47% 4.84M 31s
123650K .......... .......... .......... .......... .......... 47% 6.81M 31s
123700K .......... .......... .......... .......... .......... 47% 7.07M 31s
123750K .......... .......... .......... .......... .......... 47% 7.57M 31s
123800K .......... .......... .......... .......... .......... 47% 1.76M 31s
123850K .......... .......... .......... .......... .......... 47% 48.9M 31s
123900K .......... .......... .......... .......... .......... 47% 35.2M 31s
123950K .......... .......... .......... .......... .......... 47% 6.42M 31s
124000K .......... .......... .......... .......... .......... 47% 4.32M 31s
124050K .......... .......... .......... .......... .......... 47% 7.10M 31s
124100K .......... .......... .......... .......... .......... 47% 7.28M 31s
124150K .......... .......... .......... .......... .......... 47% 5.69M 31s
124200K .......... .......... .......... .......... .......... 47% 7.87M 31s
124250K .......... .......... .......... .......... .......... 47% 6.13M 31s
124300K .......... .......... .......... .......... .......... 47% 6.41M 31s
124350K .......... .......... .......... .......... .......... 47% 7.10M 31s
124400K .......... .......... .......... .......... .......... 47% 55.8M 31s
124450K .......... .......... .......... .......... .......... 47% 7.04M 31s
124500K .......... .......... .......... .......... .......... 47% 17.2M 31s
124550K .......... .......... .......... .......... .......... 47% 8.05M 31s
124600K .......... .......... .......... .......... .......... 47% 8.05M 31s
124650K .......... .......... .......... .......... .......... 47% 11.4M 31s
124700K .......... .......... .......... .......... .......... 47% 5.82M 31s
124750K .......... .......... .......... .......... .......... 47% 10.6M 31s
124800K .......... .......... .......... .......... .......... 47% 7.90M 31s
124850K .......... .......... .......... .......... .......... 47% 2.30M 31s
124900K .......... .......... .......... .......... .......... 47% 99.4M 31s
124950K .......... .......... .......... .......... .......... 47% 64.8M 31s
125000K .......... .......... .......... .......... .......... 47% 14.7M 31s
125050K .......... .......... .......... .......... .......... 47% 10.4M 31s
125100K .......... .......... .......... .......... .......... 47% 12.1M 30s
125150K .......... .......... .......... .......... .......... 47% 11.6M 30s
125200K .......... .......... .......... .......... .......... 47% 10.2M 30s
125250K .......... .......... .......... .......... .......... 47% 18.1M 30s
125300K .......... .......... .......... .......... .......... 47% 17.8M 30s
125350K .......... .......... .......... .......... .......... 47% 16.6M 30s
125400K .......... .......... .......... .......... .......... 47% 19.6M 30s
125450K .......... .......... .......... .......... .......... 47% 10.5M 30s
125500K .......... .......... .......... .......... .......... 47% 20.1M 30s
125550K .......... .......... .......... .......... .......... 47% 11.5M 30s
125600K .......... .......... .......... .......... .......... 47% 20.4M 30s
125650K .......... .......... .......... .......... .......... 47% 12.9M 30s
125700K .......... .......... .......... .......... .......... 47% 12.5M 30s
125750K .......... .......... .......... .......... .......... 47% 18.6M 30s
125800K .......... .......... .......... .......... .......... 47% 12.5M 30s
125850K .......... .......... .......... .......... .......... 48% 2.63M 30s
125900K .......... .......... .......... .......... .......... 48% 42.6M 30s
125950K .......... .......... .......... .......... .......... 48% 43.8M 30s
126000K .......... .......... .......... .......... .......... 48% 61.3M 30s
126050K .......... .......... .......... .......... .......... 48% 24.2M 30s
126100K .......... .......... .......... .......... .......... 48% 4.66M 30s
126150K .......... .......... .......... .......... .......... 48% 38.3M 30s
126200K .......... .......... .......... .......... .......... 48% 12.6M 30s
126250K .......... .......... .......... .......... .......... 48% 11.9M 30s
126300K .......... .......... .......... .......... .......... 48% 6.53M 30s
126350K .......... .......... .......... .......... .......... 48% 13.6M 30s
126400K .......... .......... .......... .......... .......... 48% 12.8M 30s
126450K .......... .......... .......... .......... .......... 48% 8.12M 30s
126500K .......... .......... .......... .......... .......... 48% 15.1M 30s
126550K .......... .......... .......... .......... .......... 48% 15.5M 30s
126600K .......... .......... .......... .......... .......... 48% 6.76M 30s
126650K .......... .......... .......... .......... .......... 48% 5.22M 30s
126700K .......... .......... .......... .......... .......... 48% 6.05M 30s
126750K .......... .......... .......... .......... .......... 48% 15.7M 30s
126800K .......... .......... .......... .......... .......... 48% 5.94M 30s
126850K .......... .......... .......... .......... .......... 48% 20.3M 30s
126900K .......... .......... .......... .......... .......... 48% 2.21M 30s
126950K .......... .......... .......... .......... .......... 48% 39.2M 30s
127000K .......... .......... .......... .......... .......... 48% 50.9M 30s
127050K .......... .......... .......... .......... .......... 48% 48.2M 30s
127100K .......... .......... .......... .......... .......... 48% 7.87M 30s
127150K .......... .......... .......... .......... .......... 48% 6.58M 30s
127200K .......... .......... .......... .......... .......... 48% 14.2M 30s
127250K .......... .......... .......... .......... .......... 48% 14.4M 30s
127300K .......... .......... .......... .......... .......... 48% 7.97M 30s
127350K .......... .......... .......... .......... .......... 48% 17.1M 30s
127400K .......... .......... .......... .......... .......... 48% 13.1M 30s
127450K .......... .......... .......... .......... .......... 48% 7.56M 30s
127500K .......... .......... .......... .......... .......... 48% 9.50M 30s
127550K .......... .......... .......... .......... .......... 48% 7.49M 30s
127600K .......... .......... .......... .......... .......... 48% 6.98M 30s
127650K .......... .......... .......... .......... .......... 48% 6.91M 30s
127700K .......... .......... .......... .......... .......... 48% 5.64M 30s
127750K .......... .......... .......... .......... .......... 48% 7.47M 30s
127800K .......... .......... .......... .......... .......... 48% 10.1M 30s
127850K .......... .......... .......... .......... .......... 48% 9.30M 30s
127900K .......... .......... .......... .......... .......... 48% 1.07M 30s
127950K .......... .......... .......... .......... .......... 48% 39.2M 30s
128000K .......... .......... .......... .......... .......... 48% 54.7M 30s
128050K .......... .......... .......... .......... .......... 48% 65.6M 29s
128100K .......... .......... .......... .......... .......... 48% 7.43M 29s
128150K .......... .......... .......... .......... .......... 48% 7.40M 29s
128200K .......... .......... .......... .......... .......... 48% 5.76M 29s
128250K .......... .......... .......... .......... .......... 48% 13.1M 29s
128300K .......... .......... .......... .......... .......... 48% 16.0M 29s
128350K .......... .......... .......... .......... .......... 48% 12.0M 29s
128400K .......... .......... .......... .......... .......... 48% 19.9M 29s
128450K .......... .......... .......... .......... .......... 49% 17.5M 29s
128500K .......... .......... .......... .......... .......... 49% 17.3M 29s
128550K .......... .......... .......... .......... .......... 49% 7.96M 29s
128600K .......... .......... .......... .......... .......... 49% 11.3M 29s
128650K .......... .......... .......... .......... .......... 49% 13.1M 29s
128700K .......... .......... .......... .......... .......... 49% 4.24M 29s
128750K .......... .......... .......... .......... .......... 49% 43.9M 29s
128800K .......... .......... .......... .......... .......... 49% 6.20M 29s
128850K .......... .......... .......... .......... .......... 49% 7.70M 29s
128900K .......... .......... .......... .......... .......... 49% 6.94M 29s
128950K .......... .......... .......... .......... .......... 49% 2.44M 29s
129000K .......... .......... .......... .......... .......... 49% 36.8M 29s
129050K .......... .......... .......... .......... .......... 49% 85.7M 29s
129100K .......... .......... .......... .......... .......... 49% 4.81M 29s
129150K .......... .......... .......... .......... .......... 49% 4.26M 29s
129200K .......... .......... .......... .......... .......... 49% 4.57M 29s
129250K .......... .......... .......... .......... .......... 49% 9.89M 29s
129300K .......... .......... .......... .......... .......... 49% 7.58M 29s
129350K .......... .......... .......... .......... .......... 49% 5.61M 29s
129400K .......... .......... .......... .......... .......... 49% 13.8M 29s
129450K .......... .......... .......... .......... .......... 49% 7.19M 29s
129500K .......... .......... .......... .......... .......... 49% 10.7M 29s
129550K .......... .......... .......... .......... .......... 49% 15.6M 29s
129600K .......... .......... .......... .......... .......... 49% 8.02M 29s
129650K .......... .......... .......... .......... .......... 49% 16.6M 29s
129700K .......... .......... .......... .......... .......... 49% 16.6M 29s
129750K .......... .......... .......... .......... .......... 49% 9.42M 29s
129800K .......... .......... .......... .......... .......... 49% 21.7M 29s
129850K .......... .......... .......... .......... .......... 49% 11.9M 29s
129900K .......... .......... .......... .......... .......... 49% 10.7M 29s
129950K .......... .......... .......... .......... .......... 49% 1.17M 29s
130000K .......... .......... .......... .......... .......... 49% 37.9M 29s
130050K .......... .......... .......... .......... .......... 49% 61.5M 29s
130100K .......... .......... .......... .......... .......... 49% 37.4M 29s
130150K .......... .......... .......... .......... .......... 49% 11.5M 29s
130200K .......... .......... .......... .......... .......... 49% 5.11M 29s
130250K .......... .......... .......... .......... .......... 49% 8.70M 29s
130300K .......... .......... .......... .......... .......... 49% 12.8M 29s
130350K .......... .......... .......... .......... .......... 49% 8.97M 29s
130400K .......... .......... .......... .......... .......... 49% 4.27M 29s
130450K .......... .......... .......... .......... .......... 49% 43.6M 29s
130500K .......... .......... .......... .......... .......... 49% 7.81M 29s
130550K .......... .......... .......... .......... .......... 49% 17.4M 29s
130600K .......... .......... .......... .......... .......... 49% 10.9M 29s
130650K .......... .......... .......... .......... .......... 49% 9.65M 29s
130700K .......... .......... .......... .......... .......... 49% 4.55M 29s
130750K .......... .......... .......... .......... .......... 49% 7.89M 29s
130800K .......... .......... .......... .......... .......... 49% 6.75M 29s
130850K .......... .......... .......... .......... .......... 49% 7.39M 29s
130900K .......... .......... .......... .......... .......... 49% 6.94M 29s
130950K .......... .......... .......... .......... .......... 49% 1.03M 29s
131000K .......... .......... .......... .......... .......... 49% 43.1M 29s
131050K .......... .......... .......... .......... .......... 50% 46.8M 29s
131100K .......... .......... .......... .......... .......... 50% 47.5M 29s
131150K .......... .......... .......... .......... .......... 50% 16.4M 29s
131200K .......... .......... .......... .......... .......... 50% 9.43M 29s
131250K .......... .......... .......... .......... .......... 50% 5.58M 28s
131300K .......... .......... .......... .......... .......... 50% 8.50M 28s
131350K .......... .......... .......... .......... .......... 50% 11.3M 28s
131400K .......... .......... .......... .......... .......... 50% 12.7M 28s
131450K .......... .......... .......... .......... .......... 50% 3.44M 28s
131500K .......... .......... .......... .......... .......... 50% 4.94M 28s
131550K .......... .......... .......... .......... .......... 50% 6.22M 28s
131600K .......... .......... .......... .......... .......... 50% 3.48M 28s
131650K .......... .......... .......... .......... .......... 50% 5.70M 28s
131700K .......... .......... .......... .......... .......... 50% 3.83M 28s
131750K .......... .......... .......... .......... .......... 50% 5.95M 28s
131800K .......... .......... .......... .......... .......... 50% 7.86M 28s
131850K .......... .......... .......... .......... .......... 50% 4.96M 28s
131900K .......... .......... .......... .......... .......... 50% 8.41M 28s
131950K .......... .......... .......... .......... .......... 50% 10.7M 28s
132000K .......... .......... .......... .......... .......... 50% 2.57M 28s
132050K .......... .......... .......... .......... .......... 50% 42.2M 28s
132100K .......... .......... .......... .......... .......... 50% 40.0M 28s
132150K .......... .......... .......... .......... .......... 50% 40.7M 28s
132200K .......... .......... .......... .......... .......... 50% 20.7M 28s
132250K .......... .......... .......... .......... .......... 50% 7.58M 28s
132300K .......... .......... .......... .......... .......... 50% 13.9M 28s
132350K .......... .......... .......... .......... .......... 50% 12.3M 28s
132400K .......... .......... .......... .......... .......... 50% 15.6M 28s
132450K .......... .......... .......... .......... .......... 50% 8.62M 28s
132500K .......... .......... .......... .......... .......... 50% 15.7M 28s
132550K .......... .......... .......... .......... .......... 50% 14.8M 28s
132600K .......... .......... .......... .......... .......... 50% 12.3M 28s
132650K .......... .......... .......... .......... .......... 50% 13.5M 28s
132700K .......... .......... .......... .......... .......... 50% 7.95M 28s
132750K .......... .......... .......... .......... .......... 50% 13.3M 28s
132800K .......... .......... .......... .......... .......... 50% 10.2M 28s
132850K .......... .......... .......... .......... .......... 50% 11.3M 28s
132900K .......... .......... .......... .......... .......... 50% 14.1M 28s
132950K .......... .......... .......... .......... .......... 50% 7.53M 28s
133000K .......... .......... .......... .......... .......... 50% 2.72M 28s
133050K .......... .......... .......... .......... .......... 50% 32.2M 28s
133100K .......... .......... .......... .......... .......... 50% 32.5M 28s
133150K .......... .......... .......... .......... .......... 50% 41.1M 28s
133200K .......... .......... .......... .......... .......... 50% 15.1M 28s
133250K .......... .......... .......... .......... .......... 50% 12.2M 28s
133300K .......... .......... .......... .......... .......... 50% 14.0M 28s
133350K .......... .......... .......... .......... .......... 50% 15.1M 28s
133400K .......... .......... .......... .......... .......... 50% 15.8M 28s
133450K .......... .......... .......... .......... .......... 50% 14.2M 28s
133500K .......... .......... .......... .......... .......... 50% 14.5M 28s
133550K .......... .......... .......... .......... .......... 50% 14.5M 28s
133600K .......... .......... .......... .......... .......... 50% 8.76M 28s
133650K .......... .......... .......... .......... .......... 50% 50.4M 28s
133700K .......... .......... .......... .......... .......... 51% 14.4M 28s
133750K .......... .......... .......... .......... .......... 51% 9.06M 28s
133800K .......... .......... .......... .......... .......... 51% 15.2M 28s
133850K .......... .......... .......... .......... .......... 51% 8.20M 28s
133900K .......... .......... .......... .......... .......... 51% 15.6M 28s
133950K .......... .......... .......... .......... .......... 51% 16.2M 28s
134000K .......... .......... .......... .......... .......... 51% 7.00M 28s
134050K .......... .......... .......... .......... .......... 51% 1.38M 28s
134100K .......... .......... .......... .......... .......... 51% 48.8M 28s
134150K .......... .......... .......... .......... .......... 51% 68.7M 28s
134200K .......... .......... .......... .......... .......... 51% 69.8M 28s
134250K .......... .......... .......... .......... .......... 51% 22.6M 28s
134300K .......... .......... .......... .......... .......... 51% 14.1M 28s
134350K .......... .......... .......... .......... .......... 51% 16.0M 28s
134400K .......... .......... .......... .......... .......... 51% 14.7M 27s
134450K .......... .......... .......... .......... .......... 51% 12.9M 27s
134500K .......... .......... .......... .......... .......... 51% 12.0M 27s
134550K .......... .......... .......... .......... .......... 51% 14.4M 27s
134600K .......... .......... .......... .......... .......... 51% 11.8M 27s
134650K .......... .......... .......... .......... .......... 51% 6.97M 27s
134700K .......... .......... .......... .......... .......... 51% 18.0M 27s
134750K .......... .......... .......... .......... .......... 51% 13.2M 27s
134800K .......... .......... .......... .......... .......... 51% 13.3M 27s
134850K .......... .......... .......... .......... .......... 51% 7.78M 27s
134900K .......... .......... .......... .......... .......... 51% 27.1M 27s
134950K .......... .......... .......... .......... .......... 51% 5.65M 27s
135000K .......... .......... .......... .......... .......... 51% 9.72M 27s
135050K .......... .......... .......... .......... .......... 51% 1.74M 27s
135100K .......... .......... .......... .......... .......... 51% 52.4M 27s
135150K .......... .......... .......... .......... .......... 51% 67.8M 27s
135200K .......... .......... .......... .......... .......... 51% 48.2M 27s
135250K .......... .......... .......... .......... .......... 51% 18.9M 27s
135300K .......... .......... .......... .......... .......... 51% 13.1M 27s
135350K .......... .......... .......... .......... .......... 51% 7.59M 27s
135400K .......... .......... .......... .......... .......... 51% 12.8M 27s
135450K .......... .......... .......... .......... .......... 51% 7.01M 27s
135500K .......... .......... .......... .......... .......... 51% 13.3M 27s
135550K .......... .......... .......... .......... .......... 51% 18.3M 27s
135600K .......... .......... .......... .......... .......... 51% 8.74M 27s
135650K .......... .......... .......... .......... .......... 51% 13.6M 27s
135700K .......... .......... .......... .......... .......... 51% 15.7M 27s
135750K .......... .......... .......... .......... .......... 51% 17.2M 27s
135800K .......... .......... .......... .......... .......... 51% 20.0M 27s
135850K .......... .......... .......... .......... .......... 51% 15.0M 27s
135900K .......... .......... .......... .......... .......... 51% 10.1M 27s
135950K .......... .......... .......... .......... .......... 51% 7.26M 27s
136000K .......... .......... .......... .......... .......... 51% 12.5M 27s
136050K .......... .......... .......... .......... .......... 51% 34.8M 27s
136100K .......... .......... .......... .......... .......... 51% 1.43M 27s
136150K .......... .......... .......... .......... .......... 51% 78.1M 27s
136200K .......... .......... .......... .......... .......... 51% 76.4M 27s
136250K .......... .......... .......... .......... .......... 51% 65.0M 27s
136300K .......... .......... .......... .......... .......... 52% 7.65M 27s
136350K .......... .......... .......... .......... .......... 52% 26.2M 27s
136400K .......... .......... .......... .......... .......... 52% 23.2M 27s
136450K .......... .......... .......... .......... .......... 52% 11.2M 27s
136500K .......... .......... .......... .......... .......... 52% 13.2M 27s
136550K .......... .......... .......... .......... .......... 52% 8.43M 27s
136600K .......... .......... .......... .......... .......... 52% 10.9M 27s
136650K .......... .......... .......... .......... .......... 52% 11.8M 27s
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136750K .......... .......... .......... .......... .......... 52% 12.0M 27s
136800K .......... .......... .......... .......... .......... 52% 42.0M 27s
136850K .......... .......... .......... .......... .......... 52% 7.77M 27s
136900K .......... .......... .......... .......... .......... 52% 10.6M 27s
136950K .......... .......... .......... .......... .......... 52% 6.95M 27s
137000K .......... .......... .......... .......... .......... 52% 72.0M 27s
137050K .......... .......... .......... .......... .......... 52% 10.5M 27s
137100K .......... .......... .......... .......... .......... 52% 1.66M 27s
137150K .......... .......... .......... .......... .......... 52% 53.8M 27s
137200K .......... .......... .......... .......... .......... 52% 63.6M 27s
137250K .......... .......... .......... .......... .......... 52% 49.4M 27s
137300K .......... .......... .......... .......... .......... 52% 25.3M 27s
137350K .......... .......... .......... .......... .......... 52% 14.8M 27s
137400K .......... .......... .......... .......... .......... 52% 21.4M 27s
137450K .......... .......... .......... .......... .......... 52% 6.53M 27s
137500K .......... .......... .......... .......... .......... 52% 15.3M 26s
137550K .......... .......... .......... .......... .......... 52% 14.9M 26s
137600K .......... .......... .......... .......... .......... 52% 6.79M 26s
137650K .......... .......... .......... .......... .......... 52% 15.9M 26s
137700K .......... .......... .......... .......... .......... 52% 12.4M 26s
137750K .......... .......... .......... .......... .......... 52% 6.99M 26s
137800K .......... .......... .......... .......... .......... 52% 10.7M 26s
137850K .......... .......... .......... .......... .......... 52% 7.61M 26s
137900K .......... .......... .......... .......... .......... 52% 10.1M 26s
137950K .......... .......... .......... .......... .......... 52% 7.87M 26s
138000K .......... .......... .......... .......... .......... 52% 13.6M 26s
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138100K .......... .......... .......... .......... .......... 52% 10.8M 26s
138150K .......... .......... .......... .......... .......... 52% 2.06M 26s
138200K .......... .......... .......... .......... .......... 52% 44.2M 26s
138250K .......... .......... .......... .......... .......... 52% 61.3M 26s
138300K .......... .......... .......... .......... .......... 52% 63.9M 26s
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138400K .......... .......... .......... .......... .......... 52% 10.0M 26s
138450K .......... .......... .......... .......... .......... 52% 7.12M 26s
138500K .......... .......... .......... .......... .......... 52% 13.9M 26s
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138700K .......... .......... .......... .......... .......... 52% 15.3M 26s
138750K .......... .......... .......... .......... .......... 52% 11.1M 26s
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138850K .......... .......... .......... .......... .......... 52% 13.8M 26s
138900K .......... .......... .......... .......... .......... 52% 13.9M 26s
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139000K .......... .......... .......... .......... .......... 53% 14.6M 26s
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139100K .......... .......... .......... .......... .......... 53% 16.3M 26s
139150K .......... .......... .......... .......... .......... 53% 2.95M 26s
139200K .......... .......... .......... .......... .......... 53% 41.5M 26s
139250K .......... .......... .......... .......... .......... 53% 46.9M 26s
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139350K .......... .......... .......... .......... .......... 53% 9.02M 26s
139400K .......... .......... .......... .......... .......... 53% 16.6M 26s
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140000K .......... .......... .......... .......... .......... 53% 6.60M 26s
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140100K .......... .......... .......... .......... .......... 53% 10.7M 26s
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140200K .......... .......... .......... .......... .......... 53% 1.87M 26s
140250K .......... .......... .......... .......... .......... 53% 61.0M 26s
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141100K .......... .......... .......... .......... .......... 53% 33.9M 25s
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141500K .......... .......... .......... .......... .......... 53% 19.1M 25s
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141600K .......... .......... .......... .......... .......... 54% 9.95M 25s
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142000K .......... .......... .......... .......... .......... 54% 6.03M 25s
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142150K .......... .......... .......... .......... .......... 54% 7.89M 25s
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142250K .......... .......... .......... .......... .......... 54% 2.15M 25s
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143000K .......... .......... .......... .......... .......... 54% 10.0M 25s
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143100K .......... .......... .......... .......... .......... 54% 9.73M 25s
143150K .......... .......... .......... .......... .......... 54% 18.6M 25s
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143450K .......... .......... .......... .......... .......... 54% 6.87M 25s
143500K .......... .......... .......... .......... .......... 54% 11.2M 25s
143550K .......... .......... .......... .......... .......... 54% 32.6M 25s
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143700K .......... .......... .......... .......... .......... 54% 8.99M 25s
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143850K .......... .......... .......... .......... .......... 54% 10.6M 25s
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144000K .......... .......... .......... .......... .......... 54% 32.7M 24s
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144250K .......... .......... .......... .......... .......... 55% 51.5M 24s
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144900K .......... .......... .......... .......... .......... 55% 12.3M 24s
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145000K .......... .......... .......... .......... .......... 55% 21.9M 24s
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145100K .......... .......... .......... .......... .......... 55% 17.5M 24s
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145200K .......... .......... .......... .......... .......... 55% 10.2M 24s
145250K .......... .......... .......... .......... .......... 55% 15.6M 24s
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145400K .......... .......... .......... .......... .......... 55% 68.7M 24s
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145900K .......... .......... .......... .......... .......... 55% 17.3M 24s
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146000K .......... .......... .......... .......... .......... 55% 20.4M 24s
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146100K .......... .......... .......... .......... .......... 55% 14.9M 24s
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146250K .......... .......... .......... .......... .......... 55% 9.59M 24s
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146900K .......... .......... .......... .......... .......... 56% 10.4M 24s
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147000K .......... .......... .......... .......... .......... 56% 15.8M 24s
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147100K .......... .......... .......... .......... .......... 56% 12.2M 24s
147150K .......... .......... .......... .......... .......... 56% 15.1M 24s
147200K .......... .......... .......... .......... .......... 56% 12.7M 24s
147250K .......... .......... .......... .......... .......... 56% 11.4M 24s
147300K .......... .......... .......... .......... .......... 56% 13.9M 24s
147350K .......... .......... .......... .......... .......... 56% 1.74M 24s
147400K .......... .......... .......... .......... .......... 56% 39.7M 24s
147450K .......... .......... .......... .......... .......... 56% 48.1M 23s
147500K .......... .......... .......... .......... .......... 56% 45.4M 23s
147550K .......... .......... .......... .......... .......... 56% 10.5M 23s
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147650K .......... .......... .......... .......... .......... 56% 9.99M 23s
147700K .......... .......... .......... .......... .......... 56% 10.3M 23s
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147800K .......... .......... .......... .......... .......... 56% 13.3M 23s
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147900K .......... .......... .......... .......... .......... 56% 14.4M 23s
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148000K .......... .......... .......... .......... .......... 56% 14.6M 23s
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148150K .......... .......... .......... .......... .......... 56% 45.5M 23s
148200K .......... .......... .......... .......... .......... 56% 10.4M 23s
148250K .......... .......... .......... .......... .......... 56% 11.7M 23s
148300K .......... .......... .......... .......... .......... 56% 12.4M 23s
148350K .......... .......... .......... .......... .......... 56% 9.96M 23s
148400K .......... .......... .......... .......... .......... 56% 1.54M 23s
148450K .......... .......... .......... .......... .......... 56% 42.6M 23s
148500K .......... .......... .......... .......... .......... 56% 65.6M 23s
148550K .......... .......... .......... .......... .......... 56% 53.1M 23s
148600K .......... .......... .......... .......... .......... 56% 7.83M 23s
148650K .......... .......... .......... .......... .......... 56% 11.3M 23s
148700K .......... .......... .......... .......... .......... 56% 11.7M 23s
148750K .......... .......... .......... .......... .......... 56% 10.9M 23s
148800K .......... .......... .......... .......... .......... 56% 6.53M 23s
148850K .......... .......... .......... .......... .......... 56% 6.92M 23s
148900K .......... .......... .......... .......... .......... 56% 18.2M 23s
148950K .......... .......... .......... .......... .......... 56% 12.3M 23s
149000K .......... .......... .......... .......... .......... 56% 8.20M 23s
149050K .......... .......... .......... .......... .......... 56% 7.56M 23s
149100K .......... .......... .......... .......... .......... 56% 8.41M 23s
149150K .......... .......... .......... .......... .......... 56% 17.1M 23s
149200K .......... .......... .......... .......... .......... 56% 8.68M 23s
149250K .......... .......... .......... .......... .......... 56% 7.27M 23s
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149350K .......... .......... .......... .......... .......... 56% 10.8M 23s
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149600K .......... .......... .......... .......... .......... 57% 11.1M 23s
149650K .......... .......... .......... .......... .......... 57% 17.1M 23s
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149750K .......... .......... .......... .......... .......... 57% 7.28M 23s
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149950K .......... .......... .......... .......... .......... 57% 8.72M 23s
150000K .......... .......... .......... .......... .......... 57% 7.74M 23s
150050K .......... .......... .......... .......... .......... 57% 8.08M 23s
150100K .......... .......... .......... .......... .......... 57% 9.12M 23s
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150200K .......... .......... .......... .......... .......... 57% 6.41M 23s
150250K .......... .......... .......... .......... .......... 57% 8.18M 23s
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150350K .......... .......... .......... .......... .......... 57% 7.62M 23s
150400K .......... .......... .......... .......... .......... 57% 11.2M 23s
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150500K .......... .......... .......... .......... .......... 57% 49.5M 23s
150550K .......... .......... .......... .......... .......... 57% 65.8M 23s
150600K .......... .......... .......... .......... .......... 57% 31.1M 23s
150650K .......... .......... .......... .......... .......... 57% 10.5M 23s
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150850K .......... .......... .......... .......... .......... 57% 7.94M 23s
150900K .......... .......... .......... .......... .......... 57% 7.92M 23s
150950K .......... .......... .......... .......... .......... 57% 6.99M 23s
151000K .......... .......... .......... .......... .......... 57% 11.1M 23s
151050K .......... .......... .......... .......... .......... 57% 14.7M 23s
151100K .......... .......... .......... .......... .......... 57% 7.33M 22s
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151200K .......... .......... .......... .......... .......... 57% 13.6M 22s
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151400K .......... .......... .......... .......... .......... 57% 17.5M 22s
151450K .......... .......... .......... .......... .......... 57% 2.03M 22s
151500K .......... .......... .......... .......... .......... 57% 89.1M 22s
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151600K .......... .......... .......... .......... .......... 57% 50.2M 22s
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151700K .......... .......... .......... .......... .......... 57% 5.51M 22s
151750K .......... .......... .......... .......... .......... 57% 43.3M 22s
151800K .......... .......... .......... .......... .......... 57% 27.0M 22s
151850K .......... .......... .......... .......... .......... 57% 10.2M 22s
151900K .......... .......... .......... .......... .......... 57% 21.8M 22s
151950K .......... .......... .......... .......... .......... 57% 14.9M 22s
152000K .......... .......... .......... .......... .......... 57% 10.8M 22s
152050K .......... .......... .......... .......... .......... 58% 15.2M 22s
152100K .......... .......... .......... .......... .......... 58% 9.60M 22s
152150K .......... .......... .......... .......... .......... 58% 12.5M 22s
152200K .......... .......... .......... .......... .......... 58% 11.5M 22s
152250K .......... .......... .......... .......... .......... 58% 10.8M 22s
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152350K .......... .......... .......... .......... .......... 58% 8.87M 22s
152400K .......... .......... .......... .......... .......... 58% 10.8M 22s
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152500K .......... .......... .......... .......... .......... 58% 3.40M 22s
152550K .......... .......... .......... .......... .......... 58% 66.4M 22s
152600K .......... .......... .......... .......... .......... 58% 64.3M 22s
152650K .......... .......... .......... .......... .......... 58% 73.9M 22s
152700K .......... .......... .......... .......... .......... 58% 6.53M 22s
152750K .......... .......... .......... .......... .......... 58% 50.1M 22s
152800K .......... .......... .......... .......... .......... 58% 14.9M 22s
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152900K .......... .......... .......... .......... .......... 58% 15.3M 22s
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153000K .......... .......... .......... .......... .......... 58% 12.7M 22s
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153100K .......... .......... .......... .......... .......... 58% 14.8M 22s
153150K .......... .......... .......... .......... .......... 58% 15.5M 22s
153200K .......... .......... .......... .......... .......... 58% 14.0M 22s
153250K .......... .......... .......... .......... .......... 58% 14.9M 22s
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153350K .......... .......... .......... .......... .......... 58% 12.3M 22s
153400K .......... .......... .......... .......... .......... 58% 42.7M 22s
153450K .......... .......... .......... .......... .......... 58% 6.61M 22s
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153550K .......... .......... .......... .......... .......... 58% 51.0M 22s
153600K .......... .......... .......... .......... .......... 58% 46.8M 22s
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153700K .......... .......... .......... .......... .......... 58% 19.1M 22s
153750K .......... .......... .......... .......... .......... 58% 7.16M 22s
153800K .......... .......... .......... .......... .......... 58% 12.0M 22s
153850K .......... .......... .......... .......... .......... 58% 14.6M 22s
153900K .......... .......... .......... .......... .......... 58% 8.00M 22s
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154000K .......... .......... .......... .......... .......... 58% 13.0M 22s
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154100K .......... .......... .......... .......... .......... 58% 7.05M 22s
154150K .......... .......... .......... .......... .......... 58% 16.6M 22s
154200K .......... .......... .......... .......... .......... 58% 11.2M 22s
154250K .......... .......... .......... .......... .......... 58% 6.71M 22s
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154350K .......... .......... .......... .......... .......... 58% 7.12M 22s
154400K .......... .......... .......... .......... .......... 58% 8.84M 22s
154450K .......... .......... .......... .......... .......... 58% 12.5M 22s
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154550K .......... .......... .......... .......... .......... 58% 2.35M 22s
154600K .......... .......... .......... .......... .......... 58% 51.2M 22s
154650K .......... .......... .......... .......... .......... 59% 47.7M 21s
154700K .......... .......... .......... .......... .......... 59% 11.0M 21s
154750K .......... .......... .......... .......... .......... 59% 9.29M 21s
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154900K .......... .......... .......... .......... .......... 59% 12.1M 21s
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155000K .......... .......... .......... .......... .......... 59% 11.6M 21s
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155100K .......... .......... .......... .......... .......... 59% 12.8M 21s
155150K .......... .......... .......... .......... .......... 59% 15.6M 21s
155200K .......... .......... .......... .......... .......... 59% 14.9M 21s
155250K .......... .......... .......... .......... .......... 59% 12.7M 21s
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155350K .......... .......... .......... .......... .......... 59% 12.8M 21s
155400K .......... .......... .......... .......... .......... 59% 8.20M 21s
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155650K .......... .......... .......... .......... .......... 59% 61.7M 21s
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155750K .......... .......... .......... .......... .......... 59% 12.4M 21s
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155850K .......... .......... .......... .......... .......... 59% 6.67M 21s
155900K .......... .......... .......... .......... .......... 59% 14.8M 21s
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156000K .......... .......... .......... .......... .......... 59% 21.7M 21s
156050K .......... .......... .......... .......... .......... 59% 6.47M 21s
156100K .......... .......... .......... .......... .......... 59% 8.02M 21s
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156200K .......... .......... .......... .......... .......... 59% 8.06M 21s
156250K .......... .......... .......... .......... .......... 59% 8.70M 21s
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156500K .......... .......... .......... .......... .......... 59% 12.5M 21s
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156650K .......... .......... .......... .......... .......... 59% 47.0M 21s
156700K .......... .......... .......... .......... .......... 59% 42.2M 21s
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156900K .......... .......... .......... .......... .......... 59% 9.25M 21s
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157000K .......... .......... .......... .......... .......... 59% 13.3M 21s
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157100K .......... .......... .......... .......... .......... 59% 9.42M 21s
157150K .......... .......... .......... .......... .......... 59% 16.6M 21s
157200K .......... .......... .......... .......... .......... 59% 9.30M 21s
157250K .......... .......... .......... .......... .......... 59% 49.2M 21s
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157350K .......... .......... .......... .......... .......... 60% 46.2M 21s
157400K .......... .......... .......... .......... .......... 60% 13.2M 21s
157450K .......... .......... .......... .......... .......... 60% 18.1M 21s
157500K .......... .......... .......... .......... .......... 60% 10.9M 21s
157550K .......... .......... .......... .......... .......... 60% 18.8M 21s
157600K .......... .......... .......... .......... .......... 60% 2.64M 21s
157650K .......... .......... .......... .......... .......... 60% 25.2M 21s
157700K .......... .......... .......... .......... .......... 60% 32.2M 21s
157750K .......... .......... .......... .......... .......... 60% 76.5M 21s
157800K .......... .......... .......... .......... .......... 60% 8.23M 21s
157850K .......... .......... .......... .......... .......... 60% 11.4M 21s
157900K .......... .......... .......... .......... .......... 60% 14.2M 21s
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158000K .......... .......... .......... .......... .......... 60% 7.11M 21s
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158100K .......... .......... .......... .......... .......... 60% 12.4M 21s
158150K .......... .......... .......... .......... .......... 60% 11.1M 21s
158200K .......... .......... .......... .......... .......... 60% 5.68M 21s
158250K .......... .......... .......... .......... .......... 60% 10.2M 21s
158300K .......... .......... .......... .......... .......... 60% 11.7M 21s
158350K .......... .......... .......... .......... .......... 60% 844K 21s
158400K .......... .......... .......... .......... .......... 60% 37.9M 21s
158450K .......... .......... .......... .......... .......... 60% 4.28M 21s
158500K .......... .......... .......... .......... .......... 60% 43.4M 21s
158550K .......... .......... .......... .......... .......... 60% 23.1M 21s
158600K .......... .......... .......... .......... .......... 60% 1.91M 21s
158650K .......... .......... .......... .......... .......... 60% 54.5M 20s
158700K .......... .......... .......... .......... .......... 60% 36.9M 20s
158750K .......... .......... .......... .......... .......... 60% 34.4M 20s
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158850K .......... .......... .......... .......... .......... 60% 9.32M 20s
158900K .......... .......... .......... .......... .......... 60% 11.8M 20s
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159000K .......... .......... .......... .......... .......... 60% 49.0M 20s
159050K .......... .......... .......... .......... .......... 60% 11.9M 20s
159100K .......... .......... .......... .......... .......... 60% 11.4M 20s
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159400K .......... .......... .......... .......... .......... 60% 9.21M 20s
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159500K .......... .......... .......... .......... .......... 60% 7.69M 20s
159550K .......... .......... .......... .......... .......... 60% 51.0M 20s
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159700K .......... .......... .......... .......... .......... 60% 43.6M 20s
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159900K .......... .......... .......... .......... .......... 61% 11.2M 20s
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160000K .......... .......... .......... .......... .......... 61% 10.3M 20s
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161000K .......... .......... .......... .......... .......... 61% 13.0M 20s
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161500K .......... .......... .......... .......... .......... 61% 13.8M 20s
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161600K .......... .......... .......... .......... .......... 61% 10.5M 20s
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161700K .......... .......... .......... .......... .......... 61% 1.79M 20s
161750K .......... .......... .......... .......... .......... 61% 64.6M 20s
161800K .......... .......... .......... .......... .......... 61% 52.7M 20s
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161900K .......... .......... .......... .......... .......... 61% 18.6M 20s
161950K .......... .......... .......... .......... .......... 61% 6.67M 20s
162000K .......... .......... .......... .......... .......... 61% 11.7M 20s
162050K .......... .......... .......... .......... .......... 61% 12.0M 20s
162100K .......... .......... .......... .......... .......... 61% 10.8M 20s
162150K .......... .......... .......... .......... .......... 61% 6.60M 20s
162200K .......... .......... .......... .......... .......... 61% 5.73M 20s
162250K .......... .......... .......... .......... .......... 61% 19.2M 20s
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162350K .......... .......... .......... .......... .......... 61% 11.4M 20s
162400K .......... .......... .......... .......... .......... 61% 7.40M 20s
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162500K .......... .......... .......... .......... .......... 61% 15.0M 19s
162550K .......... .......... .......... .......... .......... 62% 12.8M 19s
162600K .......... .......... .......... .......... .......... 62% 7.44M 19s
162650K .......... .......... .......... .......... .......... 62% 6.20M 19s
162700K .......... .......... .......... .......... .......... 62% 1.92M 19s
162750K .......... .......... .......... .......... .......... 62% 63.3M 19s
162800K .......... .......... .......... .......... .......... 62% 45.7M 19s
162850K .......... .......... .......... .......... .......... 62% 34.1M 19s
162900K .......... .......... .......... .......... .......... 62% 28.3M 19s
162950K .......... .......... .......... .......... .......... 62% 11.5M 19s
163000K .......... .......... .......... .......... .......... 62% 12.6M 19s
163050K .......... .......... .......... .......... .......... 62% 18.1M 19s
163100K .......... .......... .......... .......... .......... 62% 26.0M 19s
163150K .......... .......... .......... .......... .......... 62% 21.8M 19s
163200K .......... .......... .......... .......... .......... 62% 12.2M 19s
163250K .......... .......... .......... .......... .......... 62% 13.5M 19s
163300K .......... .......... .......... .......... .......... 62% 10.7M 19s
163350K .......... .......... .......... .......... .......... 62% 13.0M 19s
163400K .......... .......... .......... .......... .......... 62% 13.5M 19s
163450K .......... .......... .......... .......... .......... 62% 8.18M 19s
163500K .......... .......... .......... .......... .......... 62% 11.6M 19s
163550K .......... .......... .......... .......... .......... 62% 11.8M 19s
163600K .......... .......... .......... .......... .......... 62% 15.2M 19s
163650K .......... .......... .......... .......... .......... 62% 13.7M 19s
163700K .......... .......... .......... .......... .......... 62% 5.32M 19s
163750K .......... .......... .......... .......... .......... 62% 1.67M 19s
163800K .......... .......... .......... .......... .......... 62% 57.4M 19s
163850K .......... .......... .......... .......... .......... 62% 48.4M 19s
163900K .......... .......... .......... .......... .......... 62% 67.8M 19s
163950K .......... .......... .......... .......... .......... 62% 7.47M 19s
164000K .......... .......... .......... .......... .......... 62% 10.6M 19s
164050K .......... .......... .......... .......... .......... 62% 9.99M 19s
164100K .......... .......... .......... .......... .......... 62% 11.4M 19s
164150K .......... .......... .......... .......... .......... 62% 8.32M 19s
164200K .......... .......... .......... .......... .......... 62% 6.50M 19s
164250K .......... .......... .......... .......... .......... 62% 11.2M 19s
164300K .......... .......... .......... .......... .......... 62% 10.4M 19s
164350K .......... .......... .......... .......... .......... 62% 6.34M 19s
164400K .......... .......... .......... .......... .......... 62% 9.85M 19s
164450K .......... .......... .......... .......... .......... 62% 10.8M 19s
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164700K .......... .......... .......... .......... .......... 62% 9.79M 19s
164750K .......... .......... .......... .......... .......... 62% 1.88M 19s
164800K .......... .......... .......... .......... .......... 62% 55.8M 19s
164850K .......... .......... .......... .......... .......... 62% 41.4M 19s
164900K .......... .......... .......... .......... .......... 62% 58.5M 19s
164950K .......... .......... .......... .......... .......... 62% 18.4M 19s
165000K .......... .......... .......... .......... .......... 62% 12.1M 19s
165050K .......... .......... .......... .......... .......... 62% 14.2M 19s
165100K .......... .......... .......... .......... .......... 62% 12.9M 19s
165150K .......... .......... .......... .......... .......... 63% 16.8M 19s
165200K .......... .......... .......... .......... .......... 63% 12.0M 19s
165250K .......... .......... .......... .......... .......... 63% 8.08M 19s
165300K .......... .......... .......... .......... .......... 63% 48.9M 19s
165350K .......... .......... .......... .......... .......... 63% 8.32M 19s
165400K .......... .......... .......... .......... .......... 63% 11.1M 19s
165450K .......... .......... .......... .......... .......... 63% 10.6M 19s
165500K .......... .......... .......... .......... .......... 63% 8.71M 19s
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165600K .......... .......... .......... .......... .......... 63% 8.53M 19s
165650K .......... .......... .......... .......... .......... 63% 10.7M 19s
165700K .......... .......... .......... .......... .......... 63% 24.7M 19s
165750K .......... .......... .......... .......... .......... 63% 12.7M 19s
165800K .......... .......... .......... .......... .......... 63% 1.30M 19s
165850K .......... .......... .......... .......... .......... 63% 32.5M 19s
165900K .......... .......... .......... .......... .......... 63% 48.3M 19s
165950K .......... .......... .......... .......... .......... 63% 34.9M 19s
166000K .......... .......... .......... .......... .......... 63% 7.61M 19s
166050K .......... .......... .......... .......... .......... 63% 9.98M 19s
166100K .......... .......... .......... .......... .......... 63% 9.01M 19s
166150K .......... .......... .......... .......... .......... 63% 10.3M 19s
166200K .......... .......... .......... .......... .......... 63% 8.91M 19s
166250K .......... .......... .......... .......... .......... 63% 10.1M 19s
166300K .......... .......... .......... .......... .......... 63% 10.0M 19s
166350K .......... .......... .......... .......... .......... 63% 5.49M 19s
166400K .......... .......... .......... .......... .......... 63% 24.7M 19s
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166500K .......... .......... .......... .......... .......... 63% 8.71M 19s
166550K .......... .......... .......... .......... .......... 63% 6.02M 18s
166600K .......... .......... .......... .......... .......... 63% 42.0M 18s
166650K .......... .......... .......... .......... .......... 63% 14.8M 18s
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166750K .......... .......... .......... .......... .......... 63% 11.7M 18s
166800K .......... .......... .......... .......... .......... 63% 2.17M 18s
166850K .......... .......... .......... .......... .......... 63% 33.9M 18s
166900K .......... .......... .......... .......... .......... 63% 21.1M 18s
166950K .......... .......... .......... .......... .......... 63% 48.8M 18s
167000K .......... .......... .......... .......... .......... 63% 12.4M 18s
167050K .......... .......... .......... .......... .......... 63% 8.60M 18s
167100K .......... .......... .......... .......... .......... 63% 4.68M 18s
167150K .......... .......... .......... .......... .......... 63% 9.96M 18s
167200K .......... .......... .......... .......... .......... 63% 8.47M 18s
167250K .......... .......... .......... .......... .......... 63% 12.9M 18s
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167350K .......... .......... .......... .......... .......... 63% 12.2M 18s
167400K .......... .......... .......... .......... .......... 63% 7.38M 18s
167450K .......... .......... .......... .......... .......... 63% 11.9M 18s
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167600K .......... .......... .......... .......... .......... 63% 9.80M 18s
167650K .......... .......... .......... .......... .......... 63% 12.2M 18s
167700K .......... .......... .......... .......... .......... 63% 10.3M 18s
167750K .......... .......... .......... .......... .......... 63% 11.5M 18s
167800K .......... .......... .......... .......... .......... 64% 11.9M 18s
167850K .......... .......... .......... .......... .......... 64% 2.23M 18s
167900K .......... .......... .......... .......... .......... 64% 43.1M 18s
167950K .......... .......... .......... .......... .......... 64% 30.3M 18s
168000K .......... .......... .......... .......... .......... 64% 41.4M 18s
168050K .......... .......... .......... .......... .......... 64% 11.6M 18s
168100K .......... .......... .......... .......... .......... 64% 9.46M 18s
168150K .......... .......... .......... .......... .......... 64% 10.1M 18s
168200K .......... .......... .......... .......... .......... 64% 8.49M 18s
168250K .......... .......... .......... .......... .......... 64% 9.25M 18s
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168350K .......... .......... .......... .......... .......... 64% 39.3M 18s
168400K .......... .......... .......... .......... .......... 64% 10.3M 18s
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168500K .......... .......... .......... .......... .......... 64% 11.5M 18s
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168700K .......... .......... .......... .......... .......... 64% 11.8M 18s
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168900K .......... .......... .......... .......... .......... 64% 52.2M 18s
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169000K .......... .......... .......... .......... .......... 64% 39.9M 18s
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169100K .......... .......... .......... .......... .......... 64% 15.5M 18s
169150K .......... .......... .......... .......... .......... 64% 42.8M 18s
169200K .......... .......... .......... .......... .......... 64% 19.0M 18s
169250K .......... .......... .......... .......... .......... 64% 16.6M 18s
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170000K .......... .......... .......... .......... .......... 64% 49.0M 18s
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170100K .......... .......... .......... .......... .......... 64% 8.35M 18s
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170200K .......... .......... .......... .......... .......... 64% 5.68M 18s
170250K .......... .......... .......... .......... .......... 64% 30.2M 18s
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170400K .......... .......... .......... .......... .......... 65% 10.7M 18s
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171000K .......... .......... .......... .......... .......... 65% 44.8M 17s
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172000K .......... .......... .......... .......... .......... 65% 50.3M 17s
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172150K .......... .......... .......... .......... .......... 65% 11.8M 17s
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176150K .......... .......... .......... .......... .......... 67% 35.7M 16s
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176800K .......... .......... .......... .......... .......... 67% 12.9M 16s
176850K .......... .......... .......... .......... .......... 67% 12.1M 16s
176900K .......... .......... .......... .......... .......... 67% 20.0M 16s
176950K .......... .......... .......... .......... .......... 67% 12.9M 16s
177000K .......... .......... .......... .......... .......... 67% 14.2M 16s
177050K .......... .......... .......... .......... .......... 67% 3.62M 16s
177100K .......... .......... .......... .......... .......... 67% 34.9M 16s
177150K .......... .......... .......... .......... .......... 67% 46.8M 16s
177200K .......... .......... .......... .......... .......... 67% 32.5M 16s
177250K .......... .......... .......... .......... .......... 67% 12.0M 16s
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177400K .......... .......... .......... .......... .......... 67% 12.5M 16s
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177500K .......... .......... .......... .......... .......... 67% 8.20M 16s
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177850K .......... .......... .......... .......... .......... 67% 8.53M 16s
177900K .......... .......... .......... .......... .......... 67% 14.0M 16s
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178000K .......... .......... .......... .......... .......... 67% 19.3M 16s
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178100K .......... .......... .......... .......... .......... 67% 2.34M 16s
178150K .......... .......... .......... .......... .......... 67% 56.8M 16s
178200K .......... .......... .......... .......... .......... 67% 39.2M 16s
178250K .......... .......... .......... .......... .......... 68% 10.6M 16s
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179000K .......... .......... .......... .......... .......... 68% 18.8M 15s
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179100K .......... .......... .......... .......... .......... 68% 2.35M 15s
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179250K .......... .......... .......... .......... .......... 68% 45.6M 15s
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181000K .......... .......... .......... .......... .......... 69% 14.1M 15s
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182000K .......... .......... .......... .......... .......... 69% 12.7M 15s
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182150K .......... .......... .......... .......... .......... 69% 15.9M 15s
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182250K .......... .......... .......... .......... .......... 69% 73.1M 15s
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183000K .......... .......... .......... .......... .......... 69% 11.7M 15s
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183100K .......... .......... .......... .......... .......... 69% 5.40M 15s
183150K .......... .......... .......... .......... .......... 69% 64.4M 15s
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185250K .......... .......... .......... .......... .......... 70% 2.50M 14s
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186100K .......... .......... .......... .......... .......... 70% 8.44M 14s
186150K .......... .......... .......... .......... .......... 71% 46.2M 14s
186200K .......... .......... .......... .......... .......... 71% 9.12M 14s
186250K .......... .......... .......... .......... .......... 71% 2.18M 14s
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187000K .......... .......... .......... .......... .......... 71% 10.4M 14s
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187100K .......... .......... .......... .......... .......... 71% 13.4M 14s
187150K .......... .......... .......... .......... .......... 71% 12.5M 14s
187200K .......... .......... .......... .......... .......... 71% 12.5M 14s
187250K .......... .......... .......... .......... .......... 71% 60.0M 14s
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188000K .......... .......... .......... .......... .......... 71% 10.3M 13s
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188100K .......... .......... .......... .......... .......... 71% 42.2M 13s
188150K .......... .......... .......... .......... .......... 71% 14.0M 13s
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188250K .......... .......... .......... .......... .......... 71% 20.6M 13s
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188800K .......... .......... .......... .......... .......... 72% 16.8M 13s
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188900K .......... .......... .......... .......... .......... 72% 9.25M 13s
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189000K .......... .......... .......... .......... .......... 72% 47.1M 13s
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189100K .......... .......... .......... .......... .......... 72% 13.8M 13s
189150K .......... .......... .......... .......... .......... 72% 63.0M 13s
189200K .......... .......... .......... .......... .......... 72% 13.7M 13s
189250K .......... .......... .......... .......... .......... 72% 51.2M 13s
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189500K .......... .......... .......... .......... .......... 72% 69.0M 13s
189550K .......... .......... .......... .......... .......... 72% 111M 13s
189600K .......... .......... .......... .......... .......... 72% 11.8M 13s
189650K .......... .......... .......... .......... .......... 72% 48.5M 13s
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189850K .......... .......... .......... .......... .......... 72% 48.7M 13s
189900K .......... .......... .......... .......... .......... 72% 14.2M 13s
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190000K .......... .......... .......... .......... .......... 72% 46.7M 13s
190050K .......... .......... .......... .......... .......... 72% 11.5M 13s
190100K .......... .......... .......... .......... .......... 72% 37.5M 13s
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190200K .......... .......... .......... .......... .......... 72% 47.0M 13s
190250K .......... .......... .......... .......... .......... 72% 6.17M 13s
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190400K .......... .......... .......... .......... .......... 72% 63.9M 13s
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190600K .......... .......... .......... .......... .......... 72% 33.6M 13s
190650K .......... .......... .......... .......... .......... 72% 9.30M 13s
190700K .......... .......... .......... .......... .......... 72% 51.6M 13s
190750K .......... .......... .......... .......... .......... 72% 13.3M 13s
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190850K .......... .......... .......... .......... .......... 72% 11.3M 13s
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190950K .......... .......... .......... .......... .......... 72% 16.3M 13s
191000K .......... .......... .......... .......... .......... 72% 46.3M 13s
191050K .......... .......... .......... .......... .......... 72% 10.8M 13s
191100K .......... .......... .......... .......... .......... 72% 29.8M 13s
191150K .......... .......... .......... .......... .......... 72% 9.89M 13s
191200K .......... .......... .......... .......... .......... 72% 29.1M 13s
191250K .......... .......... .......... .......... .......... 72% 10.6M 13s
191300K .......... .......... .......... .......... .......... 72% 54.7M 13s
191350K .......... .......... .......... .......... .......... 72% 10.6M 13s
191400K .......... .......... .......... .......... .......... 73% 1.53M 13s
191450K .......... .......... .......... .......... .......... 73% 33.7M 13s
191500K .......... .......... .......... .......... .......... 73% 59.7M 13s
191550K .......... .......... .......... .......... .......... 73% 58.8M 13s
191600K .......... .......... .......... .......... .......... 73% 23.8M 13s
191650K .......... .......... .......... .......... .......... 73% 46.8M 13s
191700K .......... .......... .......... .......... .......... 73% 12.4M 13s
191750K .......... .......... .......... .......... .......... 73% 63.5M 13s
191800K .......... .......... .......... .......... .......... 73% 11.3M 13s
191850K .......... .......... .......... .......... .......... 73% 63.2M 13s
191900K .......... .......... .......... .......... .......... 73% 6.58M 13s
191950K .......... .......... .......... .......... .......... 73% 32.8M 13s
192000K .......... .......... .......... .......... .......... 73% 9.50M 13s
192050K .......... .......... .......... .......... .......... 73% 47.4M 13s
192100K .......... .......... .......... .......... .......... 73% 9.09M 13s
192150K .......... .......... .......... .......... .......... 73% 61.0M 13s
192200K .......... .......... .......... .......... .......... 73% 11.1M 12s
192250K .......... .......... .......... .......... .......... 73% 52.9M 12s
192300K .......... .......... .......... .......... .......... 73% 10.4M 12s
192350K .......... .......... .......... .......... .......... 73% 42.7M 12s
192400K .......... .......... .......... .......... .......... 73% 1.45M 12s
192450K .......... .......... .......... .......... .......... 73% 43.9M 12s
192500K .......... .......... .......... .......... .......... 73% 40.6M 12s
192550K .......... .......... .......... .......... .......... 73% 42.9M 12s
192600K .......... .......... .......... .......... .......... 73% 40.6M 12s
192650K .......... .......... .......... .......... .......... 73% 15.9M 12s
192700K .......... .......... .......... .......... .......... 73% 7.68M 12s
192750K .......... .......... .......... .......... .......... 73% 40.0M 12s
192800K .......... .......... .......... .......... .......... 73% 44.9M 12s
192850K .......... .......... .......... .......... .......... 73% 6.95M 12s
192900K .......... .......... .......... .......... .......... 73% 61.8M 12s
192950K .......... .......... .......... .......... .......... 73% 10.3M 12s
193000K .......... .......... .......... .......... .......... 73% 48.2M 12s
193050K .......... .......... .......... .......... .......... 73% 9.00M 12s
193100K .......... .......... .......... .......... .......... 73% 51.0M 12s
193150K .......... .......... .......... .......... .......... 73% 11.2M 12s
193200K .......... .......... .......... .......... .......... 73% 38.4M 12s
193250K .......... .......... .......... .......... .......... 73% 9.87M 12s
193300K .......... .......... .......... .......... .......... 73% 46.5M 12s
193350K .......... .......... .......... .......... .......... 73% 72.7M 12s
193400K .......... .......... .......... .......... .......... 73% 12.4M 12s
193450K .......... .......... .......... .......... .......... 73% 2.95M 12s
193500K .......... .......... .......... .......... .......... 73% 34.6M 12s
193550K .......... .......... .......... .......... .......... 73% 47.1M 12s
193600K .......... .......... .......... .......... .......... 73% 47.9M 12s
193650K .......... .......... .......... .......... .......... 73% 81.4M 12s
193700K .......... .......... .......... .......... .......... 73% 15.6M 12s
193750K .......... .......... .......... .......... .......... 73% 7.04M 12s
193800K .......... .......... .......... .......... .......... 73% 54.7M 12s
193850K .......... .......... .......... .......... .......... 73% 7.05M 12s
193900K .......... .......... .......... .......... .......... 73% 26.5M 12s
193950K .......... .......... .......... .......... .......... 73% 10.1M 12s
194000K .......... .......... .......... .......... .......... 74% 30.9M 12s
194050K .......... .......... .......... .......... .......... 74% 65.7M 12s
194100K .......... .......... .......... .......... .......... 74% 8.51M 12s
194150K .......... .......... .......... .......... .......... 74% 68.0M 12s
194200K .......... .......... .......... .......... .......... 74% 8.39M 12s
194250K .......... .......... .......... .......... .......... 74% 47.8M 12s
194300K .......... .......... .......... .......... .......... 74% 7.86M 12s
194350K .......... .......... .......... .......... .......... 74% 43.1M 12s
194400K .......... .......... .......... .......... .......... 74% 91.4M 12s
194450K .......... .......... .......... .......... .......... 74% 2.01M 12s
194500K .......... .......... .......... .......... .......... 74% 41.6M 12s
194550K .......... .......... .......... .......... .......... 74% 68.2M 12s
194600K .......... .......... .......... .......... .......... 74% 42.7M 12s
194650K .......... .......... .......... .......... .......... 74% 58.2M 12s
194700K .......... .......... .......... .......... .......... 74% 45.0M 12s
194750K .......... .......... .......... .......... .......... 74% 9.20M 12s
194800K .......... .......... .......... .......... .......... 74% 8.68M 12s
194850K .......... .......... .......... .......... .......... 74% 48.2M 12s
194900K .......... .......... .......... .......... .......... 74% 63.7M 12s
194950K .......... .......... .......... .......... .......... 74% 7.78M 12s
195000K .......... .......... .......... .......... .......... 74% 56.4M 12s
195050K .......... .......... .......... .......... .......... 74% 9.51M 12s
195100K .......... .......... .......... .......... .......... 74% 32.3M 12s
195150K .......... .......... .......... .......... .......... 74% 79.8M 12s
195200K .......... .......... .......... .......... .......... 74% 10.1M 12s
195250K .......... .......... .......... .......... .......... 74% 49.3M 12s
195300K .......... .......... .......... .......... .......... 74% 8.71M 12s
195350K .......... .......... .......... .......... .......... 74% 26.6M 12s
195400K .......... .......... .......... .......... .......... 74% 56.7M 12s
195450K .......... .......... .......... .......... .......... 74% 7.06M 12s
195500K .......... .......... .......... .......... .......... 74% 1.71M 12s
195550K .......... .......... .......... .......... .......... 74% 30.1M 12s
195600K .......... .......... .......... .......... .......... 74% 25.0M 12s
195650K .......... .......... .......... .......... .......... 74% 64.9M 12s
195700K .......... .......... .......... .......... .......... 74% 69.4M 12s
195750K .......... .......... .......... .......... .......... 74% 41.8M 12s
195800K .......... .......... .......... .......... .......... 74% 6.17M 12s
195850K .......... .......... .......... .......... .......... 74% 47.3M 12s
195900K .......... .......... .......... .......... .......... 74% 7.42M 12s
195950K .......... .......... .......... .......... .......... 74% 38.4M 12s
196000K .......... .......... .......... .......... .......... 74% 43.4M 12s
196050K .......... .......... .......... .......... .......... 74% 7.12M 12s
196100K .......... .......... .......... .......... .......... 74% 42.8M 12s
196150K .......... .......... .......... .......... .......... 74% 53.7M 12s
196200K .......... .......... .......... .......... .......... 74% 5.69M 12s
196250K .......... .......... .......... .......... .......... 74% 74.8M 12s
196300K .......... .......... .......... .......... .......... 74% 8.28M 12s
196350K .......... .......... .......... .......... .......... 74% 27.3M 12s
196400K .......... .......... .......... .......... .......... 74% 45.8M 12s
196450K .......... .......... .......... .......... .......... 74% 7.12M 12s
196500K .......... .......... .......... .......... .......... 74% 2.31M 12s
196550K .......... .......... .......... .......... .......... 74% 52.4M 12s
196600K .......... .......... .......... .......... .......... 75% 33.7M 12s
196650K .......... .......... .......... .......... .......... 75% 47.3M 12s
196700K .......... .......... .......... .......... .......... 75% 41.0M 12s
196750K .......... .......... .......... .......... .......... 75% 47.8M 12s
196800K .......... .......... .......... .......... .......... 75% 41.7M 12s
196850K .......... .......... .......... .......... .......... 75% 15.2M 12s
196900K .......... .......... .......... .......... .......... 75% 9.40M 12s
196950K .......... .......... .......... .......... .......... 75% 32.1M 11s
197000K .......... .......... .......... .......... .......... 75% 11.0M 11s
197050K .......... .......... .......... .......... .......... 75% 32.8M 11s
197100K .......... .......... .......... .......... .......... 75% 12.8M 11s
197150K .......... .......... .......... .......... .......... 75% 41.3M 11s
197200K .......... .......... .......... .......... .......... 75% 51.6M 11s
197250K .......... .......... .......... .......... .......... 75% 11.2M 11s
197300K .......... .......... .......... .......... .......... 75% 30.1M 11s
197350K .......... .......... .......... .......... .......... 75% 58.2M 11s
197400K .......... .......... .......... .......... .......... 75% 10.8M 11s
197450K .......... .......... .......... .......... .......... 75% 45.1M 11s
197500K .......... .......... .......... .......... .......... 75% 72.6M 11s
197550K .......... .......... .......... .......... .......... 75% 2.55M 11s
197600K .......... .......... .......... .......... .......... 75% 39.3M 11s
197650K .......... .......... .......... .......... .......... 75% 49.5M 11s
197700K .......... .......... .......... .......... .......... 75% 57.9M 11s
197750K .......... .......... .......... .......... .......... 75% 77.6M 11s
197800K .......... .......... .......... .......... .......... 75% 84.2M 11s
197850K .......... .......... .......... .......... .......... 75% 21.2M 11s
197900K .......... .......... .......... .......... .......... 75% 8.25M 11s
197950K .......... .......... .......... .......... .......... 75% 39.5M 11s
198000K .......... .......... .......... .......... .......... 75% 78.6M 11s
198050K .......... .......... .......... .......... .......... 75% 8.44M 11s
198100K .......... .......... .......... .......... .......... 75% 64.6M 11s
198150K .......... .......... .......... .......... .......... 75% 55.2M 11s
198200K .......... .......... .......... .......... .......... 75% 7.99M 11s
198250K .......... .......... .......... .......... .......... 75% 43.7M 11s
198300K .......... .......... .......... .......... .......... 75% 10.0M 11s
198350K .......... .......... .......... .......... .......... 75% 51.0M 11s
198400K .......... .......... .......... .......... .......... 75% 43.4M 11s
198450K .......... .......... .......... .......... .......... 75% 8.05M 11s
198500K .......... .......... .......... .......... .......... 75% 55.3M 11s
198550K .......... .......... .......... .......... .......... 75% 3.06M 11s
198600K .......... .......... .......... .......... .......... 75% 40.6M 11s
198650K .......... .......... .......... .......... .......... 75% 48.0M 11s
198700K .......... .......... .......... .......... .......... 75% 44.4M 11s
198750K .......... .......... .......... .......... .......... 75% 57.0M 11s
198800K .......... .......... .......... .......... .......... 75% 81.2M 11s
198850K .......... .......... .......... .......... .......... 75% 55.2M 11s
198900K .......... .......... .......... .......... .......... 75% 20.0M 11s
198950K .......... .......... .......... .......... .......... 75% 9.88M 11s
199000K .......... .......... .......... .......... .......... 75% 29.4M 11s
199050K .......... .......... .......... .......... .......... 75% 10.4M 11s
199100K .......... .......... .......... .......... .......... 75% 55.7M 11s
199150K .......... .......... .......... .......... .......... 75% 8.20M 11s
199200K .......... .......... .......... .......... .......... 75% 48.1M 11s
199250K .......... .......... .......... .......... .......... 76% 42.9M 11s
199300K .......... .......... .......... .......... .......... 76% 9.77M 11s
199350K .......... .......... .......... .......... .......... 76% 26.2M 11s
199400K .......... .......... .......... .......... .......... 76% 51.2M 11s
199450K .......... .......... .......... .......... .......... 76% 9.24M 11s
199500K .......... .......... .......... .......... .......... 76% 66.2M 11s
199550K .......... .......... .......... .......... .......... 76% 10.8M 11s
199600K .......... .......... .......... .......... .......... 76% 2.27M 11s
199650K .......... .......... .......... .......... .......... 76% 57.0M 11s
199700K .......... .......... .......... .......... .......... 76% 77.8M 11s
199750K .......... .......... .......... .......... .......... 76% 79.9M 11s
199800K .......... .......... .......... .......... .......... 76% 108M 11s
199850K .......... .......... .......... .......... .......... 76% 94.6M 11s
199900K .......... .......... .......... .......... .......... 76% 4.73M 11s
199950K .......... .......... .......... .......... .......... 76% 43.3M 11s
200000K .......... .......... .......... .......... .......... 76% 49.0M 11s
200050K .......... .......... .......... .......... .......... 76% 9.56M 11s
200100K .......... .......... .......... .......... .......... 76% 44.1M 11s
200150K .......... .......... .......... .......... .......... 76% 76.3M 11s
200200K .......... .......... .......... .......... .......... 76% 8.93M 11s
200250K .......... .......... .......... .......... .......... 76% 67.5M 11s
200300K .......... .......... .......... .......... .......... 76% 82.9M 11s
200350K .......... .......... .......... .......... .......... 76% 8.72M 11s
200400K .......... .......... .......... .......... .......... 76% 63.5M 11s
200450K .......... .......... .......... .......... .......... 76% 57.9M 11s
200500K .......... .......... .......... .......... .......... 76% 9.31M 11s
200550K .......... .......... .......... .......... .......... 76% 64.8M 11s
200600K .......... .......... .......... .......... .......... 76% 2.05M 11s
200650K .......... .......... .......... .......... .......... 76% 49.8M 11s
200700K .......... .......... .......... .......... .......... 76% 36.6M 11s
200750K .......... .......... .......... .......... .......... 76% 36.5M 11s
200800K .......... .......... .......... .......... .......... 76% 48.2M 11s
200850K .......... .......... .......... .......... .......... 76% 37.2M 11s
200900K .......... .......... .......... .......... .......... 76% 24.1M 11s
200950K .......... .......... .......... .......... .......... 76% 7.58M 11s
201000K .......... .......... .......... .......... .......... 76% 20.6M 11s
201050K .......... .......... .......... .......... .......... 76% 110M 11s
201100K .......... .......... .......... .......... .......... 76% 9.14M 11s
201150K .......... .......... .......... .......... .......... 76% 40.3M 11s
201200K .......... .......... .......... .......... .......... 76% 24.9M 11s
201250K .......... .......... .......... .......... .......... 76% 7.23M 11s
201300K .......... .......... .......... .......... .......... 76% 81.5M 11s
201350K .......... .......... .......... .......... .......... 76% 43.5M 11s
201400K .......... .......... .......... .......... .......... 76% 5.78M 11s
201450K .......... .......... .......... .......... .......... 76% 23.4M 11s
201500K .......... .......... .......... .......... .......... 76% 88.9M 11s
201550K .......... .......... .......... .......... .......... 76% 10.9M 11s
201600K .......... .......... .......... .......... .......... 76% 17.3M 11s
201650K .......... .......... .......... .......... .......... 76% 2.10M 11s
201700K .......... .......... .......... .......... .......... 76% 36.1M 10s
201750K .......... .......... .......... .......... .......... 76% 45.7M 10s
201800K .......... .......... .......... .......... .......... 76% 25.2M 10s
201850K .......... .......... .......... .......... .......... 77% 29.0M 10s
201900K .......... .......... .......... .......... .......... 77% 54.7M 10s
201950K .......... .......... .......... .......... .......... 77% 98.2M 10s
202000K .......... .......... .......... .......... .......... 77% 18.6M 10s
202050K .......... .......... .......... .......... .......... 77% 4.47M 10s
202100K .......... .......... .......... .......... .......... 77% 28.6M 10s
202150K .......... .......... .......... .......... .......... 77% 19.7M 10s
202200K .......... .......... .......... .......... .......... 77% 8.24M 10s
202250K .......... .......... .......... .......... .......... 77% 18.4M 10s
202300K .......... .......... .......... .......... .......... 77% 38.9M 10s
202350K .......... .......... .......... .......... .......... 77% 9.78M 10s
202400K .......... .......... .......... .......... .......... 77% 24.2M 10s
202450K .......... .......... .......... .......... .......... 77% 16.5M 10s
202500K .......... .......... .......... .......... .......... 77% 22.6M 10s
202550K .......... .......... .......... .......... .......... 77% 9.71M 10s
202600K .......... .......... .......... .......... .......... 77% 20.4M 10s
202650K .......... .......... .......... .......... .......... 77% 1.23M 10s
202700K .......... .......... .......... .......... .......... 77% 42.4M 10s
202750K .......... .......... .......... .......... .......... 77% 41.9M 10s
202800K .......... .......... .......... .......... .......... 77% 33.4M 10s
202850K .......... .......... .......... .......... .......... 77% 67.7M 10s
202900K .......... .......... .......... .......... .......... 77% 55.0M 10s
202950K .......... .......... .......... .......... .......... 77% 44.6M 10s
203000K .......... .......... .......... .......... .......... 77% 77.6M 10s
203050K .......... .......... .......... .......... .......... 77% 5.07M 10s
203100K .......... .......... .......... .......... .......... 77% 52.7M 10s
203150K .......... .......... .......... .......... .......... 77% 57.9M 10s
203200K .......... .......... .......... .......... .......... 77% 6.12M 10s
203250K .......... .......... .......... .......... .......... 77% 48.2M 10s
203300K .......... .......... .......... .......... .......... 77% 58.5M 10s
203350K .......... .......... .......... .......... .......... 77% 3.89M 10s
203400K .......... .......... .......... .......... .......... 77% 41.5M 10s
203450K .......... .......... .......... .......... .......... 77% 34.6M 10s
203500K .......... .......... .......... .......... .......... 77% 77.6M 10s
203550K .......... .......... .......... .......... .......... 77% 8.54M 10s
203600K .......... .......... .......... .......... .......... 77% 65.6M 10s
203650K .......... .......... .......... .......... .......... 77% 62.5M 10s
203700K .......... .......... .......... .......... .......... 77% 1.29M 10s
203750K .......... .......... .......... .......... .......... 77% 54.0M 10s
203800K .......... .......... .......... .......... .......... 77% 46.4M 10s
203850K .......... .......... .......... .......... .......... 77% 47.1M 10s
203900K .......... .......... .......... .......... .......... 77% 56.0M 10s
203950K .......... .......... .......... .......... .......... 77% 40.1M 10s
204000K .......... .......... .......... .......... .......... 77% 51.8M 10s
204050K .......... .......... .......... .......... .......... 77% 7.14M 10s
204100K .......... .......... .......... .......... .......... 77% 35.6M 10s
204150K .......... .......... .......... .......... .......... 77% 9.56M 10s
204200K .......... .......... .......... .......... .......... 77% 9.95M 10s
204250K .......... .......... .......... .......... .......... 77% 17.2M 10s
204300K .......... .......... .......... .......... .......... 77% 58.7M 10s
204350K .......... .......... .......... .......... .......... 77% 36.5M 10s
204400K .......... .......... .......... .......... .......... 77% 7.99M 10s
204450K .......... .......... .......... .......... .......... 77% 18.7M 10s
204500K .......... .......... .......... .......... .......... 78% 44.7M 10s
204550K .......... .......... .......... .......... .......... 78% 10.7M 10s
204600K .......... .......... .......... .......... .......... 78% 18.6M 10s
204650K .......... .......... .......... .......... .......... 78% 27.7M 10s
204700K .......... .......... .......... .......... .......... 78% 1.50M 10s
204750K .......... .......... .......... .......... .......... 78% 44.0M 10s
204800K .......... .......... .......... .......... .......... 78% 18.9M 10s
204850K .......... .......... .......... .......... .......... 78% 16.8M 10s
204900K .......... .......... .......... .......... .......... 78% 91.3M 10s
204950K .......... .......... .......... .......... .......... 78% 51.7M 10s
205000K .......... .......... .......... .......... .......... 78% 19.2M 10s
205050K .......... .......... .......... .......... .......... 78% 71.8M 10s
205100K .......... .......... .......... .......... .......... 78% 5.72M 10s
205150K .......... .......... .......... .......... .......... 78% 15.3M 10s
205200K .......... .......... .......... .......... .......... 78% 90.9M 10s
205250K .......... .......... .......... .......... .......... 78% 7.28M 10s
205300K .......... .......... .......... .......... .......... 78% 13.3M 10s
205350K .......... .......... .......... .......... .......... 78% 45.1M 10s
205400K .......... .......... .......... .......... .......... 78% 45.3M 10s
205450K .......... .......... .......... .......... .......... 78% 5.75M 10s
205500K .......... .......... .......... .......... .......... 78% 14.2M 10s
205550K .......... .......... .......... .......... .......... 78% 63.2M 10s
205600K .......... .......... .......... .......... .......... 78% 7.69M 10s
205650K .......... .......... .......... .......... .......... 78% 16.3M 10s
205700K .......... .......... .......... .......... .......... 78% 1.62M 10s
205750K .......... .......... .......... .......... .......... 78% 34.3M 10s
205800K .......... .......... .......... .......... .......... 78% 37.2M 10s
205850K .......... .......... .......... .......... .......... 78% 47.2M 10s
205900K .......... .......... .......... .......... .......... 78% 60.1M 10s
205950K .......... .......... .......... .......... .......... 78% 71.3M 10s
206000K .......... .......... .......... .......... .......... 78% 76.1M 10s
206050K .......... .......... .......... .......... .......... 78% 68.5M 10s
206100K .......... .......... .......... .......... .......... 78% 38.4M 10s
206150K .......... .......... .......... .......... .......... 78% 4.79M 10s
206200K .......... .......... .......... .......... .......... 78% 38.8M 10s
206250K .......... .......... .......... .......... .......... 78% 58.3M 10s
206300K .......... .......... .......... .......... .......... 78% 8.47M 10s
206350K .......... .......... .......... .......... .......... 78% 59.1M 10s
206400K .......... .......... .......... .......... .......... 78% 6.12M 10s
206450K .......... .......... .......... .......... .......... 78% 42.4M 10s
206500K .......... .......... .......... .......... .......... 78% 51.5M 10s
206550K .......... .......... .......... .......... .......... 78% 7.43M 10s
206600K .......... .......... .......... .......... .......... 78% 39.9M 10s
206650K .......... .......... .......... .......... .......... 78% 9.72M 10s
206700K .......... .......... .......... .......... .......... 78% 48.7M 10s
206750K .......... .......... .......... .......... .......... 78% 2.18M 9s
206800K .......... .......... .......... .......... .......... 78% 48.2M 9s
206850K .......... .......... .......... .......... .......... 78% 36.4M 9s
206900K .......... .......... .......... .......... .......... 78% 54.4M 9s
206950K .......... .......... .......... .......... .......... 78% 26.4M 9s
207000K .......... .......... .......... .......... .......... 78% 83.2M 9s
207050K .......... .......... .......... .......... .......... 78% 42.8M 9s
207100K .......... .......... .......... .......... .......... 79% 49.2M 9s
207150K .......... .......... .......... .......... .......... 79% 118M 9s
207200K .......... .......... .......... .......... .......... 79% 73.0M 9s
207250K .......... .......... .......... .......... .......... 79% 6.01M 9s
207300K .......... .......... .......... .......... .......... 79% 58.5M 9s
207350K .......... .......... .......... .......... .......... 79% 41.2M 9s
207400K .......... .......... .......... .......... .......... 79% 50.8M 9s
207450K .......... .......... .......... .......... .......... 79% 11.3M 9s
207500K .......... .......... .......... .......... .......... 79% 81.5M 9s
207550K .......... .......... .......... .......... .......... 79% 3.55M 9s
207600K .......... .......... .......... .......... .......... 79% 38.8M 9s
207650K .......... .......... .......... .......... .......... 79% 56.1M 9s
207700K .......... .......... .......... .......... .......... 79% 108M 9s
207750K .......... .......... .......... .......... .......... 79% 2.25M 9s
207800K .......... .......... .......... .......... .......... 79% 51.8M 9s
207850K .......... .......... .......... .......... .......... 79% 39.7M 9s
207900K .......... .......... .......... .......... .......... 79% 39.7M 9s
207950K .......... .......... .......... .......... .......... 79% 29.9M 9s
208000K .......... .......... .......... .......... .......... 79% 52.3M 9s
208050K .......... .......... .......... .......... .......... 79% 60.4M 9s
208100K .......... .......... .......... .......... .......... 79% 63.5M 9s
208150K .......... .......... .......... .......... .......... 79% 67.1M 9s
208200K .......... .......... .......... .......... .......... 79% 5.31M 9s
208250K .......... .......... .......... .......... .......... 79% 41.1M 9s
208300K .......... .......... .......... .......... .......... 79% 7.13M 9s
208350K .......... .......... .......... .......... .......... 79% 47.4M 9s
208400K .......... .......... .......... .......... .......... 79% 8.40M 9s
208450K .......... .......... .......... .......... .......... 79% 40.4M 9s
208500K .......... .......... .......... .......... .......... 79% 8.61M 9s
208550K .......... .......... .......... .......... .......... 79% 28.1M 9s
208600K .......... .......... .......... .......... .......... 79% 7.06M 9s
208650K .......... .......... .......... .......... .......... 79% 72.3M 9s
208700K .......... .......... .......... .......... .......... 79% 8.57M 9s
208750K .......... .......... .......... .......... .......... 79% 56.2M 9s
208800K .......... .......... .......... .......... .......... 79% 2.46M 9s
208850K .......... .......... .......... .......... .......... 79% 36.2M 9s
208900K .......... .......... .......... .......... .......... 79% 58.7M 9s
208950K .......... .......... .......... .......... .......... 79% 44.0M 9s
209000K .......... .......... .......... .......... .......... 79% 59.7M 9s
209050K .......... .......... .......... .......... .......... 79% 49.1M 9s
209100K .......... .......... .......... .......... .......... 79% 49.7M 9s
209150K .......... .......... .......... .......... .......... 79% 94.1M 9s
209200K .......... .......... .......... .......... .......... 79% 23.3M 9s
209250K .......... .......... .......... .......... .......... 79% 60.9M 9s
209300K .......... .......... .......... .......... .......... 79% 6.65M 9s
209350K .......... .......... .......... .......... .......... 79% 39.6M 9s
209400K .......... .......... .......... .......... .......... 79% 9.41M 9s
209450K .......... .......... .......... .......... .......... 79% 40.0M 9s
209500K .......... .......... .......... .......... .......... 79% 8.62M 9s
209550K .......... .......... .......... .......... .......... 79% 56.6M 9s
209600K .......... .......... .......... .......... .......... 79% 6.51M 9s
209650K .......... .......... .......... .......... .......... 79% 88.1M 9s
209700K .......... .......... .......... .......... .......... 79% 7.56M 9s
209750K .......... .......... .......... .......... .......... 80% 75.7M 9s
209800K .......... .......... .......... .......... .......... 80% 9.75M 9s
209850K .......... .......... .......... .......... .......... 80% 2.11M 9s
209900K .......... .......... .......... .......... .......... 80% 38.6M 9s
209950K .......... .......... .......... .......... .......... 80% 44.0M 9s
210000K .......... .......... .......... .......... .......... 80% 66.6M 9s
210050K .......... .......... .......... .......... .......... 80% 59.0M 9s
210100K .......... .......... .......... .......... .......... 80% 42.5M 9s
210150K .......... .......... .......... .......... .......... 80% 69.4M 9s
210200K .......... .......... .......... .......... .......... 80% 93.0M 9s
210250K .......... .......... .......... .......... .......... 80% 3.90M 9s
210300K .......... .......... .......... .......... .......... 80% 52.4M 9s
210350K .......... .......... .......... .......... .......... 80% 5.90M 9s
210400K .......... .......... .......... .......... .......... 80% 45.7M 9s
210450K .......... .......... .......... .......... .......... 80% 39.5M 9s
210500K .......... .......... .......... .......... .......... 80% 7.70M 9s
210550K .......... .......... .......... .......... .......... 80% 30.4M 9s
210600K .......... .......... .......... .......... .......... 80% 42.7M 9s
210650K .......... .......... .......... .......... .......... 80% 8.49M 9s
210700K .......... .......... .......... .......... .......... 80% 70.4M 9s
210750K .......... .......... .......... .......... .......... 80% 91.4M 9s
210800K .......... .......... .......... .......... .......... 80% 8.79M 9s
210850K .......... .......... .......... .......... .......... 80% 1.66M 9s
210900K .......... .......... .......... .......... .......... 80% 38.2M 9s
210950K .......... .......... .......... .......... .......... 80% 35.3M 9s
211000K .......... .......... .......... .......... .......... 80% 40.6M 9s
211050K .......... .......... .......... .......... .......... 80% 36.9M 9s
211100K .......... .......... .......... .......... .......... 80% 52.9M 9s
211150K .......... .......... .......... .......... .......... 80% 66.2M 9s
211200K .......... .......... .......... .......... .......... 80% 65.1M 9s
211250K .......... .......... .......... .......... .......... 80% 15.2M 9s
211300K .......... .......... .......... .......... .......... 80% 42.6M 9s
211350K .......... .......... .......... .......... .......... 80% 6.02M 9s
211400K .......... .......... .......... .......... .......... 80% 47.3M 9s
211450K .......... .......... .......... .......... .......... 80% 5.87M 9s
211500K .......... .......... .......... .......... .......... 80% 33.8M 9s
211550K .......... .......... .......... .......... .......... 80% 42.3M 9s
211600K .......... .......... .......... .......... .......... 80% 4.93M 9s
211650K .......... .......... .......... .......... .......... 80% 61.0M 9s
211700K .......... .......... .......... .......... .......... 80% 6.44M 9s
211750K .......... .......... .......... .......... .......... 80% 60.9M 9s
211800K .......... .......... .......... .......... .......... 80% 4.05M 9s
211850K .......... .......... .......... .......... .......... 80% 1.92M 9s
211900K .......... .......... .......... .......... .......... 80% 25.8M 8s
211950K .......... .......... .......... .......... .......... 80% 47.2M 8s
212000K .......... .......... .......... .......... .......... 80% 77.5M 8s
212050K .......... .......... .......... .......... .......... 80% 67.2M 8s
212100K .......... .......... .......... .......... .......... 80% 51.3M 8s
212150K .......... .......... .......... .......... .......... 80% 81.8M 8s
212200K .......... .......... .......... .......... .......... 80% 78.9M 8s
212250K .......... .......... .......... .......... .......... 80% 107M 8s
212300K .......... .......... .......... .......... .......... 80% 3.29M 8s
212350K .......... .......... .......... .......... .......... 81% 68.7M 8s
212400K .......... .......... .......... .......... .......... 81% 28.3M 8s
212450K .......... .......... .......... .......... .......... 81% 7.01M 8s
212500K .......... .......... .......... .......... .......... 81% 97.3M 8s
212550K .......... .......... .......... .......... .......... 81% 5.32M 8s
212600K .......... .......... .......... .......... .......... 81% 51.1M 8s
212650K .......... .......... .......... .......... .......... 81% 7.81M 8s
212700K .......... .......... .......... .......... .......... 81% 31.0M 8s
212750K .......... .......... .......... .......... .......... 81% 17.3M 8s
212800K .......... .......... .......... .......... .......... 81% 48.4M 8s
212850K .......... .......... .......... .......... .......... 81% 11.9M 8s
212900K .......... .......... .......... .......... .......... 81% 2.75M 8s
212950K .......... .......... .......... .......... .......... 81% 68.4M 8s
213000K .......... .......... .......... .......... .......... 81% 57.4M 8s
213050K .......... .......... .......... .......... .......... 81% 73.0M 8s
213100K .......... .......... .......... .......... .......... 81% 52.7M 8s
213150K .......... .......... .......... .......... .......... 81% 27.9M 8s
213200K .......... .......... .......... .......... .......... 81% 39.7M 8s
213250K .......... .......... .......... .......... .......... 81% 78.8M 8s
213300K .......... .......... .......... .......... .......... 81% 6.78M 8s
213350K .......... .......... .......... .......... .......... 81% 61.2M 8s
213400K .......... .......... .......... .......... .......... 81% 68.5M 8s
213450K .......... .......... .......... .......... .......... 81% 6.01M 8s
213500K .......... .......... .......... .......... .......... 81% 91.6M 8s
213550K .......... .......... .......... .......... .......... 81% 64.2M 8s
213600K .......... .......... .......... .......... .......... 81% 7.01M 8s
213650K .......... .......... .......... .......... .......... 81% 5.91M 8s
213700K .......... .......... .......... .......... .......... 81% 33.4M 8s
213750K .......... .......... .......... .......... .......... 81% 59.9M 8s
213800K .......... .......... .......... .......... .......... 81% 9.25M 8s
213850K .......... .......... .......... .......... .......... 81% 36.0M 8s
213900K .......... .......... .......... .......... .......... 81% 2.10M 8s
213950K .......... .......... .......... .......... .......... 81% 36.0M 8s
214000K .......... .......... .......... .......... .......... 81% 52.3M 8s
214050K .......... .......... .......... .......... .......... 81% 54.6M 8s
214100K .......... .......... .......... .......... .......... 81% 55.0M 8s
214150K .......... .......... .......... .......... .......... 81% 57.2M 8s
214200K .......... .......... .......... .......... .......... 81% 57.9M 8s
214250K .......... .......... .......... .......... .......... 81% 72.4M 8s
214300K .......... .......... .......... .......... .......... 81% 95.2M 8s
214350K .......... .......... .......... .......... .......... 81% 4.06M 8s
214400K .......... .......... .......... .......... .......... 81% 47.0M 8s
214450K .......... .......... .......... .......... .......... 81% 6.45M 8s
214500K .......... .......... .......... .......... .......... 81% 48.6M 8s
214550K .......... .......... .......... .......... .......... 81% 63.6M 8s
214600K .......... .......... .......... .......... .......... 81% 48.2M 8s
214650K .......... .......... .......... .......... .......... 81% 6.40M 8s
214700K .......... .......... .......... .......... .......... 81% 35.5M 8s
214750K .......... .......... .......... .......... .......... 81% 9.87M 8s
214800K .......... .......... .......... .......... .......... 81% 63.0M 8s
214850K .......... .......... .......... .......... .......... 81% 63.2M 8s
214900K .......... .......... .......... .......... .......... 81% 9.26M 8s
214950K .......... .......... .......... .......... .......... 81% 2.46M 8s
215000K .......... .......... .......... .......... .......... 82% 41.8M 8s
215050K .......... .......... .......... .......... .......... 82% 43.8M 8s
215100K .......... .......... .......... .......... .......... 82% 47.1M 8s
215150K .......... .......... .......... .......... .......... 82% 61.6M 8s
215200K .......... .......... .......... .......... .......... 82% 58.0M 8s
215250K .......... .......... .......... .......... .......... 82% 62.6M 8s
215300K .......... .......... .......... .......... .......... 82% 80.3M 8s
215350K .......... .......... .......... .......... .......... 82% 3.72M 8s
215400K .......... .......... .......... .......... .......... 82% 37.9M 8s
215450K .......... .......... .......... .......... .......... 82% 41.2M 8s
215500K .......... .......... .......... .......... .......... 82% 6.35M 8s
215550K .......... .......... .......... .......... .......... 82% 30.2M 8s
215600K .......... .......... .......... .......... .......... 82% 6.14M 8s
215650K .......... .......... .......... .......... .......... 82% 56.3M 8s
215700K .......... .......... .......... .......... .......... 82% 41.7M 8s
215750K .......... .......... .......... .......... .......... 82% 10.4M 8s
215800K .......... .......... .......... .......... .......... 82% 83.9M 8s
215850K .......... .......... .......... .......... .......... 82% 10.4M 8s
215900K .......... .......... .......... .......... .......... 82% 53.0M 8s
215950K .......... .......... .......... .......... .......... 82% 1.83M 8s
216000K .......... .......... .......... .......... .......... 82% 39.1M 8s
216050K .......... .......... .......... .......... .......... 82% 44.8M 8s
216100K .......... .......... .......... .......... .......... 82% 39.5M 8s
216150K .......... .......... .......... .......... .......... 82% 58.2M 8s
216200K .......... .......... .......... .......... .......... 82% 34.5M 8s
216250K .......... .......... .......... .......... .......... 82% 42.2M 8s
216300K .......... .......... .......... .......... .......... 82% 40.9M 8s
216350K .......... .......... .......... .......... .......... 82% 4.06M 8s
216400K .......... .......... .......... .......... .......... 82% 40.9M 8s
216450K .......... .......... .......... .......... .......... 82% 65.5M 8s
216500K .......... .......... .......... .......... .......... 82% 44.9M 8s
216550K .......... .......... .......... .......... .......... 82% 6.75M 8s
216600K .......... .......... .......... .......... .......... 82% 40.6M 8s
216650K .......... .......... .......... .......... .......... 82% 6.90M 8s
216700K .......... .......... .......... .......... .......... 82% 34.6M 8s
216750K .......... .......... .......... .......... .......... 82% 52.1M 8s
216800K .......... .......... .......... .......... .......... 82% 7.64M 8s
216850K .......... .......... .......... .......... .......... 82% 81.7M 8s
216900K .......... .......... .......... .......... .......... 82% 9.68M 8s
216950K .......... .......... .......... .......... .......... 82% 55.1M 8s
217000K .......... .......... .......... .......... .......... 82% 1.68M 8s
217050K .......... .......... .......... .......... .......... 82% 38.1M 8s
217100K .......... .......... .......... .......... .......... 82% 46.6M 8s
217150K .......... .......... .......... .......... .......... 82% 81.5M 8s
217200K .......... .......... .......... .......... .......... 82% 59.3M 7s
217250K .......... .......... .......... .......... .......... 82% 63.2M 7s
217300K .......... .......... .......... .......... .......... 82% 74.7M 7s
217350K .......... .......... .......... .......... .......... 82% 33.7M 7s
217400K .......... .......... .......... .......... .......... 82% 4.38M 7s
217450K .......... .......... .......... .......... .......... 82% 37.8M 7s
217500K .......... .......... .......... .......... .......... 82% 39.7M 7s
217550K .......... .......... .......... .......... .......... 82% 6.26M 7s
217600K .......... .......... .......... .......... .......... 83% 40.8M 7s
217650K .......... .......... .......... .......... .......... 83% 77.4M 7s
217700K .......... .......... .......... .......... .......... 83% 7.63M 7s
217750K .......... .......... .......... .......... .......... 83% 82.8M 7s
217800K .......... .......... .......... .......... .......... 83% 11.0M 7s
217850K .......... .......... .......... .......... .......... 83% 53.8M 7s
217900K .......... .......... .......... .......... .......... 83% 11.7M 7s
217950K .......... .......... .......... .......... .......... 83% 12.1M 7s
218000K .......... .......... .......... .......... .......... 83% 2.49M 7s
218050K .......... .......... .......... .......... .......... 83% 52.1M 7s
218100K .......... .......... .......... .......... .......... 83% 42.3M 7s
218150K .......... .......... .......... .......... .......... 83% 59.5M 7s
218200K .......... .......... .......... .......... .......... 83% 47.1M 7s
218250K .......... .......... .......... .......... .......... 83% 24.4M 7s
218300K .......... .......... .......... .......... .......... 83% 60.1M 7s
218350K .......... .......... .......... .......... .......... 83% 56.1M 7s
218400K .......... .......... .......... .......... .......... 83% 7.38M 7s
218450K .......... .......... .......... .......... .......... 83% 45.1M 7s
218500K .......... .......... .......... .......... .......... 83% 50.1M 7s
218550K .......... .......... .......... .......... .......... 83% 54.6M 7s
218600K .......... .......... .......... .......... .......... 83% 9.20M 7s
218650K .......... .......... .......... .......... .......... 83% 31.9M 7s
218700K .......... .......... .......... .......... .......... 83% 43.4M 7s
218750K .......... .......... .......... .......... .......... 83% 9.56M 7s
218800K .......... .......... .......... .......... .......... 83% 71.0M 7s
218850K .......... .......... .......... .......... .......... 83% 83.2M 7s
218900K .......... .......... .......... .......... .......... 83% 7.17M 7s
218950K .......... .......... .......... .......... .......... 83% 65.8M 7s
219000K .......... .......... .......... .......... .......... 83% 119M 7s
219050K .......... .......... .......... .......... .......... 83% 2.12M 7s
219100K .......... .......... .......... .......... .......... 83% 34.2M 7s
219150K .......... .......... .......... .......... .......... 83% 57.0M 7s
219200K .......... .......... .......... .......... .......... 83% 36.6M 7s
219250K .......... .......... .......... .......... .......... 83% 36.4M 7s
219300K .......... .......... .......... .......... .......... 83% 62.4M 7s
219350K .......... .......... .......... .......... .......... 83% 22.8M 7s
219400K .......... .......... .......... .......... .......... 83% 40.5M 7s
219450K .......... .......... .......... .......... .......... 83% 6.26M 7s
219500K .......... .......... .......... .......... .......... 83% 54.6M 7s
219550K .......... .......... .......... .......... .......... 83% 42.8M 7s
219600K .......... .......... .......... .......... .......... 83% 9.07M 7s
219650K .......... .......... .......... .......... .......... 83% 70.1M 7s
219700K .......... .......... .......... .......... .......... 83% 45.9M 7s
219750K .......... .......... .......... .......... .......... 83% 7.42M 7s
219800K .......... .......... .......... .......... .......... 83% 69.4M 7s
219850K .......... .......... .......... .......... .......... 83% 8.03M 7s
219900K .......... .......... .......... .......... .......... 83% 67.6M 7s
219950K .......... .......... .......... .......... .......... 83% 75.9M 7s
220000K .......... .......... .......... .......... .......... 83% 8.20M 7s
220050K .......... .......... .......... .......... .......... 83% 4.48M 7s
220100K .......... .......... .......... .......... .......... 83% 38.0M 7s
220150K .......... .......... .......... .......... .......... 83% 63.4M 7s
220200K .......... .......... .......... .......... .......... 84% 35.3M 7s
220250K .......... .......... .......... .......... .......... 84% 51.2M 7s
220300K .......... .......... .......... .......... .......... 84% 72.1M 7s
220350K .......... .......... .......... .......... .......... 84% 63.3M 7s
220400K .......... .......... .......... .......... .......... 84% 65.7M 7s
220450K .......... .......... .......... .......... .......... 84% 36.3M 7s
220500K .......... .......... .......... .......... .......... 84% 6.15M 7s
220550K .......... .......... .......... .......... .......... 84% 51.5M 7s
220600K .......... .......... .......... .......... .......... 84% 46.8M 7s
220650K .......... .......... .......... .......... .......... 84% 8.81M 7s
220700K .......... .......... .......... .......... .......... 84% 44.4M 7s
220750K .......... .......... .......... .......... .......... 84% 7.08M 7s
220800K .......... .......... .......... .......... .......... 84% 48.3M 7s
220850K .......... .......... .......... .......... .......... 84% 75.8M 7s
220900K .......... .......... .......... .......... .......... 84% 8.21M 7s
220950K .......... .......... .......... .......... .......... 84% 80.3M 7s
221000K .......... .......... .......... .......... .......... 84% 17.4M 7s
221050K .......... .......... .......... .......... .......... 84% 46.6M 7s
221100K .......... .......... .......... .......... .......... 84% 2.27M 7s
221150K .......... .......... .......... .......... .......... 84% 36.5M 7s
221200K .......... .......... .......... .......... .......... 84% 29.8M 7s
221250K .......... .......... .......... .......... .......... 84% 50.0M 7s
221300K .......... .......... .......... .......... .......... 84% 55.7M 7s
221350K .......... .......... .......... .......... .......... 84% 34.7M 7s
221400K .......... .......... .......... .......... .......... 84% 53.0M 7s
221450K .......... .......... .......... .......... .......... 84% 45.8M 7s
221500K .......... .......... .......... .......... .......... 84% 3.42M 7s
221550K .......... .......... .......... .......... .......... 84% 42.1M 7s
221600K .......... .......... .......... .......... .......... 84% 38.5M 7s
221650K .......... .......... .......... .......... .......... 84% 39.6M 7s
221700K .......... .......... .......... .......... .......... 84% 4.68M 7s
221750K .......... .......... .......... .......... .......... 84% 48.1M 7s
221800K .......... .......... .......... .......... .......... 84% 44.7M 7s
221850K .......... .......... .......... .......... .......... 84% 5.31M 7s
221900K .......... .......... .......... .......... .......... 84% 61.3M 7s
221950K .......... .......... .......... .......... .......... 84% 70.0M 7s
222000K .......... .......... .......... .......... .......... 84% 54.7M 7s
222050K .......... .......... .......... .......... .......... 84% 4.60M 7s
222100K .......... .......... .......... .......... .......... 84% 1.59M 7s
222150K .......... .......... .......... .......... .......... 84% 48.2M 7s
222200K .......... .......... .......... .......... .......... 84% 33.1M 7s
222250K .......... .......... .......... .......... .......... 84% 50.3M 7s
222300K .......... .......... .......... .......... .......... 84% 94.8M 7s
222350K .......... .......... .......... .......... .......... 84% 50.3M 7s
222400K .......... .......... .......... .......... .......... 84% 60.8M 7s
222450K .......... .......... .......... .......... .......... 84% 32.8M 7s
222500K .......... .......... .......... .......... .......... 84% 51.4M 7s
222550K .......... .......... .......... .......... .......... 84% 3.36M 7s
222600K .......... .......... .......... .......... .......... 84% 34.2M 6s
222650K .......... .......... .......... .......... .......... 84% 71.9M 6s
222700K .......... .......... .......... .......... .......... 84% 57.5M 6s
222750K .......... .......... .......... .......... .......... 84% 5.66M 6s
222800K .......... .......... .......... .......... .......... 84% 63.4M 6s
222850K .......... .......... .......... .......... .......... 85% 5.63M 6s
222900K .......... .......... .......... .......... .......... 85% 40.9M 6s
222950K .......... .......... .......... .......... .......... 85% 38.5M 6s
223000K .......... .......... .......... .......... .......... 85% 7.64M 6s
223050K .......... .......... .......... .......... .......... 85% 58.4M 6s
223100K .......... .......... .......... .......... .......... 85% 56.0M 6s
223150K .......... .......... .......... .......... .......... 85% 1.53M 6s
223200K .......... .......... .......... .......... .......... 85% 37.6M 6s
223250K .......... .......... .......... .......... .......... 85% 49.5M 6s
223300K .......... .......... .......... .......... .......... 85% 26.5M 6s
223350K .......... .......... .......... .......... .......... 85% 34.7M 6s
223400K .......... .......... .......... .......... .......... 85% 51.2M 6s
223450K .......... .......... .......... .......... .......... 85% 65.6M 6s
223500K .......... .......... .......... .......... .......... 85% 67.3M 6s
223550K .......... .......... .......... .......... .......... 85% 19.3M 6s
223600K .......... .......... .......... .......... .......... 85% 36.3M 6s
223650K .......... .......... .......... .......... .......... 85% 6.74M 6s
223700K .......... .......... .......... .......... .......... 85% 29.9M 6s
223750K .......... .......... .......... .......... .......... 85% 63.7M 6s
223800K .......... .......... .......... .......... .......... 85% 49.3M 6s
223850K .......... .......... .......... .......... .......... 85% 11.5M 6s
223900K .......... .......... .......... .......... .......... 85% 54.6M 6s
223950K .......... .......... .......... .......... .......... 85% 57.2M 6s
224000K .......... .......... .......... .......... .......... 85% 10.0M 6s
224050K .......... .......... .......... .......... .......... 85% 55.0M 6s
224100K .......... .......... .......... .......... .......... 85% 23.2M 6s
224150K .......... .......... .......... .......... .......... 85% 1.58M 6s
224200K .......... .......... .......... .......... .......... 85% 49.6M 6s
224250K .......... .......... .......... .......... .......... 85% 33.8M 6s
224300K .......... .......... .......... .......... .......... 85% 51.5M 6s
224350K .......... .......... .......... .......... .......... 85% 56.1M 6s
224400K .......... .......... .......... .......... .......... 85% 105M 6s
224450K .......... .......... .......... .......... .......... 85% 99.4M 6s
224500K .......... .......... .......... .......... .......... 85% 81.7M 6s
224550K .......... .......... .......... .......... .......... 85% 63.5M 6s
224600K .......... .......... .......... .......... .......... 85% 13.8M 6s
224650K .......... .......... .......... .......... .......... 85% 50.5M 6s
224700K .......... .......... .......... .......... .......... 85% 6.18M 6s
224750K .......... .......... .......... .......... .......... 85% 46.4M 6s
224800K .......... .......... .......... .......... .......... 85% 66.5M 6s
224850K .......... .......... .......... .......... .......... 85% 53.1M 6s
224900K .......... .......... .......... .......... .......... 85% 10.9M 6s
224950K .......... .......... .......... .......... .......... 85% 51.1M 6s
225000K .......... .......... .......... .......... .......... 85% 51.7M 6s
225050K .......... .......... .......... .......... .......... 85% 8.37M 6s
225100K .......... .......... .......... .......... .......... 85% 80.4M 6s
225150K .......... .......... .......... .......... .......... 85% 103M 6s
225200K .......... .......... .......... .......... .......... 85% 1.57M 6s
225250K .......... .......... .......... .......... .......... 85% 39.7M 6s
225300K .......... .......... .......... .......... .......... 85% 52.0M 6s
225350K .......... .......... .......... .......... .......... 85% 34.8M 6s
225400K .......... .......... .......... .......... .......... 85% 42.8M 6s
225450K .......... .......... .......... .......... .......... 86% 74.0M 6s
225500K .......... .......... .......... .......... .......... 86% 35.5M 6s
225550K .......... .......... .......... .......... .......... 86% 39.4M 6s
225600K .......... .......... .......... .......... .......... 86% 22.3M 6s
225650K .......... .......... .......... .......... .......... 86% 58.6M 6s
225700K .......... .......... .......... .......... .......... 86% 6.61M 6s
225750K .......... .......... .......... .......... .......... 86% 46.5M 6s
225800K .......... .......... .......... .......... .......... 86% 44.6M 6s
225850K .......... .......... .......... .......... .......... 86% 64.2M 6s
225900K .......... .......... .......... .......... .......... 86% 7.46M 6s
225950K .......... .......... .......... .......... .......... 86% 39.7M 6s
226000K .......... .......... .......... .......... .......... 86% 54.0M 6s
226050K .......... .......... .......... .......... .......... 86% 68.1M 6s
226100K .......... .......... .......... .......... .......... 86% 7.80M 6s
226150K .......... .......... .......... .......... .......... 86% 51.7M 6s
226200K .......... .......... .......... .......... .......... 86% 1.56M 6s
226250K .......... .......... .......... .......... .......... 86% 47.8M 6s
226300K .......... .......... .......... .......... .......... 86% 65.9M 6s
226350K .......... .......... .......... .......... .......... 86% 29.9M 6s
226400K .......... .......... .......... .......... .......... 86% 35.6M 6s
226450K .......... .......... .......... .......... .......... 86% 55.4M 6s
226500K .......... .......... .......... .......... .......... 86% 92.3M 6s
226550K .......... .......... .......... .......... .......... 86% 106M 6s
226600K .......... .......... .......... .......... .......... 86% 33.6M 6s
226650K .......... .......... .......... .......... .......... 86% 92.1M 6s
226700K .......... .......... .......... .......... .......... 86% 67.3M 6s
226750K .......... .......... .......... .......... .......... 86% 55.4M 6s
226800K .......... .......... .......... .......... .......... 86% 10.2M 6s
226850K .......... .......... .......... .......... .......... 86% 48.4M 6s
226900K .......... .......... .......... .......... .......... 86% 57.5M 6s
226950K .......... .......... .......... .......... .......... 86% 9.19M 6s
227000K .......... .......... .......... .......... .......... 86% 68.7M 6s
227050K .......... .......... .......... .......... .......... 86% 109M 6s
227100K .......... .......... .......... .......... .......... 86% 63.6M 6s
227150K .......... .......... .......... .......... .......... 86% 12.8M 6s
227200K .......... .......... .......... .......... .......... 86% 42.0M 6s
227250K .......... .......... .......... .......... .......... 86% 1.73M 6s
227300K .......... .......... .......... .......... .......... 86% 57.1M 6s
227350K .......... .......... .......... .......... .......... 86% 43.6M 6s
227400K .......... .......... .......... .......... .......... 86% 41.9M 6s
227450K .......... .......... .......... .......... .......... 86% 58.6M 6s
227500K .......... .......... .......... .......... .......... 86% 75.6M 6s
227550K .......... .......... .......... .......... .......... 86% 73.1M 6s
227600K .......... .......... .......... .......... .......... 86% 35.8M 6s
227650K .......... .......... .......... .......... .......... 86% 78.3M 6s
227700K .......... .......... .......... .......... .......... 86% 46.2M 6s
227750K .......... .......... .......... .......... .......... 86% 69.5M 6s
227800K .......... .......... .......... .......... .......... 86% 17.5M 6s
227850K .......... .......... .......... .......... .......... 86% 41.9M 6s
227900K .......... .......... .......... .......... .......... 86% 62.7M 6s
227950K .......... .......... .......... .......... .......... 86% 9.03M 6s
228000K .......... .......... .......... .......... .......... 86% 28.8M 6s
228050K .......... .......... .......... .......... .......... 86% 109M 6s
228100K .......... .......... .......... .......... .......... 87% 9.70M 6s
228150K .......... .......... .......... .......... .......... 87% 78.4M 6s
228200K .......... .......... .......... .......... .......... 87% 63.5M 5s
228250K .......... .......... .......... .......... .......... 87% 1.85M 5s
228300K .......... .......... .......... .......... .......... 87% 69.7M 5s
228350K .......... .......... .......... .......... .......... 87% 34.8M 5s
228400K .......... .......... .......... .......... .......... 87% 41.0M 5s
228450K .......... .......... .......... .......... .......... 87% 41.6M 5s
228500K .......... .......... .......... .......... .......... 87% 40.9M 5s
228550K .......... .......... .......... .......... .......... 87% 47.6M 5s
228600K .......... .......... .......... .......... .......... 87% 50.3M 5s
228650K .......... .......... .......... .......... .......... 87% 49.9M 5s
228700K .......... .......... .......... .......... .......... 87% 39.4M 5s
228750K .......... .......... .......... .......... .......... 87% 35.3M 5s
228800K .......... .......... .......... .......... .......... 87% 36.1M 5s
228850K .......... .......... .......... .......... .......... 87% 6.79M 5s
228900K .......... .......... .......... .......... .......... 87% 69.9M 5s
228950K .......... .......... .......... .......... .......... 87% 41.8M 5s
229000K .......... .......... .......... .......... .......... 87% 7.93M 5s
229050K .......... .......... .......... .......... .......... 87% 41.2M 5s
229100K .......... .......... .......... .......... .......... 87% 56.1M 5s
229150K .......... .......... .......... .......... .......... 87% 40.5M 5s
229200K .......... .......... .......... .......... .......... 87% 7.08M 5s
229250K .......... .......... .......... .......... .......... 87% 33.9M 5s
229300K .......... .......... .......... .......... .......... 87% 1.49M 5s
229350K .......... .......... .......... .......... .......... 87% 39.8M 5s
229400K .......... .......... .......... .......... .......... 87% 49.7M 5s
229450K .......... .......... .......... .......... .......... 87% 30.9M 5s
229500K .......... .......... .......... .......... .......... 87% 57.9M 5s
229550K .......... .......... .......... .......... .......... 87% 49.6M 5s
229600K .......... .......... .......... .......... .......... 87% 48.2M 5s
229650K .......... .......... .......... .......... .......... 87% 59.3M 5s
229700K .......... .......... .......... .......... .......... 87% 54.8M 5s
229750K .......... .......... .......... .......... .......... 87% 28.7M 5s
229800K .......... .......... .......... .......... .......... 87% 31.1M 5s
229850K .......... .......... .......... .......... .......... 87% 6.73M 5s
229900K .......... .......... .......... .......... .......... 87% 53.0M 5s
229950K .......... .......... .......... .......... .......... 87% 39.7M 5s
230000K .......... .......... .......... .......... .......... 87% 7.02M 5s
230050K .......... .......... .......... .......... .......... 87% 43.9M 5s
230100K .......... .......... .......... .......... .......... 87% 24.7M 5s
230150K .......... .......... .......... .......... .......... 87% 99.4M 5s
230200K .......... .......... .......... .......... .......... 87% 85.4M 5s
230250K .......... .......... .......... .......... .......... 87% 9.83M 5s
230300K .......... .......... .......... .......... .......... 87% 1.72M 5s
230350K .......... .......... .......... .......... .......... 87% 35.2M 5s
230400K .......... .......... .......... .......... .......... 87% 28.7M 5s
230450K .......... .......... .......... .......... .......... 87% 34.0M 5s
230500K .......... .......... .......... .......... .......... 87% 59.8M 5s
230550K .......... .......... .......... .......... .......... 87% 43.8M 5s
230600K .......... .......... .......... .......... .......... 87% 55.8M 5s
230650K .......... .......... .......... .......... .......... 87% 69.9M 5s
230700K .......... .......... .......... .......... .......... 88% 77.9M 5s
230750K .......... .......... .......... .......... .......... 88% 19.1M 5s
230800K .......... .......... .......... .......... .......... 88% 52.7M 5s
230850K .......... .......... .......... .......... .......... 88% 41.7M 5s
230900K .......... .......... .......... .......... .......... 88% 7.23M 5s
230950K .......... .......... .......... .......... .......... 88% 62.7M 5s
231000K .......... .......... .......... .......... .......... 88% 66.4M 5s
231050K .......... .......... .......... .......... .......... 88% 5.68M 5s
231100K .......... .......... .......... .......... .......... 88% 41.0M 5s
231150K .......... .......... .......... .......... .......... 88% 49.7M 5s
231200K .......... .......... .......... .......... .......... 88% 55.1M 5s
231250K .......... .......... .......... .......... .......... 88% 8.53M 5s
231300K .......... .......... .......... .......... .......... 88% 55.7M 5s
231350K .......... .......... .......... .......... .......... 88% 1.48M 5s
231400K .......... .......... .......... .......... .......... 88% 42.8M 5s
231450K .......... .......... .......... .......... .......... 88% 39.5M 5s
231500K .......... .......... .......... .......... .......... 88% 46.7M 5s
231550K .......... .......... .......... .......... .......... 88% 99.6M 5s
231600K .......... .......... .......... .......... .......... 88% 76.5M 5s
231650K .......... .......... .......... .......... .......... 88% 74.5M 5s
231700K .......... .......... .......... .......... .......... 88% 73.0M 5s
231750K .......... .......... .......... .......... .......... 88% 49.8M 5s
231800K .......... .......... .......... .......... .......... 88% 3.25M 5s
231850K .......... .......... .......... .......... .......... 88% 28.8M 5s
231900K .......... .......... .......... .......... .......... 88% 64.5M 5s
231950K .......... .......... .......... .......... .......... 88% 85.5M 5s
232000K .......... .......... .......... .......... .......... 88% 9.27M 5s
232050K .......... .......... .......... .......... .......... 88% 36.1M 5s
232100K .......... .......... .......... .......... .......... 88% 43.3M 5s
232150K .......... .......... .......... .......... .......... 88% 64.7M 5s
232200K .......... .......... .......... .......... .......... 88% 5.56M 5s
232250K .......... .......... .......... .......... .......... 88% 64.9M 5s
232300K .......... .......... .......... .......... .......... 88% 68.5M 5s
232350K .......... .......... .......... .......... .......... 88% 1.25M 5s
232400K .......... .......... .......... .......... .......... 88% 46.9M 5s
232450K .......... .......... .......... .......... .......... 88% 30.7M 5s
232500K .......... .......... .......... .......... .......... 88% 38.6M 5s
232550K .......... .......... .......... .......... .......... 88% 52.1M 5s
232600K .......... .......... .......... .......... .......... 88% 48.6M 5s
232650K .......... .......... .......... .......... .......... 88% 88.6M 5s
232700K .......... .......... .......... .......... .......... 88% 65.5M 5s
232750K .......... .......... .......... .......... .......... 88% 44.4M 5s
232800K .......... .......... .......... .......... .......... 88% 45.0M 5s
232850K .......... .......... .......... .......... .......... 88% 32.7M 5s
232900K .......... .......... .......... .......... .......... 88% 42.9M 5s
232950K .......... .......... .......... .......... .......... 88% 5.70M 5s
233000K .......... .......... .......... .......... .......... 88% 34.1M 5s
233050K .......... .......... .......... .......... .......... 88% 49.1M 5s
233100K .......... .......... .......... .......... .......... 88% 41.8M 5s
233150K .......... .......... .......... .......... .......... 88% 7.00M 5s
233200K .......... .......... .......... .......... .......... 88% 45.3M 5s
233250K .......... .......... .......... .......... .......... 88% 38.1M 5s
233300K .......... .......... .......... .......... .......... 88% 61.3M 5s
233350K .......... .......... .......... .......... .......... 89% 1.12M 5s
233400K .......... .......... .......... .......... .......... 89% 41.0M 5s
233450K .......... .......... .......... .......... .......... 89% 46.5M 5s
233500K .......... .......... .......... .......... .......... 89% 28.6M 5s
233550K .......... .......... .......... .......... .......... 89% 40.3M 5s
233600K .......... .......... .......... .......... .......... 89% 61.6M 5s
233650K .......... .......... .......... .......... .......... 89% 60.7M 5s
233700K .......... .......... .......... .......... .......... 89% 39.6M 5s
233750K .......... .......... .......... .......... .......... 89% 87.7M 5s
233800K .......... .......... .......... .......... .......... 89% 82.5M 5s
233850K .......... .......... .......... .......... .......... 89% 83.0M 5s
233900K .......... .......... .......... .......... .......... 89% 23.0M 5s
233950K .......... .......... .......... .......... .......... 89% 43.2M 5s
234000K .......... .......... .......... .......... .......... 89% 5.70M 4s
234050K .......... .......... .......... .......... .......... 89% 48.1M 4s
234100K .......... .......... .......... .......... .......... 89% 35.5M 4s
234150K .......... .......... .......... .......... .......... 89% 67.0M 4s
234200K .......... .......... .......... .......... .......... 89% 5.79M 4s
234250K .......... .......... .......... .......... .......... 89% 27.5M 4s
234300K .......... .......... .......... .......... .......... 89% 50.5M 4s
234350K .......... .......... .......... .......... .......... 89% 34.1M 4s
234400K .......... .......... .......... .......... .......... 89% 1.26M 4s
234450K .......... .......... .......... .......... .......... 89% 30.4M 4s
234500K .......... .......... .......... .......... .......... 89% 39.4M 4s
234550K .......... .......... .......... .......... .......... 89% 45.1M 4s
234600K .......... .......... .......... .......... .......... 89% 32.3M 4s
234650K .......... .......... .......... .......... .......... 89% 51.1M 4s
234700K .......... .......... .......... .......... .......... 89% 44.6M 4s
234750K .......... .......... .......... .......... .......... 89% 79.7M 4s
234800K .......... .......... .......... .......... .......... 89% 72.0M 4s
234850K .......... .......... .......... .......... .......... 89% 66.9M 4s
234900K .......... .......... .......... .......... .......... 89% 22.7M 4s
234950K .......... .......... .......... .......... .......... 89% 46.2M 4s
235000K .......... .......... .......... .......... .......... 89% 69.2M 4s
235050K .......... .......... .......... .......... .......... 89% 4.48M 4s
235100K .......... .......... .......... .......... .......... 89% 51.0M 4s
235150K .......... .......... .......... .......... .......... 89% 41.0M 4s
235200K .......... .......... .......... .......... .......... 89% 7.01M 4s
235250K .......... .......... .......... .......... .......... 89% 41.8M 4s
235300K .......... .......... .......... .......... .......... 89% 47.0M 4s
235350K .......... .......... .......... .......... .......... 89% 39.9M 4s
235400K .......... .......... .......... .......... .......... 89% 1.18M 4s
235450K .......... .......... .......... .......... .......... 89% 42.4M 4s
235500K .......... .......... .......... .......... .......... 89% 36.6M 4s
235550K .......... .......... .......... .......... .......... 89% 41.9M 4s
235600K .......... .......... .......... .......... .......... 89% 31.2M 4s
235650K .......... .......... .......... .......... .......... 89% 52.8M 4s
235700K .......... .......... .......... .......... .......... 89% 47.0M 4s
235750K .......... .......... .......... .......... .......... 89% 77.6M 4s
235800K .......... .......... .......... .......... .......... 89% 35.6M 4s
235850K .......... .......... .......... .......... .......... 89% 37.6M 4s
235900K .......... .......... .......... .......... .......... 89% 57.4M 4s
235950K .......... .......... .......... .......... .......... 90% 40.8M 4s
236000K .......... .......... .......... .......... .......... 90% 80.2M 4s
236050K .......... .......... .......... .......... .......... 90% 6.01M 4s
236100K .......... .......... .......... .......... .......... 90% 32.6M 4s
236150K .......... .......... .......... .......... .......... 90% 48.3M 4s
236200K .......... .......... .......... .......... .......... 90% 39.3M 4s
236250K .......... .......... .......... .......... .......... 90% 6.49M 4s
236300K .......... .......... .......... .......... .......... 90% 85.7M 4s
236350K .......... .......... .......... .......... .......... 90% 58.1M 4s
236400K .......... .......... .......... .......... .......... 90% 71.8M 4s
236450K .......... .......... .......... .......... .......... 90% 1.11M 4s
236500K .......... .......... .......... .......... .......... 90% 37.0M 4s
236550K .......... .......... .......... .......... .......... 90% 82.2M 4s
236600K .......... .......... .......... .......... .......... 90% 39.2M 4s
236650K .......... .......... .......... .......... .......... 90% 45.2M 4s
236700K .......... .......... .......... .......... .......... 90% 12.6M 4s
236750K .......... .......... .......... .......... .......... 90% 109M 4s
236800K .......... .......... .......... .......... .......... 90% 105M 4s
236850K .......... .......... .......... .......... .......... 90% 88.1M 4s
236900K .......... .......... .......... .......... .......... 90% 120M 4s
236950K .......... .......... .......... .......... .......... 90% 23.0M 4s
237000K .......... .......... .......... .......... .......... 90% 68.5M 4s
237050K .......... .......... .......... .......... .......... 90% 72.6M 4s
237100K .......... .......... .......... .......... .......... 90% 4.13M 4s
237150K .......... .......... .......... .......... .......... 90% 62.4M 4s
237200K .......... .......... .......... .......... .......... 90% 50.2M 4s
237250K .......... .......... .......... .......... .......... 90% 5.75M 4s
237300K .......... .......... .......... .......... .......... 90% 46.2M 4s
237350K .......... .......... .......... .......... .......... 90% 52.9M 4s
237400K .......... .......... .......... .......... .......... 90% 6.85M 4s
237450K .......... .......... .......... .......... .......... 90% 1.38M 4s
237500K .......... .......... .......... .......... .......... 90% 50.7M 4s
237550K .......... .......... .......... .......... .......... 90% 40.7M 4s
237600K .......... .......... .......... .......... .......... 90% 38.8M 4s
237650K .......... .......... .......... .......... .......... 90% 50.9M 4s
237700K .......... .......... .......... .......... .......... 90% 66.4M 4s
237750K .......... .......... .......... .......... .......... 90% 70.3M 4s
237800K .......... .......... .......... .......... .......... 90% 46.1M 4s
237850K .......... .......... .......... .......... .......... 90% 41.0M 4s
237900K .......... .......... .......... .......... .......... 90% 61.7M 4s
237950K .......... .......... .......... .......... .......... 90% 44.4M 4s
238000K .......... .......... .......... .......... .......... 90% 4.33M 4s
238050K .......... .......... .......... .......... .......... 90% 48.4M 4s
238100K .......... .......... .......... .......... .......... 90% 43.4M 4s
238150K .......... .......... .......... .......... .......... 90% 57.6M 4s
238200K .......... .......... .......... .......... .......... 90% 8.71M 4s
238250K .......... .......... .......... .......... .......... 90% 40.2M 4s
238300K .......... .......... .......... .......... .......... 90% 34.1M 4s
238350K .......... .......... .......... .......... .......... 90% 44.8M 4s
238400K .......... .......... .......... .......... .......... 90% 6.67M 4s
238450K .......... .......... .......... .......... .......... 90% 36.4M 4s
238500K .......... .......... .......... .......... .......... 90% 1.39M 4s
238550K .......... .......... .......... .......... .......... 91% 49.9M 4s
238600K .......... .......... .......... .......... .......... 91% 36.6M 4s
238650K .......... .......... .......... .......... .......... 91% 31.7M 4s
238700K .......... .......... .......... .......... .......... 91% 37.7M 4s
238750K .......... .......... .......... .......... .......... 91% 65.5M 4s
238800K .......... .......... .......... .......... .......... 91% 44.7M 4s
238850K .......... .......... .......... .......... .......... 91% 59.5M 4s
238900K .......... .......... .......... .......... .......... 91% 79.3M 4s
238950K .......... .......... .......... .......... .......... 91% 68.1M 4s
239000K .......... .......... .......... .......... .......... 91% 67.6M 4s
239050K .......... .......... .......... .......... .......... 91% 12.9M 4s
239100K .......... .......... .......... .......... .......... 91% 40.7M 4s
239150K .......... .......... .......... .......... .......... 91% 5.06M 4s
239200K .......... .......... .......... .......... .......... 91% 13.0M 4s
239250K .......... .......... .......... .......... .......... 91% 74.7M 4s
239300K .......... .......... .......... .......... .......... 91% 75.6M 4s
239350K .......... .......... .......... .......... .......... 91% 8.19M 4s
239400K .......... .......... .......... .......... .......... 91% 66.4M 4s
239450K .......... .......... .......... .......... .......... 91% 44.8M 4s
239500K .......... .......... .......... .......... .......... 91% 1.23M 4s
239550K .......... .......... .......... .......... .......... 91% 39.3M 4s
239600K .......... .......... .......... .......... .......... 91% 41.5M 4s
239650K .......... .......... .......... .......... .......... 91% 31.8M 4s
239700K .......... .......... .......... .......... .......... 91% 38.5M 4s
239750K .......... .......... .......... .......... .......... 91% 51.5M 4s
239800K .......... .......... .......... .......... .......... 91% 55.4M 4s
239850K .......... .......... .......... .......... .......... 91% 67.3M 4s
239900K .......... .......... .......... .......... .......... 91% 83.8M 4s
239950K .......... .......... .......... .......... .......... 91% 45.9M 3s
240000K .......... .......... .......... .......... .......... 91% 65.7M 3s
240050K .......... .......... .......... .......... .......... 91% 25.1M 3s
240100K .......... .......... .......... .......... .......... 91% 35.9M 3s
240150K .......... .......... .......... .......... .......... 91% 45.8M 3s
240200K .......... .......... .......... .......... .......... 91% 5.08M 3s
240250K .......... .......... .......... .......... .......... 91% 47.7M 3s
240300K .......... .......... .......... .......... .......... 91% 52.2M 3s
240350K .......... .......... .......... .......... .......... 91% 8.30M 3s
240400K .......... .......... .......... .......... .......... 91% 44.8M 3s
240450K .......... .......... .......... .......... .......... 91% 32.7M 3s
240500K .......... .......... .......... .......... .......... 91% 50.3M 3s
240550K .......... .......... .......... .......... .......... 91% 1.27M 3s
240600K .......... .......... .......... .......... .......... 91% 53.6M 3s
240650K .......... .......... .......... .......... .......... 91% 38.3M 3s
240700K .......... .......... .......... .......... .......... 91% 48.9M 3s
240750K .......... .......... .......... .......... .......... 91% 40.4M 3s
240800K .......... .......... .......... .......... .......... 91% 51.0M 3s
240850K .......... .......... .......... .......... .......... 91% 59.0M 3s
240900K .......... .......... .......... .......... .......... 91% 85.2M 3s
240950K .......... .......... .......... .......... .......... 91% 50.6M 3s
241000K .......... .......... .......... .......... .......... 91% 51.9M 3s
241050K .......... .......... .......... .......... .......... 91% 34.5M 3s
241100K .......... .......... .......... .......... .......... 91% 48.4M 3s
241150K .......... .......... .......... .......... .......... 91% 88.8M 3s
241200K .......... .......... .......... .......... .......... 92% 5.88M 3s
241250K .......... .......... .......... .......... .......... 92% 45.8M 3s
241300K .......... .......... .......... .......... .......... 92% 67.2M 3s
241350K .......... .......... .......... .......... .......... 92% 56.3M 3s
241400K .......... .......... .......... .......... .......... 92% 9.21M 3s
241450K .......... .......... .......... .......... .......... 92% 43.0M 3s
241500K .......... .......... .......... .......... .......... 92% 45.4M 3s
241550K .......... .......... .......... .......... .......... 92% 1.35M 3s
241600K .......... .......... .......... .......... .......... 92% 50.2M 3s
241650K .......... .......... .......... .......... .......... 92% 56.2M 3s
241700K .......... .......... .......... .......... .......... 92% 28.2M 3s
241750K .......... .......... .......... .......... .......... 92% 45.9M 3s
241800K .......... .......... .......... .......... .......... 92% 48.9M 3s
241850K .......... .......... .......... .......... .......... 92% 59.0M 3s
241900K .......... .......... .......... .......... .......... 92% 62.1M 3s
241950K .......... .......... .......... .......... .......... 92% 43.1M 3s
242000K .......... .......... .......... .......... .......... 92% 28.9M 3s
242050K .......... .......... .......... .......... .......... 92% 52.7M 3s
242100K .......... .......... .......... .......... .......... 92% 61.8M 3s
242150K .......... .......... .......... .......... .......... 92% 69.9M 3s
242200K .......... .......... .......... .......... .......... 92% 97.1M 3s
242250K .......... .......... .......... .......... .......... 92% 6.80M 3s
242300K .......... .......... .......... .......... .......... 92% 70.4M 3s
242350K .......... .......... .......... .......... .......... 92% 45.8M 3s
242400K .......... .......... .......... .......... .......... 92% 6.70M 3s
242450K .......... .......... .......... .......... .......... 92% 32.4M 3s
242500K .......... .......... .......... .......... .......... 92% 55.9M 3s
242550K .......... .......... .......... .......... .......... 92% 78.6M 3s
242600K .......... .......... .......... .......... .......... 92% 1.29M 3s
242650K .......... .......... .......... .......... .......... 92% 43.5M 3s
242700K .......... .......... .......... .......... .......... 92% 34.2M 3s
242750K .......... .......... .......... .......... .......... 92% 29.1M 3s
242800K .......... .......... .......... .......... .......... 92% 67.3M 3s
242850K .......... .......... .......... .......... .......... 92% 54.7M 3s
242900K .......... .......... .......... .......... .......... 92% 83.2M 3s
242950K .......... .......... .......... .......... .......... 92% 67.1M 3s
243000K .......... .......... .......... .......... .......... 92% 67.3M 3s
243050K .......... .......... .......... .......... .......... 92% 69.6M 3s
243100K .......... .......... .......... .......... .......... 92% 36.5M 3s
243150K .......... .......... .......... .......... .......... 92% 46.4M 3s
243200K .......... .......... .......... .......... .......... 92% 60.4M 3s
243250K .......... .......... .......... .......... .......... 92% 6.01M 3s
243300K .......... .......... .......... .......... .......... 92% 58.4M 3s
243350K .......... .......... .......... .......... .......... 92% 50.3M 3s
243400K .......... .......... .......... .......... .......... 92% 72.8M 3s
243450K .......... .......... .......... .......... .......... 92% 9.39M 3s
243500K .......... .......... .......... .......... .......... 92% 69.3M 3s
243550K .......... .......... .......... .......... .......... 92% 49.3M 3s
243600K .......... .......... .......... .......... .......... 92% 1.36M 3s
243650K .......... .......... .......... .......... .......... 92% 35.3M 3s
243700K .......... .......... .......... .......... .......... 92% 38.8M 3s
243750K .......... .......... .......... .......... .......... 92% 43.6M 3s
243800K .......... .......... .......... .......... .......... 93% 55.8M 3s
243850K .......... .......... .......... .......... .......... 93% 39.3M 3s
243900K .......... .......... .......... .......... .......... 93% 61.7M 3s
243950K .......... .......... .......... .......... .......... 93% 73.9M 3s
244000K .......... .......... .......... .......... .......... 93% 90.9M 3s
244050K .......... .......... .......... .......... .......... 93% 73.3M 3s
244100K .......... .......... .......... .......... .......... 93% 62.9M 3s
244150K .......... .......... .......... .......... .......... 93% 18.3M 3s
244200K .......... .......... .......... .......... .......... 93% 28.6M 3s
244250K .......... .......... .......... .......... .......... 93% 83.8M 3s
244300K .......... .......... .......... .......... .......... 93% 6.32M 3s
244350K .......... .......... .......... .......... .......... 93% 32.0M 3s
244400K .......... .......... .......... .......... .......... 93% 43.4M 3s
244450K .......... .......... .......... .......... .......... 93% 36.5M 3s
244500K .......... .......... .......... .......... .......... 93% 7.54M 3s
244550K .......... .......... .......... .......... .......... 93% 66.3M 3s
244600K .......... .......... .......... .......... .......... 93% 32.7M 3s
244650K .......... .......... .......... .......... .......... 93% 1.53M 3s
244700K .......... .......... .......... .......... .......... 93% 41.6M 3s
244750K .......... .......... .......... .......... .......... 93% 37.9M 3s
244800K .......... .......... .......... .......... .......... 93% 38.4M 3s
244850K .......... .......... .......... .......... .......... 93% 40.5M 3s
244900K .......... .......... .......... .......... .......... 93% 77.8M 3s
244950K .......... .......... .......... .......... .......... 93% 46.6M 3s
245000K .......... .......... .......... .......... .......... 93% 80.7M 3s
245050K .......... .......... .......... .......... .......... 93% 40.2M 3s
245100K .......... .......... .......... .......... .......... 93% 37.0M 3s
245150K .......... .......... .......... .......... .......... 93% 55.0M 3s
245200K .......... .......... .......... .......... .......... 93% 41.2M 3s
245250K .......... .......... .......... .......... .......... 93% 70.9M 3s
245300K .......... .......... .......... .......... .......... 93% 7.70M 3s
245350K .......... .......... .......... .......... .......... 93% 67.6M 3s
245400K .......... .......... .......... .......... .......... 93% 76.3M 3s
245450K .......... .......... .......... .......... .......... 93% 65.3M 3s
245500K .......... .......... .......... .......... .......... 93% 6.15M 3s
245550K .......... .......... .......... .......... .......... 93% 63.3M 3s
245600K .......... .......... .......... .......... .......... 93% 53.8M 3s
245650K .......... .......... .......... .......... .......... 93% 1.32M 3s
245700K .......... .......... .......... .......... .......... 93% 42.4M 3s
245750K .......... .......... .......... .......... .......... 93% 37.8M 3s
245800K .......... .......... .......... .......... .......... 93% 42.4M 3s
245850K .......... .......... .......... .......... .......... 93% 25.1M 3s
245900K .......... .......... .......... .......... .......... 93% 52.5M 3s
245950K .......... .......... .......... .......... .......... 93% 43.6M 3s
246000K .......... .......... .......... .......... .......... 93% 70.7M 3s
246050K .......... .......... .......... .......... .......... 93% 73.1M 2s
246100K .......... .......... .......... .......... .......... 93% 56.7M 2s
246150K .......... .......... .......... .......... .......... 93% 69.2M 2s
246200K .......... .......... .......... .......... .......... 93% 22.6M 2s
246250K .......... .......... .......... .......... .......... 93% 43.8M 2s
246300K .......... .......... .......... .......... .......... 93% 44.1M 2s
246350K .......... .......... .......... .......... .......... 93% 5.62M 2s
246400K .......... .......... .......... .......... .......... 93% 76.7M 2s
246450K .......... .......... .......... .......... .......... 94% 62.2M 2s
246500K .......... .......... .......... .......... .......... 94% 7.52M 2s
246550K .......... .......... .......... .......... .......... 94% 36.5M 2s
246600K .......... .......... .......... .......... .......... 94% 57.9M 2s
246650K .......... .......... .......... .......... .......... 94% 63.6M 2s
246700K .......... .......... .......... .......... .......... 94% 1.55M 2s
246750K .......... .......... .......... .......... .......... 94% 55.0M 2s
246800K .......... .......... .......... .......... .......... 94% 33.5M 2s
246850K .......... .......... .......... .......... .......... 94% 37.0M 2s
246900K .......... .......... .......... .......... .......... 94% 60.6M 2s
246950K .......... .......... .......... .......... .......... 94% 45.4M 2s
247000K .......... .......... .......... .......... .......... 94% 47.9M 2s
247050K .......... .......... .......... .......... .......... 94% 52.7M 2s
247100K .......... .......... .......... .......... .......... 94% 45.0M 2s
247150K .......... .......... .......... .......... .......... 94% 92.3M 2s
247200K .......... .......... .......... .......... .......... 94% 68.4M 2s
247250K .......... .......... .......... .......... .......... 94% 68.8M 2s
247300K .......... .......... .......... .......... .......... 94% 86.4M 2s
247350K .......... .......... .......... .......... .......... 94% 8.05M 2s
247400K .......... .......... .......... .......... .......... 94% 27.8M 2s
247450K .......... .......... .......... .......... .......... 94% 35.2M 2s
247500K .......... .......... .......... .......... .......... 94% 82.2M 2s
247550K .......... .......... .......... .......... .......... 94% 11.5M 2s
247600K .......... .......... .......... .......... .......... 94% 51.9M 2s
247650K .......... .......... .......... .......... .......... 94% 65.5M 2s
247700K .......... .......... .......... .......... .......... 94% 1.39M 2s
247750K .......... .......... .......... .......... .......... 94% 38.8M 2s
247800K .......... .......... .......... .......... .......... 94% 50.9M 2s
247850K .......... .......... .......... .......... .......... 94% 35.2M 2s
247900K .......... .......... .......... .......... .......... 94% 44.6M 2s
247950K .......... .......... .......... .......... .......... 94% 62.9M 2s
248000K .......... .......... .......... .......... .......... 94% 80.2M 2s
248050K .......... .......... .......... .......... .......... 94% 66.7M 2s
248100K .......... .......... .......... .......... .......... 94% 64.9M 2s
248150K .......... .......... .......... .......... .......... 94% 92.3M 2s
248200K .......... .......... .......... .......... .......... 94% 73.5M 2s
248250K .......... .......... .......... .......... .......... 94% 40.5M 2s
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249100K .......... .......... .......... .......... .......... 95% 48.7M 2s
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262150K .......... .......... .......... .......... ..... 100% 36.7M=40s
2024-04-27 17:49:33 (6.45 MB/s) - ‘ESPbeta.tgz’ saved [268487989/268487989]
+ 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:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:169]]
ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,0,999)"
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
--> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000158 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:176]]
ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,14,999)"
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
--> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000164 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:183]]
iend must not be less than ibeg when evaluating "slice(e3,4,-1)"
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
--> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (illegal_pmtr_index) in Branch Brch_000317 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:384]]
index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000332 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:402]]
index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000346 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:418]]
row index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000360 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:434]]
row index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000367 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:442]]
row index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000374 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:450]]
column index must be between 1 and 3
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000381 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:458]]
column index must be between 1 and 3
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (UNKNOWN) in Branch Brch_001805 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:1914]]
signal 1 thrown by user
--> catching signal 1 (UNKNOWN)
ERROR:: (illegal_value) in Branch Brch_001813 at [[/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions.csm:1924]]
vertex and base must be different
--> catching signal -225 (illegal_value)
==> serveESP completed successfully with no verification data
real 0m1.636s
user 0m0.038s
sys 0m0.038s
+ 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 0m0.366s
user 0m0.383s
sys 0m0.035s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m2.940s
user 0m4.014s
sys 0m0.509s
+ 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 0m0.655s
user 0m0.726s
sys 0m0.040s
+ 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 0m0.441s
user 0m0.654s
sys 0m0.041s
+ 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 0m0.533s
user 0m0.707s
sys 0m0.032s
+ 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 0m4.247s
user 0m5.946s
sys 0m0.368s
+ 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 0m44.945s
user 1m8.353s
sys 0m3.232s
+ 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 0m0.484s
user 0m0.672s
sys 0m0.030s
+ 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 0m40.194s
user 1m7.592s
sys 0m5.533s
+ 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 0m0.248s
user 0m0.215s
sys 0m0.030s
+ 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 0m0.420s
user 0m0.673s
sys 0m0.019s
+ 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 0m0.131s
user 0m0.175s
sys 0m0.014s
+ 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 0m0.358s
user 0m0.441s
sys 0m0.021s
+ 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 2.133s
OK
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m6.211s
user 0m9.694s
sys 0m0.292s
++ 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 27.331s
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 = 0.023 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4283 6322
AFLR2 GG : Nodes, Faces = 6128 10012
AFLR2 GG : Nodes, Faces = 7863 13482
AFLR2 GG : Nodes, Faces = 9464 16684
AFLR2 GG : Nodes, Faces = 10948 19652
AFLR2 GG : Nodes, Faces = 12322 22400
AFLR2 GG : Nodes, Faces = 13619 24994
AFLR2 GG : Nodes, Faces = 14829 27414
AFLR2 GG : Nodes, Faces = 15981 29718
AFLR2 GG : Nodes, Faces = 17082 31920
AFLR2 GG : Nodes, Faces = 18110 33976
AFLR2 GG : Nodes, Faces = 19081 35918
AFLR2 GG : Nodes, Faces = 20014 37784
AFLR2 GG : Nodes, Faces = 20924 39604
AFLR2 GG : Nodes, Faces = 21782 41320
AFLR2 GG : Nodes, Faces = 22595 42946
AFLR2 GG : Nodes, Faces = 23377 44510
AFLR2 GG : Nodes, Faces = 24129 46014
AFLR2 GG : Nodes, Faces = 24840 47436
AFLR2 GG : Nodes, Faces = 25522 48800
AFLR2 GG : Nodes, Faces = 26170 50096
AFLR2 GG : Nodes, Faces = 26793 51342
AFLR2 GG : Nodes, Faces = 27346 52448
AFLR2 GG : Nodes, Faces = 27846 53448
AFLR2 GG : Nodes, Faces = 28280 54316
AFLR2 GG : Nodes, Faces = 28652 55060
AFLR2 GG : Nodes, Faces = 28920 55596
AFLR2 GG : Nodes, Faces = 29143 56042
AFLR2 GG : Nodes, Faces = 29358 56472
AFLR2 GG : Nodes, Faces = 29550 56856
AFLR2 GG : Nodes, Faces = 29693 57142
AFLR2 GG : Nodes, Faces = 29805 57366
AFLR2 GG : Nodes, Faces = 29875 57506
AFLR2 GG : Nodes, Faces = 29895 57546
AFLR2 GG : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.062 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.006 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2224 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2224 2224
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 446 894
AFLR2 IG : Nodes, Faces = 892 1786
AFLR2 IG : Nodes, Faces = 918 1838
AFLR2 IG : Nodes, Faces = 1033 2068
AFLR2 IG : Nodes, Faces = 1133 2268
AFLR2 IG : Nodes, Faces = 1233 2468
AFLR2 IG : Nodes, Faces = 1333 2668
AFLR2 IG : Nodes, Faces = 1338 2678
AFLR2 IG : Nodes, Faces = 1433 2868
AFLR2 IG : Nodes, Faces = 1533 3068
AFLR2 IG : Nodes, Faces = 1633 3268
AFLR2 IG : Nodes, Faces = 1733 3468
AFLR2 IG : Nodes, Faces = 1784 3570
AFLR2 IG : Nodes, Faces = 1833 3668
AFLR2 IG : Nodes, Faces = 1858 3718
AFLR2 IG : Nodes, Faces = 2224 4450
AFLR2 IG : Nodes, Faces = 2228 4450
AFLR2 IG : Nodes, Faces = 2224 2224
AFLR2 : CPU Time = 0.025 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2224 2224
AFLR2 GG : Nodes, Faces = 4122 6020
AFLR2 GG : Nodes, Faces = 5812 9400
AFLR2 GG : Nodes, Faces = 7299 12374
AFLR2 GG : Nodes, Faces = 8574 14924
AFLR2 GG : Nodes, Faces = 9729 17234
AFLR2 GG : Nodes, Faces = 10787 19350
AFLR2 GG : Nodes, Faces = 11767 21310
AFLR2 GG : Nodes, Faces = 12683 23142
AFLR2 GG : Nodes, Faces = 13516 24808
AFLR2 GG : Nodes, Faces = 14278 26332
AFLR2 GG : Nodes, Faces = 14999 27774
AFLR2 GG : Nodes, Faces = 15682 29140
AFLR2 GG : Nodes, Faces = 16312 30400
AFLR2 GG : Nodes, Faces = 16899 31574
AFLR2 GG : Nodes, Faces = 17451 32678
AFLR2 GG : Nodes, Faces = 17959 33694
AFLR2 GG : Nodes, Faces = 18443 34662
AFLR2 GG : Nodes, Faces = 18877 35530
AFLR2 GG : Nodes, Faces = 19283 36342
AFLR2 GG : Nodes, Faces = 19650 37076
AFLR2 GG : Nodes, Faces = 19994 37764
AFLR2 GG : Nodes, Faces = 20325 38426
AFLR2 GG : Nodes, Faces = 20638 39052
AFLR2 GG : Nodes, Faces = 20940 39656
AFLR2 GG : Nodes, Faces = 21240 40256
AFLR2 GG : Nodes, Faces = 21523 40822
AFLR2 GG : Nodes, Faces = 21792 41360
AFLR2 GG : Nodes, Faces = 22053 41882
AFLR2 GG : Nodes, Faces = 22305 42386
AFLR2 GG : Nodes, Faces = 22521 42818
AFLR2 GG : Nodes, Faces = 22696 43168
AFLR2 GG : Nodes, Faces = 22829 43434
AFLR2 GG : Nodes, Faces = 22953 43682
AFLR2 GG : Nodes, Faces = 23050 43876
AFLR2 GG : Nodes, Faces = 23110 43996
AFLR2 GG : Nodes, Faces = 23139 44054
AFLR2 GG : Nodes, Faces = 23157 44090
AFLR2 GG : Nodes, Faces = 23175 44126
AFLR2 GG : Nodes, Faces = 23183 44142
AFLR2 GG : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.058 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.005 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
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 = 0.022 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 = 0.060 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.007 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2224 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2224 2224
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 446 894
AFLR2 IG : Nodes, Faces = 892 1786
AFLR2 IG : Nodes, Faces = 918 1838
AFLR2 IG : Nodes, Faces = 1033 2068
AFLR2 IG : Nodes, Faces = 1133 2268
AFLR2 IG : Nodes, Faces = 1233 2468
AFLR2 IG : Nodes, Faces = 1333 2668
AFLR2 IG : Nodes, Faces = 1338 2678
AFLR2 IG : Nodes, Faces = 1433 2868
AFLR2 IG : Nodes, Faces = 1533 3068
AFLR2 IG : Nodes, Faces = 1633 3268
AFLR2 IG : Nodes, Faces = 1733 3468
AFLR2 IG : Nodes, Faces = 1784 3570
AFLR2 IG : Nodes, Faces = 1833 3668
AFLR2 IG : Nodes, Faces = 1858 3718
AFLR2 IG : Nodes, Faces = 2224 4450
AFLR2 IG : Nodes, Faces = 2228 4450
AFLR2 IG : Nodes, Faces = 2224 2224
AFLR2 : CPU Time = 0.024 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 = 0.055 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.005 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
ok
test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.026 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 = 0.060 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.006 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 48 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 10 22
AFLR2 IG : Nodes, Faces = 20 42
AFLR2 IG : Nodes, Faces = 30 62
AFLR2 IG : Nodes, Faces = 40 82
AFLR2 IG : Nodes, Faces = 45 92
AFLR2 IG : Nodes, Faces = 46 94
AFLR2 IG : Nodes, Faces = 48 98
AFLR2 IG : Nodes, Faces = 52 98
AFLR2 IG : Nodes, Faces = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 48 48
AFLR2 GG : Nodes, Faces = 88 128
AFLR2 GG : Nodes, Faces = 109 170
AFLR2 GG : Nodes, Faces = 124 200
AFLR2 GG : Nodes, Faces = 136 224
AFLR2 GG : Nodes, Faces = 148 248
AFLR2 GG : Nodes, Faces = 161 274
AFLR2 GG : Nodes, Faces = 171 294
AFLR2 GG : Nodes, Faces = 181 314
AFLR2 GG : Nodes, Faces = 187 326
AFLR2 GG : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 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 = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.011 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 = 0.006 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 = 0.011 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 = 0.005 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS 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:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Getting volume mesh
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:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Rib_Root, index = 1
Name = Skin, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 46
Number of elements = 44
Number of triangle elements = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes = 47
Total number of elements = 44
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 46
Number of elements = 44
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 44
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 47
Combined Number of elements = 45
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 44
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 3
Surface 2: Number of points found for aero-spline = 6
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
8 automatic connections were made for capsConnect Rib_Root (node id 1)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
ok
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice control surface data
VLM control surface name - Elevator
VLM control surface name - LeftAileron
VLM control surface name - RightAileron
VLM control surface name - Rudder
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... skipped 'No flowCart executable'
test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable'
test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable'
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable'
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable'
test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Wing1, index = 1
Name = trailingEdge, index = 2
Writing FAST file ....
Finished writing FAST file
Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 9
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = nodeBody, index = 8
Name = farfield, index = 9
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000111F3000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7000111F3000 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
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000111F3000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7000111F3000 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
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000111F3000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7000111F3000 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
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000111F3000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7000111F3000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ok
test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = nodeBody, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ok
test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Writing 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: 0.206521
Creating surface mesh ...
Surface mesh seconds: 0.040638
Recovering boundaries...
Boundary recovery seconds: 0.131516
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.058163
Recovering Delaunayness...
Delaunay recovery seconds: 0.060735
Refining mesh...
18972 insertions, added 13254 points, 701278 tetrahedra in queue.
6317 insertions, added 2883 points, 614952 tetrahedra in queue.
8421 insertions, added 2047 points, 103425 tetrahedra in queue.
Refinement seconds: 2.68269
Smoothing vertices...
Mesh smoothing seconds: 2.53671
Improving mesh...
Mesh improvement seconds: 0.054973
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.024851
Total running seconds: 5.79771
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: 0.192586
Creating surface mesh ...
Surface mesh seconds: 0.037575
Recovering boundaries...
Boundary recovery seconds: 0.124019
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.054537
Recovering Delaunayness...
Delaunay recovery seconds: 0.061844
Refining mesh...
18972 insertions, added 13254 points, 701278 tetrahedra in queue.
6317 insertions, added 2883 points, 614952 tetrahedra in queue.
8421 insertions, added 2047 points, 103425 tetrahedra in queue.
Refinement seconds: 2.64339
Smoothing vertices...
Mesh smoothing seconds: 2.64445
Improving mesh...
Mesh improvement seconds: 0.05376
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.018595
Total running seconds: 5.83153
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 = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 225 396
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 225
Number of elements = 450
Number of tris = 396
Number of quad = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 915
Number of elements = 4865
Number of triangles = 922
Number of quadrilatarals = 0
Number of tetrahedrals = 3943
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 = 325
Number of elements = 1582
Number of triangles = 496
Number of quadrilatarals = 0
Number of tetrahedrals = 1086
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 = 975
Number of elements = 5204
Number of triangles = 874
Number of quadrilatarals = 0
Number of tetrahedrals = 4330
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
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 = 2189
Number of elements = 9805
Number of triangles = 3992
Number of quadrilatarals = 0
Number of tetrahedrals = 5813
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 = 915
Number of elements = 4865
Number of triangles = 922
Number of quadrilatarals = 0
Number of tetrahedrals = 3943
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 = 79
Number of elements = 345
Number of triangles = 136
Number of quadrilatarals = 0
Number of tetrahedrals = 209
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 = 305
Number of elements = 1472
Number of triangles = 468
Number of quadrilatarals = 0
Number of tetrahedrals = 1004
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
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
*** ERROR 200212 : duplicate boundary edges found ***
ERROR
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... *** ERROR 200212 : duplicate boundary edges found ***
FAIL
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... *** ERROR 200212 : duplicate boundary edges found ***
FAIL
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
*** ERROR 200212 : duplicate boundary edges found ***
ERROR
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
*** ERROR 200212 : duplicate boundary edges found ***
ERROR
test_reenter (test_su2.TestSU2.test_reenter) ... *** ERROR 200212 : duplicate boundary edges found ***
ERROR
test_units (test_su2.TestSU2.test_units) ... *** ERROR 200212 : duplicate boundary edges found ***
ERROR
test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting surface mesh for body 1 (of 7)
Getting surface mesh for body 2 (of 7)
Getting surface mesh for body 3 (of 7)
Getting surface mesh for body 4 (of 7)
Getting surface mesh for body 5 (of 7)
Getting surface mesh for body 6 (of 7)
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7000111F3000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1141E4E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000111F3000 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
caps_filter Warning: No bodies with capsAIM = tetgenAIM!
Body 1 capsAIM = aflr4AIM;aflr3AIM;platoAIM
Body 2 capsAIM = aflr4AIM;aflr3AIM;platoAIM
caps_filter Warning: No bodies with capsAIM = egadsTessAIM!
Body 1 capsAIM = aflr4AIM;aflr3AIM;platoAIM
Body 2 capsAIM = aflr4AIM;aflr3AIM;platoAIM
ERROR
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
======================================================================
ERROR: test_inputs (test_su2.TestSU2.test_inputs)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 102, in test_inputs
self.myAnalysis.preAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
Error: AFLR4 mesh generation failed...
An EGADS file with all AFLR4 parameters
has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================
======================================================================
ERROR: test_journal (test_su2.TestSU2.test_journal)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 357, in test_journal
line_total = self.run_journal(myProblem, -1)
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 310, in run_journal
su2.preAnalysis(); line += 1
^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
Error: AFLR4 mesh generation failed...
An EGADS file with all AFLR4 parameters
has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================
======================================================================
ERROR: test_phase (test_su2.TestSU2.test_phase)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 226, in test_phase
su2.preAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
Error: AFLR4 mesh generation failed...
An EGADS file with all AFLR4 parameters
has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================
======================================================================
ERROR: test_reenter (test_su2.TestSU2.test_reenter)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 152, in test_reenter
self.myAnalysis.preAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
Error: AFLR4 mesh generation failed...
An EGADS file with all AFLR4 parameters
has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================
======================================================================
ERROR: test_units (test_su2.TestSU2.test_units)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 194, in test_units
myAnalysis.preAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis
self._analysisObj.preAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error):
================================================================================
aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212
aflr4_Interface.c:588 in aflr4_Surface_Mesh():
Error: AFLR4 mesh generation failed...
An EGADS file with all AFLR4 parameters
has been written to 'aflr4_debug.egads'
aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212
Problem during AFLR4 surface meshing
transferValues for Surface_Mesh from Surface_Mesh = 200212
transferValues for Mesh from Volume_Mesh = 200212
================================================================================
======================================================================
ERROR: test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_tetgen.py", line 167, in test_faceMatch_MultiDomain
tetgen.runAnalysis()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis
self._analysisObj.execute()
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_SOURCEERR:
================================================================================
egadsTessAIM.c:420 in aimUpdateState():
Error: No Bodies!
transferValues for Surface_Mesh from Surface_Mesh = -330
================================================================================
======================================================================
FAIL: test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 142, in test_invalidBoundary
self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND")
AssertionError: 'UNKNOWN_ERROR' != 'CAPS_NOTFOUND'
- UNKNOWN_ERROR
+ CAPS_NOTFOUND
======================================================================
FAIL: test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 124, in test_invalidBoundaryName
self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND")
AssertionError: 'UNKNOWN_ERROR' != 'CAPS_NOTFOUND'
- UNKNOWN_ERROR
+ CAPS_NOTFOUND
----------------------------------------------------------------------
Ran 143 tests in 529.272s
FAILED (failures=2, errors=6, skipped=15)
CAPS Error: Cannot open /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/su2_problem/Scratch/capsRestart/Problem!
CAPS Warning: caps_writeProblem = -333 (caps_close)!
make: *** [test] Error 1
Build step 'Conditional step (single)' marked build as failure
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE