Started by upstream project "ESP_bPreBuilt" build number 77
originally caused by:
Started by user galbramc
Running as galbramc
[EnvInject] - Loading node environment variables.
Building remotely on macys_VM in workspace /Users/jenkins/workspace/ESP_bPreBuilt
[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_bPreBuilt
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-07-27T23:59:51.894 -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 2518
Checking out a fresh workspace because /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-07-27T23:59:51.894 -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 882
Checking out a fresh workspace because /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023 doesn't exist
Cleaning local Directory CAPS/training/2023
Checking out svn+ssh://acdl.mit.edu/home/svnroot/CAPS/training/2023 at revision '2024-07-27T23:59:51.894 -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 4251
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [macys_VM] is in [[macys, macys_VM, master, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-rhel7, reynolds-ubuntu16, reynolds-ubuntu18, reynolds-ubuntu20]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[ESP_bPreBuilt] $ /bin/bash -xe /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jenkins14803164292654395812.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_PreBuilt.sh
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.15
++ SU2_VERSION=8.0.1
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export MPLBACKEND=agg
++ MPLBACKEND=agg
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ macys_VM == \r\e\y\n\o\l\d\s ]]
++ [[ '' == *\.\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
++ export ESP_UDC_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/personalUdc
++ ESP_UDC_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/personalUdc
++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ macys_VM == *\r\e\y\n\o\l\d\s* ]]
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
+++ [[ -r /usr/local/etc/profile.d/bash_completion.sh ]]
+++ . /usr/local/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
+++ export PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d '/Users/jenkins/util/ESP/OpenCASCADE-.?'
ls: /Users/jenkins/util/ESP/OpenCASCADE-.?: No such file or directory
++ export CASROOT=
++ CASROOT=
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/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_bPreBuilt/ESP//lib:/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_bPreBuilt/ESP//lib:/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_11.5.15
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.15
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.1
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.1
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.1/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-v8.0.1/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-v8.0.1/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.1/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-v8.0.1/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-v8.0.1/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
++ export PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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-v8.0.1/bin
++ PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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-v8.0.1/bin
++ export PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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-v8.0.1/bin
++ PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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-v8.0.1/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ [[ macys_VM == \m\a\c\y\s* ]]
++ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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_bPreBuilt/ESP//bin/python
++ ln -s /usr/local/bin/python3-config /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config
++ ln -s /usr/local/bin/virtualenv /Users/jenkins/workspace/ESP_bPreBuilt/ESP//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_bPreBuilt/ESP//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
++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/data
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
++ uname -s
+ [[ Darwin == *\D\a\r\w\i\n* ]]
+ DESKTOP=/Users/jenkins/Desktop
+ OSI=macos
++ uname -m
+ ARCH=x86_64
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESP126-macos-x86_64.tgz
--2024-07-28 00:46:28-- https://acdl.mit.edu/ESP/archive/ESP126-macos-x86_64.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: 545954930 (521M) [application/x-gzip]
Saving to: ‘ESP126-macos-x86_64.tgz’
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13000K .......... .......... .......... .......... .......... 2% 72.0M 29s
13050K .......... .......... .......... .......... .......... 2% 86.7M 29s
13100K .......... .......... .......... .......... .......... 2% 10.3M 29s
13150K .......... .......... .......... .......... .......... 2% 616K 32s
13200K .......... .......... .......... .......... .......... 2% 108M 32s
13250K .......... .......... .......... .......... .......... 2% 146M 32s
13300K .......... .......... .......... .......... .......... 2% 138M 32s
13350K .......... .......... .......... .......... .......... 2% 143M 32s
13400K .......... .......... .......... .......... .......... 2% 104K 50s
13450K .......... .......... .......... .......... .......... 2% 170M 50s
13500K .......... .......... .......... .......... .......... 2% 224M 50s
13550K .......... .......... .......... .......... .......... 2% 118M 50s
13600K .......... .......... .......... .......... .......... 2% 161M 50s
13650K .......... .......... .......... .......... .......... 2% 34.9M 50s
13700K .......... .......... .......... .......... .......... 2% 155M 49s
13750K .......... .......... .......... .......... .......... 2% 159M 49s
13800K .......... .......... .......... .......... .......... 2% 84.5M 49s
13850K .......... .......... .......... .......... .......... 2% 81.7M 49s
13900K .......... .......... .......... .......... .......... 2% 114M 49s
13950K .......... .......... .......... .......... .......... 2% 146M 49s
14000K .......... .......... .......... .......... .......... 2% 162M 48s
14050K .......... .......... .......... .......... .......... 2% 173M 48s
14100K .......... .......... .......... .......... .......... 2% 178M 48s
14150K .......... .......... .......... .......... .......... 2% 206M 48s
14200K .......... .......... .......... .......... .......... 2% 181M 48s
14250K .......... .......... .......... .......... .......... 2% 182M 48s
14300K .......... .......... .......... .......... .......... 2% 156M 47s
14350K .......... .......... .......... .......... .......... 2% 153M 47s
14400K .......... .......... .......... .......... .......... 2% 209M 47s
14450K .......... .......... .......... .......... .......... 2% 158M 47s
14500K .......... .......... .......... .......... .......... 2% 210M 47s
14550K .......... .......... .......... .......... .......... 2% 216M 47s
14600K .......... .......... .......... .......... .......... 2% 38.7M 46s
14650K .......... .......... .......... .......... .......... 2% 124M 46s
14700K .......... .......... .......... .......... .......... 2% 110M 46s
14750K .......... .......... .......... .......... .......... 2% 50.7M 46s
14800K .......... .......... .......... .......... .......... 2% 5.06M 46s
14850K .......... .......... .......... .......... .......... 2% 100M 46s
14900K .......... .......... .......... .......... .......... 2% 109M 46s
14950K .......... .......... .......... .......... .......... 2% 79.3M 46s
15000K .......... .......... .......... .......... .......... 2% 120M 46s
15050K .......... .......... .......... .......... .......... 2% 170M 46s
15100K .......... .......... .......... .......... .......... 2% 7.98M 46s
15150K .......... .......... .......... .......... .......... 2% 91.6M 45s
15200K .......... .......... .......... .......... .......... 2% 73.5M 45s
15250K .......... .......... .......... .......... .......... 2% 171M 45s
15300K .......... .......... .......... .......... .......... 2% 138M 45s
15350K .......... .......... .......... .......... .......... 2% 1.34M 46s
15400K .......... .......... .......... .......... .......... 2% 149M 46s
15450K .......... .......... .......... .......... .......... 2% 133M 46s
15500K .......... .......... .......... .......... .......... 2% 32.9M 46s
15550K .......... .......... .......... .......... .......... 2% 139M 46s
15600K .......... .......... .......... .......... .......... 2% 150M 45s
15650K .......... .......... .......... .......... .......... 2% 176M 45s
15700K .......... .......... .......... .......... .......... 2% 175M 45s
15750K .......... .......... .......... .......... .......... 2% 197M 45s
15800K .......... .......... .......... .......... .......... 2% 195M 45s
15850K .......... .......... .......... .......... .......... 2% 166M 45s
15900K .......... .......... .......... .......... .......... 2% 57.7M 45s
15950K .......... .......... .......... .......... .......... 3% 140M 44s
16000K .......... .......... .......... .......... .......... 3% 119M 44s
16050K .......... .......... .......... .......... .......... 3% 188M 44s
16100K .......... .......... .......... .......... .......... 3% 153M 44s
16150K .......... .......... .......... .......... .......... 3% 141M 44s
16200K .......... .......... .......... .......... .......... 3% 153M 44s
16250K .......... .......... .......... .......... .......... 3% 182M 44s
16300K .......... .......... .......... .......... .......... 3% 61.7M 44s
16350K .......... .......... .......... .......... .......... 3% 178M 43s
16400K .......... .......... .......... .......... .......... 3% 271M 43s
16450K .......... .......... .......... .......... .......... 3% 116M 43s
16500K .......... .......... .......... .......... .......... 3% 4.56M 43s
16550K .......... .......... .......... .......... .......... 3% 150M 43s
16600K .......... .......... .......... .......... .......... 3% 162M 43s
16650K .......... .......... .......... .......... .......... 3% 185M 43s
16700K .......... .......... .......... .......... .......... 3% 122M 43s
16750K .......... .......... .......... .......... .......... 3% 189M 43s
16800K .......... .......... .......... .......... .......... 3% 4.95M 43s
16850K .......... .......... .......... .......... .......... 3% 149M 43s
16900K .......... .......... .......... .......... .......... 3% 213M 43s
16950K .......... .......... .......... .......... .......... 3% 155M 43s
17000K .......... .......... .......... .......... .......... 3% 203M 42s
17050K .......... .......... .......... .......... .......... 3% 196M 42s
17100K .......... .......... .......... .......... .......... 3% 4.84M 43s
17150K .......... .......... .......... .......... .......... 3% 180M 42s
17200K .......... .......... .......... .......... .......... 3% 184M 42s
17250K .......... .......... .......... .......... .......... 3% 182M 42s
17300K .......... .......... .......... .......... .......... 3% 161M 42s
17350K .......... .......... .......... .......... .......... 3% 101M 42s
17400K .......... .......... .......... .......... .......... 3% 1.63M 43s
17450K .......... .......... .......... .......... .......... 3% 84.8M 43s
17500K .......... .......... .......... .......... .......... 3% 157M 42s
17550K .......... .......... .......... .......... .......... 3% 152M 42s
17600K .......... .......... .......... .......... .......... 3% 176M 42s
17650K .......... .......... .......... .......... .......... 3% 209M 42s
17700K .......... .......... .......... .......... .......... 3% 145M 42s
17750K .......... .......... .......... .......... .......... 3% 174M 42s
17800K .......... .......... .......... .......... .......... 3% 217M 42s
17850K .......... .......... .......... .......... .......... 3% 145M 42s
17900K .......... .......... .......... .......... .......... 3% 187M 42s
17950K .......... .......... .......... .......... .......... 3% 132M 41s
18000K .......... .......... .......... .......... .......... 3% 175M 41s
18050K .......... .......... .......... .......... .......... 3% 192M 41s
18100K .......... .......... .......... .......... .......... 3% 147M 41s
18150K .......... .......... .......... .......... .......... 3% 174M 41s
18200K .......... .......... .......... .......... .......... 3% 160M 41s
18250K .......... .......... .......... .......... .......... 3% 174M 41s
18300K .......... .......... .......... .......... .......... 3% 303M 41s
18350K .......... .......... .......... .......... .......... 3% 15.6M 41s
18400K .......... .......... .......... .......... .......... 3% 145M 41s
18450K .......... .......... .......... .......... .......... 3% 128M 40s
18500K .......... .......... .......... .......... .......... 3% 152M 40s
18550K .......... .......... .......... .......... .......... 3% 9.12M 40s
18600K .......... .......... .......... .......... .......... 3% 155M 40s
18650K .......... .......... .......... .......... .......... 3% 167M 40s
18700K .......... .......... .......... .......... .......... 3% 5.99M 40s
18750K .......... .......... .......... .......... .......... 3% 66.6M 40s
18800K .......... .......... .......... .......... .......... 3% 77.5M 40s
18850K .......... .......... .......... .......... .......... 3% 130M 40s
18900K .......... .......... .......... .......... .......... 3% 7.53M 40s
18950K .......... .......... .......... .......... .......... 3% 72.7M 40s
19000K .......... .......... .......... .......... .......... 3% 114M 40s
19050K .......... .......... .......... .......... .......... 3% 3.32M 40s
19100K .......... .......... .......... .......... .......... 3% 144M 40s
19150K .......... .......... .......... .......... .......... 3% 216M 40s
19200K .......... .......... .......... .......... .......... 3% 186M 40s
19250K .......... .......... .......... .......... .......... 3% 210M 40s
19300K .......... .......... .......... .......... .......... 3% 136M 40s
19350K .......... .......... .......... .......... .......... 3% 160M 40s
19400K .......... .......... .......... .......... .......... 3% 206M 39s
19450K .......... .......... .......... .......... .......... 3% 443K 42s
19500K .......... .......... .......... .......... .......... 3% 167M 42s
19550K .......... .......... .......... .......... .......... 3% 120M 42s
19600K .......... .......... .......... .......... .......... 3% 144M 42s
19650K .......... .......... .......... .......... .......... 3% 63.2M 42s
19700K .......... .......... .......... .......... .......... 3% 97.3M 42s
19750K .......... .......... .......... .......... .......... 3% 38.4M 42s
19800K .......... .......... .......... .......... .......... 3% 4.75M 42s
19850K .......... .......... .......... .......... .......... 3% 25.3M 42s
19900K .......... .......... .......... .......... .......... 3% 135M 42s
19950K .......... .......... .......... .......... .......... 3% 142M 42s
20000K .......... .......... .......... .......... .......... 3% 206M 42s
20050K .......... .......... .......... .......... .......... 3% 199M 41s
20100K .......... .......... .......... .......... .......... 3% 179M 41s
20150K .......... .......... .......... .......... .......... 3% 198M 41s
20200K .......... .......... .......... .......... .......... 3% 138M 41s
20250K .......... .......... .......... .......... .......... 3% 203M 41s
20300K .......... .......... .......... .......... .......... 3% 38.7M 41s
20350K .......... .......... .......... .......... .......... 3% 61.2M 41s
20400K .......... .......... .......... .......... .......... 3% 179M 41s
20450K .......... .......... .......... .......... .......... 3% 102M 41s
20500K .......... .......... .......... .......... .......... 3% 174M 41s
20550K .......... .......... .......... .......... .......... 3% 137M 41s
20600K .......... .......... .......... .......... .......... 3% 154M 40s
20650K .......... .......... .......... .......... .......... 3% 198M 40s
20700K .......... .......... .......... .......... .......... 3% 160M 40s
20750K .......... .......... .......... .......... .......... 3% 197M 40s
20800K .......... .......... .......... .......... .......... 3% 189M 40s
20850K .......... .......... .......... .......... .......... 3% 165M 40s
20900K .......... .......... .......... .......... .......... 3% 132M 40s
20950K .......... .......... .......... .......... .......... 3% 176M 40s
21000K .......... .......... .......... .......... .......... 3% 7.17M 40s
21050K .......... .......... .......... .......... .......... 3% 81.1M 40s
21100K .......... .......... .......... .......... .......... 3% 108M 40s
21150K .......... .......... .......... .......... .......... 3% 127M 40s
21200K .......... .......... .......... .......... .......... 3% 139M 40s
21250K .......... .......... .......... .......... .......... 3% 138M 39s
21300K .......... .......... .......... .......... .......... 4% 135M 39s
21350K .......... .......... .......... .......... .......... 4% 7.29M 39s
21400K .......... .......... .......... .......... .......... 4% 127M 39s
21450K .......... .......... .......... .......... .......... 4% 170M 39s
21500K .......... .......... .......... .......... .......... 4% 3.07M 40s
21550K .......... .......... .......... .......... .......... 4% 125M 39s
21600K .......... .......... .......... .......... .......... 4% 94.4M 39s
21650K .......... .......... .......... .......... .......... 4% 133M 39s
21700K .......... .......... .......... .......... .......... 4% 114M 39s
21750K .......... .......... .......... .......... .......... 4% 157M 39s
21800K .......... .......... .......... .......... .......... 4% 176M 39s
21850K .......... .......... .......... .......... .......... 4% 170M 39s
21900K .......... .......... .......... .......... .......... 4% 184M 39s
21950K .......... .......... .......... .......... .......... 4% 155M 39s
22000K .......... .......... .......... .......... .......... 4% 5.13M 39s
22050K .......... .......... .......... .......... .......... 4% 90.4M 39s
22100K .......... .......... .......... .......... .......... 4% 132M 39s
22150K .......... .......... .......... .......... .......... 4% 150M 39s
22200K .......... .......... .......... .......... .......... 4% 164M 39s
22250K .......... .......... .......... .......... .......... 4% 2.44M 39s
22300K .......... .......... .......... .......... .......... 4% 169M 39s
22350K .......... .......... .......... .......... .......... 4% 95.6M 39s
22400K .......... .......... .......... .......... .......... 4% 5.85M 39s
22450K .......... .......... .......... .......... .......... 4% 65.0M 39s
22500K .......... .......... .......... .......... .......... 4% 111M 39s
22550K .......... .......... .......... .......... .......... 4% 94.3M 39s
22600K .......... .......... .......... .......... .......... 4% 97.1M 39s
22650K .......... .......... .......... .......... .......... 4% 167M 38s
22700K .......... .......... .......... .......... .......... 4% 128M 38s
22750K .......... .......... .......... .......... .......... 4% 28.2M 38s
22800K .......... .......... .......... .......... .......... 4% 119M 38s
22850K .......... .......... .......... .......... .......... 4% 3.91M 38s
22900K .......... .......... .......... .......... .......... 4% 82.8M 38s
22950K .......... .......... .......... .......... .......... 4% 112M 38s
23000K .......... .......... .......... .......... .......... 4% 59.8M 38s
23050K .......... .......... .......... .......... .......... 4% 77.9M 38s
23100K .......... .......... .......... .......... .......... 4% 95.9M 38s
23150K .......... .......... .......... .......... .......... 4% 112M 38s
23200K .......... .......... .......... .......... .......... 4% 111M 38s
23250K .......... .......... .......... .......... .......... 4% 7.00M 38s
23300K .......... .......... .......... .......... .......... 4% 173M 38s
23350K .......... .......... .......... .......... .......... 4% 150M 38s
23400K .......... .......... .......... .......... .......... 4% 226M 38s
23450K .......... .......... .......... .......... .......... 4% 178M 38s
23500K .......... .......... .......... .......... .......... 4% 11.9M 38s
23550K .......... .......... .......... .......... .......... 4% 95.4K 49s
23600K .......... .......... .......... .......... .......... 4% 131M 49s
23650K .......... .......... .......... .......... .......... 4% 186M 49s
23700K .......... .......... .......... .......... .......... 4% 59.3M 49s
23750K .......... .......... .......... .......... .......... 4% 57.0M 49s
23800K .......... .......... .......... .......... .......... 4% 74.2M 48s
23850K .......... .......... .......... .......... .......... 4% 79.9M 48s
23900K .......... .......... .......... .......... .......... 4% 169M 48s
23950K .......... .......... .......... .......... .......... 4% 156M 48s
24000K .......... .......... .......... .......... .......... 4% 127M 48s
24050K .......... .......... .......... .......... .......... 4% 133M 48s
24100K .......... .......... .......... .......... .......... 4% 127M 48s
24150K .......... .......... .......... .......... .......... 4% 134M 48s
24200K .......... .......... .......... .......... .......... 4% 185M 48s
24250K .......... .......... .......... .......... .......... 4% 191M 48s
24300K .......... .......... .......... .......... .......... 4% 162M 47s
24350K .......... .......... .......... .......... .......... 4% 95.7M 47s
24400K .......... .......... .......... .......... .......... 4% 137M 47s
24450K .......... .......... .......... .......... .......... 4% 161M 47s
24500K .......... .......... .......... .......... .......... 4% 196M 47s
24550K .......... .......... .......... .......... .......... 4% 32.7M 47s
24600K .......... .......... .......... .......... .......... 4% 110M 47s
24650K .......... .......... .......... .......... .......... 4% 104M 47s
24700K .......... .......... .......... .......... .......... 4% 60.1M 47s
24750K .......... .......... .......... .......... .......... 4% 5.06M 47s
24800K .......... .......... .......... .......... .......... 4% 206M 47s
24850K .......... .......... .......... .......... .......... 4% 98.8M 47s
24900K .......... .......... .......... .......... .......... 4% 159M 47s
24950K .......... .......... .......... .......... .......... 4% 156M 46s
25000K .......... .......... .......... .......... .......... 4% 51.3M 46s
25050K .......... .......... .......... .......... .......... 4% 150M 46s
25100K .......... .......... .......... .......... .......... 4% 4.30M 46s
25150K .......... .......... .......... .......... .......... 4% 147M 46s
25200K .......... .......... .......... .......... .......... 4% 107M 46s
25250K .......... .......... .......... .......... .......... 4% 112M 46s
25300K .......... .......... .......... .......... .......... 4% 71.9M 46s
25350K .......... .......... .......... .......... .......... 4% 176M 46s
25400K .......... .......... .......... .......... .......... 4% 186M 46s
25450K .......... .......... .......... .......... .......... 4% 160M 46s
25500K .......... .......... .......... .......... .......... 4% 1.24M 47s
25550K .......... .......... .......... .......... .......... 4% 168M 46s
25600K .......... .......... .......... .......... .......... 4% 469K 48s
25650K .......... .......... .......... .......... .......... 4% 185M 48s
25700K .......... .......... .......... .......... .......... 4% 7.32M 48s
25750K .......... .......... .......... .......... .......... 4% 206M 48s
25800K .......... .......... .......... .......... .......... 4% 216M 48s
25850K .......... .......... .......... .......... .......... 4% 182M 48s
25900K .......... .......... .......... .......... .......... 4% 27.9M 48s
25950K .......... .......... .......... .......... .......... 4% 113M 48s
26000K .......... .......... .......... .......... .......... 4% 155M 48s
26050K .......... .......... .......... .......... .......... 4% 167M 48s
26100K .......... .......... .......... .......... .......... 4% 151M 48s
26150K .......... .......... .......... .......... .......... 4% 183M 48s
26200K .......... .......... .......... .......... .......... 4% 74.2M 48s
26250K .......... .......... .......... .......... .......... 4% 86.6M 47s
26300K .......... .......... .......... .......... .......... 4% 64.5M 47s
26350K .......... .......... .......... .......... .......... 4% 157M 47s
26400K .......... .......... .......... .......... .......... 4% 190M 47s
26450K .......... .......... .......... .......... .......... 4% 173M 47s
26500K .......... .......... .......... .......... .......... 4% 3.36M 47s
26550K .......... .......... .......... .......... .......... 4% 202M 47s
26600K .......... .......... .......... .......... .......... 4% 149M 47s
26650K .......... .......... .......... .......... .......... 5% 221M 47s
26700K .......... .......... .......... .......... .......... 5% 108M 47s
26750K .......... .......... .......... .......... .......... 5% 99.0M 47s
26800K .......... .......... .......... .......... .......... 5% 223M 47s
26850K .......... .......... .......... .......... .......... 5% 195M 47s
26900K .......... .......... .......... .......... .......... 5% 229M 47s
26950K .......... .......... .......... .......... .......... 5% 137M 46s
27000K .......... .......... .......... .......... .......... 5% 144M 46s
27050K .......... .......... .......... .......... .......... 5% 171M 46s
27100K .......... .......... .......... .......... .......... 5% 121M 46s
27150K .......... .......... .......... .......... .......... 5% 199M 46s
27200K .......... .......... .......... .......... .......... 5% 2.28M 46s
27250K .......... .......... .......... .......... .......... 5% 210M 46s
27300K .......... .......... .......... .......... .......... 5% 171M 46s
27350K .......... .......... .......... .......... .......... 5% 178M 46s
27400K .......... .......... .......... .......... .......... 5% 216M 46s
27450K .......... .......... .......... .......... .......... 5% 146M 46s
27500K .......... .......... .......... .......... .......... 5% 150M 46s
27550K .......... .......... .......... .......... .......... 5% 203M 46s
27600K .......... .......... .......... .......... .......... 5% 10.0M 46s
27650K .......... .......... .......... .......... .......... 5% 166M 46s
27700K .......... .......... .......... .......... .......... 5% 186M 46s
27750K .......... .......... .......... .......... .......... 5% 196M 46s
27800K .......... .......... .......... .......... .......... 5% 208M 46s
27850K .......... .......... .......... .......... .......... 5% 9.32M 46s
27900K .......... .......... .......... .......... .......... 5% 197M 45s
27950K .......... .......... .......... .......... .......... 5% 195M 45s
28000K .......... .......... .......... .......... .......... 5% 219M 45s
28050K .......... .......... .......... .......... .......... 5% 8.34M 45s
28100K .......... .......... .......... .......... .......... 5% 99.0M 45s
28150K .......... .......... .......... .......... .......... 5% 155M 45s
28200K .......... .......... .......... .......... .......... 5% 126M 45s
28250K .......... .......... .......... .......... .......... 5% 8.90M 45s
28300K .......... .......... .......... .......... .......... 5% 47.5M 45s
28350K .......... .......... .......... .......... .......... 5% 154M 45s
28400K .......... .......... .......... .......... .......... 5% 61.4M 45s
28450K .......... .......... .......... .......... .......... 5% 8.87M 45s
28500K .......... .......... .......... .......... .......... 5% 138M 45s
28550K .......... .......... .......... .......... .......... 5% 211M 45s
28600K .......... .......... .......... .......... .......... 5% 109M 45s
28650K .......... .......... .......... .......... .......... 5% 480K 46s
28700K .......... .......... .......... .......... .......... 5% 18.0M 46s
28750K .......... .......... .......... .......... .......... 5% 119M 46s
28800K .......... .......... .......... .......... .......... 5% 180M 46s
28850K .......... .......... .......... .......... .......... 5% 62.9M 46s
28900K .......... .......... .......... .......... .......... 5% 78.6M 46s
28950K .......... .......... .......... .......... .......... 5% 35.5M 46s
29000K .......... .......... .......... .......... .......... 5% 42.6M 46s
29050K .......... .......... .......... .......... .......... 5% 37.6M 46s
29100K .......... .......... .......... .......... .......... 5% 16.9M 46s
29150K .......... .......... .......... .......... .......... 5% 97.1M 46s
29200K .......... .......... .......... .......... .......... 5% 37.4M 46s
29250K .......... .......... .......... .......... .......... 5% 42.6M 46s
29300K .......... .......... .......... .......... .......... 5% 51.7M 46s
29350K .......... .......... .......... .......... .......... 5% 74.2M 46s
29400K .......... .......... .......... .......... .......... 5% 50.0M 45s
29450K .......... .......... .......... .......... .......... 5% 59.7M 45s
29500K .......... .......... .......... .......... .......... 5% 80.8M 45s
29550K .......... .......... .......... .......... .......... 5% 66.0M 45s
29600K .......... .......... .......... .......... .......... 5% 49.8M 45s
29650K .......... .......... .......... .......... .......... 5% 58.3M 45s
29700K .......... .......... .......... .......... .......... 5% 114K 52s
29750K .......... .......... .......... .......... .......... 5% 139M 52s
29800K .......... .......... .......... .......... .......... 5% 162K 58s
29850K .......... .......... .......... .......... .......... 5% 449K 59s
29900K .......... .......... .......... .......... .......... 5% 129M 59s
29950K .......... .......... .......... .......... .......... 5% 133M 59s
30000K .......... .......... .......... .......... .......... 5% 8.99M 59s
30050K .......... .......... .......... .......... .......... 5% 138M 59s
30100K .......... .......... .......... .......... .......... 5% 103M 59s
30150K .......... .......... .......... .......... .......... 5% 85.2M 59s
30200K .......... .......... .......... .......... .......... 5% 146M 59s
30250K .......... .......... .......... .......... .......... 5% 140M 59s
30300K .......... .......... .......... .......... .......... 5% 163M 59s
30350K .......... .......... .......... .......... .......... 5% 114M 58s
30400K .......... .......... .......... .......... .......... 5% 109M 58s
30450K .......... .......... .......... .......... .......... 5% 15.1M 58s
30500K .......... .......... .......... .......... .......... 5% 127M 58s
30550K .......... .......... .......... .......... .......... 5% 124M 58s
30600K .......... .......... .......... .......... .......... 5% 75.6M 58s
30650K .......... .......... .......... .......... .......... 5% 114M 58s
30700K .......... .......... .......... .......... .......... 5% 1.41M 58s
30750K .......... .......... .......... .......... .......... 5% 37.8M 58s
30800K .......... .......... .......... .......... .......... 5% 138M 58s
30850K .......... .......... .......... .......... .......... 5% 123M 58s
30900K .......... .......... .......... .......... .......... 5% 35.6M 58s
30950K .......... .......... .......... .......... .......... 5% 67.1M 58s
31000K .......... .......... .......... .......... .......... 5% 82.3M 58s
31050K .......... .......... .......... .......... .......... 5% 105M 58s
31100K .......... .......... .......... .......... .......... 5% 167M 58s
31150K .......... .......... .......... .......... .......... 5% 100M 58s
31200K .......... .......... .......... .......... .......... 5% 162M 57s
31250K .......... .......... .......... .......... .......... 5% 222M 57s
31300K .......... .......... .......... .......... .......... 5% 214M 57s
31350K .......... .......... .......... .......... .......... 5% 86.3M 57s
31400K .......... .......... .......... .......... .......... 5% 147M 57s
31450K .......... .......... .......... .......... .......... 5% 110M 57s
31500K .......... .......... .......... .......... .......... 5% 122M 57s
31550K .......... .......... .......... .......... .......... 5% 210M 57s
31600K .......... .......... .......... .......... .......... 5% 200M 57s
31650K .......... .......... .......... .......... .......... 5% 221M 57s
31700K .......... .......... .......... .......... .......... 5% 116M 57s
31750K .......... .......... .......... .......... .......... 5% 164M 56s
31800K .......... .......... .......... .......... .......... 5% 111M 56s
31850K .......... .......... .......... .......... .......... 5% 181M 56s
31900K .......... .......... .......... .......... .......... 5% 9.13M 56s
31950K .......... .......... .......... .......... .......... 6% 84.6M 56s
32000K .......... .......... .......... .......... .......... 6% 139M 56s
32050K .......... .......... .......... .......... .......... 6% 214M 56s
32100K .......... .......... .......... .......... .......... 6% 176M 56s
32150K .......... .......... .......... .......... .......... 6% 224M 56s
32200K .......... .......... .......... .......... .......... 6% 4.90M 56s
32250K .......... .......... .......... .......... .......... 6% 84.9M 56s
32300K .......... .......... .......... .......... .......... 6% 150M 56s
32350K .......... .......... .......... .......... .......... 6% 131M 56s
32400K .......... .......... .......... .......... .......... 6% 207M 56s
32450K .......... .......... .......... .......... .......... 6% 133M 55s
32500K .......... .......... .......... .......... .......... 6% 182M 55s
32550K .......... .......... .......... .......... .......... 6% 4.17M 55s
32600K .......... .......... .......... .......... .......... 6% 109M 55s
32650K .......... .......... .......... .......... .......... 6% 145M 55s
32700K .......... .......... .......... .......... .......... 6% 123M 55s
32750K .......... .......... .......... .......... .......... 6% 965K 56s
32800K .......... .......... .......... .......... .......... 6% 226M 56s
32850K .......... .......... .......... .......... .......... 6% 168M 56s
32900K .......... .......... .......... .......... .......... 6% 205M 56s
32950K .......... .......... .......... .......... .......... 6% 172M 56s
33000K .......... .......... .......... .......... .......... 6% 58.9M 56s
33050K .......... .......... .......... .......... .......... 6% 117M 55s
33100K .......... .......... .......... .......... .......... 6% 49.2M 55s
33150K .......... .......... .......... .......... .......... 6% 186M 55s
33200K .......... .......... .......... .......... .......... 6% 176M 55s
33250K .......... .......... .......... .......... .......... 6% 208M 55s
33300K .......... .......... .......... .......... .......... 6% 208M 55s
33350K .......... .......... .......... .......... .......... 6% 191M 55s
33400K .......... .......... .......... .......... .......... 6% 197M 55s
33450K .......... .......... .......... .......... .......... 6% 141M 55s
33500K .......... .......... .......... .......... .......... 6% 171M 55s
33550K .......... .......... .......... .......... .......... 6% 176M 55s
33600K .......... .......... .......... .......... .......... 6% 151M 55s
33650K .......... .......... .......... .......... .......... 6% 149M 54s
33700K .......... .......... .......... .......... .......... 6% 181M 54s
33750K .......... .......... .......... .......... .......... 6% 176M 54s
33800K .......... .......... .......... .......... .......... 6% 226M 54s
33850K .......... .......... .......... .......... .......... 6% 110M 54s
33900K .......... .......... .......... .......... .......... 6% 113M 54s
33950K .......... .......... .......... .......... .......... 6% 2.70M 54s
34000K .......... .......... .......... .......... .......... 6% 78.9M 54s
34050K .......... .......... .......... .......... .......... 6% 128M 54s
34100K .......... .......... .......... .......... .......... 6% 69.4M 54s
34150K .......... .......... .......... .......... .......... 6% 148M 54s
34200K .......... .......... .......... .......... .......... 6% 201M 54s
34250K .......... .......... .......... .......... .......... 6% 177M 54s
34300K .......... .......... .......... .......... .......... 6% 213M 54s
34350K .......... .......... .......... .......... .......... 6% 117M 54s
34400K .......... .......... .......... .......... .......... 6% 91.4M 54s
34450K .......... .......... .......... .......... .......... 6% 188M 53s
34500K .......... .......... .......... .......... .......... 6% 307M 53s
34550K .......... .......... .......... .......... .......... 6% 305M 53s
34600K .......... .......... .......... .......... .......... 6% 193M 53s
34650K .......... .......... .......... .......... .......... 6% 2.14M 53s
34700K .......... .......... .......... .......... .......... 6% 183M 53s
34750K .......... .......... .......... .......... .......... 6% 209M 53s
34800K .......... .......... .......... .......... .......... 6% 96.1M 53s
34850K .......... .......... .......... .......... .......... 6% 112M 53s
34900K .......... .......... .......... .......... .......... 6% 151M 53s
34950K .......... .......... .......... .......... .......... 6% 158M 53s
35000K .......... .......... .......... .......... .......... 6% 161M 53s
35050K .......... .......... .......... .......... .......... 6% 168M 53s
35100K .......... .......... .......... .......... .......... 6% 161M 53s
35150K .......... .......... .......... .......... .......... 6% 137M 53s
35200K .......... .......... .......... .......... .......... 6% 146M 53s
35250K .......... .......... .......... .......... .......... 6% 162M 53s
35300K .......... .......... .......... .......... .......... 6% 6.63M 53s
35350K .......... .......... .......... .......... .......... 6% 182M 52s
35400K .......... .......... .......... .......... .......... 6% 183M 52s
35450K .......... .......... .......... .......... .......... 6% 128M 52s
35500K .......... .......... .......... .......... .......... 6% 158M 52s
35550K .......... .......... .......... .......... .......... 6% 224M 52s
35600K .......... .......... .......... .......... .......... 6% 185M 52s
35650K .......... .......... .......... .......... .......... 6% 224M 52s
35700K .......... .......... .......... .......... .......... 6% 5.44M 52s
35750K .......... .......... .......... .......... .......... 6% 145M 52s
35800K .......... .......... .......... .......... .......... 6% 2.18M 52s
35850K .......... .......... .......... .......... .......... 6% 8.36M 52s
35900K .......... .......... .......... .......... .......... 6% 12.9M 52s
35950K .......... .......... .......... .......... .......... 6% 3.22M 52s
36000K .......... .......... .......... .......... .......... 6% 41.5M 52s
36050K .......... .......... .......... .......... .......... 6% 22.4M 52s
36100K .......... .......... .......... .......... .......... 6% 32.4M 52s
36150K .......... .......... .......... .......... .......... 6% 29.5M 52s
36200K .......... .......... .......... .......... .......... 6% 29.0M 52s
36250K .......... .......... .......... .......... .......... 6% 17.6M 52s
36300K .......... .......... .......... .......... .......... 6% 15.0M 52s
36350K .......... .......... .......... .......... .......... 6% 12.0M 52s
36400K .......... .......... .......... .......... .......... 6% 14.5M 52s
36450K .......... .......... .......... .......... .......... 6% 9.14M 52s
36500K .......... .......... .......... .......... .......... 6% 12.9M 52s
36550K .......... .......... .......... .......... .......... 6% 97.1M 52s
36600K .......... .......... .......... .......... .......... 6% 39.9M 52s
36650K .......... .......... .......... .......... .......... 6% 62.7M 52s
36700K .......... .......... .......... .......... .......... 6% 35.5M 52s
36750K .......... .......... .......... .......... .......... 6% 29.7M 52s
36800K .......... .......... .......... .......... .......... 6% 49.4M 52s
36850K .......... .......... .......... .......... .......... 6% 912K 52s
36900K .......... .......... .......... .......... .......... 6% 27.9M 52s
36950K .......... .......... .......... .......... .......... 6% 101M 52s
37000K .......... .......... .......... .......... .......... 6% 116M 52s
37050K .......... .......... .......... .......... .......... 6% 216M 52s
37100K .......... .......... .......... .......... .......... 6% 71.4M 52s
37150K .......... .......... .......... .......... .......... 6% 10.6M 52s
37200K .......... .......... .......... .......... .......... 6% 109M 52s
37250K .......... .......... .......... .......... .......... 6% 4.10M 52s
37300K .......... .......... .......... .......... .......... 7% 73.4M 52s
37350K .......... .......... .......... .......... .......... 7% 56.4M 52s
37400K .......... .......... .......... .......... .......... 7% 216M 52s
37450K .......... .......... .......... .......... .......... 7% 186M 52s
37500K .......... .......... .......... .......... .......... 7% 197M 52s
37550K .......... .......... .......... .......... .......... 7% 204M 51s
37600K .......... .......... .......... .......... .......... 7% 150M 51s
37650K .......... .......... .......... .......... .......... 7% 17.9M 51s
37700K .......... .......... .......... .......... .......... 7% 5.86M 51s
37750K .......... .......... .......... .......... .......... 7% 69.6M 51s
37800K .......... .......... .......... .......... .......... 7% 8.13M 51s
37850K .......... .......... .......... .......... .......... 7% 10.0M 51s
37900K .......... .......... .......... .......... .......... 7% 83.5M 51s
37950K .......... .......... .......... .......... .......... 7% 169M 51s
38000K .......... .......... .......... .......... .......... 7% 198M 51s
38050K .......... .......... .......... .......... .......... 7% 215M 51s
38100K .......... .......... .......... .......... .......... 7% 184M 51s
38150K .......... .......... .......... .......... .......... 7% 185M 51s
38200K .......... .......... .......... .......... .......... 7% 225M 51s
38250K .......... .......... .......... .......... .......... 7% 289M 51s
38300K .......... .......... .......... .......... .......... 7% 274M 51s
38350K .......... .......... .......... .......... .......... 7% 192M 51s
38400K .......... .......... .......... .......... .......... 7% 208M 51s
38450K .......... .......... .......... .......... .......... 7% 78.4M 51s
38500K .......... .......... .......... .......... .......... 7% 95.7M 50s
38550K .......... .......... .......... .......... .......... 7% 120M 50s
38600K .......... .......... .......... .......... .......... 7% 42.8M 50s
38650K .......... .......... .......... .......... .......... 7% 208M 50s
38700K .......... .......... .......... .......... .......... 7% 178M 50s
38750K .......... .......... .......... .......... .......... 7% 211M 50s
38800K .......... .......... .......... .......... .......... 7% 195M 50s
38850K .......... .......... .......... .......... .......... 7% 176M 50s
38900K .......... .......... .......... .......... .......... 7% 157M 50s
38950K .......... .......... .......... .......... .......... 7% 185M 50s
39000K .......... .......... .......... .......... .......... 7% 193M 50s
39050K .......... .......... .......... .......... .......... 7% 11.9M 50s
39100K .......... .......... .......... .......... .......... 7% 18.0M 50s
39150K .......... .......... .......... .......... .......... 7% 99.4M 50s
39200K .......... .......... .......... .......... .......... 7% 159M 50s
39250K .......... .......... .......... .......... .......... 7% 6.89M 50s
39300K .......... .......... .......... .......... .......... 7% 100M 50s
39350K .......... .......... .......... .......... .......... 7% 111M 50s
39400K .......... .......... .......... .......... .......... 7% 189M 49s
39450K .......... .......... .......... .......... .......... 7% 182M 49s
39500K .......... .......... .......... .......... .......... 7% 220M 49s
39550K .......... .......... .......... .......... .......... 7% 198M 49s
39600K .......... .......... .......... .......... .......... 7% 9.76M 49s
39650K .......... .......... .......... .......... .......... 7% 203M 49s
39700K .......... .......... .......... .......... .......... 7% 130M 49s
39750K .......... .......... .......... .......... .......... 7% 206M 49s
39800K .......... .......... .......... .......... .......... 7% 196M 49s
39850K .......... .......... .......... .......... .......... 7% 6.62M 49s
39900K .......... .......... .......... .......... .......... 7% 536K 50s
39950K .......... .......... .......... .......... .......... 7% 124M 50s
40000K .......... .......... .......... .......... .......... 7% 127M 50s
40050K .......... .......... .......... .......... .......... 7% 148M 50s
40100K .......... .......... .......... .......... .......... 7% 55.9M 50s
40150K .......... .......... .......... .......... .......... 7% 47.0M 50s
40200K .......... .......... .......... .......... .......... 7% 21.5M 50s
40250K .......... .......... .......... .......... .......... 7% 127M 50s
40300K .......... .......... .......... .......... .......... 7% 24.0M 50s
40350K .......... .......... .......... .......... .......... 7% 111M 50s
40400K .......... .......... .......... .......... .......... 7% 28.0M 50s
40450K .......... .......... .......... .......... .......... 7% 154M 50s
40500K .......... .......... .......... .......... .......... 7% 150M 49s
40550K .......... .......... .......... .......... .......... 7% 57.0M 49s
40600K .......... .......... .......... .......... .......... 7% 158M 49s
40650K .......... .......... .......... .......... .......... 7% 201M 49s
40700K .......... .......... .......... .......... .......... 7% 149M 49s
40750K .......... .......... .......... .......... .......... 7% 190M 49s
40800K .......... .......... .......... .......... .......... 7% 153M 49s
40850K .......... .......... .......... .......... .......... 7% 205M 49s
40900K .......... .......... .......... .......... .......... 7% 305M 49s
40950K .......... .......... .......... .......... .......... 7% 268K 51s
41000K .......... .......... .......... .......... .......... 7% 23.7M 51s
41050K .......... .......... .......... .......... .......... 7% 109M 51s
41100K .......... .......... .......... .......... .......... 7% 173M 51s
41150K .......... .......... .......... .......... .......... 7% 26.2M 51s
41200K .......... .......... .......... .......... .......... 7% 114M 51s
41250K .......... .......... .......... .......... .......... 7% 170M 51s
41300K .......... .......... .......... .......... .......... 7% 46.6M 51s
41350K .......... .......... .......... .......... .......... 7% 133M 51s
41400K .......... .......... .......... .......... .......... 7% 244M 51s
41450K .......... .......... .......... .......... .......... 7% 212M 51s
41500K .......... .......... .......... .......... .......... 7% 124M 50s
41550K .......... .......... .......... .......... .......... 7% 97.1M 50s
41600K .......... .......... .......... .......... .......... 7% 110M 50s
41650K .......... .......... .......... .......... .......... 7% 97.5M 50s
41700K .......... .......... .......... .......... .......... 7% 205M 50s
41750K .......... .......... .......... .......... .......... 7% 189M 50s
41800K .......... .......... .......... .......... .......... 7% 26.8M 50s
41850K .......... .......... .......... .......... .......... 7% 92.0M 50s
41900K .......... .......... .......... .......... .......... 7% 146M 50s
41950K .......... .......... .......... .......... .......... 7% 36.2M 50s
42000K .......... .......... .......... .......... .......... 7% 145M 50s
42050K .......... .......... .......... .......... .......... 7% 26.3M 50s
42100K .......... .......... .......... .......... .......... 7% 138M 50s
42150K .......... .......... .......... .......... .......... 7% 50.7M 50s
42200K .......... .......... .......... .......... .......... 7% 115M 50s
42250K .......... .......... .......... .......... .......... 7% 134M 50s
42300K .......... .......... .......... .......... .......... 7% 175M 50s
42350K .......... .......... .......... .......... .......... 7% 108M 50s
42400K .......... .......... .......... .......... .......... 7% 153M 49s
42450K .......... .......... .......... .......... .......... 7% 8.12M 49s
42500K .......... .......... .......... .......... .......... 7% 118M 49s
42550K .......... .......... .......... .......... .......... 7% 139M 49s
42600K .......... .......... .......... .......... .......... 7% 101M 49s
42650K .......... .......... .......... .......... .......... 8% 150M 49s
42700K .......... .......... .......... .......... .......... 8% 6.39M 49s
42750K .......... .......... .......... .......... .......... 8% 97.1M 49s
42800K .......... .......... .......... .......... .......... 8% 203M 49s
42850K .......... .......... .......... .......... .......... 8% 156M 49s
42900K .......... .......... .......... .......... .......... 8% 119M 49s
42950K .......... .......... .......... .......... .......... 8% 26.4M 49s
43000K .......... .......... .......... .......... .......... 8% 263K 51s
43050K .......... .......... .......... .......... .......... 8% 210M 51s
43100K .......... .......... .......... .......... .......... 8% 24.9M 51s
43150K .......... .......... .......... .......... .......... 8% 118M 51s
43200K .......... .......... .......... .......... .......... 8% 89.6M 51s
43250K .......... .......... .......... .......... .......... 8% 102M 51s
43300K .......... .......... .......... .......... .......... 8% 69.9M 51s
43350K .......... .......... .......... .......... .......... 8% 111M 51s
43400K .......... .......... .......... .......... .......... 8% 174M 51s
43450K .......... .......... .......... .......... .......... 8% 105M 51s
43500K .......... .......... .......... .......... .......... 8% 27.0M 51s
43550K .......... .......... .......... .......... .......... 8% 169M 50s
43600K .......... .......... .......... .......... .......... 8% 158M 50s
43650K .......... .......... .......... .......... .......... 8% 210M 50s
43700K .......... .......... .......... .......... .......... 8% 27.7M 50s
43750K .......... .......... .......... .......... .......... 8% 190M 50s
43800K .......... .......... .......... .......... .......... 8% 186M 50s
43850K .......... .......... .......... .......... .......... 8% 169M 50s
43900K .......... .......... .......... .......... .......... 8% 170M 50s
43950K .......... .......... .......... .......... .......... 8% 196M 50s
44000K .......... .......... .......... .......... .......... 8% 26.0M 50s
44050K .......... .......... .......... .......... .......... 8% 119M 50s
44100K .......... .......... .......... .......... .......... 8% 42.0M 50s
44150K .......... .......... .......... .......... .......... 8% 144M 50s
44200K .......... .......... .......... .......... .......... 8% 184M 50s
44250K .......... .......... .......... .......... .......... 8% 190M 50s
44300K .......... .......... .......... .......... .......... 8% 209M 50s
44350K .......... .......... .......... .......... .......... 8% 28.8M 50s
44400K .......... .......... .......... .......... .......... 8% 208M 50s
44450K .......... .......... .......... .......... .......... 8% 196M 49s
44500K .......... .......... .......... .......... .......... 8% 29.7M 49s
44550K .......... .......... .......... .......... .......... 8% 160M 49s
44600K .......... .......... .......... .......... .......... 8% 87.0M 49s
44650K .......... .......... .......... .......... .......... 8% 192M 49s
44700K .......... .......... .......... .......... .......... 8% 29.7M 49s
44750K .......... .......... .......... .......... .......... 8% 111M 49s
44800K .......... .......... .......... .......... .......... 8% 7.03M 49s
44850K .......... .......... .......... .......... .......... 8% 111M 49s
44900K .......... .......... .......... .......... .......... 8% 142M 49s
44950K .......... .......... .......... .......... .......... 8% 144M 49s
45000K .......... .......... .......... .......... .......... 8% 144M 49s
45050K .......... .......... .......... .......... .......... 8% 379K 50s
45100K .......... .......... .......... .......... .......... 8% 17.7M 50s
45150K .......... .......... .......... .......... .......... 8% 95.2M 50s
45200K .......... .......... .......... .......... .......... 8% 56.6M 50s
45250K .......... .......... .......... .......... .......... 8% 97.7M 50s
45300K .......... .......... .......... .......... .......... 8% 51.3M 50s
45350K .......... .......... .......... .......... .......... 8% 140M 50s
45400K .......... .......... .......... .......... .......... 8% 67.3M 50s
45450K .......... .......... .......... .......... .......... 8% 122M 50s
45500K .......... .......... .......... .......... .......... 8% 126M 50s
45550K .......... .......... .......... .......... .......... 8% 182M 50s
45600K .......... .......... .......... .......... .......... 8% 122M 50s
45650K .......... .......... .......... .......... .......... 8% 133M 50s
45700K .......... .......... .......... .......... .......... 8% 121M 50s
45750K .......... .......... .......... .......... .......... 8% 225M 50s
45800K .......... .......... .......... .......... .......... 8% 207M 50s
45850K .......... .......... .......... .......... .......... 8% 147M 49s
45900K .......... .......... .......... .......... .......... 8% 191M 49s
45950K .......... .......... .......... .......... .......... 8% 189M 49s
46000K .......... .......... .......... .......... .......... 8% 28.9M 49s
46050K .......... .......... .......... .......... .......... 8% 4.04M 49s
46100K .......... .......... .......... .......... .......... 8% 126M 49s
46150K .......... .......... .......... .......... .......... 8% 45.1M 49s
46200K .......... .......... .......... .......... .......... 8% 138M 49s
46250K .......... .......... .......... .......... .......... 8% 150M 49s
46300K .......... .......... .......... .......... .......... 8% 144M 49s
46350K .......... .......... .......... .......... .......... 8% 24.4M 49s
46400K .......... .......... .......... .......... .......... 8% 29.0M 49s
46450K .......... .......... .......... .......... .......... 8% 17.0M 49s
46500K .......... .......... .......... .......... .......... 8% 112M 49s
46550K .......... .......... .......... .......... .......... 8% 157M 49s
46600K .......... .......... .......... .......... .......... 8% 138M 49s
46650K .......... .......... .......... .......... .......... 8% 177M 49s
46700K .......... .......... .......... .......... .......... 8% 172M 49s
46750K .......... .......... .......... .......... .......... 8% 189M 49s
46800K .......... .......... .......... .......... .......... 8% 165M 49s
46850K .......... .......... .......... .......... .......... 8% 155M 49s
46900K .......... .......... .......... .......... .......... 8% 195M 49s
46950K .......... .......... .......... .......... .......... 8% 7.88M 49s
47000K .......... .......... .......... .......... .......... 8% 138M 48s
47050K .......... .......... .......... .......... .......... 8% 140M 48s
47100K .......... .......... .......... .......... .......... 8% 108M 48s
47150K .......... .......... .......... .......... .......... 8% 168M 48s
47200K .......... .......... .......... .......... .......... 8% 156M 48s
47250K .......... .......... .......... .......... .......... 8% 6.56M 48s
47300K .......... .......... .......... .......... .......... 8% 95.6M 48s
47350K .......... .......... .......... .......... .......... 8% 28.5M 48s
47400K .......... .......... .......... .......... .......... 8% 228M 48s
47450K .......... .......... .......... .......... .......... 8% 231M 48s
47500K .......... .......... .......... .......... .......... 8% 4.58M 48s
47550K .......... .......... .......... .......... .......... 8% 103M 48s
47600K .......... .......... .......... .......... .......... 8% 127M 48s
47650K .......... .......... .......... .......... .......... 8% 180M 48s
47700K .......... .......... .......... .......... .......... 8% 114M 48s
47750K .......... .......... .......... .......... .......... 8% 56.8M 48s
47800K .......... .......... .......... .......... .......... 8% 8.20M 48s
47850K .......... .......... .......... .......... .......... 8% 141M 48s
47900K .......... .......... .......... .......... .......... 8% 114M 48s
47950K .......... .......... .......... .......... .......... 9% 58.5M 48s
48000K .......... .......... .......... .......... .......... 9% 180M 48s
48050K .......... .......... .......... .......... .......... 9% 6.67M 48s
48100K .......... .......... .......... .......... .......... 9% 532K 49s
48150K .......... .......... .......... .......... .......... 9% 56.1M 49s
48200K .......... .......... .......... .......... .......... 9% 43.8M 49s
48250K .......... .......... .......... .......... .......... 9% 110M 48s
48300K .......... .......... .......... .......... .......... 9% 83.0M 48s
48350K .......... .......... .......... .......... .......... 9% 149M 48s
48400K .......... .......... .......... .......... .......... 9% 195M 48s
48450K .......... .......... .......... .......... .......... 9% 111M 48s
48500K .......... .......... .......... .......... .......... 9% 99.0M 48s
48550K .......... .......... .......... .......... .......... 9% 18.2M 48s
48600K .......... .......... .......... .......... .......... 9% 151M 48s
48650K .......... .......... .......... .......... .......... 9% 181M 48s
48700K .......... .......... .......... .......... .......... 9% 130M 48s
48750K .......... .......... .......... .......... .......... 9% 135M 48s
48800K .......... .......... .......... .......... .......... 9% 159M 48s
48850K .......... .......... .......... .......... .......... 9% 26.3M 48s
48900K .......... .......... .......... .......... .......... 9% 184M 48s
48950K .......... .......... .......... .......... .......... 9% 148M 48s
49000K .......... .......... .......... .......... .......... 9% 164M 48s
49050K .......... .......... .......... .......... .......... 9% 132M 48s
49100K .......... .......... .......... .......... .......... 9% 49.9M 48s
49150K .......... .......... .......... .......... .......... 9% 158M 48s
49200K .......... .......... .......... .......... .......... 9% 20.3M 48s
49250K .......... .......... .......... .......... .......... 9% 70.0M 48s
49300K .......... .......... .......... .......... .......... 9% 180M 47s
49350K .......... .......... .......... .......... .......... 9% 183M 47s
49400K .......... .......... .......... .......... .......... 9% 142M 47s
49450K .......... .......... .......... .......... .......... 9% 145M 47s
49500K .......... .......... .......... .......... .......... 9% 144M 47s
49550K .......... .......... .......... .......... .......... 9% 117M 47s
49600K .......... .......... .......... .......... .......... 9% 7.45M 47s
49650K .......... .......... .......... .......... .......... 9% 131M 47s
49700K .......... .......... .......... .......... .......... 9% 9.62M 47s
49750K .......... .......... .......... .......... .......... 9% 166M 47s
49800K .......... .......... .......... .......... .......... 9% 202M 47s
49850K .......... .......... .......... .......... .......... 9% 11.0M 47s
49900K .......... .......... .......... .......... .......... 9% 127M 47s
49950K .......... .......... .......... .......... .......... 9% 69.0M 47s
50000K .......... .......... .......... .......... .......... 9% 212M 47s
50050K .......... .......... .......... .......... .......... 9% 186M 47s
50100K .......... .......... .......... .......... .......... 9% 168M 47s
50150K .......... .......... .......... .......... .......... 9% 1.36M 47s
50200K .......... .......... .......... .......... .......... 9% 131M 47s
50250K .......... .......... .......... .......... .......... 9% 135M 47s
50300K .......... .......... .......... .......... .......... 9% 97.7M 47s
50350K .......... .......... .......... .......... .......... 9% 161M 47s
50400K .......... .......... .......... .......... .......... 9% 197M 47s
50450K .......... .......... .......... .......... .......... 9% 15.1M 47s
50500K .......... .......... .......... .......... .......... 9% 199M 47s
50550K .......... .......... .......... .......... .......... 9% 200M 47s
50600K .......... .......... .......... .......... .......... 9% 174M 47s
50650K .......... .......... .......... .......... .......... 9% 204M 47s
50700K .......... .......... .......... .......... .......... 9% 175M 47s
50750K .......... .......... .......... .......... .......... 9% 42.6M 47s
50800K .......... .......... .......... .......... .......... 9% 163M 47s
50850K .......... .......... .......... .......... .......... 9% 129M 46s
50900K .......... .......... .......... .......... .......... 9% 198M 46s
50950K .......... .......... .......... .......... .......... 9% 181M 46s
51000K .......... .......... .......... .......... .......... 9% 207M 46s
51050K .......... .......... .......... .......... .......... 9% 178M 46s
51100K .......... .......... .......... .......... .......... 9% 192M 46s
51150K .......... .......... .......... .......... .......... 9% 219M 46s
51200K .......... .......... .......... .......... .......... 9% 121M 46s
51250K .......... .......... .......... .......... .......... 9% 309M 46s
51300K .......... .......... .......... .......... .......... 9% 291M 46s
51350K .......... .......... .......... .......... .......... 9% 8.42M 46s
51400K .......... .......... .......... .......... .......... 9% 136M 46s
51450K .......... .......... .......... .......... .......... 9% 143M 46s
51500K .......... .......... .......... .......... .......... 9% 95.2M 46s
51550K .......... .......... .......... .......... .......... 9% 163M 46s
51600K .......... .......... .......... .......... .......... 9% 4.35M 46s
51650K .......... .......... .......... .......... .......... 9% 174M 46s
51700K .......... .......... .......... .......... .......... 9% 130M 46s
51750K .......... .......... .......... .......... .......... 9% 115M 46s
51800K .......... .......... .......... .......... .......... 9% 181M 46s
51850K .......... .......... .......... .......... .......... 9% 137M 46s
51900K .......... .......... .......... .......... .......... 9% 5.62M 46s
51950K .......... .......... .......... .......... .......... 9% 183M 46s
52000K .......... .......... .......... .......... .......... 9% 158M 46s
52050K .......... .......... .......... .......... .......... 9% 128M 46s
52100K .......... .......... .......... .......... .......... 9% 166M 46s
52150K .......... .......... .......... .......... .......... 9% 162M 46s
52200K .......... .......... .......... .......... .......... 9% 2.09M 46s
52250K .......... .......... .......... .......... .......... 9% 136M 46s
52300K .......... .......... .......... .......... .......... 9% 164M 46s
52350K .......... .......... .......... .......... .......... 9% 184M 46s
52400K .......... .......... .......... .......... .......... 9% 220M 46s
52450K .......... .......... .......... .......... .......... 9% 178M 45s
52500K .......... .......... .......... .......... .......... 9% 158M 45s
52550K .......... .......... .......... .......... .......... 9% 147M 45s
52600K .......... .......... .......... .......... .......... 9% 164M 45s
52650K .......... .......... .......... .......... .......... 9% 117M 45s
52700K .......... .......... .......... .......... .......... 9% 153M 45s
52750K .......... .......... .......... .......... .......... 9% 226M 45s
52800K .......... .......... .......... .......... .......... 9% 217M 45s
52850K .......... .......... .......... .......... .......... 9% 171M 45s
52900K .......... .......... .......... .......... .......... 9% 199M 45s
52950K .......... .......... .......... .......... .......... 9% 2.74M 45s
53000K .......... .......... .......... .......... .......... 9% 48.3M 45s
53050K .......... .......... .......... .......... .......... 9% 4.98M 45s
53100K .......... .......... .......... .......... .......... 9% 180M 45s
53150K .......... .......... .......... .......... .......... 9% 239M 45s
53200K .......... .......... .......... .......... .......... 9% 124M 45s
53250K .......... .......... .......... .......... .......... 9% 188M 45s
53300K .......... .......... .......... .......... .......... 10% 5.59M 45s
53350K .......... .......... .......... .......... .......... 10% 125M 45s
53400K .......... .......... .......... .......... .......... 10% 135M 45s
53450K .......... .......... .......... .......... .......... 10% 191M 45s
53500K .......... .......... .......... .......... .......... 10% 219M 45s
53550K .......... .......... .......... .......... .......... 10% 254M 45s
53600K .......... .......... .......... .......... .......... 10% 171M 45s
53650K .......... .......... .......... .......... .......... 10% 191M 45s
53700K .......... .......... .......... .......... .......... 10% 179M 45s
53750K .......... .......... .......... .......... .......... 10% 174M 45s
53800K .......... .......... .......... .......... .......... 10% 210M 45s
53850K .......... .......... .......... .......... .......... 10% 166M 45s
53900K .......... .......... .......... .......... .......... 10% 208M 44s
53950K .......... .......... .......... .......... .......... 10% 186M 44s
54000K .......... .......... .......... .......... .......... 10% 235M 44s
54050K .......... .......... .......... .......... .......... 10% 229M 44s
54100K .......... .......... .......... .......... .......... 10% 202M 44s
54150K .......... .......... .......... .......... .......... 10% 236M 44s
54200K .......... .......... .......... .......... .......... 10% 11.3M 44s
54250K .......... .......... .......... .......... .......... 10% 318K 46s
54300K .......... .......... .......... .......... .......... 10% 231M 46s
54350K .......... .......... .......... .......... .......... 10% 73.4M 46s
54400K .......... .......... .......... .......... .......... 10% 65.3M 45s
54450K .......... .......... .......... .......... .......... 10% 18.1M 45s
54500K .......... .......... .......... .......... .......... 10% 114M 45s
54550K .......... .......... .......... .......... .......... 10% 25.8M 45s
54600K .......... .......... .......... .......... .......... 10% 136M 45s
54650K .......... .......... .......... .......... .......... 10% 137M 45s
54700K .......... .......... .......... .......... .......... 10% 113M 45s
54750K .......... .......... .......... .......... .......... 10% 263M 45s
54800K .......... .......... .......... .......... .......... 10% 191M 45s
54850K .......... .......... .......... .......... .......... 10% 176M 45s
54900K .......... .......... .......... .......... .......... 10% 199M 45s
54950K .......... .......... .......... .......... .......... 10% 189M 45s
55000K .......... .......... .......... .......... .......... 10% 151M 45s
55050K .......... .......... .......... .......... .......... 10% 188M 45s
55100K .......... .......... .......... .......... .......... 10% 18.8M 45s
55150K .......... .......... .......... .......... .......... 10% 305M 45s
55200K .......... .......... .......... .......... .......... 10% 258M 45s
55250K .......... .......... .......... .......... .......... 10% 224M 45s
55300K .......... .......... .......... .......... .......... 10% 330M 45s
55350K .......... .......... .......... .......... .......... 10% 286M 45s
55400K .......... .......... .......... .......... .......... 10% 286M 45s
55450K .......... .......... .......... .......... .......... 10% 24.1M 45s
55500K .......... .......... .......... .......... .......... 10% 113M 45s
55550K .......... .......... .......... .......... .......... 10% 179M 45s
55600K .......... .......... .......... .......... .......... 10% 156M 45s
55650K .......... .......... .......... .......... .......... 10% 214M 44s
55700K .......... .......... .......... .......... .......... 10% 198M 44s
55750K .......... .......... .......... .......... .......... 10% 6.57M 44s
55800K .......... .......... .......... .......... .......... 10% 172M 44s
55850K .......... .......... .......... .......... .......... 10% 118M 44s
55900K .......... .......... .......... .......... .......... 10% 79.7M 44s
55950K .......... .......... .......... .......... .......... 10% 187M 44s
56000K .......... .......... .......... .......... .......... 10% 5.92M 44s
56050K .......... .......... .......... .......... .......... 10% 105M 44s
56100K .......... .......... .......... .......... .......... 10% 181M 44s
56150K .......... .......... .......... .......... .......... 10% 89.4M 44s
56200K .......... .......... .......... .......... .......... 10% 145M 44s
56250K .......... .......... .......... .......... .......... 10% 163M 44s
56300K .......... .......... .......... .......... .......... 10% 4.96M 44s
56350K .......... .......... .......... .......... .......... 10% 151M 44s
56400K .......... .......... .......... .......... .......... 10% 141M 44s
56450K .......... .......... .......... .......... .......... 10% 142M 44s
56500K .......... .......... .......... .......... .......... 10% 191M 44s
56550K .......... .......... .......... .......... .......... 10% 211M 44s
56600K .......... .......... .......... .......... .......... 10% 6.26M 44s
56650K .......... .......... .......... .......... .......... 10% 103M 44s
56700K .......... .......... .......... .......... .......... 10% 87.2M 44s
56750K .......... .......... .......... .......... .......... 10% 206M 44s
56800K .......... .......... .......... .......... .......... 10% 145M 44s
56850K .......... .......... .......... .......... .......... 10% 263M 44s
56900K .......... .......... .......... .......... .......... 10% 177M 44s
56950K .......... .......... .......... .......... .......... 10% 5.33M 44s
57000K .......... .......... .......... .......... .......... 10% 9.87M 44s
57050K .......... .......... .......... .......... .......... 10% 215M 44s
57100K .......... .......... .......... .......... .......... 10% 186M 44s
57150K .......... .......... .......... .......... .......... 10% 161M 44s
57200K .......... .......... .......... .......... .......... 10% 203M 44s
57250K .......... .......... .......... .......... .......... 10% 249M 44s
57300K .......... .......... .......... .......... .......... 10% 32.7M 44s
57350K .......... .......... .......... .......... .......... 10% 2.69M 44s
57400K .......... .......... .......... .......... .......... 10% 189M 44s
57450K .......... .......... .......... .......... .......... 10% 164M 44s
57500K .......... .......... .......... .......... .......... 10% 5.21M 44s
57550K .......... .......... .......... .......... .......... 10% 162M 44s
57600K .......... .......... .......... .......... .......... 10% 108M 44s
57650K .......... .......... .......... .......... .......... 10% 95.9M 43s
57700K .......... .......... .......... .......... .......... 10% 130M 43s
57750K .......... .......... .......... .......... .......... 10% 106M 43s
57800K .......... .......... .......... .......... .......... 10% 65.5M 43s
57850K .......... .......... .......... .......... .......... 10% 21.2M 43s
57900K .......... .......... .......... .......... .......... 10% 92.0M 43s
57950K .......... .......... .......... .......... .......... 10% 89.4M 43s
58000K .......... .......... .......... .......... .......... 10% 108M 43s
58050K .......... .......... .......... .......... .......... 10% 129M 43s
58100K .......... .......... .......... .......... .......... 10% 148M 43s
58150K .......... .......... .......... .......... .......... 10% 127M 43s
58200K .......... .......... .......... .......... .......... 10% 14.1M 43s
58250K .......... .......... .......... .......... .......... 10% 125M 43s
58300K .......... .......... .......... .......... .......... 10% 84.0M 43s
58350K .......... .......... .......... .......... .......... 10% 100M 43s
58400K .......... .......... .......... .......... .......... 10% 105M 43s
58450K .......... .......... .......... .......... .......... 10% 74.1M 43s
58500K .......... .......... .......... .......... .......... 10% 147M 43s
58550K .......... .......... .......... .......... .......... 10% 179M 43s
58600K .......... .......... .......... .......... .......... 11% 21.7M 43s
58650K .......... .......... .......... .......... .......... 11% 8.27M 43s
58700K .......... .......... .......... .......... .......... 11% 59.3M 43s
58750K .......... .......... .......... .......... .......... 11% 195M 43s
58800K .......... .......... .......... .......... .......... 11% 109M 43s
58850K .......... .......... .......... .......... .......... 11% 62.0M 43s
58900K .......... .......... .......... .......... .......... 11% 173M 43s
58950K .......... .......... .......... .......... .......... 11% 6.15M 43s
59000K .......... .......... .......... .......... .......... 11% 120M 43s
59050K .......... .......... .......... .......... .......... 11% 168M 43s
59100K .......... .......... .......... .......... .......... 11% 152M 43s
59150K .......... .......... .......... .......... .......... 11% 209M 42s
59200K .......... .......... .......... .......... .......... 11% 111M 42s
59250K .......... .......... .......... .......... .......... 11% 7.16M 42s
59300K .......... .......... .......... .......... .......... 11% 148M 42s
59350K .......... .......... .......... .......... .......... 11% 119M 42s
59400K .......... .......... .......... .......... .......... 11% 186M 42s
59450K .......... .......... .......... .......... .......... 11% 57.6M 42s
59500K .......... .......... .......... .......... .......... 11% 173M 42s
59550K .......... .......... .......... .......... .......... 11% 8.21M 42s
59600K .......... .......... .......... .......... .......... 11% 56.4M 42s
59650K .......... .......... .......... .......... .......... 11% 29.9M 42s
59700K .......... .......... .......... .......... .......... 11% 159M 42s
59750K .......... .......... .......... .......... .......... 11% 15.7M 42s
59800K .......... .......... .......... .......... .......... 11% 219M 42s
59850K .......... .......... .......... .......... .......... 11% 18.5M 42s
59900K .......... .......... .......... .......... .......... 11% 143M 42s
59950K .......... .......... .......... .......... .......... 11% 132M 42s
60000K .......... .......... .......... .......... .......... 11% 126M 42s
60050K .......... .......... .......... .......... .......... 11% 216M 42s
60100K .......... .......... .......... .......... .......... 11% 5.36M 42s
60150K .......... .......... .......... .......... .......... 11% 99.0M 42s
60200K .......... .......... .......... .......... .......... 11% 128M 42s
60250K .......... .......... .......... .......... .......... 11% 217M 42s
60300K .......... .......... .......... .......... .......... 11% 201M 42s
60350K .......... .......... .......... .......... .......... 11% 166M 42s
60400K .......... .......... .......... .......... .......... 11% 637K 42s
60450K .......... .......... .......... .......... .......... 11% 102M 42s
60500K .......... .......... .......... .......... .......... 11% 140M 42s
60550K .......... .......... .......... .......... .......... 11% 127M 42s
60600K .......... .......... .......... .......... .......... 11% 20.9M 42s
60650K .......... .......... .......... .......... .......... 11% 141M 42s
60700K .......... .......... .......... .......... .......... 11% 78.9M 42s
60750K .......... .......... .......... .......... .......... 11% 106M 42s
60800K .......... .......... .......... .......... .......... 11% 5.36M 42s
60850K .......... .......... .......... .......... .......... 11% 125M 42s
60900K .......... .......... .......... .......... .......... 11% 49.5M 42s
60950K .......... .......... .......... .......... .......... 11% 50.5M 42s
61000K .......... .......... .......... .......... .......... 11% 144M 42s
61050K .......... .......... .......... .......... .......... 11% 123M 42s
61100K .......... .......... .......... .......... .......... 11% 144M 42s
61150K .......... .......... .......... .......... .......... 11% 43.6M 42s
61200K .......... .......... .......... .......... .......... 11% 101M 42s
61250K .......... .......... .......... .......... .......... 11% 86.1M 42s
61300K .......... .......... .......... .......... .......... 11% 88.9M 42s
61350K .......... .......... .......... .......... .......... 11% 25.1M 42s
61400K .......... .......... .......... .......... .......... 11% 3.01M 42s
61450K .......... .......... .......... .......... .......... 11% 111M 42s
61500K .......... .......... .......... .......... .......... 11% 166M 42s
61550K .......... .......... .......... .......... .......... 11% 99.4M 42s
61600K .......... .......... .......... .......... .......... 11% 120M 42s
61650K .......... .......... .......... .......... .......... 11% 28.4M 42s
61700K .......... .......... .......... .......... .......... 11% 95.6M 42s
61750K .......... .......... .......... .......... .......... 11% 173M 42s
61800K .......... .......... .......... .......... .......... 11% 112M 42s
61850K .......... .......... .......... .......... .......... 11% 158M 42s
61900K .......... .......... .......... .......... .......... 11% 49.8M 42s
61950K .......... .......... .......... .......... .......... 11% 138M 42s
62000K .......... .......... .......... .......... .......... 11% 151M 42s
62050K .......... .......... .......... .......... .......... 11% 157M 41s
62100K .......... .......... .......... .......... .......... 11% 145M 41s
62150K .......... .......... .......... .......... .......... 11% 150M 41s
62200K .......... .......... .......... .......... .......... 11% 179M 41s
62250K .......... .......... .......... .......... .......... 11% 30.1M 41s
62300K .......... .......... .......... .......... .......... 11% 233M 41s
62350K .......... .......... .......... .......... .......... 11% 191M 41s
62400K .......... .......... .......... .......... .......... 11% 277M 41s
62450K .......... .......... .......... .......... .......... 11% 396K 42s
62500K .......... .......... .......... .......... .......... 11% 78.9M 42s
62550K .......... .......... .......... .......... .......... 11% 15.3M 42s
62600K .......... .......... .......... .......... .......... 11% 91.8M 42s
62650K .......... .......... .......... .......... .......... 11% 22.9M 42s
62700K .......... .......... .......... .......... .......... 11% 33.3M 42s
62750K .......... .......... .......... .......... .......... 11% 61.7M 42s
62800K .......... .......... .......... .......... .......... 11% 77.6M 42s
62850K .......... .......... .......... .......... .......... 11% 71.1M 42s
62900K .......... .......... .......... .......... .......... 11% 205M 42s
62950K .......... .......... .......... .......... .......... 11% 135M 42s
63000K .......... .......... .......... .......... .......... 11% 184M 42s
63050K .......... .......... .......... .......... .......... 11% 27.4M 42s
63100K .......... .......... .......... .......... .......... 11% 186M 42s
63150K .......... .......... .......... .......... .......... 11% 296M 42s
63200K .......... .......... .......... .......... .......... 11% 148M 42s
63250K .......... .......... .......... .......... .......... 11% 28.8M 42s
63300K .......... .......... .......... .......... .......... 11% 29.6M 42s
63350K .......... .......... .......... .......... .......... 11% 25.8M 42s
63400K .......... .......... .......... .......... .......... 11% 113M 42s
63450K .......... .......... .......... .......... .......... 11% 103M 42s
63500K .......... .......... .......... .......... .......... 11% 130M 42s
63550K .......... .......... .......... .......... .......... 11% 170M 41s
63600K .......... .......... .......... .......... .......... 11% 114M 41s
63650K .......... .......... .......... .......... .......... 11% 108M 41s
63700K .......... .......... .......... .......... .......... 11% 162M 41s
63750K .......... .......... .......... .......... .......... 11% 190M 41s
63800K .......... .......... .......... .......... .......... 11% 268M 41s
63850K .......... .......... .......... .......... .......... 11% 133M 41s
63900K .......... .......... .......... .......... .......... 11% 169M 41s
63950K .......... .......... .......... .......... .......... 12% 7.87M 41s
64000K .......... .......... .......... .......... .......... 12% 118M 41s
64050K .......... .......... .......... .......... .......... 12% 166M 41s
64100K .......... .......... .......... .......... .......... 12% 146M 41s
64150K .......... .......... .......... .......... .......... 12% 24.9M 41s
64200K .......... .......... .......... .......... .......... 12% 3.39M 41s
64250K .......... .......... .......... .......... .......... 12% 133M 41s
64300K .......... .......... .......... .......... .......... 12% 191M 41s
64350K .......... .......... .......... .......... .......... 12% 181M 41s
64400K .......... .......... .......... .......... .......... 12% 150M 41s
64450K .......... .......... .......... .......... .......... 12% 127M 41s
64500K .......... .......... .......... .......... .......... 12% 255K 42s
64550K .......... .......... .......... .......... .......... 12% 156M 42s
64600K .......... .......... .......... .......... .......... 12% 132M 42s
64650K .......... .......... .......... .......... .......... 12% 81.8M 42s
64700K .......... .......... .......... .......... .......... 12% 144M 42s
64750K .......... .......... .......... .......... .......... 12% 202M 42s
64800K .......... .......... .......... .......... .......... 12% 105M 42s
64850K .......... .......... .......... .......... .......... 12% 3.79M 42s
64900K .......... .......... .......... .......... .......... 12% 114M 42s
64950K .......... .......... .......... .......... .......... 12% 140M 42s
65000K .......... .......... .......... .......... .......... 12% 7.49M 42s
65050K .......... .......... .......... .......... .......... 12% 28.5M 42s
65100K .......... .......... .......... .......... .......... 12% 52.3M 42s
65150K .......... .......... .......... .......... .......... 12% 207M 42s
65200K .......... .......... .......... .......... .......... 12% 27.9M 42s
65250K .......... .......... .......... .......... .......... 12% 36.4M 42s
65300K .......... .......... .......... .......... .......... 12% 28.2M 42s
65350K .......... .......... .......... .......... .......... 12% 180M 42s
65400K .......... .......... .......... .......... .......... 12% 208M 42s
65450K .......... .......... .......... .......... .......... 12% 176M 42s
65500K .......... .......... .......... .......... .......... 12% 140M 42s
65550K .......... .......... .......... .......... .......... 12% 161M 42s
65600K .......... .......... .......... .......... .......... 12% 27.4M 42s
65650K .......... .......... .......... .......... .......... 12% 173M 42s
65700K .......... .......... .......... .......... .......... 12% 140M 42s
65750K .......... .......... .......... .......... .......... 12% 91.4M 42s
65800K .......... .......... .......... .......... .......... 12% 25.0M 42s
65850K .......... .......... .......... .......... .......... 12% 142M 42s
65900K .......... .......... .......... .......... .......... 12% 56.0M 42s
65950K .......... .......... .......... .......... .......... 12% 156M 42s
66000K .......... .......... .......... .......... .......... 12% 208M 42s
66050K .......... .......... .......... .......... .......... 12% 138M 42s
66100K .......... .......... .......... .......... .......... 12% 170M 42s
66150K .......... .......... .......... .......... .......... 12% 189M 41s
66200K .......... .......... .......... .......... .......... 12% 154M 41s
66250K .......... .......... .......... .......... .......... 12% 200M 41s
66300K .......... .......... .......... .......... .......... 12% 57.6M 41s
66350K .......... .......... .......... .......... .......... 12% 25.9M 41s
66400K .......... .......... .......... .......... .......... 12% 26.1M 41s
66450K .......... .......... .......... .......... .......... 12% 247M 41s
66500K .......... .......... .......... .......... .......... 12% 307M 41s
66550K .......... .......... .......... .......... .......... 12% 2.88M 41s
66600K .......... .......... .......... .......... .......... 12% 149M 41s
66650K .......... .......... .......... .......... .......... 12% 180M 41s
66700K .......... .......... .......... .......... .......... 12% 153M 41s
66750K .......... .......... .......... .......... .......... 12% 28.7M 41s
66800K .......... .......... .......... .......... .......... 12% 212M 41s
66850K .......... .......... .......... .......... .......... 12% 177M 41s
66900K .......... .......... .......... .......... .......... 12% 199M 41s
66950K .......... .......... .......... .......... .......... 12% 151M 41s
67000K .......... .......... .......... .......... .......... 12% 22.3M 41s
67050K .......... .......... .......... .......... .......... 12% 103M 41s
67100K .......... .......... .......... .......... .......... 12% 125M 41s
67150K .......... .......... .......... .......... .......... 12% 18.1M 41s
67200K .......... .......... .......... .......... .......... 12% 13.3M 41s
67250K .......... .......... .......... .......... .......... 12% 67.3M 41s
67300K .......... .......... .......... .......... .......... 12% 214M 41s
67350K .......... .......... .......... .......... .......... 12% 5.00M 41s
67400K .......... .......... .......... .......... .......... 12% 98.2M 41s
67450K .......... .......... .......... .......... .......... 12% 104M 41s
67500K .......... .......... .......... .......... .......... 12% 115M 41s
67550K .......... .......... .......... .......... .......... 12% 3.56M 41s
67600K .......... .......... .......... .......... .......... 12% 15.3M 41s
67650K .......... .......... .......... .......... .......... 12% 162M 41s
67700K .......... .......... .......... .......... .......... 12% 166M 41s
67750K .......... .......... .......... .......... .......... 12% 190M 41s
67800K .......... .......... .......... .......... .......... 12% 168M 41s
67850K .......... .......... .......... .......... .......... 12% 142M 41s
67900K .......... .......... .......... .......... .......... 12% 189M 41s
67950K .......... .......... .......... .......... .......... 12% 61.0M 41s
68000K .......... .......... .......... .......... .......... 12% 29.6M 41s
68050K .......... .......... .......... .......... .......... 12% 27.7M 41s
68100K .......... .......... .......... .......... .......... 12% 131M 41s
68150K .......... .......... .......... .......... .......... 12% 151M 41s
68200K .......... .......... .......... .......... .......... 12% 132M 41s
68250K .......... .......... .......... .......... .......... 12% 4.66M 41s
68300K .......... .......... .......... .......... .......... 12% 20.5M 41s
68350K .......... .......... .......... .......... .......... 12% 167M 41s
68400K .......... .......... .......... .......... .......... 12% 29.6M 41s
68450K .......... .......... .......... .......... .......... 12% 36.1M 40s
68500K .......... .......... .......... .......... .......... 12% 53.1M 40s
68550K .......... .......... .......... .......... .......... 12% 194M 40s
68600K .......... .......... .......... .......... .......... 12% 4.15M 40s
68650K .......... .......... .......... .......... .......... 12% 139M 40s
68700K .......... .......... .......... .......... .......... 12% 110M 40s
68750K .......... .......... .......... .......... .......... 12% 191M 40s
68800K .......... .......... .......... .......... .......... 12% 187M 40s
68850K .......... .......... .......... .......... .......... 12% 26.7M 40s
68900K .......... .......... .......... .......... .......... 12% 189M 40s
68950K .......... .......... .......... .......... .......... 12% 936K 41s
69000K .......... .......... .......... .......... .......... 12% 118M 41s
69050K .......... .......... .......... .......... .......... 12% 41.3M 41s
69100K .......... .......... .......... .......... .......... 12% 87.5M 41s
69150K .......... .......... .......... .......... .......... 12% 191M 41s
69200K .......... .......... .......... .......... .......... 12% 183M 40s
69250K .......... .......... .......... .......... .......... 12% 222M 40s
69300K .......... .......... .......... .......... .......... 13% 260M 40s
69350K .......... .......... .......... .......... .......... 13% 6.33M 40s
69400K .......... .......... .......... .......... .......... 13% 3.31M 40s
69450K .......... .......... .......... .......... .......... 13% 61.2M 40s
69500K .......... .......... .......... .......... .......... 13% 110M 40s
69550K .......... .......... .......... .......... .......... 13% 152M 40s
69600K .......... .......... .......... .......... .......... 13% 4.73M 40s
69650K .......... .......... .......... .......... .......... 13% 148M 40s
69700K .......... .......... .......... .......... .......... 13% 113M 40s
69750K .......... .......... .......... .......... .......... 13% 29.5M 40s
69800K .......... .......... .......... .......... .......... 13% 29.8M 40s
69850K .......... .......... .......... .......... .......... 13% 37.3M 40s
69900K .......... .......... .......... .......... .......... 13% 21.8M 40s
69950K .......... .......... .......... .......... .......... 13% 32.1M 40s
70000K .......... .......... .......... .......... .......... 13% 49.8M 40s
70050K .......... .......... .......... .......... .......... 13% 55.6M 40s
70100K .......... .......... .......... .......... .......... 13% 49.3M 40s
70150K .......... .......... .......... .......... .......... 13% 20.0M 40s
70200K .......... .......... .......... .......... .......... 13% 14.4M 40s
70250K .......... .......... .......... .......... .......... 13% 57.5M 40s
70300K .......... .......... .......... .......... .......... 13% 39.6M 40s
70350K .......... .......... .......... .......... .......... 13% 75.6M 40s
70400K .......... .......... .......... .......... .......... 13% 27.9M 40s
70450K .......... .......... .......... .......... .......... 13% 57.6M 40s
70500K .......... .......... .......... .......... .......... 13% 159M 40s
70550K .......... .......... .......... .......... .......... 13% 93.4M 40s
70600K .......... .......... .......... .......... .......... 13% 138M 40s
70650K .......... .......... .......... .......... .......... 13% 9.90M 40s
70700K .......... .......... .......... .......... .......... 13% 29.8M 40s
70750K .......... .......... .......... .......... .......... 13% 154M 40s
70800K .......... .......... .......... .......... .......... 13% 167M 40s
70850K .......... .......... .......... .......... .......... 13% 143M 40s
70900K .......... .......... .......... .......... .......... 13% 150M 40s
70950K .......... .......... .......... .......... .......... 13% 9.20M 40s
71000K .......... .......... .......... .......... .......... 13% 206M 40s
71050K .......... .......... .......... .......... .......... 13% 198M 40s
71100K .......... .......... .......... .......... .......... 13% 3.86M 40s
71150K .......... .......... .......... .......... .......... 13% 107M 40s
71200K .......... .......... .......... .......... .......... 13% 128M 40s
71250K .......... .......... .......... .......... .......... 13% 203M 40s
71300K .......... .......... .......... .......... .......... 13% 12.5M 40s
71350K .......... .......... .......... .......... .......... 13% 66.5M 40s
71400K .......... .......... .......... .......... .......... 13% 203M 40s
71450K .......... .......... .......... .......... .......... 13% 4.82M 40s
71500K .......... .......... .......... .......... .......... 13% 74.9M 40s
71550K .......... .......... .......... .......... .......... 13% 123M 40s
71600K .......... .......... .......... .......... .......... 13% 133M 40s
71650K .......... .......... .......... .......... .......... 13% 3.64M 40s
71700K .......... .......... .......... .......... .......... 13% 51.8M 40s
71750K .......... .......... .......... .......... .......... 13% 27.3M 40s
71800K .......... .......... .......... .......... .......... 13% 48.6M 40s
71850K .......... .......... .......... .......... .......... 13% 20.4M 40s
71900K .......... .......... .......... .......... .......... 13% 56.3M 40s
71950K .......... .......... .......... .......... .......... 13% 137M 39s
72000K .......... .......... .......... .......... .......... 13% 59.0M 39s
72050K .......... .......... .......... .......... .......... 13% 13.0M 39s
72100K .......... .......... .......... .......... .......... 13% 16.6M 39s
72150K .......... .......... .......... .......... .......... 13% 110M 39s
72200K .......... .......... .......... .......... .......... 13% 12.6M 39s
72250K .......... .......... .......... .......... .......... 13% 80.3M 39s
72300K .......... .......... .......... .......... .......... 13% 6.05M 39s
72350K .......... .......... .......... .......... .......... 13% 86.4M 39s
72400K .......... .......... .......... .......... .......... 13% 152M 39s
72450K .......... .......... .......... .......... .......... 13% 184M 39s
72500K .......... .......... .......... .......... .......... 13% 217M 39s
72550K .......... .......... .......... .......... .......... 13% 210M 39s
72600K .......... .......... .......... .......... .......... 13% 96.7M 39s
72650K .......... .......... .......... .......... .......... 13% 5.51M 39s
72700K .......... .......... .......... .......... .......... 13% 527K 40s
72750K .......... .......... .......... .......... .......... 13% 19.8M 40s
72800K .......... .......... .......... .......... .......... 13% 13.9M 40s
72850K .......... .......... .......... .......... .......... 13% 92.0M 40s
72900K .......... .......... .......... .......... .......... 13% 152M 40s
72950K .......... .......... .......... .......... .......... 13% 99.4M 40s
73000K .......... .......... .......... .......... .......... 13% 88.8M 40s
73050K .......... .......... .......... .......... .......... 13% 66.4M 40s
73100K .......... .......... .......... .......... .......... 13% 85.8M 40s
73150K .......... .......... .......... .......... .......... 13% 95.9M 40s
73200K .......... .......... .......... .......... .......... 13% 71.4M 40s
73250K .......... .......... .......... .......... .......... 13% 107M 40s
73300K .......... .......... .......... .......... .......... 13% 126M 40s
73350K .......... .......... .......... .......... .......... 13% 143M 39s
73400K .......... .......... .......... .......... .......... 13% 92.7M 39s
73450K .......... .......... .......... .......... .......... 13% 108M 39s
73500K .......... .......... .......... .......... .......... 13% 191M 39s
73550K .......... .......... .......... .......... .......... 13% 177M 39s
73600K .......... .......... .......... .......... .......... 13% 80.7M 39s
73650K .......... .......... .......... .......... .......... 13% 189M 39s
73700K .......... .......... .......... .......... .......... 13% 171M 39s
73750K .......... .......... .......... .......... .......... 13% 144M 39s
73800K .......... .......... .......... .......... .......... 13% 114M 39s
73850K .......... .......... .......... .......... .......... 13% 113M 39s
73900K .......... .......... .......... .......... .......... 13% 8.91M 39s
73950K .......... .......... .......... .......... .......... 13% 143M 39s
74000K .......... .......... .......... .......... .......... 13% 126M 39s
74050K .......... .......... .......... .......... .......... 13% 97.3M 39s
74100K .......... .......... .......... .......... .......... 13% 104M 39s
74150K .......... .......... .......... .......... .......... 13% 174M 39s
74200K .......... .......... .......... .......... .......... 13% 4.86M 39s
74250K .......... .......... .......... .......... .......... 13% 158M 39s
74300K .......... .......... .......... .......... .......... 13% 46.0M 39s
74350K .......... .......... .......... .......... .......... 13% 59.3M 39s
74400K .......... .......... .......... .......... .......... 13% 71.5M 39s
74450K .......... .......... .......... .......... .......... 13% 122M 39s
74500K .......... .......... .......... .......... .......... 13% 4.52M 39s
74550K .......... .......... .......... .......... .......... 13% 87.8M 39s
74600K .......... .......... .......... .......... .......... 14% 127M 39s
74650K .......... .......... .......... .......... .......... 14% 174M 39s
74700K .......... .......... .......... .......... .......... 14% 53.8M 39s
74750K .......... .......... .......... .......... .......... 14% 1.11M 39s
74800K .......... .......... .......... .......... .......... 14% 103M 39s
74850K .......... .......... .......... .......... .......... 14% 66.6M 39s
74900K .......... .......... .......... .......... .......... 14% 130M 39s
74950K .......... .......... .......... .......... .......... 14% 92.0M 39s
75000K .......... .......... .......... .......... .......... 14% 212M 39s
75050K .......... .......... .......... .......... .......... 14% 194M 39s
75100K .......... .......... .......... .......... .......... 14% 70.5M 39s
75150K .......... .......... .......... .......... .......... 14% 195M 39s
75200K .......... .......... .......... .......... .......... 14% 141M 39s
75250K .......... .......... .......... .......... .......... 14% 97.7M 39s
75300K .......... .......... .......... .......... .......... 14% 175M 39s
75350K .......... .......... .......... .......... .......... 14% 178M 39s
75400K .......... .......... .......... .......... .......... 14% 156M 39s
75450K .......... .......... .......... .......... .......... 14% 121M 39s
75500K .......... .......... .......... .......... .......... 14% 165M 39s
75550K .......... .......... .......... .......... .......... 14% 203M 39s
75600K .......... .......... .......... .......... .......... 14% 185M 39s
75650K .......... .......... .......... .......... .......... 14% 156M 39s
75700K .......... .......... .......... .......... .......... 14% 136M 39s
75750K .......... .......... .......... .......... .......... 14% 6.23M 39s
75800K .......... .......... .......... .......... .......... 14% 102M 39s
75850K .......... .......... .......... .......... .......... 14% 106M 39s
75900K .......... .......... .......... .......... .......... 14% 191M 39s
75950K .......... .......... .......... .......... .......... 14% 181M 39s
76000K .......... .......... .......... .......... .......... 14% 119M 38s
76050K .......... .......... .......... .......... .......... 14% 2.79M 39s
76100K .......... .......... .......... .......... .......... 14% 92.7M 39s
76150K .......... .......... .......... .......... .......... 14% 198M 38s
76200K .......... .......... .......... .......... .......... 14% 4.37M 39s
76250K .......... .......... .......... .......... .......... 14% 101M 39s
76300K .......... .......... .......... .......... .......... 14% 63.9M 38s
76350K .......... .......... .......... .......... .......... 14% 108M 38s
76400K .......... .......... .......... .......... .......... 14% 115M 38s
76450K .......... .......... .......... .......... .......... 14% 127M 38s
76500K .......... .......... .......... .......... .......... 14% 148M 38s
76550K .......... .......... .......... .......... .......... 14% 203M 38s
76600K .......... .......... .......... .......... .......... 14% 119M 38s
76650K .......... .......... .......... .......... .......... 14% 134M 38s
76700K .......... .......... .......... .......... .......... 14% 27.9M 38s
76750K .......... .......... .......... .......... .......... 14% 99.6M 38s
76800K .......... .......... .......... .......... .......... 14% 383K 39s
76850K .......... .......... .......... .......... .......... 14% 157M 39s
76900K .......... .......... .......... .......... .......... 14% 130M 39s
76950K .......... .......... .......... .......... .......... 14% 87.3M 39s
77000K .......... .......... .......... .......... .......... 14% 26.0M 39s
77050K .......... .......... .......... .......... .......... 14% 64.2M 39s
77100K .......... .......... .......... .......... .......... 14% 4.93M 39s
77150K .......... .......... .......... .......... .......... 14% 25.8M 39s
77200K .......... .......... .......... .......... .......... 14% 97.3M 39s
77250K .......... .......... .......... .......... .......... 14% 140M 39s
77300K .......... .......... .......... .......... .......... 14% 158M 39s
77350K .......... .......... .......... .......... .......... 14% 182M 39s
77400K .......... .......... .......... .......... .......... 14% 159M 39s
77450K .......... .......... .......... .......... .......... 14% 28.9M 39s
77500K .......... .......... .......... .......... .......... 14% 204M 39s
77550K .......... .......... .......... .......... .......... 14% 191M 39s
77600K .......... .......... .......... .......... .......... 14% 198M 39s
77650K .......... .......... .......... .......... .......... 14% 189M 39s
77700K .......... .......... .......... .......... .......... 14% 178M 39s
77750K .......... .......... .......... .......... .......... 14% 188M 39s
77800K .......... .......... .......... .......... .......... 14% 7.30M 39s
77850K .......... .......... .......... .......... .......... 14% 183M 39s
77900K .......... .......... .......... .......... .......... 14% 182M 39s
77950K .......... .......... .......... .......... .......... 14% 28.4M 38s
78000K .......... .......... .......... .......... .......... 14% 21.8M 38s
78050K .......... .......... .......... .......... .......... 14% 174M 38s
78100K .......... .......... .......... .......... .......... 14% 156M 38s
78150K .......... .......... .......... .......... .......... 14% 208M 38s
78200K .......... .......... .......... .......... .......... 14% 28.8M 38s
78250K .......... .......... .......... .......... .......... 14% 28.5M 38s
78300K .......... .......... .......... .......... .......... 14% 48.8M 38s
78350K .......... .......... .......... .......... .......... 14% 26.2M 38s
78400K .......... .......... .......... .......... .......... 14% 136M 38s
78450K .......... .......... .......... .......... .......... 14% 123M 38s
78500K .......... .......... .......... .......... .......... 14% 51.6M 38s
78550K .......... .......... .......... .......... .......... 14% 2.36M 38s
78600K .......... .......... .......... .......... .......... 14% 86.3M 38s
78650K .......... .......... .......... .......... .......... 14% 196M 38s
78700K .......... .......... .......... .......... .......... 14% 89.1M 38s
78750K .......... .......... .......... .......... .......... 14% 159M 38s
78800K .......... .......... .......... .......... .......... 14% 168M 38s
78850K .......... .......... .......... .......... .......... 14% 338K 39s
78900K .......... .......... .......... .......... .......... 14% 82.6M 39s
78950K .......... .......... .......... .......... .......... 14% 21.1M 39s
79000K .......... .......... .......... .......... .......... 14% 191M 39s
79050K .......... .......... .......... .......... .......... 14% 195M 39s
79100K .......... .......... .......... .......... .......... 14% 76.7M 39s
79150K .......... .......... .......... .......... .......... 14% 31.6M 39s
79200K .......... .......... .......... .......... .......... 14% 93.7M 39s
79250K .......... .......... .......... .......... .......... 14% 145M 39s
79300K .......... .......... .......... .......... .......... 14% 178M 39s
79350K .......... .......... .......... .......... .......... 14% 144M 39s
79400K .......... .......... .......... .......... .......... 14% 170M 39s
79450K .......... .......... .......... .......... .......... 14% 98.0M 39s
79500K .......... .......... .......... .......... .......... 14% 190M 39s
79550K .......... .......... .......... .......... .......... 14% 98.6M 39s
79600K .......... .......... .......... .......... .......... 14% 187M 39s
79650K .......... .......... .......... .......... .......... 14% 231M 39s
79700K .......... .......... .......... .......... .......... 14% 206M 39s
79750K .......... .......... .......... .......... .......... 14% 191M 39s
79800K .......... .......... .......... .......... .......... 14% 212M 39s
79850K .......... .......... .......... .......... .......... 14% 104M 39s
79900K .......... .......... .......... .......... .......... 14% 103M 38s
79950K .......... .......... .......... .......... .......... 15% 170M 38s
80000K .......... .......... .......... .......... .......... 15% 195M 38s
80050K .......... .......... .......... .......... .......... 15% 13.3M 38s
80100K .......... .......... .......... .......... .......... 15% 152M 38s
80150K .......... .......... .......... .......... .......... 15% 245M 38s
80200K .......... .......... .......... .......... .......... 15% 84.6M 38s
80250K .......... .......... .......... .......... .......... 15% 202M 38s
80300K .......... .......... .......... .......... .......... 15% 8.37M 38s
80350K .......... .......... .......... .......... .......... 15% 139M 38s
80400K .......... .......... .......... .......... .......... 15% 152M 38s
80450K .......... .......... .......... .......... .......... 15% 138M 38s
80500K .......... .......... .......... .......... .......... 15% 18.2M 38s
80550K .......... .......... .......... .......... .......... 15% 120M 38s
80600K .......... .......... .......... .......... .......... 15% 5.04M 38s
80650K .......... .......... .......... .......... .......... 15% 195M 38s
80700K .......... .......... .......... .......... .......... 15% 198M 38s
80750K .......... .......... .......... .......... .......... 15% 17.3M 38s
80800K .......... .......... .......... .......... .......... 15% 72.4M 38s
80850K .......... .......... .......... .......... .......... 15% 781K 38s
80900K .......... .......... .......... .......... .......... 15% 107M 38s
80950K .......... .......... .......... .......... .......... 15% 98.8M 38s
81000K .......... .......... .......... .......... .......... 15% 86.1M 38s
81050K .......... .......... .......... .......... .......... 15% 130M 38s
81100K .......... .......... .......... .......... .......... 15% 155M 38s
81150K .......... .......... .......... .......... .......... 15% 186M 38s
81200K .......... .......... .......... .......... .......... 15% 136M 38s
81250K .......... .......... .......... .......... .......... 15% 194M 38s
81300K .......... .......... .......... .......... .......... 15% 86.4M 38s
81350K .......... .......... .......... .......... .......... 15% 102M 38s
81400K .......... .......... .......... .......... .......... 15% 152M 38s
81450K .......... .......... .......... .......... .......... 15% 222M 38s
81500K .......... .......... .......... .......... .......... 15% 184M 38s
81550K .......... .......... .......... .......... .......... 15% 131M 38s
81600K .......... .......... .......... .......... .......... 15% 229M 38s
81650K .......... .......... .......... .......... .......... 15% 287M 38s
81700K .......... .......... .......... .......... .......... 15% 258M 38s
81750K .......... .......... .......... .......... .......... 15% 236M 38s
81800K .......... .......... .......... .......... .......... 15% 291M 38s
81850K .......... .......... .......... .......... .......... 15% 265M 38s
81900K .......... .......... .......... .......... .......... 15% 2.87M 38s
81950K .......... .......... .......... .......... .......... 15% 104M 38s
82000K .......... .......... .......... .......... .......... 15% 126M 38s
82050K .......... .......... .......... .......... .......... 15% 108M 38s
82100K .......... .......... .......... .......... .......... 15% 136M 38s
82150K .......... .......... .......... .......... .......... 15% 119M 38s
82200K .......... .......... .......... .......... .......... 15% 110M 38s
82250K .......... .......... .......... .......... .......... 15% 131M 38s
82300K .......... .......... .......... .......... .......... 15% 200M 38s
82350K .......... .......... .......... .......... .......... 15% 91.4M 38s
82400K .......... .......... .......... .......... .......... 15% 169M 38s
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82500K .......... .......... .......... .......... .......... 15% 162M 38s
82550K .......... .......... .......... .......... .......... 15% 135M 38s
82600K .......... .......... .......... .......... .......... 15% 8.80M 38s
82650K .......... .......... .......... .......... .......... 15% 216M 38s
82700K .......... .......... .......... .......... .......... 15% 73.9M 38s
82750K .......... .......... .......... .......... .......... 15% 107M 38s
82800K .......... .......... .......... .......... .......... 15% 110M 38s
82850K .......... .......... .......... .......... .......... 15% 6.26M 38s
82900K .......... .......... .......... .......... .......... 15% 2.23M 38s
82950K .......... .......... .......... .......... .......... 15% 163M 38s
83000K .......... .......... .......... .......... .......... 15% 207M 38s
83050K .......... .......... .......... .......... .......... 15% 128M 38s
83100K .......... .......... .......... .......... .......... 15% 173M 38s
83150K .......... .......... .......... .......... .......... 15% 117M 38s
83200K .......... .......... .......... .......... .......... 15% 48.7M 38s
83250K .......... .......... .......... .......... .......... 15% 157M 38s
83300K .......... .......... .......... .......... .......... 15% 133M 38s
83350K .......... .......... .......... .......... .......... 15% 142M 37s
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83500K .......... .......... .......... .......... .......... 15% 197M 37s
83550K .......... .......... .......... .......... .......... 15% 114M 37s
83600K .......... .......... .......... .......... .......... 15% 71.7M 37s
83650K .......... .......... .......... .......... .......... 15% 210M 37s
83700K .......... .......... .......... .......... .......... 15% 127M 37s
83750K .......... .......... .......... .......... .......... 15% 13.4M 37s
83800K .......... .......... .......... .......... .......... 15% 126M 37s
83850K .......... .......... .......... .......... .......... 15% 2.46M 37s
83900K .......... .......... .......... .......... .......... 15% 9.25M 37s
83950K .......... .......... .......... .......... .......... 15% 2.22M 37s
84000K .......... .......... .......... .......... .......... 15% 15.6M 37s
84050K .......... .......... .......... .......... .......... 15% 164M 37s
84100K .......... .......... .......... .......... .......... 15% 194M 37s
84150K .......... .......... .......... .......... .......... 15% 182M 37s
84200K .......... .......... .......... .......... .......... 15% 105M 37s
84250K .......... .......... .......... .......... .......... 15% 116M 37s
84300K .......... .......... .......... .......... .......... 15% 158M 37s
84350K .......... .......... .......... .......... .......... 15% 139M 37s
84400K .......... .......... .......... .......... .......... 15% 8.27M 37s
84450K .......... .......... .......... .......... .......... 15% 76.2M 37s
84500K .......... .......... .......... .......... .......... 15% 157M 37s
84550K .......... .......... .......... .......... .......... 15% 173M 37s
84600K .......... .......... .......... .......... .......... 15% 72.9M 37s
84650K .......... .......... .......... .......... .......... 15% 6.47M 37s
84700K .......... .......... .......... .......... .......... 15% 125M 37s
84750K .......... .......... .......... .......... .......... 15% 119M 37s
84800K .......... .......... .......... .......... .......... 15% 174M 37s
84850K .......... .......... .......... .......... .......... 15% 110M 37s
84900K .......... .......... .......... .......... .......... 15% 8.34M 37s
84950K .......... .......... .......... .......... .......... 15% 4.96M 37s
85000K .......... .......... .......... .......... .......... 15% 99.4M 37s
85050K .......... .......... .......... .......... .......... 15% 85.7M 37s
85100K .......... .......... .......... .......... .......... 15% 136M 37s
85150K .......... .......... .......... .......... .......... 15% 141M 37s
85200K .......... .......... .......... .......... .......... 15% 112M 37s
85250K .......... .......... .......... .......... .......... 15% 126M 37s
85300K .......... .......... .......... .......... .......... 16% 96.5M 37s
85350K .......... .......... .......... .......... .......... 16% 29.3M 37s
85400K .......... .......... .......... .......... .......... 16% 149M 37s
85450K .......... .......... .......... .......... .......... 16% 16.2M 37s
85500K .......... .......... .......... .......... .......... 16% 25.8M 37s
85550K .......... .......... .......... .......... .......... 16% 165M 37s
85600K .......... .......... .......... .......... .......... 16% 56.4M 37s
85650K .......... .......... .......... .......... .......... 16% 93.2M 37s
85700K .......... .......... .......... .......... .......... 16% 27.7M 37s
85750K .......... .......... .......... .......... .......... 16% 6.95M 37s
85800K .......... .......... .......... .......... .......... 16% 131M 37s
85850K .......... .......... .......... .......... .......... 16% 75.8M 37s
85900K .......... .......... .......... .......... .......... 16% 92.7M 37s
85950K .......... .......... .......... .......... .......... 16% 18.7M 37s
86000K .......... .......... .......... .......... .......... 16% 7.01M 37s
86050K .......... .......... .......... .......... .......... 16% 125M 37s
86100K .......... .......... .......... .......... .......... 16% 127M 37s
86150K .......... .......... .......... .......... .......... 16% 129M 37s
86200K .......... .......... .......... .......... .......... 16% 136M 37s
86250K .......... .......... .......... .......... .......... 16% 7.12M 37s
86300K .......... .......... .......... .......... .......... 16% 166M 37s
86350K .......... .......... .......... .......... .......... 16% 134M 37s
86400K .......... .......... .......... .......... .......... 16% 118M 37s
86450K .......... .......... .......... .......... .......... 16% 168M 37s
86500K .......... .......... .......... .......... .......... 16% 243M 37s
86550K .......... .......... .......... .......... .......... 16% 7.85M 37s
86600K .......... .......... .......... .......... .......... 16% 132M 37s
86650K .......... .......... .......... .......... .......... 16% 104M 37s
86700K .......... .......... .......... .......... .......... 16% 132M 36s
86750K .......... .......... .......... .......... .......... 16% 212M 36s
86800K .......... .......... .......... .......... .......... 16% 6.83M 36s
86850K .......... .......... .......... .......... .......... 16% 106M 36s
86900K .......... .......... .......... .......... .......... 16% 124M 36s
86950K .......... .......... .......... .......... .......... 16% 87.2M 36s
87000K .......... .......... .......... .......... .......... 16% 764K 37s
87050K .......... .......... .......... .......... .......... 16% 61.6M 37s
87100K .......... .......... .......... .......... .......... 16% 22.8M 37s
87150K .......... .......... .......... .......... .......... 16% 93.0M 37s
87200K .......... .......... .......... .......... .......... 16% 73.5M 37s
87250K .......... .......... .......... .......... .......... 16% 48.6M 37s
87300K .......... .......... .......... .......... .......... 16% 84.8M 37s
87350K .......... .......... .......... .......... .......... 16% 50.7M 37s
87400K .......... .......... .......... .......... .......... 16% 136M 37s
87450K .......... .......... .......... .......... .......... 16% 3.35M 37s
87500K .......... .......... .......... .......... .......... 16% 6.71M 37s
87550K .......... .......... .......... .......... .......... 16% 120M 37s
87600K .......... .......... .......... .......... .......... 16% 8.41M 37s
87650K .......... .......... .......... .......... .......... 16% 1.42M 37s
87700K .......... .......... .......... .......... .......... 16% 25.2M 37s
87750K .......... .......... .......... .......... .......... 16% 28.9M 37s
87800K .......... .......... .......... .......... .......... 16% 11.4M 37s
87850K .......... .......... .......... .......... .......... 16% 38.4M 37s
87900K .......... .......... .......... .......... .......... 16% 50.3M 37s
87950K .......... .......... .......... .......... .......... 16% 1.91M 37s
88000K .......... .......... .......... .......... .......... 16% 46.7M 37s
88050K .......... .......... .......... .......... .......... 16% 4.02M 37s
88100K .......... .......... .......... .......... .......... 16% 103M 37s
88150K .......... .......... .......... .......... .......... 16% 91.8M 37s
88200K .......... .......... .......... .......... .......... 16% 137M 37s
88250K .......... .......... .......... .......... .......... 16% 81.2M 37s
88300K .......... .......... .......... .......... .......... 16% 85.7M 37s
88350K .......... .......... .......... .......... .......... 16% 19.6M 37s
88400K .......... .......... .......... .......... .......... 16% 6.33M 37s
88450K .......... .......... .......... .......... .......... 16% 8.12M 37s
88500K .......... .......... .......... .......... .......... 16% 19.5M 37s
88550K .......... .......... .......... .......... .......... 16% 91.8M 37s
88600K .......... .......... .......... .......... .......... 16% 11.8M 37s
88650K .......... .......... .......... .......... .......... 16% 20.0M 37s
88700K .......... .......... .......... .......... .......... 16% 65.6M 37s
88750K .......... .......... .......... .......... .......... 16% 155M 37s
88800K .......... .......... .......... .......... .......... 16% 195M 37s
88850K .......... .......... .......... .......... .......... 16% 167M 37s
88900K .......... .......... .......... .......... .......... 16% 62.8M 37s
88950K .......... .......... .......... .......... .......... 16% 31.1M 37s
89000K .......... .......... .......... .......... .......... 16% 72.7M 36s
89050K .......... .......... .......... .......... .......... 16% 70.0K 40s
89100K .......... .......... .......... .......... .......... 16% 91.1M 40s
89150K .......... .......... .......... .......... .......... 16% 80.2M 40s
89200K .......... .......... .......... .......... .......... 16% 176M 40s
89250K .......... .......... .......... .......... .......... 16% 161M 40s
89300K .......... .......... .......... .......... .......... 16% 105M 40s
89350K .......... .......... .......... .......... .......... 16% 140M 40s
89400K .......... .......... .......... .......... .......... 16% 130M 40s
89450K .......... .......... .......... .......... .......... 16% 92.8M 40s
89500K .......... .......... .......... .......... .......... 16% 173M 40s
89550K .......... .......... .......... .......... .......... 16% 181M 40s
89600K .......... .......... .......... .......... .......... 16% 14.5M 40s
89650K .......... .......... .......... .......... .......... 16% 179M 40s
89700K .......... .......... .......... .......... .......... 16% 65.7M 40s
89750K .......... .......... .......... .......... .......... 16% 98.8M 40s
89800K .......... .......... .......... .......... .......... 16% 313M 40s
89850K .......... .......... .......... .......... .......... 16% 249M 40s
89900K .......... .......... .......... .......... .......... 16% 30.7M 40s
89950K .......... .......... .......... .......... .......... 16% 151M 40s
90000K .......... .......... .......... .......... .......... 16% 98.0M 40s
90050K .......... .......... .......... .......... .......... 16% 164M 40s
90100K .......... .......... .......... .......... .......... 16% 154M 40s
90150K .......... .......... .......... .......... .......... 16% 223M 40s
90200K .......... .......... .......... .......... .......... 16% 128M 39s
90250K .......... .......... .......... .......... .......... 16% 236M 39s
90300K .......... .......... .......... .......... .......... 16% 233M 39s
90350K .......... .......... .......... .......... .......... 16% 203M 39s
90400K .......... .......... .......... .......... .......... 16% 46.1M 39s
90450K .......... .......... .......... .......... .......... 16% 19.6M 39s
90500K .......... .......... .......... .......... .......... 16% 164M 39s
90550K .......... .......... .......... .......... .......... 16% 4.20M 39s
90600K .......... .......... .......... .......... .......... 17% 121M 39s
90650K .......... .......... .......... .......... .......... 17% 138M 39s
90700K .......... .......... .......... .......... .......... 17% 138M 39s
90750K .......... .......... .......... .......... .......... 17% 292M 39s
90800K .......... .......... .......... .......... .......... 17% 8.73M 39s
90850K .......... .......... .......... .......... .......... 17% 92.1M 39s
90900K .......... .......... .......... .......... .......... 17% 41.9M 39s
90950K .......... .......... .......... .......... .......... 17% 112M 39s
91000K .......... .......... .......... .......... .......... 17% 172M 39s
91050K .......... .......... .......... .......... .......... 17% 56.0M 39s
91100K .......... .......... .......... .......... .......... 17% 3.81M 39s
91150K .......... .......... .......... .......... .......... 17% 140M 39s
91200K .......... .......... .......... .......... .......... 17% 129M 39s
91250K .......... .......... .......... .......... .......... 17% 130M 39s
91300K .......... .......... .......... .......... .......... 17% 95.2M 39s
91350K .......... .......... .......... .......... .......... 17% 110M 39s
91400K .......... .......... .......... .......... .......... 17% 5.90M 39s
91450K .......... .......... .......... .......... .......... 17% 118M 39s
91500K .......... .......... .......... .......... .......... 17% 20.4M 39s
91550K .......... .......... .......... .......... .......... 17% 135M 39s
91600K .......... .......... .......... .......... .......... 17% 122M 39s
91650K .......... .......... .......... .......... .......... 17% 5.47M 39s
91700K .......... .......... .......... .......... .......... 17% 63.2M 39s
91750K .......... .......... .......... .......... .......... 17% 166M 39s
91800K .......... .......... .......... .......... .......... 17% 125M 39s
91850K .......... .......... .......... .......... .......... 17% 142M 39s
91900K .......... .......... .......... .......... .......... 17% 27.1M 39s
91950K .......... .......... .......... .......... .......... 17% 10.5M 39s
92000K .......... .......... .......... .......... .......... 17% 112M 39s
92050K .......... .......... .......... .......... .......... 17% 129M 39s
92100K .......... .......... .......... .......... .......... 17% 50.6M 39s
92150K .......... .......... .......... .......... .......... 17% 2.11M 39s
92200K .......... .......... .......... .......... .......... 17% 55.9M 39s
92250K .......... .......... .......... .......... .......... 17% 119M 39s
92300K .......... .......... .......... .......... .......... 17% 166M 39s
92350K .......... .......... .......... .......... .......... 17% 120M 39s
92400K .......... .......... .......... .......... .......... 17% 168M 39s
92450K .......... .......... .......... .......... .......... 17% 73.8M 39s
92500K .......... .......... .......... .......... .......... 17% 86.6M 39s
92550K .......... .......... .......... .......... .......... 17% 204M 39s
92600K .......... .......... .......... .......... .......... 17% 153M 39s
92650K .......... .......... .......... .......... .......... 17% 140M 39s
92700K .......... .......... .......... .......... .......... 17% 136M 39s
92750K .......... .......... .......... .......... .......... 17% 21.2M 39s
92800K .......... .......... .......... .......... .......... 17% 79.3M 39s
92850K .......... .......... .......... .......... .......... 17% 99.4M 39s
92900K .......... .......... .......... .......... .......... 17% 121M 39s
92950K .......... .......... .......... .......... .......... 17% 6.86M 39s
93000K .......... .......... .......... .......... .......... 17% 148M 39s
93050K .......... .......... .......... .......... .......... 17% 7.62M 39s
93100K .......... .......... .......... .......... .......... 17% 80.4M 39s
93150K .......... .......... .......... .......... .......... 17% 147M 39s
93200K .......... .......... .......... .......... .......... 17% 145M 39s
93250K .......... .......... .......... .......... .......... 17% 15.7M 39s
93300K .......... .......... .......... .......... .......... 17% 141M 38s
93350K .......... .......... .......... .......... .......... 17% 9.29M 38s
93400K .......... .......... .......... .......... .......... 17% 151M 38s
93450K .......... .......... .......... .......... .......... 17% 162M 38s
93500K .......... .......... .......... .......... .......... 17% 137M 38s
93550K .......... .......... .......... .......... .......... 17% 8.36M 38s
93600K .......... .......... .......... .......... .......... 17% 120M 38s
93650K .......... .......... .......... .......... .......... 17% 6.54M 38s
93700K .......... .......... .......... .......... .......... 17% 142M 38s
93750K .......... .......... .......... .......... .......... 17% 151M 38s
93800K .......... .......... .......... .......... .......... 17% 162M 38s
93850K .......... .......... .......... .......... .......... 17% 7.14M 38s
93900K .......... .......... .......... .......... .......... 17% 176M 38s
93950K .......... .......... .......... .......... .......... 17% 5.31M 38s
94000K .......... .......... .......... .......... .......... 17% 120M 38s
94050K .......... .......... .......... .......... .......... 17% 180M 38s
94100K .......... .......... .......... .......... .......... 17% 152M 38s
94150K .......... .......... .......... .......... .......... 17% 14.3M 38s
94200K .......... .......... .......... .......... .......... 17% 607K 39s
94250K .......... .......... .......... .......... .......... 17% 117M 39s
94300K .......... .......... .......... .......... .......... 17% 104M 39s
94350K .......... .......... .......... .......... .......... 17% 86.4M 39s
94400K .......... .......... .......... .......... .......... 17% 198M 39s
94450K .......... .......... .......... .......... .......... 17% 65.9M 38s
94500K .......... .......... .......... .......... .......... 17% 162M 38s
94550K .......... .......... .......... .......... .......... 17% 98.2M 38s
94600K .......... .......... .......... .......... .......... 17% 184M 38s
94650K .......... .......... .......... .......... .......... 17% 105M 38s
94700K .......... .......... .......... .......... .......... 17% 98.6M 38s
94750K .......... .......... .......... .......... .......... 17% 161M 38s
94800K .......... .......... .......... .......... .......... 17% 195M 38s
94850K .......... .......... .......... .......... .......... 17% 150M 38s
94900K .......... .......... .......... .......... .......... 17% 192M 38s
94950K .......... .......... .......... .......... .......... 17% 120M 38s
95000K .......... .......... .......... .......... .......... 17% 114M 38s
95050K .......... .......... .......... .......... .......... 17% 188M 38s
95100K .......... .......... .......... .......... .......... 17% 91.6M 38s
95150K .......... .......... .......... .......... .......... 17% 193M 38s
95200K .......... .......... .......... .......... .......... 17% 142M 38s
95250K .......... .......... .......... .......... .......... 17% 109M 38s
95300K .......... .......... .......... .......... .......... 17% 173M 38s
95350K .......... .......... .......... .......... .......... 17% 107M 38s
95400K .......... .......... .......... .......... .......... 17% 9.48M 38s
95450K .......... .......... .......... .......... .......... 17% 89.9M 38s
95500K .......... .......... .......... .......... .......... 17% 76.1M 38s
95550K .......... .......... .......... .......... .......... 17% 136M 38s
95600K .......... .......... .......... .......... .......... 17% 84.8M 38s
95650K .......... .......... .......... .......... .......... 17% 89.1M 38s
95700K .......... .......... .......... .......... .......... 17% 4.48M 38s
95750K .......... .......... .......... .......... .......... 17% 120M 38s
95800K .......... .......... .......... .......... .......... 17% 109M 38s
95850K .......... .......... .......... .......... .......... 17% 167M 38s
95900K .......... .......... .......... .......... .......... 17% 150M 38s
95950K .......... .......... .......... .......... .......... 18% 5.70M 38s
96000K .......... .......... .......... .......... .......... 18% 152M 38s
96050K .......... .......... .......... .......... .......... 18% 158M 38s
96100K .......... .......... .......... .......... .......... 18% 89.8M 38s
96150K .......... .......... .......... .......... .......... 18% 127M 38s
96200K .......... .......... .......... .......... .......... 18% 117M 38s
96250K .......... .......... .......... .......... .......... 18% 296K 39s
96300K .......... .......... .......... .......... .......... 18% 60.7M 39s
96350K .......... .......... .......... .......... .......... 18% 149M 39s
96400K .......... .......... .......... .......... .......... 18% 159M 38s
96450K .......... .......... .......... .......... .......... 18% 162M 38s
96500K .......... .......... .......... .......... .......... 18% 198M 38s
96550K .......... .......... .......... .......... .......... 18% 42.5M 38s
96600K .......... .......... .......... .......... .......... 18% 158M 38s
96650K .......... .......... .......... .......... .......... 18% 40.0M 38s
96700K .......... .......... .......... .......... .......... 18% 128M 38s
96750K .......... .......... .......... .......... .......... 18% 136M 38s
96800K .......... .......... .......... .......... .......... 18% 85.1M 38s
96850K .......... .......... .......... .......... .......... 18% 114M 38s
96900K .......... .......... .......... .......... .......... 18% 156M 38s
96950K .......... .......... .......... .......... .......... 18% 84.3M 38s
97000K .......... .......... .......... .......... .......... 18% 108M 38s
97050K .......... .......... .......... .......... .......... 18% 127M 38s
97100K .......... .......... .......... .......... .......... 18% 117M 38s
97150K .......... .......... .......... .......... .......... 18% 157M 38s
97200K .......... .......... .......... .......... .......... 18% 134M 38s
97250K .......... .......... .......... .......... .......... 18% 908K 38s
97300K .......... .......... .......... .......... .......... 18% 7.71M 38s
97350K .......... .......... .......... .......... .......... 18% 39.7M 38s
97400K .......... .......... .......... .......... .......... 18% 84.2M 38s
97450K .......... .......... .......... .......... .......... 18% 63.6M 38s
97500K .......... .......... .......... .......... .......... 18% 174M 38s
97550K .......... .......... .......... .......... .......... 18% 97.9M 38s
97600K .......... .......... .......... .......... .......... 18% 14.2M 38s
97650K .......... .......... .......... .......... .......... 18% 94.8M 38s
97700K .......... .......... .......... .......... .......... 18% 80.4M 38s
97750K .......... .......... .......... .......... .......... 18% 13.0M 38s
97800K .......... .......... .......... .......... .......... 18% 16.6M 38s
97850K .......... .......... .......... .......... .......... 18% 52.7M 38s
97900K .......... .......... .......... .......... .......... 18% 11.4M 38s
97950K .......... .......... .......... .......... .......... 18% 12.6M 38s
98000K .......... .......... .......... .......... .......... 18% 55.8M 38s
98050K .......... .......... .......... .......... .......... 18% 38.4M 38s
98100K .......... .......... .......... .......... .......... 18% 8.80M 38s
98150K .......... .......... .......... .......... .......... 18% 52.7M 38s
98200K .......... .......... .......... .......... .......... 18% 127M 38s
98250K .......... .......... .......... .......... .......... 18% 93.2M 38s
98300K .......... .......... .......... .......... .......... 18% 2.74M 38s
98350K .......... .......... .......... .......... .......... 18% 92.8M 38s
98400K .......... .......... .......... .......... .......... 18% 24.8M 38s
98450K .......... .......... .......... .......... .......... 18% 20.0M 38s
98500K .......... .......... .......... .......... .......... 18% 111M 38s
98550K .......... .......... .......... .......... .......... 18% 45.2M 38s
98600K .......... .......... .......... .......... .......... 18% 41.9M 38s
98650K .......... .......... .......... .......... .......... 18% 136M 38s
98700K .......... .......... .......... .......... .......... 18% 59.4M 38s
98750K .......... .......... .......... .......... .......... 18% 46.0M 38s
98800K .......... .......... .......... .......... .......... 18% 42.8M 38s
98850K .......... .......... .......... .......... .......... 18% 23.9M 38s
98900K .......... .......... .......... .......... .......... 18% 66.5M 38s
98950K .......... .......... .......... .......... .......... 18% 12.0M 38s
99000K .......... .......... .......... .......... .......... 18% 180M 38s
99050K .......... .......... .......... .......... .......... 18% 35.7M 38s
99100K .......... .......... .......... .......... .......... 18% 108M 38s
99150K .......... .......... .......... .......... .......... 18% 87.5M 38s
99200K .......... .......... .......... .......... .......... 18% 26.1M 38s
99250K .......... .......... .......... .......... .......... 18% 125M 38s
99300K .......... .......... .......... .......... .......... 18% 3.74M 38s
99350K .......... .......... .......... .......... .......... 18% 1.13M 38s
99400K .......... .......... .......... .......... .......... 18% 3.94M 38s
99450K .......... .......... .......... .......... .......... 18% 16.3M 38s
99500K .......... .......... .......... .......... .......... 18% 10.1M 38s
99550K .......... .......... .......... .......... .......... 18% 16.9M 38s
99600K .......... .......... .......... .......... .......... 18% 73.1M 38s
99650K .......... .......... .......... .......... .......... 18% 23.1M 38s
99700K .......... .......... .......... .......... .......... 18% 7.64M 38s
99750K .......... .......... .......... .......... .......... 18% 7.52M 38s
99800K .......... .......... .......... .......... .......... 18% 4.72M 38s
99850K .......... .......... .......... .......... .......... 18% 16.1M 38s
99900K .......... .......... .......... .......... .......... 18% 1.44M 38s
99950K .......... .......... .......... .......... .......... 18% 93.2M 38s
100000K .......... .......... .......... .......... .......... 18% 189M 38s
100050K .......... .......... .......... .......... .......... 18% 39.8M 38s
100100K .......... .......... .......... .......... .......... 18% 8.48M 38s
100150K .......... .......... .......... .......... .......... 18% 34.7M 38s
100200K .......... .......... .......... .......... .......... 18% 32.9M 38s
100250K .......... .......... .......... .......... .......... 18% 39.8M 38s
100300K .......... .......... .......... .......... .......... 18% 6.68M 38s
100350K .......... .......... .......... .......... .......... 18% 15.5M 38s
100400K .......... .......... .......... .......... .......... 18% 123M 38s
100450K .......... .......... .......... .......... .......... 18% 157M 38s
100500K .......... .......... .......... .......... .......... 18% 68.6M 38s
100550K .......... .......... .......... .......... .......... 18% 35.0M 38s
100600K .......... .......... .......... .......... .......... 18% 147M 38s
100650K .......... .......... .......... .......... .......... 18% 205M 38s
100700K .......... .......... .......... .......... .......... 18% 151M 38s
100750K .......... .......... .......... .......... .......... 18% 11.8M 38s
100800K .......... .......... .......... .......... .......... 18% 84.5M 38s
100850K .......... .......... .......... .......... .......... 18% 128M 38s
100900K .......... .......... .......... .......... .......... 18% 170M 38s
100950K .......... .......... .......... .......... .......... 18% 128M 38s
101000K .......... .......... .......... .......... .......... 18% 50.1M 38s
101050K .......... .......... .......... .......... .......... 18% 176M 38s
101100K .......... .......... .......... .......... .......... 18% 144M 38s
101150K .......... .......... .......... .......... .......... 18% 189M 38s
101200K .......... .......... .......... .......... .......... 18% 142M 38s
101250K .......... .......... .......... .......... .......... 18% 178M 38s
101300K .......... .......... .......... .......... .......... 19% 24.2M 38s
101350K .......... .......... .......... .......... .......... 19% 6.50M 38s
101400K .......... .......... .......... .......... .......... 19% 29.0M 38s
101450K .......... .......... .......... .......... .......... 19% 78.5M 38s
101500K .......... .......... .......... .......... .......... 19% 25.6M 38s
101550K .......... .......... .......... .......... .......... 19% 109M 38s
101600K .......... .......... .......... .......... .......... 19% 14.3M 38s
101650K .......... .......... .......... .......... .......... 19% 104M 38s
101700K .......... .......... .......... .......... .......... 19% 142M 37s
101750K .......... .......... .......... .......... .......... 19% 102M 37s
101800K .......... .......... .......... .......... .......... 19% 162M 37s
101850K .......... .......... .......... .......... .......... 19% 21.7M 37s
101900K .......... .......... .......... .......... .......... 19% 78.9M 37s
101950K .......... .......... .......... .......... .......... 19% 67.3M 37s
102000K .......... .......... .......... .......... .......... 19% 77.9M 37s
102050K .......... .......... .......... .......... .......... 19% 66.1M 37s
102100K .......... .......... .......... .......... .......... 19% 74.8M 37s
102150K .......... .......... .......... .......... .......... 19% 91.1M 37s
102200K .......... .......... .......... .......... .......... 19% 95.6M 37s
102250K .......... .......... .......... .......... .......... 19% 166M 37s
102300K .......... .......... .......... .......... .......... 19% 109M 37s
102350K .......... .......... .......... .......... .......... 19% 130M 37s
102400K .......... .......... .......... .......... .......... 19% 1.68M 37s
102450K .......... .......... .......... .......... .......... 19% 72.9M 37s
102500K .......... .......... .......... .......... .......... 19% 49.2M 37s
102550K .......... .......... .......... .......... .......... 19% 56.8M 37s
102600K .......... .......... .......... .......... .......... 19% 69.3M 37s
102650K .......... .......... .......... .......... .......... 19% 134M 37s
102700K .......... .......... .......... .......... .......... 19% 74.8M 37s
102750K .......... .......... .......... .......... .......... 19% 19.7M 37s
102800K .......... .......... .......... .......... .......... 19% 96.7M 37s
102850K .......... .......... .......... .......... .......... 19% 92.8M 37s
102900K .......... .......... .......... .......... .......... 19% 90.1M 37s
102950K .......... .......... .......... .......... .......... 19% 91.1M 37s
103000K .......... .......... .......... .......... .......... 19% 86.9M 37s
103050K .......... .......... .......... .......... .......... 19% 63.1M 37s
103100K .......... .......... .......... .......... .......... 19% 93.5M 37s
103150K .......... .......... .......... .......... .......... 19% 27.0M 37s
103200K .......... .......... .......... .......... .......... 19% 92.0M 37s
103250K .......... .......... .......... .......... .......... 19% 79.8M 37s
103300K .......... .......... .......... .......... .......... 19% 189M 37s
103350K .......... .......... .......... .......... .......... 19% 87.7M 37s
103400K .......... .......... .......... .......... .......... 19% 82.1M 37s
103450K .......... .......... .......... .......... .......... 19% 15.0M 37s
103500K .......... .......... .......... .......... .......... 19% 71.0M 37s
103550K .......... .......... .......... .......... .......... 19% 27.7M 37s
103600K .......... .......... .......... .......... .......... 19% 121M 37s
103650K .......... .......... .......... .......... .......... 19% 58.7M 37s
103700K .......... .......... .......... .......... .......... 19% 20.6M 37s
103750K .......... .......... .......... .......... .......... 19% 31.4M 37s
103800K .......... .......... .......... .......... .......... 19% 91.3M 37s
103850K .......... .......... .......... .......... .......... 19% 130M 37s
103900K .......... .......... .......... .......... .......... 19% 81.0M 37s
103950K .......... .......... .......... .......... .......... 19% 98.6M 37s
104000K .......... .......... .......... .......... .......... 19% 5.47M 37s
104050K .......... .......... .......... .......... .......... 19% 159M 37s
104100K .......... .......... .......... .......... .......... 19% 93.2M 37s
104150K .......... .......... .......... .......... .......... 19% 87.2M 37s
104200K .......... .......... .......... .......... .......... 19% 1.26M 37s
104250K .......... .......... .......... .......... .......... 19% 18.5M 37s
104300K .......... .......... .......... .......... .......... 19% 38.5M 37s
104350K .......... .......... .......... .......... .......... 19% 6.34M 37s
104400K .......... .......... .......... .......... .......... 19% 131M 37s
104450K .......... .......... .......... .......... .......... 19% 12.4M 37s
104500K .......... .......... .......... .......... .......... 19% 78.9M 37s
104550K .......... .......... .......... .......... .......... 19% 63.5M 37s
104600K .......... .......... .......... .......... .......... 19% 99.2M 37s
104650K .......... .......... .......... .......... .......... 19% 142M 37s
104700K .......... .......... .......... .......... .......... 19% 94.1M 37s
104750K .......... .......... .......... .......... .......... 19% 70.8M 37s
104800K .......... .......... .......... .......... .......... 19% 131M 37s
104850K .......... .......... .......... .......... .......... 19% 30.7M 37s
104900K .......... .......... .......... .......... .......... 19% 133M 37s
104950K .......... .......... .......... .......... .......... 19% 25.0M 37s
105000K .......... .......... .......... .......... .......... 19% 54.8M 37s
105050K .......... .......... .......... .......... .......... 19% 73.6M 37s
105100K .......... .......... .......... .......... .......... 19% 130M 37s
105150K .......... .......... .......... .......... .......... 19% 9.14M 37s
105200K .......... .......... .......... .......... .......... 19% 91.4M 37s
105250K .......... .......... .......... .......... .......... 19% 70.6M 37s
105300K .......... .......... .......... .......... .......... 19% 144M 36s
105350K .......... .......... .......... .......... .......... 19% 77.8M 36s
105400K .......... .......... .......... .......... .......... 19% 220M 36s
105450K .......... .......... .......... .......... .......... 19% 3.30M 36s
105500K .......... .......... .......... .......... .......... 19% 7.91M 36s
105550K .......... .......... .......... .......... .......... 19% 180M 36s
105600K .......... .......... .......... .......... .......... 19% 15.5M 36s
105650K .......... .......... .......... .......... .......... 19% 37.6M 36s
105700K .......... .......... .......... .......... .......... 19% 8.55M 36s
105750K .......... .......... .......... .......... .......... 19% 13.4M 36s
105800K .......... .......... .......... .......... .......... 19% 119M 36s
105850K .......... .......... .......... .......... .......... 19% 26.4M 36s
105900K .......... .......... .......... .......... .......... 19% 189M 36s
105950K .......... .......... .......... .......... .......... 19% 49.6M 36s
106000K .......... .......... .......... .......... .......... 19% 176M 36s
106050K .......... .......... .......... .......... .......... 19% 149M 36s
106100K .......... .......... .......... .......... .......... 19% 121M 36s
106150K .......... .......... .......... .......... .......... 19% 138M 36s
106200K .......... .......... .......... .......... .......... 19% 141M 36s
106250K .......... .......... .......... .......... .......... 19% 200M 36s
106300K .......... .......... .......... .......... .......... 19% 247M 36s
106350K .......... .......... .......... .......... .......... 19% 7.22M 36s
106400K .......... .......... .......... .......... .......... 19% 152M 36s
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106500K .......... .......... .......... .......... .......... 19% 85.4M 37s
106550K .......... .......... .......... .......... .......... 19% 157M 37s
106600K .......... .......... .......... .......... .......... 20% 92.3M 37s
106650K .......... .......... .......... .......... .......... 20% 215M 37s
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106750K .......... .......... .......... .......... .......... 20% 117M 37s
106800K .......... .......... .......... .......... .......... 20% 72.1M 37s
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106900K .......... .......... .......... .......... .......... 20% 91.3M 37s
106950K .......... .......... .......... .......... .......... 20% 155M 37s
107000K .......... .......... .......... .......... .......... 20% 67.6M 36s
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107100K .......... .......... .......... .......... .......... 20% 111M 36s
107150K .......... .......... .......... .......... .......... 20% 120M 36s
107200K .......... .......... .......... .......... .......... 20% 102M 36s
107250K .......... .......... .......... .......... .......... 20% 224M 36s
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107450K .......... .......... .......... .......... .......... 20% 62.9M 36s
107500K .......... .......... .......... .......... .......... 20% 320K 37s
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107650K .......... .......... .......... .......... .......... 20% 16.9M 37s
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107850K .......... .......... .......... .......... .......... 20% 49.0M 37s
107900K .......... .......... .......... .......... .......... 20% 169M 37s
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108000K .......... .......... .......... .......... .......... 20% 159M 37s
108050K .......... .......... .......... .......... .......... 20% 154M 37s
108100K .......... .......... .......... .......... .......... 20% 176M 37s
108150K .......... .......... .......... .......... .......... 20% 126M 37s
108200K .......... .......... .......... .......... .......... 20% 31.7M 37s
108250K .......... .......... .......... .......... .......... 20% 38.9M 37s
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108400K .......... .......... .......... .......... .......... 20% 59.8M 37s
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108700K .......... .......... .......... .......... .......... 20% 3.93M 37s
108750K .......... .......... .......... .......... .......... 20% 96.9M 36s
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109000K .......... .......... .......... .......... .......... 20% 194M 36s
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109100K .......... .......... .......... .......... .......... 20% 189M 36s
109150K .......... .......... .......... .......... .......... 20% 24.3M 36s
109200K .......... .......... .......... .......... .......... 20% 121M 36s
109250K .......... .......... .......... .......... .......... 20% 11.4M 36s
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109400K .......... .......... .......... .......... .......... 20% 8.76M 36s
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109900K .......... .......... .......... .......... .......... 20% 17.8M 36s
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110000K .......... .......... .......... .......... .......... 20% 7.86M 36s
110050K .......... .......... .......... .......... .......... 20% 108M 36s
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110250K .......... .......... .......... .......... .......... 20% 27.6M 36s
110300K .......... .......... .......... .......... .......... 20% 101M 36s
110350K .......... .......... .......... .......... .......... 20% 2.48M 36s
110400K .......... .......... .......... .......... .......... 20% 199M 36s
110450K .......... .......... .......... .......... .......... 20% 114M 36s
110500K .......... .......... .......... .......... .......... 20% 211M 36s
110550K .......... .......... .......... .......... .......... 20% 2.73M 36s
110600K .......... .......... .......... .......... .......... 20% 86.0M 36s
110650K .......... .......... .......... .......... .......... 20% 151M 36s
110700K .......... .......... .......... .......... .......... 20% 43.6M 36s
110750K .......... .......... .......... .......... .......... 20% 195M 36s
110800K .......... .......... .......... .......... .......... 20% 217M 36s
110850K .......... .......... .......... .......... .......... 20% 180M 36s
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110950K .......... .......... .......... .......... .......... 20% 118M 36s
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111100K .......... .......... .......... .......... .......... 20% 286M 36s
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111200K .......... .......... .......... .......... .......... 20% 85.8M 36s
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111350K .......... .......... .......... .......... .......... 20% 13.0M 36s
111400K .......... .......... .......... .......... .......... 20% 207M 36s
111450K .......... .......... .......... .......... .......... 20% 72.1M 36s
111500K .......... .......... .......... .......... .......... 20% 8.54M 36s
111550K .......... .......... .......... .......... .......... 20% 92.8M 36s
111600K .......... .......... .......... .......... .......... 20% 3.31M 36s
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111800K .......... .......... .......... .......... .......... 20% 63.6M 36s
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111900K .......... .......... .......... .......... .......... 20% 142M 36s
111950K .......... .......... .......... .......... .......... 21% 144M 36s
112000K .......... .......... .......... .......... .......... 21% 63.4M 36s
112050K .......... .......... .......... .......... .......... 21% 71.9M 36s
112100K .......... .......... .......... .......... .......... 21% 8.33M 36s
112150K .......... .......... .......... .......... .......... 21% 189M 36s
112200K .......... .......... .......... .......... .......... 21% 90.8M 36s
112250K .......... .......... .......... .......... .......... 21% 55.4M 36s
112300K .......... .......... .......... .......... .......... 21% 13.3M 36s
112350K .......... .......... .......... .......... .......... 21% 81.5M 36s
112400K .......... .......... .......... .......... .......... 21% 172M 36s
112450K .......... .......... .......... .......... .......... 21% 6.05M 36s
112500K .......... .......... .......... .......... .......... 21% 87.5M 36s
112550K .......... .......... .......... .......... .......... 21% 105M 36s
112600K .......... .......... .......... .......... .......... 21% 249K 36s
112650K .......... .......... .......... .......... .......... 21% 93.5M 36s
112700K .......... .......... .......... .......... .......... 21% 134M 36s
112750K .......... .......... .......... .......... .......... 21% 214M 36s
112800K .......... .......... .......... .......... .......... 21% 217M 36s
112850K .......... .......... .......... .......... .......... 21% 24.7M 36s
112900K .......... .......... .......... .......... .......... 21% 113M 36s
112950K .......... .......... .......... .......... .......... 21% 15.5M 36s
113000K .......... .......... .......... .......... .......... 21% 48.1M 36s
113050K .......... .......... .......... .......... .......... 21% 103M 36s
113100K .......... .......... .......... .......... .......... 21% 144M 36s
113150K .......... .......... .......... .......... .......... 21% 171M 36s
113200K .......... .......... .......... .......... .......... 21% 6.22M 36s
113250K .......... .......... .......... .......... .......... 21% 6.49M 36s
113300K .......... .......... .......... .......... .......... 21% 12.9M 36s
113350K .......... .......... .......... .......... .......... 21% 4.38M 36s
113400K .......... .......... .......... .......... .......... 21% 9.26M 36s
113450K .......... .......... .......... .......... .......... 21% 3.76M 36s
113500K .......... .......... .......... .......... .......... 21% 2.25M 36s
113550K .......... .......... .......... .......... .......... 21% 5.99M 36s
113600K .......... .......... .......... .......... .......... 21% 101M 36s
113650K .......... .......... .......... .......... .......... 21% 3.09M 36s
113700K .......... .......... .......... .......... .......... 21% 31.0M 36s
113750K .......... .......... .......... .......... .......... 21% 38.3M 36s
113800K .......... .......... .......... .......... .......... 21% 95.7M 36s
113850K .......... .......... .......... .......... .......... 21% 89.8M 36s
113900K .......... .......... .......... .......... .......... 21% 130M 36s
113950K .......... .......... .......... .......... .......... 21% 37.1M 36s
114000K .......... .......... .......... .......... .......... 21% 52.9M 36s
114050K .......... .......... .......... .......... .......... 21% 45.8M 36s
114100K .......... .......... .......... .......... .......... 21% 94.1M 36s
114150K .......... .......... .......... .......... .......... 21% 126M 36s
114200K .......... .......... .......... .......... .......... 21% 72.0M 36s
114250K .......... .......... .......... .......... .......... 21% 128M 36s
114300K .......... .......... .......... .......... .......... 21% 104M 36s
114350K .......... .......... .......... .......... .......... 21% 27.4M 36s
114400K .......... .......... .......... .......... .......... 21% 160M 36s
114450K .......... .......... .......... .......... .......... 21% 67.6M 36s
114500K .......... .......... .......... .......... .......... 21% 230M 36s
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114600K .......... .......... .......... .......... .......... 21% 53.9M 36s
114650K .......... .......... .......... .......... .......... 21% 21.6M 36s
114700K .......... .......... .......... .......... .......... 21% 2.35M 36s
114750K .......... .......... .......... .......... .......... 21% 2.00M 36s
114800K .......... .......... .......... .......... .......... 21% 9.38M 36s
114850K .......... .......... .......... .......... .......... 21% 178M 36s
114900K .......... .......... .......... .......... .......... 21% 114M 36s
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115000K .......... .......... .......... .......... .......... 21% 101M 36s
115050K .......... .......... .......... .......... .......... 21% 39.8M 36s
115100K .......... .......... .......... .......... .......... 21% 3.79M 36s
115150K .......... .......... .......... .......... .......... 21% 14.8M 36s
115200K .......... .......... .......... .......... .......... 21% 38.4M 36s
115250K .......... .......... .......... .......... .......... 21% 80.0M 36s
115300K .......... .......... .......... .......... .......... 21% 13.9M 36s
115350K .......... .......... .......... .......... .......... 21% 27.6M 36s
115400K .......... .......... .......... .......... .......... 21% 67.5M 36s
115450K .......... .......... .......... .......... .......... 21% 18.4M 36s
115500K .......... .......... .......... .......... .......... 21% 67.9M 36s
115550K .......... .......... .......... .......... .......... 21% 65.6M 36s
115600K .......... .......... .......... .......... .......... 21% 10.5M 36s
115650K .......... .......... .......... .......... .......... 21% 5.55M 36s
115700K .......... .......... .......... .......... .......... 21% 5.68M 36s
115750K .......... .......... .......... .......... .......... 21% 57.2M 36s
115800K .......... .......... .......... .......... .......... 21% 29.5M 36s
115850K .......... .......... .......... .......... .......... 21% 5.10M 36s
115900K .......... .......... .......... .......... .......... 21% 52.6M 36s
115950K .......... .......... .......... .......... .......... 21% 66.0M 36s
116000K .......... .......... .......... .......... .......... 21% 170M 36s
116050K .......... .......... .......... .......... .......... 21% 65.5M 36s
116100K .......... .......... .......... .......... .......... 21% 87.7M 36s
116150K .......... .......... .......... .......... .......... 21% 41.3M 36s
116200K .......... .......... .......... .......... .......... 21% 31.9M 36s
116250K .......... .......... .......... .......... .......... 21% 14.9M 36s
116300K .......... .......... .......... .......... .......... 21% 73.9M 36s
116350K .......... .......... .......... .......... .......... 21% 118M 36s
116400K .......... .......... .......... .......... .......... 21% 28.6M 36s
116450K .......... .......... .......... .......... .......... 21% 54.4M 36s
116500K .......... .......... .......... .......... .......... 21% 64.1M 36s
116550K .......... .......... .......... .......... .......... 21% 54.9M 36s
116600K .......... .......... .......... .......... .......... 21% 76.4M 36s
116650K .......... .......... .......... .......... .......... 21% 86.0M 36s
116700K .......... .......... .......... .......... .......... 21% 42.6M 36s
116750K .......... .......... .......... .......... .......... 21% 108M 36s
116800K .......... .......... .......... .......... .......... 21% 164M 35s
116850K .......... .......... .......... .......... .......... 21% 60.6M 35s
116900K .......... .......... .......... .......... .......... 21% 95.0M 35s
116950K .......... .......... .......... .......... .......... 21% 93.2M 35s
117000K .......... .......... .......... .......... .......... 21% 22.4M 35s
117050K .......... .......... .......... .......... .......... 21% 31.7M 35s
117100K .......... .......... .......... .......... .......... 21% 82.9M 35s
117150K .......... .......... .......... .......... .......... 21% 58.7M 35s
117200K .......... .......... .......... .......... .......... 21% 52.0M 35s
117250K .......... .......... .......... .......... .......... 22% 8.92M 35s
117300K .......... .......... .......... .......... .......... 22% 27.0M 35s
117350K .......... .......... .......... .......... .......... 22% 51.8M 35s
117400K .......... .......... .......... .......... .......... 22% 46.5M 35s
117450K .......... .......... .......... .......... .......... 22% 87.5M 35s
117500K .......... .......... .......... .......... .......... 22% 97.7M 35s
117550K .......... .......... .......... .......... .......... 22% 66.5M 35s
117600K .......... .......... .......... .......... .......... 22% 114M 35s
117650K .......... .......... .......... .......... .......... 22% 31.9M 35s
117700K .......... .......... .......... .......... .......... 22% 7.31M 35s
117750K .......... .......... .......... .......... .......... 22% 2.35M 35s
117800K .......... .......... .......... .......... .......... 22% 52.4M 35s
117850K .......... .......... .......... .......... .......... 22% 56.1M 35s
117900K .......... .......... .......... .......... .......... 22% 88.1M 35s
117950K .......... .......... .......... .......... .......... 22% 91.4M 35s
118000K .......... .......... .......... .......... .......... 22% 69.5M 35s
118050K .......... .......... .......... .......... .......... 22% 24.3M 35s
118100K .......... .......... .......... .......... .......... 22% 52.1M 35s
118150K .......... .......... .......... .......... .......... 22% 64.2M 35s
118200K .......... .......... .......... .......... .......... 22% 25.0M 35s
118250K .......... .......... .......... .......... .......... 22% 97.7M 35s
118300K .......... .......... .......... .......... .......... 22% 109M 35s
118350K .......... .......... .......... .......... .......... 22% 38.9M 35s
118400K .......... .......... .......... .......... .......... 22% 186M 35s
118450K .......... .......... .......... .......... .......... 22% 62.0M 35s
118500K .......... .......... .......... .......... .......... 22% 22.0M 35s
118550K .......... .......... .......... .......... .......... 22% 108M 35s
118600K .......... .......... .......... .......... .......... 22% 137M 35s
118650K .......... .......... .......... .......... .......... 22% 76.1M 35s
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118750K .......... .......... .......... .......... .......... 22% 9.63M 35s
118800K .......... .......... .......... .......... .......... 22% 74.5M 35s
118850K .......... .......... .......... .......... .......... 22% 55.7M 35s
118900K .......... .......... .......... .......... .......... 22% 182M 35s
118950K .......... .......... .......... .......... .......... 22% 93.7M 35s
119000K .......... .......... .......... .......... .......... 22% 113M 35s
119050K .......... .......... .......... .......... .......... 22% 4.47M 35s
119100K .......... .......... .......... .......... .......... 22% 54.2M 35s
119150K .......... .......... .......... .......... .......... 22% 66.5M 35s
119200K .......... .......... .......... .......... .......... 22% 17.8M 35s
119250K .......... .......... .......... .......... .......... 22% 68.2M 35s
119300K .......... .......... .......... .......... .......... 22% 144M 35s
119350K .......... .......... .......... .......... .......... 22% 7.14M 35s
119400K .......... .......... .......... .......... .......... 22% 78.0M 35s
119450K .......... .......... .......... .......... .......... 22% 26.0M 35s
119500K .......... .......... .......... .......... .......... 22% 40.5M 35s
119550K .......... .......... .......... .......... .......... 22% 106M 35s
119600K .......... .......... .......... .......... .......... 22% 7.98M 35s
119650K .......... .......... .......... .......... .......... 22% 18.6M 35s
119700K .......... .......... .......... .......... .......... 22% 140M 35s
119750K .......... .......... .......... .......... .......... 22% 187M 35s
119800K .......... .......... .......... .......... .......... 22% 1.23M 35s
119850K .......... .......... .......... .......... .......... 22% 43.5M 35s
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119950K .......... .......... .......... .......... .......... 22% 79.5M 35s
120000K .......... .......... .......... .......... .......... 22% 45.7M 35s
120050K .......... .......... .......... .......... .......... 22% 5.75M 35s
120100K .......... .......... .......... .......... .......... 22% 36.9M 35s
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120200K .......... .......... .......... .......... .......... 22% 33.3M 35s
120250K .......... .......... .......... .......... .......... 22% 78.0M 35s
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120900K .......... .......... .......... .......... .......... 22% 22.7M 35s
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121000K .......... .......... .......... .......... .......... 22% 162M 35s
121050K .......... .......... .......... .......... .......... 22% 74.2M 35s
121100K .......... .......... .......... .......... .......... 22% 82.5M 34s
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121200K .......... .......... .......... .......... .......... 22% 119M 34s
121250K .......... .......... .......... .......... .......... 22% 92.8M 34s
121300K .......... .......... .......... .......... .......... 22% 23.0M 34s
121350K .......... .......... .......... .......... .......... 22% 93.9M 34s
121400K .......... .......... .......... .......... .......... 22% 74.4M 34s
121450K .......... .......... .......... .......... .......... 22% 71.0M 34s
121500K .......... .......... .......... .......... .......... 22% 198M 34s
121550K .......... .......... .......... .......... .......... 22% 75.0M 34s
121600K .......... .......... .......... .......... .......... 22% 44.4M 34s
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121700K .......... .......... .......... .......... .......... 22% 6.66M 34s
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121800K .......... .......... .......... .......... .......... 22% 118M 34s
121850K .......... .......... .......... .......... .......... 22% 314K 35s
121900K .......... .......... .......... .......... .......... 22% 76.5M 35s
121950K .......... .......... .......... .......... .......... 22% 68.7M 35s
122000K .......... .......... .......... .......... .......... 22% 33.3M 35s
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122100K .......... .......... .......... .......... .......... 22% 81.9M 35s
122150K .......... .......... .......... .......... .......... 22% 159M 35s
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122250K .......... .......... .......... .......... .......... 22% 86.6M 35s
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122400K .......... .......... .......... .......... .......... 22% 71.2M 35s
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122500K .......... .......... .......... .......... .......... 22% 64.9M 35s
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122800K .......... .......... .......... .......... .......... 23% 17.6M 35s
122850K .......... .......... .......... .......... .......... 23% 965K 35s
122900K .......... .......... .......... .......... .......... 23% 19.9M 35s
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123000K .......... .......... .......... .......... .......... 23% 21.5M 35s
123050K .......... .......... .......... .......... .......... 23% 13.1M 35s
123100K .......... .......... .......... .......... .......... 23% 11.1M 35s
123150K .......... .......... .......... .......... .......... 23% 25.4M 35s
123200K .......... .......... .......... .......... .......... 23% 34.6M 35s
123250K .......... .......... .......... .......... .......... 23% 28.0M 35s
123300K .......... .......... .......... .......... .......... 23% 5.70M 35s
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123400K .......... .......... .......... .......... .......... 23% 36.6M 35s
123450K .......... .......... .......... .......... .......... 23% 4.68M 35s
123500K .......... .......... .......... .......... .......... 23% 36.0M 35s
123550K .......... .......... .......... .......... .......... 23% 17.9M 35s
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123700K .......... .......... .......... .......... .......... 23% 97.7M 35s
123750K .......... .......... .......... .......... .......... 23% 219M 35s
123800K .......... .......... .......... .......... .......... 23% 1.02M 35s
123850K .......... .......... .......... .......... .......... 23% 2.58M 35s
123900K .......... .......... .......... .......... .......... 23% 12.6M 35s
123950K .......... .......... .......... .......... .......... 23% 45.1M 35s
124000K .......... .......... .......... .......... .......... 23% 64.7M 35s
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124100K .......... .......... .......... .......... .......... 23% 98.8M 35s
124150K .......... .......... .......... .......... .......... 23% 170M 35s
124200K .......... .......... .......... .......... .......... 23% 52.1M 35s
124250K .......... .......... .......... .......... .......... 23% 80.0M 35s
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124350K .......... .......... .......... .......... .......... 23% 93.4M 35s
124400K .......... .......... .......... .......... .......... 23% 127M 35s
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124600K .......... .......... .......... .......... .......... 23% 96.9M 35s
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124750K .......... .......... .......... .......... .......... 23% 193M 34s
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124850K .......... .......... .......... .......... .......... 23% 24.8M 34s
124900K .......... .......... .......... .......... .......... 23% 7.94M 34s
124950K .......... .......... .......... .......... .......... 23% 39.9M 34s
125000K .......... .......... .......... .......... .......... 23% 96.7M 34s
125050K .......... .......... .......... .......... .......... 23% 92.3M 34s
125100K .......... .......... .......... .......... .......... 23% 102M 34s
125150K .......... .......... .......... .......... .......... 23% 133M 34s
125200K .......... .......... .......... .......... .......... 23% 108M 34s
125250K .......... .......... .......... .......... .......... 23% 27.2M 34s
125300K .......... .......... .......... .......... .......... 23% 108M 34s
125350K .......... .......... .......... .......... .......... 23% 83.0M 34s
125400K .......... .......... .......... .......... .......... 23% 25.8M 34s
125450K .......... .......... .......... .......... .......... 23% 78.3M 34s
125500K .......... .......... .......... .......... .......... 23% 140M 34s
125550K .......... .......... .......... .......... .......... 23% 19.9M 34s
125600K .......... .......... .......... .......... .......... 23% 110M 34s
125650K .......... .......... .......... .......... .......... 23% 17.7M 34s
125700K .......... .......... .......... .......... .......... 23% 36.0M 34s
125750K .......... .......... .......... .......... .......... 23% 162M 34s
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125850K .......... .......... .......... .......... .......... 23% 105M 34s
125900K .......... .......... .......... .......... .......... 23% 3.08M 34s
125950K .......... .......... .......... .......... .......... 23% 4.80M 34s
126000K .......... .......... .......... .......... .......... 23% 67.7M 34s
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126100K .......... .......... .......... .......... .......... 23% 29.1M 34s
126150K .......... .......... .......... .......... .......... 23% 11.5M 34s
126200K .......... .......... .......... .......... .......... 23% 18.2M 34s
126250K .......... .......... .......... .......... .......... 23% 92.1M 34s
126300K .......... .......... .......... .......... .......... 23% 86.1M 34s
126350K .......... .......... .......... .......... .......... 23% 74.9M 34s
126400K .......... .......... .......... .......... .......... 23% 79.8M 34s
126450K .......... .......... .......... .......... .......... 23% 4.41M 34s
126500K .......... .......... .......... .......... .......... 23% 59.3M 34s
126550K .......... .......... .......... .......... .......... 23% 92.0M 34s
126600K .......... .......... .......... .......... .......... 23% 76.9M 34s
126650K .......... .......... .......... .......... .......... 23% 57.9M 34s
126700K .......... .......... .......... .......... .......... 23% 73.0M 34s
126750K .......... .......... .......... .......... .......... 23% 129M 34s
126800K .......... .......... .......... .......... .......... 23% 75.2M 34s
126850K .......... .......... .......... .......... .......... 23% 64.5M 34s
126900K .......... .......... .......... .......... .......... 23% 139M 34s
126950K .......... .......... .......... .......... .......... 23% 103M 34s
127000K .......... .......... .......... .......... .......... 23% 62.5M 34s
127050K .......... .......... .......... .......... .......... 23% 59.5M 34s
127100K .......... .......... .......... .......... .......... 23% 20.7M 34s
127150K .......... .......... .......... .......... .......... 23% 70.6M 34s
127200K .......... .......... .......... .......... .......... 23% 25.8M 34s
127250K .......... .......... .......... .......... .......... 23% 70.5M 34s
127300K .......... .......... .......... .......... .......... 23% 122M 34s
127350K .......... .......... .......... .......... .......... 23% 138M 34s
127400K .......... .......... .......... .......... .......... 23% 67.8M 34s
127450K .......... .......... .......... .......... .......... 23% 40.1M 34s
127500K .......... .......... .......... .......... .......... 23% 50.8M 34s
127550K .......... .......... .......... .......... .......... 23% 39.1M 34s
127600K .......... .......... .......... .......... .......... 23% 20.5M 34s
127650K .......... .......... .......... .......... .......... 23% 179M 34s
127700K .......... .......... .......... .......... .......... 23% 93.7M 34s
127750K .......... .......... .......... .......... .......... 23% 26.2M 34s
127800K .......... .......... .......... .......... .......... 23% 12.1M 34s
127850K .......... .......... .......... .......... .......... 23% 20.6M 34s
127900K .......... .......... .......... .......... .......... 23% 108M 34s
127950K .......... .......... .......... .......... .......... 24% 84.2M 34s
128000K .......... .......... .......... .......... .......... 24% 6.01M 34s
128050K .......... .......... .......... .......... .......... 24% 59.8M 34s
128100K .......... .......... .......... .......... .......... 24% 79.4M 34s
128150K .......... .......... .......... .......... .......... 24% 107M 34s
128200K .......... .......... .......... .......... .......... 24% 81.5M 34s
128250K .......... .......... .......... .......... .......... 24% 89.9M 34s
128300K .......... .......... .......... .......... .......... 24% 80.3M 34s
128350K .......... .......... .......... .......... .......... 24% 69.1M 34s
128400K .......... .......... .......... .......... .......... 24% 14.3M 34s
128450K .......... .......... .......... .......... .......... 24% 47.5M 34s
128500K .......... .......... .......... .......... .......... 24% 67.9M 34s
128550K .......... .......... .......... .......... .......... 24% 131M 34s
128600K .......... .......... .......... .......... .......... 24% 81.9M 34s
128650K .......... .......... .......... .......... .......... 24% 80.2M 34s
128700K .......... .......... .......... .......... .......... 24% 89.9M 34s
128750K .......... .......... .......... .......... .......... 24% 4.51M 34s
128800K .......... .......... .......... .......... .......... 24% 99.9M 34s
128850K .......... .......... .......... .......... .......... 24% 24.2M 33s
128900K .......... .......... .......... .......... .......... 24% 81.2M 33s
128950K .......... .......... .......... .......... .......... 24% 71.0M 33s
129000K .......... .......... .......... .......... .......... 24% 8.49M 33s
129050K .......... .......... .......... .......... .......... 24% 48.1M 33s
129100K .......... .......... .......... .......... .......... 24% 100M 33s
129150K .......... .......... .......... .......... .......... 24% 139M 33s
129200K .......... .......... .......... .......... .......... 24% 106M 33s
129250K .......... .......... .......... .......... .......... 24% 79.9M 33s
129300K .......... .......... .......... .......... .......... 24% 146M 33s
129350K .......... .......... .......... .......... .......... 24% 7.52M 33s
129400K .......... .......... .......... .......... .......... 24% 81.0M 33s
129450K .......... .......... .......... .......... .......... 24% 22.7M 33s
129500K .......... .......... .......... .......... .......... 24% 166M 33s
129550K .......... .......... .......... .......... .......... 24% 171M 33s
129600K .......... .......... .......... .......... .......... 24% 15.4M 33s
129650K .......... .......... .......... .......... .......... 24% 13.1M 33s
129700K .......... .......... .......... .......... .......... 24% 62.3M 33s
129750K .......... .......... .......... .......... .......... 24% 143M 33s
129800K .......... .......... .......... .......... .......... 24% 111M 33s
129850K .......... .......... .......... .......... .......... 24% 88.1M 33s
129900K .......... .......... .......... .......... .......... 24% 152M 33s
129950K .......... .......... .......... .......... .......... 24% 5.76M 33s
130000K .......... .......... .......... .......... .......... 24% 69.9M 33s
130050K .......... .......... .......... .......... .......... 24% 4.63M 33s
130100K .......... .......... .......... .......... .......... 24% 90.6M 33s
130150K .......... .......... .......... .......... .......... 24% 82.9M 33s
130200K .......... .......... .......... .......... .......... 24% 108M 33s
130250K .......... .......... .......... .......... .......... 24% 98.4M 33s
130300K .......... .......... .......... .......... .......... 24% 205M 33s
130350K .......... .......... .......... .......... .......... 24% 206M 33s
130400K .......... .......... .......... .......... .......... 24% 228M 33s
130450K .......... .......... .......... .......... .......... 24% 171M 33s
130500K .......... .......... .......... .......... .......... 24% 121M 33s
130550K .......... .......... .......... .......... .......... 24% 10.1M 33s
130600K .......... .......... .......... .......... .......... 24% 71.8M 33s
130650K .......... .......... .......... .......... .......... 24% 183M 33s
130700K .......... .......... .......... .......... .......... 24% 101M 33s
130750K .......... .......... .......... .......... .......... 24% 12.6M 33s
130800K .......... .......... .......... .......... .......... 24% 134M 33s
130850K .......... .......... .......... .......... .......... 24% 91.4M 33s
130900K .......... .......... .......... .......... .......... 24% 184M 33s
130950K .......... .......... .......... .......... .......... 24% 6.46M 33s
131000K .......... .......... .......... .......... .......... 24% 112M 33s
131050K .......... .......... .......... .......... .......... 24% 88.0M 33s
131100K .......... .......... .......... .......... .......... 24% 72.0M 33s
131150K .......... .......... .......... .......... .......... 24% 19.4M 33s
131200K .......... .......... .......... .......... .......... 24% 169M 33s
131250K .......... .......... .......... .......... .......... 24% 152M 33s
131300K .......... .......... .......... .......... .......... 24% 5.70M 33s
131350K .......... .......... .......... .......... .......... 24% 181M 33s
131400K .......... .......... .......... .......... .......... 24% 144M 33s
131450K .......... .......... .......... .......... .......... 24% 109M 33s
131500K .......... .......... .......... .......... .......... 24% 4.39M 33s
131550K .......... .......... .......... .......... .......... 24% 43.1M 33s
131600K .......... .......... .......... .......... .......... 24% 60.3M 33s
131650K .......... .......... .......... .......... .......... 24% 128M 33s
131700K .......... .......... .......... .......... .......... 24% 178M 33s
131750K .......... .......... .......... .......... .......... 24% 133M 33s
131800K .......... .......... .......... .......... .......... 24% 148M 33s
131850K .......... .......... .......... .......... .......... 24% 156M 33s
131900K .......... .......... .......... .......... .......... 24% 7.73M 33s
131950K .......... .......... .......... .......... .......... 24% 66.6M 33s
132000K .......... .......... .......... .......... .......... 24% 13.5M 33s
132050K .......... .......... .......... .......... .......... 24% 5.81M 33s
132100K .......... .......... .......... .......... .......... 24% 88.8M 33s
132150K .......... .......... .......... .......... .......... 24% 143M 33s
132200K .......... .......... .......... .......... .......... 24% 162M 33s
132250K .......... .......... .......... .......... .......... 24% 19.6M 33s
132300K .......... .......... .......... .......... .......... 24% 197M 33s
132350K .......... .......... .......... .......... .......... 24% 124M 33s
132400K .......... .......... .......... .......... .......... 24% 198M 33s
132450K .......... .......... .......... .......... .......... 24% 220M 33s
132500K .......... .......... .......... .......... .......... 24% 120M 33s
132550K .......... .......... .......... .......... .......... 24% 4.98M 33s
132600K .......... .......... .......... .......... .......... 24% 147M 33s
132650K .......... .......... .......... .......... .......... 24% 186M 33s
132700K .......... .......... .......... .......... .......... 24% 41.0M 33s
132750K .......... .......... .......... .......... .......... 24% 71.4M 33s
132800K .......... .......... .......... .......... .......... 24% 146M 33s
132850K .......... .......... .......... .......... .......... 24% 8.24M 33s
132900K .......... .......... .......... .......... .......... 24% 82.3M 33s
132950K .......... .......... .......... .......... .......... 24% 163M 33s
133000K .......... .......... .......... .......... .......... 24% 143M 33s
133050K .......... .......... .......... .......... .......... 24% 133M 33s
133100K .......... .......... .......... .......... .......... 24% 115M 33s
133150K .......... .......... .......... .......... .......... 24% 5.92M 33s
133200K .......... .......... .......... .......... .......... 24% 73.6M 33s
133250K .......... .......... .......... .......... .......... 25% 150M 33s
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133900K .......... .......... .......... .......... .......... 25% 77.5M 32s
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134000K .......... .......... .......... .......... .......... 25% 108M 32s
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134100K .......... .......... .......... .......... .......... 25% 2.54M 32s
134150K .......... .......... .......... .......... .......... 25% 125M 32s
134200K .......... .......... .......... .......... .......... 25% 65.3M 32s
134250K .......... .......... .......... .......... .......... 25% 126M 32s
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134850K .......... .......... .......... .......... .......... 25% 30.7M 32s
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135000K .......... .......... .......... .......... .......... 25% 194M 32s
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135100K .......... .......... .......... .......... .......... 25% 71.2M 32s
135150K .......... .......... .......... .......... .......... 25% 3.44M 32s
135200K .......... .......... .......... .......... .......... 25% 104M 32s
135250K .......... .......... .......... .......... .......... 25% 121M 32s
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135350K .......... .......... .......... .......... .......... 25% 99.9M 32s
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135700K .......... .......... .......... .......... .......... 25% 6.95M 32s
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135900K .......... .......... .......... .......... .......... 25% 179M 32s
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136000K .......... .......... .......... .......... .......... 25% 64.5M 32s
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136100K .......... .......... .......... .......... .......... 25% 174M 32s
136150K .......... .......... .......... .......... .......... 25% 150M 32s
136200K .......... .......... .......... .......... .......... 25% 174M 32s
136250K .......... .......... .......... .......... .......... 25% 192M 32s
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136950K .......... .......... .......... .......... .......... 25% 6.30M 32s
137000K .......... .......... .......... .......... .......... 25% 73.4M 32s
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137100K .......... .......... .......... .......... .......... 25% 174M 32s
137150K .......... .......... .......... .......... .......... 25% 173M 32s
137200K .......... .......... .......... .......... .......... 25% 4.51M 32s
137250K .......... .......... .......... .......... .......... 25% 7.37M 32s
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137800K .......... .......... .......... .......... .......... 25% 88.9M 32s
137850K .......... .......... .......... .......... .......... 25% 6.41M 32s
137900K .......... .......... .......... .......... .......... 25% 75.6M 32s
137950K .......... .......... .......... .......... .......... 25% 87.2M 32s
138000K .......... .......... .......... .......... .......... 25% 110M 32s
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138100K .......... .......... .......... .......... .......... 25% 61.9M 32s
138150K .......... .......... .......... .......... .......... 25% 101M 31s
138200K .......... .......... .......... .......... .......... 25% 587K 32s
138250K .......... .......... .......... .......... .......... 25% 51.0M 32s
138300K .......... .......... .......... .......... .......... 25% 34.7M 32s
138350K .......... .......... .......... .......... .......... 25% 124M 32s
138400K .......... .......... .......... .......... .......... 25% 81.4M 32s
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138500K .......... .......... .......... .......... .......... 25% 34.0M 32s
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138700K .......... .......... .......... .......... .......... 26% 64.4M 32s
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138850K .......... .......... .......... .......... .......... 26% 139M 32s
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140000K .......... .......... .......... .......... .......... 26% 59.0M 31s
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141700K .......... .......... .......... .......... .......... 26% 91.8M 31s
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141800K .......... .......... .......... .......... .......... 26% 5.05M 31s
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141900K .......... .......... .......... .......... .......... 26% 11.7M 31s
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142000K .......... .......... .......... .......... .......... 26% 82.6M 31s
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142100K .......... .......... .......... .......... .......... 26% 50.4M 31s
142150K .......... .......... .......... .......... .......... 26% 4.21M 31s
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142250K .......... .......... .......... .......... .......... 26% 2.71M 31s
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142500K .......... .......... .......... .......... .......... 26% 19.6M 31s
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142800K .......... .......... .......... .......... .......... 26% 53.1M 31s
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142900K .......... .......... .......... .......... .......... 26% 68.4M 31s
142950K .......... .......... .......... .......... .......... 26% 73.9M 31s
143000K .......... .......... .......... .......... .......... 26% 34.5M 31s
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143100K .......... .......... .......... .......... .......... 26% 39.7M 31s
143150K .......... .......... .......... .......... .......... 26% 19.3M 31s
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143250K .......... .......... .......... .......... .......... 26% 25.1M 31s
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143550K .......... .......... .......... .......... .......... 26% 81.7M 31s
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143900K .......... .......... .......... .......... .......... 26% 92.1M 31s
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145100K .......... .......... .......... .......... .......... 27% 8.85M 30s
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145200K .......... .......... .......... .......... .......... 27% 28.5M 30s
145250K .......... .......... .......... .......... .......... 27% 26.8M 30s
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145850K .......... .......... .......... .......... .......... 27% 76.8M 30s
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146000K .......... .......... .......... .......... .......... 27% 24.0M 30s
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146100K .......... .......... .......... .......... .......... 27% 77.3M 30s
146150K .......... .......... .......... .......... .......... 27% 97.9M 30s
146200K .......... .......... .......... .......... .......... 27% 89.8M 30s
146250K .......... .......... .......... .......... .......... 27% 4.25M 30s
146300K .......... .......... .......... .......... .......... 27% 86.1M 30s
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146400K .......... .......... .......... .......... .......... 27% 22.7M 30s
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146500K .......... .......... .......... .......... .......... 27% 77.6M 30s
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146650K .......... .......... .......... .......... .......... 27% 98.6M 30s
146700K .......... .......... .......... .......... .......... 27% 8.37M 30s
146750K .......... .......... .......... .......... .......... 27% 97.7M 30s
146800K .......... .......... .......... .......... .......... 27% 67.4M 30s
146850K .......... .......... .......... .......... .......... 27% 57.9M 30s
146900K .......... .......... .......... .......... .......... 27% 97.5M 30s
146950K .......... .......... .......... .......... .......... 27% 96.1M 30s
147000K .......... .......... .......... .......... .......... 27% 4.77M 30s
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147250K .......... .......... .......... .......... .......... 27% 93.2M 30s
147300K .......... .......... .......... .......... .......... 27% 144M 30s
147350K .......... .......... .......... .......... .......... 27% 139M 30s
147400K .......... .......... .......... .......... .......... 27% 146M 30s
147450K .......... .......... .......... .......... .......... 27% 67.9M 30s
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148000K .......... .......... .......... .......... .......... 27% 151M 30s
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148100K .......... .......... .......... .......... .......... 27% 72.9M 30s
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148200K .......... .......... .......... .......... .......... 27% 4.93M 30s
148250K .......... .......... .......... .......... .......... 27% 171M 30s
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149250K .......... .......... .......... .......... .......... 28% 56.8M 30s
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150000K .......... .......... .......... .......... .......... 28% 52.9M 30s
150050K .......... .......... .......... .......... .......... 28% 195M 30s
150100K .......... .......... .......... .......... .......... 28% 96.1M 30s
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150250K .......... .......... .......... .......... .......... 28% 22.5M 30s
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150700K .......... .......... .......... .......... .......... 28% 7.97M 30s
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151000K .......... .......... .......... .......... .......... 28% 148M 29s
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151500K .......... .......... .......... .......... .......... 28% 153M 29s
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151600K .......... .......... .......... .......... .......... 28% 7.91M 29s
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151850K .......... .......... .......... .......... .......... 28% 5.24M 29s
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152000K .......... .......... .......... .......... .......... 28% 144M 29s
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152100K .......... .......... .......... .......... .......... 28% 71.1M 29s
152150K .......... .......... .......... .......... .......... 28% 73.0M 29s
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152250K .......... .......... .......... .......... .......... 28% 5.16M 29s
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152500K .......... .......... .......... .......... .......... 28% 3.73M 29s
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153000K .......... .......... .......... .......... .......... 28% 140M 29s
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153150K .......... .......... .......... .......... .......... 28% 6.14M 29s
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153250K .......... .......... .......... .......... .......... 28% 176M 29s
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153900K .......... .......... .......... .......... .......... 28% 81.4M 29s
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154200K .......... .......... .......... .......... .......... 28% 104M 29s
154250K .......... .......... .......... .......... .......... 28% 204M 29s
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154650K .......... .......... .......... .......... .......... 29% 97.1M 29s
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155000K .......... .......... .......... .......... .......... 29% 81.7M 29s
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155150K .......... .......... .......... .......... .......... 29% 126M 29s
155200K .......... .......... .......... .......... .......... 29% 3.21M 29s
155250K .......... .......... .......... .......... .......... 29% 287M 29s
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155650K .......... .......... .......... .......... .......... 29% 99.6M 29s
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156250K .......... .......... .......... .......... .......... 29% 92.8M 29s
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156900K .......... .......... .......... .......... .......... 29% 90.8M 29s
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157250K .......... .......... .......... .......... .......... 29% 11.9M 29s
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157850K .......... .......... .......... .......... .......... 29% 8.89M 29s
157900K .......... .......... .......... .......... .......... 29% 75.9M 29s
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158000K .......... .......... .......... .......... .......... 29% 77.6M 29s
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158100K .......... .......... .......... .......... .......... 29% 149M 29s
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161800K .......... .......... .......... .......... .......... 30% 50.9M 28s
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162050K .......... .......... .......... .......... .......... 30% 235M 28s
162100K .......... .......... .......... .......... .......... 30% 162M 28s
162150K .......... .......... .......... .......... .......... 30% 171M 28s
162200K .......... .......... .......... .......... .......... 30% 195M 28s
162250K .......... .......... .......... .......... .......... 30% 166M 28s
162300K .......... .......... .......... .......... .......... 30% 198M 28s
162350K .......... .......... .......... .......... .......... 30% 159M 28s
162400K .......... .......... .......... .......... .......... 30% 196M 28s
162450K .......... .......... .......... .......... .......... 30% 155M 28s
162500K .......... .......... .......... .......... .......... 30% 210M 28s
162550K .......... .......... .......... .......... .......... 30% 213M 28s
162600K .......... .......... .......... .......... .......... 30% 182M 28s
162650K .......... .......... .......... .......... .......... 30% 218M 28s
162700K .......... .......... .......... .......... .......... 30% 178M 28s
162750K .......... .......... .......... .......... .......... 30% 15.2M 28s
162800K .......... .......... .......... .......... .......... 30% 43.7M 28s
162850K .......... .......... .......... .......... .......... 30% 102M 28s
162900K .......... .......... .......... .......... .......... 30% 126M 28s
162950K .......... .......... .......... .......... .......... 30% 140M 28s
163000K .......... .......... .......... .......... .......... 30% 7.94M 28s
163050K .......... .......... .......... .......... .......... 30% 191M 28s
163100K .......... .......... .......... .......... .......... 30% 146M 28s
163150K .......... .......... .......... .......... .......... 30% 7.97M 28s
163200K .......... .......... .......... .......... .......... 30% 66.3M 28s
163250K .......... .......... .......... .......... .......... 30% 154M 28s
163300K .......... .......... .......... .......... .......... 30% 150M 28s
163350K .......... .......... .......... .......... .......... 30% 170M 28s
163400K .......... .......... .......... .......... .......... 30% 5.30M 28s
163450K .......... .......... .......... .......... .......... 30% 166M 28s
163500K .......... .......... .......... .......... .......... 30% 147M 28s
163550K .......... .......... .......... .......... .......... 30% 190M 28s
163600K .......... .......... .......... .......... .......... 30% 168M 28s
163650K .......... .......... .......... .......... .......... 30% 169M 28s
163700K .......... .......... .......... .......... .......... 30% 4.54M 28s
163750K .......... .......... .......... .......... .......... 30% 142M 28s
163800K .......... .......... .......... .......... .......... 30% 122M 28s
163850K .......... .......... .......... .......... .......... 30% 128M 28s
163900K .......... .......... .......... .......... .......... 30% 195M 28s
163950K .......... .......... .......... .......... .......... 30% 5.96M 28s
164000K .......... .......... .......... .......... .......... 30% 40.5M 28s
164050K .......... .......... .......... .......... .......... 30% 90.8M 28s
164100K .......... .......... .......... .......... .......... 30% 56.1M 28s
164150K .......... .......... .......... .......... .......... 30% 84.6M 28s
164200K .......... .......... .......... .......... .......... 30% 94.8M 28s
164250K .......... .......... .......... .......... .......... 30% 126M 28s
164300K .......... .......... .......... .......... .......... 30% 181M 28s
164350K .......... .......... .......... .......... .......... 30% 5.05M 28s
164400K .......... .......... .......... .......... .......... 30% 30.5M 28s
164450K .......... .......... .......... .......... .......... 30% 92.7M 28s
164500K .......... .......... .......... .......... .......... 30% 121M 27s
164550K .......... .......... .......... .......... .......... 30% 167M 27s
164600K .......... .......... .......... .......... .......... 30% 165M 27s
164650K .......... .......... .......... .......... .......... 30% 11.2M 27s
164700K .......... .......... .......... .......... .......... 30% 13.2M 27s
164750K .......... .......... .......... .......... .......... 30% 28.8M 27s
164800K .......... .......... .......... .......... .......... 30% 43.6M 27s
164850K .......... .......... .......... .......... .......... 30% 4.46M 27s
164900K .......... .......... .......... .......... .......... 30% 4.73M 27s
164950K .......... .......... .......... .......... .......... 30% 7.97M 27s
165000K .......... .......... .......... .......... .......... 30% 6.14M 27s
165050K .......... .......... .......... .......... .......... 30% 20.1M 27s
165100K .......... .......... .......... .......... .......... 30% 21.1M 27s
165150K .......... .......... .......... .......... .......... 30% 5.77M 27s
165200K .......... .......... .......... .......... .......... 30% 13.7M 27s
165250K .......... .......... .......... .......... .......... 31% 174M 27s
165300K .......... .......... .......... .......... .......... 31% 195M 27s
165350K .......... .......... .......... .......... .......... 31% 110M 27s
165400K .......... .......... .......... .......... .......... 31% 22.8M 27s
165450K .......... .......... .......... .......... .......... 31% 3.50M 27s
165500K .......... .......... .......... .......... .......... 31% 122M 27s
165550K .......... .......... .......... .......... .......... 31% 23.1M 27s
165600K .......... .......... .......... .......... .......... 31% 27.1M 27s
165650K .......... .......... .......... .......... .......... 31% 15.8M 27s
165700K .......... .......... .......... .......... .......... 31% 16.4M 27s
165750K .......... .......... .......... .......... .......... 31% 68.5M 27s
165800K .......... .......... .......... .......... .......... 31% 51.6M 27s
165850K .......... .......... .......... .......... .......... 31% 52.4M 27s
165900K .......... .......... .......... .......... .......... 31% 148M 27s
165950K .......... .......... .......... .......... .......... 31% 154M 27s
166000K .......... .......... .......... .......... .......... 31% 214M 27s
166050K .......... .......... .......... .......... .......... 31% 176M 27s
166100K .......... .......... .......... .......... .......... 31% 137M 27s
166150K .......... .......... .......... .......... .......... 31% 184M 27s
166200K .......... .......... .......... .......... .......... 31% 130M 27s
166250K .......... .......... .......... .......... .......... 31% 158M 27s
166300K .......... .......... .......... .......... .......... 31% 205M 27s
166350K .......... .......... .......... .......... .......... 31% 150M 27s
166400K .......... .......... .......... .......... .......... 31% 166M 27s
166450K .......... .......... .......... .......... .......... 31% 7.28M 27s
166500K .......... .......... .......... .......... .......... 31% 137M 27s
166550K .......... .......... .......... .......... .......... 31% 25.1M 27s
166600K .......... .......... .......... .......... .......... 31% 19.4M 27s
166650K .......... .......... .......... .......... .......... 31% 125M 27s
166700K .......... .......... .......... .......... .......... 31% 143M 27s
166750K .......... .......... .......... .......... .......... 31% 140M 27s
166800K .......... .......... .......... .......... .......... 31% 122M 27s
166850K .......... .......... .......... .......... .......... 31% 137M 27s
166900K .......... .......... .......... .......... .......... 31% 136M 27s
166950K .......... .......... .......... .......... .......... 31% 12.4M 27s
167000K .......... .......... .......... .......... .......... 31% 24.5M 27s
167050K .......... .......... .......... .......... .......... 31% 26.5M 27s
167100K .......... .......... .......... .......... .......... 31% 68.0M 27s
167150K .......... .......... .......... .......... .......... 31% 27.7M 27s
167200K .......... .......... .......... .......... .......... 31% 116M 27s
167250K .......... .......... .......... .......... .......... 31% 124M 27s
167300K .......... .......... .......... .......... .......... 31% 13.9M 27s
167350K .......... .......... .......... .......... .......... 31% 26.3M 27s
167400K .......... .......... .......... .......... .......... 31% 132M 27s
167450K .......... .......... .......... .......... .......... 31% 96.3M 27s
167500K .......... .......... .......... .......... .......... 31% 171M 27s
167550K .......... .......... .......... .......... .......... 31% 231M 27s
167600K .......... .......... .......... .......... .......... 31% 5.82M 27s
167650K .......... .......... .......... .......... .......... 31% 143M 27s
167700K .......... .......... .......... .......... .......... 31% 146M 27s
167750K .......... .......... .......... .......... .......... 31% 189M 27s
167800K .......... .......... .......... .......... .......... 31% 170M 27s
167850K .......... .......... .......... .......... .......... 31% 161M 27s
167900K .......... .......... .......... .......... .......... 31% 285K 27s
167950K .......... .......... .......... .......... .......... 31% 69.0M 27s
168000K .......... .......... .......... .......... .......... 31% 121M 27s
168050K .......... .......... .......... .......... .......... 31% 75.0M 27s
168100K .......... .......... .......... .......... .......... 31% 93.5M 27s
168150K .......... .......... .......... .......... .......... 31% 92.5M 27s
168200K .......... .......... .......... .......... .......... 31% 86.4M 27s
168250K .......... .......... .......... .......... .......... 31% 39.2M 27s
168300K .......... .......... .......... .......... .......... 31% 129M 27s
168350K .......... .......... .......... .......... .......... 31% 119M 27s
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168550K .......... .......... .......... .......... .......... 31% 113M 27s
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168650K .......... .......... .......... .......... .......... 31% 15.3M 27s
168700K .......... .......... .......... .......... .......... 31% 134M 27s
168750K .......... .......... .......... .......... .......... 31% 203M 27s
168800K .......... .......... .......... .......... .......... 31% 213M 27s
168850K .......... .......... .......... .......... .......... 31% 154M 27s
168900K .......... .......... .......... .......... .......... 31% 203M 27s
168950K .......... .......... .......... .......... .......... 31% 752K 27s
169000K .......... .......... .......... .......... .......... 31% 61.3M 27s
169050K .......... .......... .......... .......... .......... 31% 92.5M 27s
169100K .......... .......... .......... .......... .......... 31% 121M 27s
169150K .......... .......... .......... .......... .......... 31% 18.6M 27s
169200K .......... .......... .......... .......... .......... 31% 57.8M 27s
169250K .......... .......... .......... .......... .......... 31% 78.1M 27s
169300K .......... .......... .......... .......... .......... 31% 127M 27s
169350K .......... .......... .......... .......... .......... 31% 105M 27s
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169450K .......... .......... .......... .......... .......... 31% 141M 27s
169500K .......... .......... .......... .......... .......... 31% 160M 27s
169550K .......... .......... .......... .......... .......... 31% 121M 27s
169600K .......... .......... .......... .......... .......... 31% 26.2M 27s
169650K .......... .......... .......... .......... .......... 31% 174M 27s
169700K .......... .......... .......... .......... .......... 31% 90.1M 27s
169750K .......... .......... .......... .......... .......... 31% 86.6M 27s
169800K .......... .......... .......... .......... .......... 31% 105M 27s
169850K .......... .......... .......... .......... .......... 31% 98.2M 27s
169900K .......... .......... .......... .......... .......... 31% 195M 27s
169950K .......... .......... .......... .......... .......... 31% 9.40M 27s
170000K .......... .......... .......... .......... .......... 31% 93.4M 27s
170050K .......... .......... .......... .......... .......... 31% 153M 27s
170100K .......... .......... .......... .......... .......... 31% 146M 27s
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170200K .......... .......... .......... .......... .......... 31% 142M 27s
170250K .......... .......... .......... .......... .......... 31% 138M 27s
170300K .......... .......... .......... .......... .......... 31% 188M 27s
170350K .......... .......... .......... .......... .......... 31% 94.6M 27s
170400K .......... .......... .......... .......... .......... 31% 20.2M 27s
170450K .......... .......... .......... .......... .......... 31% 10.0M 27s
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170550K .......... .......... .......... .......... .......... 31% 213M 27s
170600K .......... .......... .......... .......... .......... 32% 2.93M 27s
170650K .......... .......... .......... .......... .......... 32% 56.1M 27s
170700K .......... .......... .......... .......... .......... 32% 55.9M 27s
170750K .......... .......... .......... .......... .......... 32% 59.5M 27s
170800K .......... .......... .......... .......... .......... 32% 72.9M 27s
170850K .......... .......... .......... .......... .......... 32% 23.8M 27s
170900K .......... .......... .......... .......... .......... 32% 13.4M 27s
170950K .......... .......... .......... .......... .......... 32% 177M 27s
171000K .......... .......... .......... .......... .......... 32% 3.52M 27s
171050K .......... .......... .......... .......... .......... 32% 120M 27s
171100K .......... .......... .......... .......... .......... 32% 95.9M 27s
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171200K .......... .......... .......... .......... .......... 32% 140M 27s
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171450K .......... .......... .......... .......... .......... 32% 175M 27s
171500K .......... .......... .......... .......... .......... 32% 163M 27s
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171600K .......... .......... .......... .......... .......... 32% 138M 27s
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171700K .......... .......... .......... .......... .......... 32% 53.7M 27s
171750K .......... .......... .......... .......... .......... 32% 174M 27s
171800K .......... .......... .......... .......... .......... 32% 9.09M 27s
171850K .......... .......... .......... .......... .......... 32% 98.8M 27s
171900K .......... .......... .......... .......... .......... 32% 138M 27s
171950K .......... .......... .......... .......... .......... 32% 31.1M 27s
172000K .......... .......... .......... .......... .......... 32% 2.53M 27s
172050K .......... .......... .......... .......... .......... 32% 3.36M 27s
172100K .......... .......... .......... .......... .......... 32% 78.8M 27s
172150K .......... .......... .......... .......... .......... 32% 101M 27s
172200K .......... .......... .......... .......... .......... 32% 90.3M 27s
172250K .......... .......... .......... .......... .......... 32% 141M 27s
172300K .......... .......... .......... .......... .......... 32% 152M 27s
172350K .......... .......... .......... .......... .......... 32% 171M 27s
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172500K .......... .......... .......... .......... .......... 32% 172M 27s
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172750K .......... .......... .......... .......... .......... 32% 169M 27s
172800K .......... .......... .......... .......... .......... 32% 236M 27s
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172900K .......... .......... .......... .......... .......... 32% 261M 27s
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173000K .......... .......... .......... .......... .......... 32% 1.45M 27s
173050K .......... .......... .......... .......... .......... 32% 3.05M 27s
173100K .......... .......... .......... .......... .......... 32% 16.8M 27s
173150K .......... .......... .......... .......... .......... 32% 141M 27s
173200K .......... .......... .......... .......... .......... 32% 13.8M 27s
173250K .......... .......... .......... .......... .......... 32% 115M 27s
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173450K .......... .......... .......... .......... .......... 32% 26.4M 27s
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173750K .......... .......... .......... .......... .......... 32% 150M 27s
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173850K .......... .......... .......... .......... .......... 32% 122M 27s
173900K .......... .......... .......... .......... .......... 32% 168M 27s
173950K .......... .......... .......... .......... .......... 32% 27.1M 27s
174000K .......... .......... .......... .......... .......... 32% 126M 27s
174050K .......... .......... .......... .......... .......... 32% 4.36M 27s
174100K .......... .......... .......... .......... .......... 32% 78.6M 27s
174150K .......... .......... .......... .......... .......... 32% 33.3M 27s
174200K .......... .......... .......... .......... .......... 32% 51.4M 27s
174250K .......... .......... .......... .......... .......... 32% 28.4M 26s
174300K .......... .......... .......... .......... .......... 32% 166M 26s
174350K .......... .......... .......... .......... .......... 32% 13.2M 26s
174400K .......... .......... .......... .......... .......... 32% 186M 26s
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174550K .......... .......... .......... .......... .......... 32% 274M 26s
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174650K .......... .......... .......... .......... .......... 32% 243M 26s
174700K .......... .......... .......... .......... .......... 32% 28.1M 26s
174750K .......... .......... .......... .......... .......... 32% 134M 26s
174800K .......... .......... .......... .......... .......... 32% 8.53M 26s
174850K .......... .......... .......... .......... .......... 32% 74.3M 26s
174900K .......... .......... .......... .......... .......... 32% 148M 26s
174950K .......... .......... .......... .......... .......... 32% 166M 26s
175000K .......... .......... .......... .......... .......... 32% 194M 26s
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175100K .......... .......... .......... .......... .......... 32% 15.1M 26s
175150K .......... .......... .......... .......... .......... 32% 213M 26s
175200K .......... .......... .......... .......... .......... 32% 136M 26s
175250K .......... .......... .......... .......... .......... 32% 260M 26s
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175350K .......... .......... .......... .......... .......... 32% 95.7M 26s
175400K .......... .......... .......... .......... .......... 32% 8.29M 26s
175450K .......... .......... .......... .......... .......... 32% 118M 26s
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175600K .......... .......... .......... .......... .......... 32% 15.9M 26s
175650K .......... .......... .......... .......... .......... 32% 178M 26s
175700K .......... .......... .......... .......... .......... 32% 6.26M 26s
175750K .......... .......... .......... .......... .......... 32% 165M 26s
175800K .......... .......... .......... .......... .......... 32% 124M 26s
175850K .......... .......... .......... .......... .......... 32% 147M 26s
175900K .......... .......... .......... .......... .......... 33% 30.0M 26s
175950K .......... .......... .......... .......... .......... 33% 6.55M 26s
176000K .......... .......... .......... .......... .......... 33% 180M 26s
176050K .......... .......... .......... .......... .......... 33% 145M 26s
176100K .......... .......... .......... .......... .......... 33% 570K 26s
176150K .......... .......... .......... .......... .......... 33% 124M 26s
176200K .......... .......... .......... .......... .......... 33% 63.0M 26s
176250K .......... .......... .......... .......... .......... 33% 172M 26s
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176450K .......... .......... .......... .......... .......... 33% 25.8M 26s
176500K .......... .......... .......... .......... .......... 33% 117M 26s
176550K .......... .......... .......... .......... .......... 33% 27.4M 26s
176600K .......... .......... .......... .......... .......... 33% 96.5M 26s
176650K .......... .......... .......... .......... .......... 33% 103M 26s
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176750K .......... .......... .......... .......... .......... 33% 126M 26s
176800K .......... .......... .......... .......... .......... 33% 133M 26s
176850K .......... .......... .......... .......... .......... 33% 145M 26s
176900K .......... .......... .......... .......... .......... 33% 160M 26s
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177000K .......... .......... .......... .......... .......... 33% 189M 26s
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177100K .......... .......... .......... .......... .......... 33% 196M 26s
177150K .......... .......... .......... .......... .......... 33% 123M 26s
177200K .......... .......... .......... .......... .......... 33% 29.0M 26s
177250K .......... .......... .......... .......... .......... 33% 182M 26s
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178250K .......... .......... .......... .......... .......... 33% 81.4M 26s
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191600K .......... .......... .......... .......... .......... 35% 162M 25s
191650K .......... .......... .......... .......... .......... 35% 126M 25s
191700K .......... .......... .......... .......... .......... 35% 108M 25s
191750K .......... .......... .......... .......... .......... 35% 157M 25s
191800K .......... .......... .......... .......... .......... 35% 124M 25s
191850K .......... .......... .......... .......... .......... 35% 37.9M 25s
191900K .......... .......... .......... .......... .......... 36% 159M 25s
191950K .......... .......... .......... .......... .......... 36% 171M 25s
192000K .......... .......... .......... .......... .......... 36% 207M 25s
192050K .......... .......... .......... .......... .......... 36% 110M 25s
192100K .......... .......... .......... .......... .......... 36% 114M 25s
192150K .......... .......... .......... .......... .......... 36% 133M 25s
192200K .......... .......... .......... .......... .......... 36% 127M 25s
192250K .......... .......... .......... .......... .......... 36% 195M 25s
192300K .......... .......... .......... .......... .......... 36% 209M 25s
192350K .......... .......... .......... .......... .......... 36% 154M 25s
192400K .......... .......... .......... .......... .......... 36% 148M 25s
192450K .......... .......... .......... .......... .......... 36% 151M 25s
192500K .......... .......... .......... .......... .......... 36% 160M 25s
192550K .......... .......... .......... .......... .......... 36% 131M 25s
192600K .......... .......... .......... .......... .......... 36% 99.0M 25s
192650K .......... .......... .......... .......... .......... 36% 205M 25s
192700K .......... .......... .......... .......... .......... 36% 13.0M 25s
192750K .......... .......... .......... .......... .......... 36% 131M 25s
192800K .......... .......... .......... .......... .......... 36% 91.3M 25s
192850K .......... .......... .......... .......... .......... 36% 112M 25s
192900K .......... .......... .......... .......... .......... 36% 106M 25s
192950K .......... .......... .......... .......... .......... 36% 100M 25s
193000K .......... .......... .......... .......... .......... 36% 5.23M 25s
193050K .......... .......... .......... .......... .......... 36% 101M 25s
193100K .......... .......... .......... .......... .......... 36% 97.9M 25s
193150K .......... .......... .......... .......... .......... 36% 148M 25s
193200K .......... .......... .......... .......... .......... 36% 111M 25s
193250K .......... .......... .......... .......... .......... 36% 132M 25s
193300K .......... .......... .......... .......... .......... 36% 6.62M 25s
193350K .......... .......... .......... .......... .......... 36% 79.8M 25s
193400K .......... .......... .......... .......... .......... 36% 116M 25s
193450K .......... .......... .......... .......... .......... 36% 81.5M 25s
193500K .......... .......... .......... .......... .......... 36% 822K 25s
193550K .......... .......... .......... .......... .......... 36% 108M 25s
193600K .......... .......... .......... .......... .......... 36% 78.5M 25s
193650K .......... .......... .......... .......... .......... 36% 62.1M 25s
193700K .......... .......... .......... .......... .......... 36% 23.7M 25s
193750K .......... .......... .......... .......... .......... 36% 111M 25s
193800K .......... .......... .......... .......... .......... 36% 181M 25s
193850K .......... .......... .......... .......... .......... 36% 163M 25s
193900K .......... .......... .......... .......... .......... 36% 51.5M 25s
193950K .......... .......... .......... .......... .......... 36% 95.9M 25s
194000K .......... .......... .......... .......... .......... 36% 89.9M 25s
194050K .......... .......... .......... .......... .......... 36% 190M 25s
194100K .......... .......... .......... .......... .......... 36% 177M 24s
194150K .......... .......... .......... .......... .......... 36% 183M 24s
194200K .......... .......... .......... .......... .......... 36% 173M 24s
194250K .......... .......... .......... .......... .......... 36% 195M 24s
194300K .......... .......... .......... .......... .......... 36% 204M 24s
194350K .......... .......... .......... .......... .......... 36% 185M 24s
194400K .......... .......... .......... .......... .......... 36% 210M 24s
194450K .......... .......... .......... .......... .......... 36% 167M 24s
194500K .......... .......... .......... .......... .......... 36% 203M 24s
194550K .......... .......... .......... .......... .......... 36% 158M 24s
194600K .......... .......... .......... .......... .......... 36% 180M 24s
194650K .......... .......... .......... .......... .......... 36% 173M 24s
194700K .......... .......... .......... .......... .......... 36% 167M 24s
194750K .......... .......... .......... .......... .......... 36% 6.19M 24s
194800K .......... .......... .......... .......... .......... 36% 191M 24s
194850K .......... .......... .......... .......... .......... 36% 139M 24s
194900K .......... .......... .......... .......... .......... 36% 205M 24s
194950K .......... .......... .......... .......... .......... 36% 159M 24s
195000K .......... .......... .......... .......... .......... 36% 186M 24s
195050K .......... .......... .......... .......... .......... 36% 5.08M 24s
195100K .......... .......... .......... .......... .......... 36% 5.03M 24s
195150K .......... .......... .......... .......... .......... 36% 28.6M 24s
195200K .......... .......... .......... .......... .......... 36% 105M 24s
195250K .......... .......... .......... .......... .......... 36% 169M 24s
195300K .......... .......... .......... .......... .......... 36% 220M 24s
195350K .......... .......... .......... .......... .......... 36% 205M 24s
195400K .......... .......... .......... .......... .......... 36% 178M 24s
195450K .......... .......... .......... .......... .......... 36% 155M 24s
195500K .......... .......... .......... .......... .......... 36% 168M 24s
195550K .......... .......... .......... .......... .......... 36% 105M 24s
195600K .......... .......... .......... .......... .......... 36% 6.96M 24s
195650K .......... .......... .......... .......... .......... 36% 124M 24s
195700K .......... .......... .......... .......... .......... 36% 115M 24s
195750K .......... .......... .......... .......... .......... 36% 156M 24s
195800K .......... .......... .......... .......... .......... 36% 95.2M 24s
195850K .......... .......... .......... .......... .......... 36% 146M 24s
195900K .......... .......... .......... .......... .......... 36% 4.04M 24s
195950K .......... .......... .......... .......... .......... 36% 178M 24s
196000K .......... .......... .......... .......... .......... 36% 198M 24s
196050K .......... .......... .......... .......... .......... 36% 133M 24s
196100K .......... .......... .......... .......... .......... 36% 120M 24s
196150K .......... .......... .......... .......... .......... 36% 139M 24s
196200K .......... .......... .......... .......... .......... 36% 7.43M 24s
196250K .......... .......... .......... .......... .......... 36% 94.1M 24s
196300K .......... .......... .......... .......... .......... 36% 145M 24s
196350K .......... .......... .......... .......... .......... 36% 174M 24s
196400K .......... .......... .......... .......... .......... 36% 258M 24s
196450K .......... .......... .......... .......... .......... 36% 172M 24s
196500K .......... .......... .......... .......... .......... 36% 4.68M 24s
196550K .......... .......... .......... .......... .......... 36% 189M 24s
196600K .......... .......... .......... .......... .......... 36% 2.34M 24s
196650K .......... .......... .......... .......... .......... 36% 68.4M 24s
196700K .......... .......... .......... .......... .......... 36% 86.9M 24s
196750K .......... .......... .......... .......... .......... 36% 88.3M 24s
196800K .......... .......... .......... .......... .......... 36% 155M 24s
196850K .......... .......... .......... .......... .......... 36% 159M 24s
196900K .......... .......... .......... .......... .......... 36% 191M 24s
196950K .......... .......... .......... .......... .......... 36% 154M 24s
197000K .......... .......... .......... .......... .......... 36% 150M 24s
197050K .......... .......... .......... .......... .......... 36% 7.30M 24s
197100K .......... .......... .......... .......... .......... 36% 80.0M 24s
197150K .......... .......... .......... .......... .......... 36% 152M 24s
197200K .......... .......... .......... .......... .......... 36% 142M 24s
197250K .......... .......... .......... .......... .......... 37% 164M 24s
197300K .......... .......... .......... .......... .......... 37% 184M 24s
197350K .......... .......... .......... .......... .......... 37% 7.06M 24s
197400K .......... .......... .......... .......... .......... 37% 108M 24s
197450K .......... .......... .......... .......... .......... 37% 144M 24s
197500K .......... .......... .......... .......... .......... 37% 132M 24s
197550K .......... .......... .......... .......... .......... 37% 186M 24s
197600K .......... .......... .......... .......... .......... 37% 590K 24s
197650K .......... .......... .......... .......... .......... 37% 141M 24s
197700K .......... .......... .......... .......... .......... 37% 82.3M 24s
197750K .......... .......... .......... .......... .......... 37% 127M 24s
197800K .......... .......... .......... .......... .......... 37% 28.4M 24s
197850K .......... .......... .......... .......... .......... 37% 87.5M 24s
197900K .......... .......... .......... .......... .......... 37% 82.5M 24s
197950K .......... .......... .......... .......... .......... 37% 73.8M 24s
198000K .......... .......... .......... .......... .......... 37% 105M 24s
198050K .......... .......... .......... .......... .......... 37% 66.3M 24s
198100K .......... .......... .......... .......... .......... 37% 135M 24s
198150K .......... .......... .......... .......... .......... 37% 133M 24s
198200K .......... .......... .......... .......... .......... 37% 97.7M 24s
198250K .......... .......... .......... .......... .......... 37% 114M 24s
198300K .......... .......... .......... .......... .......... 37% 98.4M 24s
198350K .......... .......... .......... .......... .......... 37% 168M 24s
198400K .......... .......... .......... .......... .......... 37% 211M 24s
198450K .......... .......... .......... .......... .......... 37% 191M 24s
198500K .......... .......... .......... .......... .......... 37% 173M 24s
198550K .......... .......... .......... .......... .......... 37% 197M 24s
198600K .......... .......... .......... .......... .......... 37% 186M 24s
198650K .......... .......... .......... .......... .......... 37% 559K 24s
198700K .......... .......... .......... .......... .......... 37% 95.6M 24s
198750K .......... .......... .......... .......... .......... 37% 51.3M 24s
198800K .......... .......... .......... .......... .......... 37% 81.5M 24s
198850K .......... .......... .......... .......... .......... 37% 54.1M 24s
198900K .......... .......... .......... .......... .......... 37% 119M 24s
198950K .......... .......... .......... .......... .......... 37% 117M 24s
199000K .......... .......... .......... .......... .......... 37% 114M 24s
199050K .......... .......... .......... .......... .......... 37% 143M 24s
199100K .......... .......... .......... .......... .......... 37% 193M 24s
199150K .......... .......... .......... .......... .......... 37% 221M 24s
199200K .......... .......... .......... .......... .......... 37% 180M 24s
199250K .......... .......... .......... .......... .......... 37% 221M 24s
199300K .......... .......... .......... .......... .......... 37% 253M 24s
199350K .......... .......... .......... .......... .......... 37% 181M 24s
199400K .......... .......... .......... .......... .......... 37% 196M 24s
199450K .......... .......... .......... .......... .......... 37% 181M 24s
199500K .......... .......... .......... .......... .......... 37% 212M 24s
199550K .......... .......... .......... .......... .......... 37% 190M 24s
199600K .......... .......... .......... .......... .......... 37% 191M 24s
199650K .......... .......... .......... .......... .......... 37% 2.61M 24s
199700K .......... .......... .......... .......... .......... 37% 84.2M 24s
199750K .......... .......... .......... .......... .......... 37% 180M 24s
199800K .......... .......... .......... .......... .......... 37% 222M 24s
199850K .......... .......... .......... .......... .......... 37% 193M 24s
199900K .......... .......... .......... .......... .......... 37% 221M 24s
199950K .......... .......... .......... .......... .......... 37% 183M 24s
200000K .......... .......... .......... .......... .......... 37% 223M 24s
200050K .......... .......... .......... .......... .......... 37% 227M 24s
200100K .......... .......... .......... .......... .......... 37% 194M 24s
200150K .......... .......... .......... .......... .......... 37% 218M 24s
200200K .......... .......... .......... .......... .......... 37% 194M 24s
200250K .......... .......... .......... .......... .......... 37% 199M 24s
200300K .......... .......... .......... .......... .......... 37% 210M 24s
200350K .......... .......... .......... .......... .......... 37% 192M 24s
200400K .......... .......... .......... .......... .......... 37% 8.86M 24s
200450K .......... .......... .......... .......... .......... 37% 143M 24s
200500K .......... .......... .......... .......... .......... 37% 186M 24s
200550K .......... .......... .......... .......... .......... 37% 120M 24s
200600K .......... .......... .......... .......... .......... 37% 86.4M 24s
200650K .......... .......... .......... .......... .......... 37% 156M 24s
200700K .......... .......... .......... .......... .......... 37% 1.65M 24s
200750K .......... .......... .......... .......... .......... 37% 117M 24s
200800K .......... .......... .......... .......... .......... 37% 159M 24s
200850K .......... .......... .......... .......... .......... 37% 119M 24s
200900K .......... .......... .......... .......... .......... 37% 158M 24s
200950K .......... .......... .......... .......... .......... 37% 144M 24s
201000K .......... .......... .......... .......... .......... 37% 101M 24s
201050K .......... .......... .......... .......... .......... 37% 153M 24s
201100K .......... .......... .......... .......... .......... 37% 203M 24s
201150K .......... .......... .......... .......... .......... 37% 211M 24s
201200K .......... .......... .......... .......... .......... 37% 159M 24s
201250K .......... .......... .......... .......... .......... 37% 182M 24s
201300K .......... .......... .......... .......... .......... 37% 193M 24s
201350K .......... .......... .......... .......... .......... 37% 188M 24s
201400K .......... .......... .......... .......... .......... 37% 214M 24s
201450K .......... .......... .......... .......... .......... 37% 187M 24s
201500K .......... .......... .......... .......... .......... 37% 209M 24s
201550K .......... .......... .......... .......... .......... 37% 228M 24s
201600K .......... .......... .......... .......... .......... 37% 189M 24s
201650K .......... .......... .......... .......... .......... 37% 225M 24s
201700K .......... .......... .......... .......... .......... 37% 89.9M 24s
201750K .......... .......... .......... .......... .......... 37% 119M 24s
201800K .......... .......... .......... .......... .......... 37% 202M 24s
201850K .......... .......... .......... .......... .......... 37% 86.6M 24s
201900K .......... .......... .......... .......... .......... 37% 176M 24s
201950K .......... .......... .......... .......... .......... 37% 173M 24s
202000K .......... .......... .......... .......... .......... 37% 197M 24s
202050K .......... .......... .......... .......... .......... 37% 205M 24s
202100K .......... .......... .......... .......... .......... 37% 13.7M 24s
202150K .......... .......... .......... .......... .......... 37% 198M 24s
202200K .......... .......... .......... .......... .......... 37% 6.33M 24s
202250K .......... .......... .......... .......... .......... 37% 78.3M 24s
202300K .......... .......... .......... .......... .......... 37% 211M 24s
202350K .......... .......... .......... .......... .......... 37% 187M 24s
202400K .......... .......... .......... .......... .......... 37% 216M 24s
202450K .......... .......... .......... .......... .......... 37% 21.0M 24s
202500K .......... .......... .......... .......... .......... 37% 109M 24s
202550K .......... .......... .......... .......... .......... 37% 7.08M 24s
202600K .......... .......... .......... .......... .......... 38% 176M 24s
202650K .......... .......... .......... .......... .......... 38% 193M 24s
202700K .......... .......... .......... .......... .......... 38% 164M 24s
202750K .......... .......... .......... .......... .......... 38% 633K 24s
202800K .......... .......... .......... .......... .......... 38% 93.0M 24s
202850K .......... .......... .......... .......... .......... 38% 124M 24s
202900K .......... .......... .......... .......... .......... 38% 42.4M 24s
202950K .......... .......... .......... .......... .......... 38% 126M 24s
203000K .......... .......... .......... .......... .......... 38% 62.8M 24s
203050K .......... .......... .......... .......... .......... 38% 133M 24s
203100K .......... .......... .......... .......... .......... 38% 113M 24s
203150K .......... .......... .......... .......... .......... 38% 104M 24s
203200K .......... .......... .......... .......... .......... 38% 119M 24s
203250K .......... .......... .......... .......... .......... 38% 111M 24s
203300K .......... .......... .......... .......... .......... 38% 169M 24s
203350K .......... .......... .......... .......... .......... 38% 87.0M 24s
203400K .......... .......... .......... .......... .......... 38% 158M 24s
203450K .......... .......... .......... .......... .......... 38% 104M 24s
203500K .......... .......... .......... .......... .......... 38% 152M 24s
203550K .......... .......... .......... .......... .......... 38% 152M 23s
203600K .......... .......... .......... .......... .......... 38% 137M 23s
203650K .......... .......... .......... .......... .......... 38% 167M 23s
203700K .......... .......... .......... .......... .......... 38% 149M 23s
203750K .......... .......... .......... .......... .......... 38% 5.45M 23s
203800K .......... .......... .......... .......... .......... 38% 208M 23s
203850K .......... .......... .......... .......... .......... 38% 55.7M 23s
203900K .......... .......... .......... .......... .......... 38% 209M 23s
203950K .......... .......... .......... .......... .......... 38% 8.87M 23s
204000K .......... .......... .......... .......... .......... 38% 224M 23s
204050K .......... .......... .......... .......... .......... 38% 176M 23s
204100K .......... .......... .......... .......... .......... 38% 200M 23s
204150K .......... .......... .......... .......... .......... 38% 136M 23s
204200K .......... .......... .......... .......... .......... 38% 107M 23s
204250K .......... .......... .......... .......... .......... 38% 157M 23s
204300K .......... .......... .......... .......... .......... 38% 1.69M 23s
204350K .......... .......... .......... .......... .......... 38% 56.6M 23s
204400K .......... .......... .......... .......... .......... 38% 93.0M 23s
204450K .......... .......... .......... .......... .......... 38% 167M 23s
204500K .......... .......... .......... .......... .......... 38% 153M 23s
204550K .......... .......... .......... .......... .......... 38% 120M 23s
204600K .......... .......... .......... .......... .......... 38% 100M 23s
204650K .......... .......... .......... .......... .......... 38% 210M 23s
204700K .......... .......... .......... .......... .......... 38% 8.34M 23s
204750K .......... .......... .......... .......... .......... 38% 131M 23s
204800K .......... .......... .......... .......... .......... 38% 1.05M 23s
204850K .......... .......... .......... .......... .......... 38% 119M 23s
204900K .......... .......... .......... .......... .......... 38% 176M 23s
204950K .......... .......... .......... .......... .......... 38% 152M 23s
205000K .......... .......... .......... .......... .......... 38% 86.3M 23s
205050K .......... .......... .......... .......... .......... 38% 58.2M 23s
205100K .......... .......... .......... .......... .......... 38% 44.8M 23s
205150K .......... .......... .......... .......... .......... 38% 198M 23s
205200K .......... .......... .......... .......... .......... 38% 72.2M 23s
205250K .......... .......... .......... .......... .......... 38% 184M 23s
205300K .......... .......... .......... .......... .......... 38% 202M 23s
205350K .......... .......... .......... .......... .......... 38% 178M 23s
205400K .......... .......... .......... .......... .......... 38% 196M 23s
205450K .......... .......... .......... .......... .......... 38% 180M 23s
205500K .......... .......... .......... .......... .......... 38% 214M 23s
205550K .......... .......... .......... .......... .......... 38% 213M 23s
205600K .......... .......... .......... .......... .......... 38% 188M 23s
205650K .......... .......... .......... .......... .......... 38% 191M 23s
205700K .......... .......... .......... .......... .......... 38% 177M 23s
205750K .......... .......... .......... .......... .......... 38% 224M 23s
205800K .......... .......... .......... .......... .......... 38% 224M 23s
205850K .......... .......... .......... .......... .......... 38% 221M 23s
205900K .......... .......... .......... .......... .......... 38% 307M 23s
205950K .......... .......... .......... .......... .......... 38% 260M 23s
206000K .......... .......... .......... .......... .......... 38% 11.2M 23s
206050K .......... .......... .......... .......... .......... 38% 174M 23s
206100K .......... .......... .......... .......... .......... 38% 191M 23s
206150K .......... .......... .......... .......... .......... 38% 161M 23s
206200K .......... .......... .......... .......... .......... 38% 189M 23s
206250K .......... .......... .......... .......... .......... 38% 198M 23s
206300K .......... .......... .......... .......... .......... 38% 7.85M 23s
206350K .......... .......... .......... .......... .......... 38% 143M 23s
206400K .......... .......... .......... .......... .......... 38% 208M 23s
206450K .......... .......... .......... .......... .......... 38% 154M 23s
206500K .......... .......... .......... .......... .......... 38% 186M 23s
206550K .......... .......... .......... .......... .......... 38% 201M 23s
206600K .......... .......... .......... .......... .......... 38% 6.48M 23s
206650K .......... .......... .......... .......... .......... 38% 121M 23s
206700K .......... .......... .......... .......... .......... 38% 174M 23s
206750K .......... .......... .......... .......... .......... 38% 248M 23s
206800K .......... .......... .......... .......... .......... 38% 289M 23s
206850K .......... .......... .......... .......... .......... 38% 836K 23s
206900K .......... .......... .......... .......... .......... 38% 93.7M 23s
206950K .......... .......... .......... .......... .......... 38% 73.4M 23s
207000K .......... .......... .......... .......... .......... 38% 38.3M 23s
207050K .......... .......... .......... .......... .......... 38% 82.3M 23s
207100K .......... .......... .......... .......... .......... 38% 40.6M 23s
207150K .......... .......... .......... .......... .......... 38% 74.1M 23s
207200K .......... .......... .......... .......... .......... 38% 51.0M 23s
207250K .......... .......... .......... .......... .......... 38% 195M 23s
207300K .......... .......... .......... .......... .......... 38% 198M 23s
207350K .......... .......... .......... .......... .......... 38% 166M 23s
207400K .......... .......... .......... .......... .......... 38% 191M 23s
207450K .......... .......... .......... .......... .......... 38% 155M 23s
207500K .......... .......... .......... .......... .......... 38% 189M 23s
207550K .......... .......... .......... .......... .......... 38% 183M 23s
207600K .......... .......... .......... .......... .......... 38% 128M 23s
207650K .......... .......... .......... .......... .......... 38% 307M 23s
207700K .......... .......... .......... .......... .......... 38% 248M 23s
207750K .......... .......... .......... .......... .......... 38% 276M 23s
207800K .......... .......... .......... .......... .......... 38% 273M 23s
207850K .......... .......... .......... .......... .......... 38% 12.4M 23s
207900K .......... .......... .......... .......... .......... 39% 148M 23s
207950K .......... .......... .......... .......... .......... 39% 106M 23s
208000K .......... .......... .......... .......... .......... 39% 164M 23s
208050K .......... .......... .......... .......... .......... 39% 153M 23s
208100K .......... .......... .......... .......... .......... 39% 98.4M 23s
208150K .......... .......... .......... .......... .......... 39% 210M 23s
208200K .......... .......... .......... .......... .......... 39% 159M 23s
208250K .......... .......... .......... .......... .......... 39% 149M 23s
208300K .......... .......... .......... .......... .......... 39% 228M 23s
208350K .......... .......... .......... .......... .......... 39% 151M 23s
208400K .......... .......... .......... .......... .......... 39% 14.5M 23s
208450K .......... .......... .......... .......... .......... 39% 48.3M 23s
208500K .......... .......... .......... .......... .......... 39% 132M 23s
208550K .......... .......... .......... .......... .......... 39% 157M 23s
208600K .......... .......... .......... .......... .......... 39% 178M 23s
208650K .......... .......... .......... .......... .......... 39% 16.6M 23s
208700K .......... .......... .......... .......... .......... 39% 39.7M 23s
208750K .......... .......... .......... .......... .......... 39% 83.5M 23s
208800K .......... .......... .......... .......... .......... 39% 23.2M 23s
208850K .......... .......... .......... .......... .......... 39% 12.9M 23s
208900K .......... .......... .......... .......... .......... 39% 119M 23s
208950K .......... .......... .......... .......... .......... 39% 135M 23s
209000K .......... .......... .......... .......... .......... 39% 153M 23s
209050K .......... .......... .......... .......... .......... 39% 142M 23s
209100K .......... .......... .......... .......... .......... 39% 121M 23s
209150K .......... .......... .......... .......... .......... 39% 5.87M 23s
209200K .......... .......... .......... .......... .......... 39% 128M 23s
209250K .......... .......... .......... .......... .......... 39% 77.3M 23s
209300K .......... .......... .......... .......... .......... 39% 97.1M 23s
209350K .......... .......... .......... .......... .......... 39% 119M 23s
209400K .......... .......... .......... .......... .......... 39% 4.99M 23s
209450K .......... .......... .......... .......... .......... 39% 148M 23s
209500K .......... .......... .......... .......... .......... 39% 70.4M 23s
209550K .......... .......... .......... .......... .......... 39% 90.1M 23s
209600K .......... .......... .......... .......... .......... 39% 65.9M 23s
209650K .......... .......... .......... .......... .......... 39% 150M 23s
209700K .......... .......... .......... .......... .......... 39% 99.2M 23s
209750K .......... .......... .......... .......... .......... 39% 96.5M 23s
209800K .......... .......... .......... .......... .......... 39% 10.6M 23s
209850K .......... .......... .......... .......... .......... 39% 112M 23s
209900K .......... .......... .......... .......... .......... 39% 396K 23s
209950K .......... .......... .......... .......... .......... 39% 94.3M 23s
210000K .......... .......... .......... .......... .......... 39% 109M 23s
210050K .......... .......... .......... .......... .......... 39% 99.6M 23s
210100K .......... .......... .......... .......... .......... 39% 112M 23s
210150K .......... .......... .......... .......... .......... 39% 148M 23s
210200K .......... .......... .......... .......... .......... 39% 168M 23s
210250K .......... .......... .......... .......... .......... 39% 201M 23s
210300K .......... .......... .......... .......... .......... 39% 133M 23s
210350K .......... .......... .......... .......... .......... 39% 180M 23s
210400K .......... .......... .......... .......... .......... 39% 203M 23s
210450K .......... .......... .......... .......... .......... 39% 154M 23s
210500K .......... .......... .......... .......... .......... 39% 153M 23s
210550K .......... .......... .......... .......... .......... 39% 120M 23s
210600K .......... .......... .......... .......... .......... 39% 110M 23s
210650K .......... .......... .......... .......... .......... 39% 153M 23s
210700K .......... .......... .......... .......... .......... 39% 180M 23s
210750K .......... .......... .......... .......... .......... 39% 189M 23s
210800K .......... .......... .......... .......... .......... 39% 201M 23s
210850K .......... .......... .......... .......... .......... 39% 153M 23s
210900K .......... .......... .......... .......... .......... 39% 1.31M 23s
210950K .......... .......... .......... .......... .......... 39% 25.0M 23s
211000K .......... .......... .......... .......... .......... 39% 54.0M 23s
211050K .......... .......... .......... .......... .......... 39% 108M 23s
211100K .......... .......... .......... .......... .......... 39% 144M 23s
211150K .......... .......... .......... .......... .......... 39% 184M 23s
211200K .......... .......... .......... .......... .......... 39% 116M 23s
211250K .......... .......... .......... .......... .......... 39% 166M 23s
211300K .......... .......... .......... .......... .......... 39% 215M 23s
211350K .......... .......... .......... .......... .......... 39% 137M 23s
211400K .......... .......... .......... .......... .......... 39% 119M 23s
211450K .......... .......... .......... .......... .......... 39% 124M 23s
211500K .......... .......... .......... .......... .......... 39% 119M 23s
211550K .......... .......... .......... .......... .......... 39% 198M 23s
211600K .......... .......... .......... .......... .......... 39% 125M 23s
211650K .......... .......... .......... .......... .......... 39% 124M 23s
211700K .......... .......... .......... .......... .......... 39% 126M 23s
211750K .......... .......... .......... .......... .......... 39% 86.9M 23s
211800K .......... .......... .......... .......... .......... 39% 104M 23s
211850K .......... .......... .......... .......... .......... 39% 97.9M 23s
211900K .......... .......... .......... .......... .......... 39% 104M 23s
211950K .......... .......... .......... .......... .......... 39% 60.3M 23s
212000K .......... .......... .......... .......... .......... 39% 213M 23s
212050K .......... .......... .......... .......... .......... 39% 139M 23s
212100K .......... .......... .......... .......... .......... 39% 28.8M 23s
212150K .......... .......... .......... .......... .......... 39% 189M 23s
212200K .......... .......... .......... .......... .......... 39% 89.6M 23s
212250K .......... .......... .......... .......... .......... 39% 153M 23s
212300K .......... .......... .......... .......... .......... 39% 131M 23s
212350K .......... .......... .......... .......... .......... 39% 15.4M 23s
212400K .......... .......... .......... .......... .......... 39% 98.4M 23s
212450K .......... .......... .......... .......... .......... 39% 6.13M 23s
212500K .......... .......... .......... .......... .......... 39% 165M 23s
212550K .......... .......... .......... .......... .......... 39% 158M 23s
212600K .......... .......... .......... .......... .......... 39% 89.9M 23s
212650K .......... .......... .......... .......... .......... 39% 149M 23s
212700K .......... .......... .......... .......... .......... 39% 4.42M 23s
212750K .......... .......... .......... .......... .......... 39% 115M 23s
212800K .......... .......... .......... .......... .......... 39% 182M 23s
212850K .......... .......... .......... .......... .......... 39% 130M 23s
212900K .......... .......... .......... .......... .......... 39% 178M 23s
212950K .......... .......... .......... .......... .......... 39% 4.15M 23s
213000K .......... .......... .......... .......... .......... 39% 152M 23s
213050K .......... .......... .......... .......... .......... 39% 80.0M 23s
213100K .......... .......... .......... .......... .......... 39% 66.5M 23s
213150K .......... .......... .......... .......... .......... 39% 94.3M 23s
213200K .......... .......... .......... .......... .......... 39% 142M 22s
213250K .......... .......... .......... .......... .......... 40% 219M 22s
213300K .......... .......... .......... .......... .......... 40% 4.08M 22s
213350K .......... .......... .......... .......... .......... 40% 127M 22s
213400K .......... .......... .......... .......... .......... 40% 77.6M 22s
213450K .......... .......... .......... .......... .......... 40% 136M 22s
213500K .......... .......... .......... .......... .......... 40% 195M 22s
213550K .......... .......... .......... .......... .......... 40% 189M 22s
213600K .......... .......... .......... .......... .......... 40% 110M 22s
213650K .......... .......... .......... .......... .......... 40% 191M 22s
213700K .......... .......... .......... .......... .......... 40% 8.57M 22s
213750K .......... .......... .......... .......... .......... 40% 47.5M 22s
213800K .......... .......... .......... .......... .......... 40% 90.9M 22s
213850K .......... .......... .......... .......... .......... 40% 107M 22s
213900K .......... .......... .......... .......... .......... 40% 156M 22s
213950K .......... .......... .......... .......... .......... 40% 4.60M 22s
214000K .......... .......... .......... .......... .......... 40% 305K 23s
214050K .......... .......... .......... .......... .......... 40% 117M 23s
214100K .......... .......... .......... .......... .......... 40% 111M 23s
214150K .......... .......... .......... .......... .......... 40% 103M 23s
214200K .......... .......... .......... .......... .......... 40% 108M 23s
214250K .......... .......... .......... .......... .......... 40% 162M 23s
214300K .......... .......... .......... .......... .......... 40% 126M 23s
214350K .......... .......... .......... .......... .......... 40% 44.3M 23s
214400K .......... .......... .......... .......... .......... 40% 93.0M 23s
214450K .......... .......... .......... .......... .......... 40% 112M 23s
214500K .......... .......... .......... .......... .......... 40% 172M 23s
214550K .......... .......... .......... .......... .......... 40% 188M 23s
214600K .......... .......... .......... .......... .......... 40% 180M 23s
214650K .......... .......... .......... .......... .......... 40% 192M 23s
214700K .......... .......... .......... .......... .......... 40% 120M 23s
214750K .......... .......... .......... .......... .......... 40% 126M 23s
214800K .......... .......... .......... .......... .......... 40% 142M 23s
214850K .......... .......... .......... .......... .......... 40% 142M 23s
214900K .......... .......... .......... .......... .......... 40% 147M 23s
214950K .......... .......... .......... .......... .......... 40% 143M 22s
215000K .......... .......... .......... .......... .......... 40% 415K 23s
215050K .......... .......... .......... .......... .......... 40% 121M 23s
215100K .......... .......... .......... .......... .......... 40% 137M 23s
215150K .......... .......... .......... .......... .......... 40% 160M 23s
215200K .......... .......... .......... .......... .......... 40% 70.6M 23s
215250K .......... .......... .......... .......... .......... 40% 202M 23s
215300K .......... .......... .......... .......... .......... 40% 212M 23s
215350K .......... .......... .......... .......... .......... 40% 89.8M 23s
215400K .......... .......... .......... .......... .......... 40% 160M 23s
215450K .......... .......... .......... .......... .......... 40% 5.18M 23s
215500K .......... .......... .......... .......... .......... 40% 180M 23s
215550K .......... .......... .......... .......... .......... 40% 107M 23s
215600K .......... .......... .......... .......... .......... 40% 164M 23s
215650K .......... .......... .......... .......... .......... 40% 81.4M 23s
215700K .......... .......... .......... .......... .......... 40% 213M 23s
215750K .......... .......... .......... .......... .......... 40% 174M 23s
215800K .......... .......... .......... .......... .......... 40% 81.1M 23s
215850K .......... .......... .......... .......... .......... 40% 116M 23s
215900K .......... .......... .......... .......... .......... 40% 226M 23s
215950K .......... .......... .......... .......... .......... 40% 154M 23s
216000K .......... .......... .......... .......... .......... 40% 195M 23s
216050K .......... .......... .......... .......... .......... 40% 170M 23s
216100K .......... .......... .......... .......... .......... 40% 152M 22s
216150K .......... .......... .......... .......... .......... 40% 89.9M 22s
216200K .......... .......... .......... .......... .......... 40% 48.9M 22s
216250K .......... .......... .......... .......... .......... 40% 62.7M 22s
216300K .......... .......... .......... .......... .......... 40% 57.7M 22s
216350K .......... .......... .......... .......... .......... 40% 52.2M 22s
216400K .......... .......... .......... .......... .......... 40% 83.8M 22s
216450K .......... .......... .......... .......... .......... 40% 87.8M 22s
216500K .......... .......... .......... .......... .......... 40% 173M 22s
216550K .......... .......... .......... .......... .......... 40% 128M 22s
216600K .......... .......... .......... .......... .......... 40% 40.3M 22s
216650K .......... .......... .......... .......... .......... 40% 154M 22s
216700K .......... .......... .......... .......... .......... 40% 193M 22s
216750K .......... .......... .......... .......... .......... 40% 161M 22s
216800K .......... .......... .......... .......... .......... 40% 163M 22s
216850K .......... .......... .......... .......... .......... 40% 174M 22s
216900K .......... .......... .......... .......... .......... 40% 4.43M 22s
216950K .......... .......... .......... .......... .......... 40% 45.7M 22s
217000K .......... .......... .......... .......... .......... 40% 122M 22s
217050K .......... .......... .......... .......... .......... 40% 132M 22s
217100K .......... .......... .......... .......... .......... 40% 102M 22s
217150K .......... .......... .......... .......... .......... 40% 153M 22s
217200K .......... .......... .......... .......... .......... 40% 7.18M 22s
217250K .......... .......... .......... .......... .......... 40% 96.3M 22s
217300K .......... .......... .......... .......... .......... 40% 72.1M 22s
217350K .......... .......... .......... .......... .......... 40% 126M 22s
217400K .......... .......... .......... .......... .......... 40% 174M 22s
217450K .......... .......... .......... .......... .......... 40% 147M 22s
217500K .......... .......... .......... .......... .......... 40% 201M 22s
217550K .......... .......... .......... .......... .......... 40% 6.65M 22s
217600K .......... .......... .......... .......... .......... 40% 159M 22s
217650K .......... .......... .......... .......... .......... 40% 168M 22s
217700K .......... .......... .......... .......... .......... 40% 165M 22s
217750K .......... .......... .......... .......... .......... 40% 185M 22s
217800K .......... .......... .......... .......... .......... 40% 5.94M 22s
217850K .......... .......... .......... .......... .......... 40% 108M 22s
217900K .......... .......... .......... .......... .......... 40% 180M 22s
217950K .......... .......... .......... .......... .......... 40% 151M 22s
218000K .......... .......... .......... .......... .......... 40% 188M 22s
218050K .......... .......... .......... .......... .......... 40% 142M 22s
218100K .......... .......... .......... .......... .......... 40% 1.26M 22s
218150K .......... .......... .......... .......... .......... 40% 92.3M 22s
218200K .......... .......... .......... .......... .......... 40% 135M 22s
218250K .......... .......... .......... .......... .......... 40% 107M 22s
218300K .......... .......... .......... .......... .......... 40% 108M 22s
218350K .......... .......... .......... .......... .......... 40% 65.8M 22s
218400K .......... .......... .......... .......... .......... 40% 191M 22s
218450K .......... .......... .......... .......... .......... 40% 92.8M 22s
218500K .......... .......... .......... .......... .......... 40% 126M 22s
218550K .......... .......... .......... .......... .......... 41% 151M 22s
218600K .......... .......... .......... .......... .......... 41% 115M 22s
218650K .......... .......... .......... .......... .......... 41% 154M 22s
218700K .......... .......... .......... .......... .......... 41% 93.7M 22s
218750K .......... .......... .......... .......... .......... 41% 141M 22s
218800K .......... .......... .......... .......... .......... 41% 125M 22s
218850K .......... .......... .......... .......... .......... 41% 115M 22s
218900K .......... .......... .......... .......... .......... 41% 128M 22s
218950K .......... .......... .......... .......... .......... 41% 137M 22s
219000K .......... .......... .......... .......... .......... 41% 171M 22s
219050K .......... .......... .......... .......... .......... 41% 136M 22s
219100K .......... .......... .......... .......... .......... 41% 125M 22s
219150K .......... .......... .......... .......... .......... 41% 129M 22s
219200K .......... .......... .......... .......... .......... 41% 128M 22s
219250K .......... .......... .......... .......... .......... 41% 158M 22s
219300K .......... .......... .......... .......... .......... 41% 8.31M 22s
219350K .......... .......... .......... .......... .......... 41% 158M 22s
219400K .......... .......... .......... .......... .......... 41% 174M 22s
219450K .......... .......... .......... .......... .......... 41% 187M 22s
219500K .......... .......... .......... .......... .......... 41% 217M 22s
219550K .......... .......... .......... .......... .......... 41% 132M 22s
219600K .......... .......... .......... .......... .......... 41% 4.78M 22s
219650K .......... .......... .......... .......... .......... 41% 6.81M 22s
219700K .......... .......... .......... .......... .......... 41% 95.2M 22s
219750K .......... .......... .......... .......... .......... 41% 86.0M 22s
219800K .......... .......... .......... .......... .......... 41% 150M 22s
219850K .......... .......... .......... .......... .......... 41% 35.1M 22s
219900K .......... .......... .......... .......... .......... 41% 145M 22s
219950K .......... .......... .......... .......... .......... 41% 179M 22s
220000K .......... .......... .......... .......... .......... 41% 208M 22s
220050K .......... .......... .......... .......... .......... 41% 168M 22s
220100K .......... .......... .......... .......... .......... 41% 152M 22s
220150K .......... .......... .......... .......... .......... 41% 1.22M 22s
220200K .......... .......... .......... .......... .......... 41% 136M 22s
220250K .......... .......... .......... .......... .......... 41% 109M 22s
220300K .......... .......... .......... .......... .......... 41% 171M 22s
220350K .......... .......... .......... .......... .......... 41% 97.9M 22s
220400K .......... .......... .......... .......... .......... 41% 175M 22s
220450K .......... .......... .......... .......... .......... 41% 168M 22s
220500K .......... .......... .......... .......... .......... 41% 169M 22s
220550K .......... .......... .......... .......... .......... 41% 178M 22s
220600K .......... .......... .......... .......... .......... 41% 115M 22s
220650K .......... .......... .......... .......... .......... 41% 171M 22s
220700K .......... .......... .......... .......... .......... 41% 172M 22s
220750K .......... .......... .......... .......... .......... 41% 164M 22s
220800K .......... .......... .......... .......... .......... 41% 170M 22s
220850K .......... .......... .......... .......... .......... 41% 116M 22s
220900K .......... .......... .......... .......... .......... 41% 158M 22s
220950K .......... .......... .......... .......... .......... 41% 125M 22s
221000K .......... .......... .......... .......... .......... 41% 103M 22s
221050K .......... .......... .......... .......... .......... 41% 78.8M 22s
221100K .......... .......... .......... .......... .......... 41% 183M 22s
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221200K .......... .......... .......... .......... .......... 41% 114M 22s
221250K .......... .......... .......... .......... .......... 41% 152M 22s
221300K .......... .......... .......... .......... .......... 41% 140M 22s
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221400K .......... .......... .......... .......... .......... 41% 128M 22s
221450K .......... .......... .......... .......... .......... 41% 139M 22s
221500K .......... .......... .......... .......... .......... 41% 160M 22s
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221600K .......... .......... .......... .......... .......... 41% 7.54M 22s
221650K .......... .......... .......... .......... .......... 41% 144M 22s
221700K .......... .......... .......... .......... .......... 41% 180M 22s
221750K .......... .......... .......... .......... .......... 41% 211M 22s
221800K .......... .......... .......... .......... .......... 41% 152M 22s
221850K .......... .......... .......... .......... .......... 41% 6.35M 22s
221900K .......... .......... .......... .......... .......... 41% 244M 22s
221950K .......... .......... .......... .......... .......... 41% 174M 22s
222000K .......... .......... .......... .......... .......... 41% 158M 22s
222050K .......... .......... .......... .......... .......... 41% 182M 22s
222100K .......... .......... .......... .......... .......... 41% 7.15M 22s
222150K .......... .......... .......... .......... .......... 41% 119M 22s
222200K .......... .......... .......... .......... .......... 41% 634K 22s
222250K .......... .......... .......... .......... .......... 41% 44.1M 22s
222300K .......... .......... .......... .......... .......... 41% 163M 22s
222350K .......... .......... .......... .......... .......... 41% 143M 22s
222400K .......... .......... .......... .......... .......... 41% 54.6M 22s
222450K .......... .......... .......... .......... .......... 41% 110M 22s
222500K .......... .......... .......... .......... .......... 41% 119M 22s
222550K .......... .......... .......... .......... .......... 41% 114M 22s
222600K .......... .......... .......... .......... .......... 41% 121M 22s
222650K .......... .......... .......... .......... .......... 41% 176M 22s
222700K .......... .......... .......... .......... .......... 41% 214M 22s
222750K .......... .......... .......... .......... .......... 41% 231M 22s
222800K .......... .......... .......... .......... .......... 41% 172M 22s
222850K .......... .......... .......... .......... .......... 41% 194M 22s
222900K .......... .......... .......... .......... .......... 41% 166M 22s
222950K .......... .......... .......... .......... .......... 41% 233M 22s
223000K .......... .......... .......... .......... .......... 41% 282M 22s
223050K .......... .......... .......... .......... .......... 41% 263M 22s
223100K .......... .......... .......... .......... .......... 41% 229M 22s
223150K .......... .......... .......... .......... .......... 41% 216M 22s
223200K .......... .......... .......... .......... .......... 41% 4.09M 22s
223250K .......... .......... .......... .......... .......... 41% 101M 22s
223300K .......... .......... .......... .......... .......... 41% 93.4M 22s
223350K .......... .......... .......... .......... .......... 41% 81.7M 22s
223400K .......... .......... .......... .......... .......... 41% 92.7M 22s
223450K .......... .......... .......... .......... .......... 41% 99.0M 22s
223500K .......... .......... .......... .......... .......... 41% 200M 22s
223550K .......... .......... .......... .......... .......... 41% 193M 22s
223600K .......... .......... .......... .......... .......... 41% 172M 22s
223650K .......... .......... .......... .......... .......... 41% 191M 22s
223700K .......... .......... .......... .......... .......... 41% 175M 22s
223750K .......... .......... .......... .......... .......... 41% 191M 22s
223800K .......... .......... .......... .......... .......... 41% 195M 22s
223850K .......... .......... .......... .......... .......... 41% 16.3M 22s
223900K .......... .......... .......... .......... .......... 42% 197M 22s
223950K .......... .......... .......... .......... .......... 42% 89.1M 22s
224000K .......... .......... .......... .......... .......... 42% 158M 22s
224050K .......... .......... .......... .......... .......... 42% 23.4M 22s
224100K .......... .......... .......... .......... .......... 42% 6.83M 22s
224150K .......... .......... .......... .......... .......... 42% 95.0M 22s
224200K .......... .......... .......... .......... .......... 42% 68.0M 22s
224250K .......... .......... .......... .......... .......... 42% 24.9M 22s
224300K .......... .......... .......... .......... .......... 42% 166M 22s
224350K .......... .......... .......... .......... .......... 42% 7.94M 22s
224400K .......... .......... .......... .......... .......... 42% 147M 22s
224450K .......... .......... .......... .......... .......... 42% 268M 22s
224500K .......... .......... .......... .......... .......... 42% 66.3M 22s
224550K .......... .......... .......... .......... .......... 42% 175M 22s
224600K .......... .......... .......... .......... .......... 42% 215M 22s
224650K .......... .......... .......... .......... .......... 42% 14.9M 22s
224700K .......... .......... .......... .......... .......... 42% 88.1M 22s
224750K .......... .......... .......... .......... .......... 42% 112M 22s
224800K .......... .......... .......... .......... .......... 42% 22.1M 21s
224850K .......... .......... .......... .......... .......... 42% 104M 21s
224900K .......... .......... .......... .......... .......... 42% 136M 21s
224950K .......... .......... .......... .......... .......... 42% 6.34M 21s
225000K .......... .......... .......... .......... .......... 42% 184M 21s
225050K .......... .......... .......... .......... .......... 42% 202M 21s
225100K .......... .......... .......... .......... .......... 42% 153M 21s
225150K .......... .......... .......... .......... .......... 42% 218M 21s
225200K .......... .......... .......... .......... .......... 42% 181M 21s
225250K .......... .......... .......... .......... .......... 42% 2.43M 21s
225300K .......... .......... .......... .......... .......... 42% 180M 21s
225350K .......... .......... .......... .......... .......... 42% 156M 21s
225400K .......... .......... .......... .......... .......... 42% 161M 21s
225450K .......... .......... .......... .......... .......... 42% 190M 21s
225500K .......... .......... .......... .......... .......... 42% 154M 21s
225550K .......... .......... .......... .......... .......... 42% 138M 21s
225600K .......... .......... .......... .......... .......... 42% 164M 21s
225650K .......... .......... .......... .......... .......... 42% 158M 21s
225700K .......... .......... .......... .......... .......... 42% 126M 21s
225750K .......... .......... .......... .......... .......... 42% 174M 21s
225800K .......... .......... .......... .......... .......... 42% 216M 21s
225850K .......... .......... .......... .......... .......... 42% 156M 21s
225900K .......... .......... .......... .......... .......... 42% 209M 21s
225950K .......... .......... .......... .......... .......... 42% 7.60M 21s
226000K .......... .......... .......... .......... .......... 42% 166M 21s
226050K .......... .......... .......... .......... .......... 42% 138M 21s
226100K .......... .......... .......... .......... .......... 42% 58.8M 21s
226150K .......... .......... .......... .......... .......... 42% 195M 21s
226200K .......... .......... .......... .......... .......... 42% 149M 21s
226250K .......... .......... .......... .......... .......... 42% 10.2M 21s
226300K .......... .......... .......... .......... .......... 42% 3.47M 21s
226350K .......... .......... .......... .......... .......... 42% 140M 21s
226400K .......... .......... .......... .......... .......... 42% 81.5M 21s
226450K .......... .......... .......... .......... .......... 42% 167M 21s
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226650K .......... .......... .......... .......... .......... 42% 216M 21s
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226850K .......... .......... .......... .......... .......... 42% 179M 21s
226900K .......... .......... .......... .......... .......... 42% 180M 21s
226950K .......... .......... .......... .......... .......... 42% 4.20M 21s
227000K .......... .......... .......... .......... .......... 42% 154M 21s
227050K .......... .......... .......... .......... .......... 42% 195M 21s
227100K .......... .......... .......... .......... .......... 42% 94.4M 21s
227150K .......... .......... .......... .......... .......... 42% 131M 21s
227200K .......... .......... .......... .......... .......... 42% 185M 21s
227250K .......... .......... .......... .......... .......... 42% 6.72M 21s
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227350K .......... .......... .......... .......... .......... 42% 176M 21s
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227550K .......... .......... .......... .......... .......... 42% 10.6M 21s
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227800K .......... .......... .......... .......... .......... 42% 7.72M 21s
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227900K .......... .......... .......... .......... .......... 42% 108M 21s
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228000K .......... .......... .......... .......... .......... 42% 230M 21s
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228100K .......... .......... .......... .......... .......... 42% 12.7M 21s
228150K .......... .......... .......... .......... .......... 42% 181M 21s
228200K .......... .......... .......... .......... .......... 42% 96.7M 21s
228250K .......... .......... .......... .......... .......... 42% 210M 21s
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228400K .......... .......... .......... .......... .......... 42% 93.4M 21s
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228800K .......... .......... .......... .......... .......... 42% 99.9M 21s
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228900K .......... .......... .......... .......... .......... 42% 91.8M 21s
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229000K .......... .......... .......... .......... .......... 42% 162M 21s
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229100K .......... .......... .......... .......... .......... 42% 113M 21s
229150K .......... .......... .......... .......... .......... 42% 141M 21s
229200K .......... .......... .......... .......... .......... 42% 63.2M 21s
229250K .......... .......... .......... .......... .......... 43% 141M 21s
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229350K .......... .......... .......... .......... .......... 43% 16.1M 21s
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229450K .......... .......... .......... .......... .......... 43% 70.0M 21s
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229550K .......... .......... .......... .......... .......... 43% 93.0M 21s
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229850K .......... .......... .......... .......... .......... 43% 7.60M 21s
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229950K .......... .......... .......... .......... .......... 43% 71.1M 21s
230000K .......... .......... .......... .......... .......... 43% 144M 21s
230050K .......... .......... .......... .......... .......... 43% 122M 21s
230100K .......... .......... .......... .......... .......... 43% 155M 21s
230150K .......... .......... .......... .......... .......... 43% 12.1M 21s
230200K .......... .......... .......... .......... .......... 43% 54.1M 21s
230250K .......... .......... .......... .......... .......... 43% 88.9M 21s
230300K .......... .......... .......... .......... .......... 43% 112M 21s
230350K .......... .......... .......... .......... .......... 43% 18.0M 21s
230400K .......... .......... .......... .......... .......... 43% 1.34M 21s
230450K .......... .......... .......... .......... .......... 43% 137M 21s
230500K .......... .......... .......... .......... .......... 43% 164M 21s
230550K .......... .......... .......... .......... .......... 43% 74.5M 21s
230600K .......... .......... .......... .......... .......... 43% 29.7M 21s
230650K .......... .......... .......... .......... .......... 43% 68.8M 21s
230700K .......... .......... .......... .......... .......... 43% 83.5M 21s
230750K .......... .......... .......... .......... .......... 43% 130M 21s
230800K .......... .......... .......... .......... .......... 43% 76.1M 21s
230850K .......... .......... .......... .......... .......... 43% 124M 21s
230900K .......... .......... .......... .......... .......... 43% 178M 21s
230950K .......... .......... .......... .......... .......... 43% 80.7M 21s
231000K .......... .......... .......... .......... .......... 43% 218M 21s
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231100K .......... .......... .......... .......... .......... 43% 105M 21s
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231300K .......... .......... .......... .......... .......... 43% 213M 21s
231350K .......... .......... .......... .......... .......... 43% 72.9M 21s
231400K .......... .......... .......... .......... .......... 43% 1.05M 21s
231450K .......... .......... .......... .......... .......... 43% 155M 21s
231500K .......... .......... .......... .......... .......... 43% 209M 21s
231550K .......... .......... .......... .......... .......... 43% 182M 21s
231600K .......... .......... .......... .......... .......... 43% 33.8M 21s
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231750K .......... .......... .......... .......... .......... 43% 166M 21s
231800K .......... .......... .......... .......... .......... 43% 174M 21s
231850K .......... .......... .......... .......... .......... 43% 139M 21s
231900K .......... .......... .......... .......... .......... 43% 205M 21s
231950K .......... .......... .......... .......... .......... 43% 184M 21s
232000K .......... .......... .......... .......... .......... 43% 156M 21s
232050K .......... .......... .......... .......... .......... 43% 53.3M 21s
232100K .......... .......... .......... .......... .......... 43% 170M 21s
232150K .......... .......... .......... .......... .......... 43% 206M 21s
232200K .......... .......... .......... .......... .......... 43% 197M 21s
232250K .......... .......... .......... .......... .......... 43% 229M 21s
232300K .......... .......... .......... .......... .......... 43% 221M 21s
232350K .......... .......... .......... .......... .......... 43% 180M 21s
232400K .......... .......... .......... .......... .......... 43% 210M 21s
232450K .......... .......... .......... .......... .......... 43% 9.14M 21s
232500K .......... .......... .......... .......... .......... 43% 158M 21s
232550K .......... .......... .......... .......... .......... 43% 202M 21s
232600K .......... .......... .......... .......... .......... 43% 190M 21s
232650K .......... .......... .......... .......... .......... 43% 223M 21s
232700K .......... .......... .......... .......... .......... 43% 195M 21s
232750K .......... .......... .......... .......... .......... 43% 200M 21s
232800K .......... .......... .......... .......... .......... 43% 198M 21s
232850K .......... .......... .......... .......... .......... 43% 168M 21s
232900K .......... .......... .......... .......... .......... 43% 9.27M 21s
232950K .......... .......... .......... .......... .......... 43% 163M 21s
233000K .......... .......... .......... .......... .......... 43% 225M 21s
233050K .......... .......... .......... .......... .......... 43% 237M 21s
233100K .......... .......... .......... .......... .......... 43% 180M 21s
233150K .......... .......... .......... .......... .......... 43% 17.4M 21s
233200K .......... .......... .......... .......... .......... 43% 8.68M 21s
233250K .......... .......... .......... .......... .......... 43% 70.3M 21s
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233400K .......... .......... .......... .......... .......... 43% 185M 21s
233450K .......... .......... .......... .......... .......... 43% 425K 21s
233500K .......... .......... .......... .......... .......... 43% 84.5M 21s
233550K .......... .......... .......... .......... .......... 43% 67.4M 21s
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233900K .......... .......... .......... .......... .......... 43% 174M 21s
233950K .......... .......... .......... .......... .......... 43% 150M 21s
234000K .......... .......... .......... .......... .......... 43% 205M 21s
234050K .......... .......... .......... .......... .......... 43% 203M 21s
234100K .......... .......... .......... .......... .......... 43% 73.1M 21s
234150K .......... .......... .......... .......... .......... 43% 125M 21s
234200K .......... .......... .......... .......... .......... 43% 75.7M 21s
234250K .......... .......... .......... .......... .......... 43% 108M 21s
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234550K .......... .......... .......... .......... .......... 44% 86.4M 21s
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234700K .......... .......... .......... .......... .......... 44% 75.5M 21s
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234850K .......... .......... .......... .......... .......... 44% 71.6M 21s
234900K .......... .......... .......... .......... .......... 44% 124M 21s
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235000K .......... .......... .......... .......... .......... 44% 128M 21s
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235100K .......... .......... .......... .......... .......... 44% 125M 21s
235150K .......... .......... .......... .......... .......... 44% 135M 21s
235200K .......... .......... .......... .......... .......... 44% 159M 21s
235250K .......... .......... .......... .......... .......... 44% 270M 21s
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235400K .......... .......... .......... .......... .......... 44% 225M 21s
235450K .......... .......... .......... .......... .......... 44% 268M 21s
235500K .......... .......... .......... .......... .......... 44% 202M 21s
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235600K .......... .......... .......... .......... .......... 44% 56.7M 21s
235650K .......... .......... .......... .......... .......... 44% 193M 21s
235700K .......... .......... .......... .......... .......... 44% 6.54M 21s
235750K .......... .......... .......... .......... .......... 44% 153M 21s
235800K .......... .......... .......... .......... .......... 44% 100M 21s
235850K .......... .......... .......... .......... .......... 44% 136M 21s
235900K .......... .......... .......... .......... .......... 44% 133M 21s
235950K .......... .......... .......... .......... .......... 44% 32.8M 21s
236000K .......... .......... .......... .......... .......... 44% 8.11M 21s
236050K .......... .......... .......... .......... .......... 44% 210M 21s
236100K .......... .......... .......... .......... .......... 44% 161M 21s
236150K .......... .......... .......... .......... .......... 44% 212M 21s
236200K .......... .......... .......... .......... .......... 44% 176M 21s
236250K .......... .......... .......... .......... .......... 44% 5.32M 21s
236300K .......... .......... .......... .......... .......... 44% 120M 21s
236350K .......... .......... .......... .......... .......... 44% 139M 21s
236400K .......... .......... .......... .......... .......... 44% 170M 21s
236450K .......... .......... .......... .......... .......... 44% 241M 21s
236500K .......... .......... .......... .......... .......... 44% 260K 21s
236550K .......... .......... .......... .......... .......... 44% 94.8M 21s
236600K .......... .......... .......... .......... .......... 44% 124M 21s
236650K .......... .......... .......... .......... .......... 44% 76.5M 21s
236700K .......... .......... .......... .......... .......... 44% 71.4M 21s
236750K .......... .......... .......... .......... .......... 44% 126M 21s
236800K .......... .......... .......... .......... .......... 44% 95.4M 21s
236850K .......... .......... .......... .......... .......... 44% 94.6M 21s
236900K .......... .......... .......... .......... .......... 44% 157M 21s
236950K .......... .......... .......... .......... .......... 44% 17.2M 21s
237000K .......... .......... .......... .......... .......... 44% 148M 21s
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237100K .......... .......... .......... .......... .......... 44% 23.2M 21s
237150K .......... .......... .......... .......... .......... 44% 134M 21s
237200K .......... .......... .......... .......... .......... 44% 91.1M 21s
237250K .......... .......... .......... .......... .......... 44% 123M 21s
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237350K .......... .......... .......... .......... .......... 44% 95.4M 21s
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242150K .......... .......... .......... .......... .......... 45% 61.6M 20s
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251100K .......... .......... .......... .......... .......... 47% 89.4M 20s
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251500K .......... .......... .......... .......... .......... 47% 139M 20s
251550K .......... .......... .......... .......... .......... 47% 28.3M 20s
251600K .......... .......... .......... .......... .......... 47% 26.9M 20s
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251700K .......... .......... .......... .......... .......... 47% 146M 20s
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251800K .......... .......... .......... .......... .......... 47% 164M 20s
251850K .......... .......... .......... .......... .......... 47% 24.8M 20s
251900K .......... .......... .......... .......... .......... 47% 1.72M 20s
251950K .......... .......... .......... .......... .......... 47% 106M 20s
252000K .......... .......... .......... .......... .......... 47% 75.5M 20s
252050K .......... .......... .......... .......... .......... 47% 82.9M 20s
252100K .......... .......... .......... .......... .......... 47% 48.6M 20s
252150K .......... .......... .......... .......... .......... 47% 64.3M 20s
252200K .......... .......... .......... .......... .......... 47% 45.1M 20s
252250K .......... .......... .......... .......... .......... 47% 58.2M 20s
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253100K .......... .......... .......... .......... .......... 47% 26.5M 19s
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255100K .......... .......... .......... .......... .......... 47% 89.6M 19s
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256000K .......... .......... .......... .......... .......... 48% 2.02M 19s
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256100K .......... .......... .......... .......... .......... 48% 25.6M 19s
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266450K .......... .......... .......... .......... .......... 49% 142M 18s
266500K .......... .......... .......... .......... .......... 49% 140M 18s
266550K .......... .......... .......... .......... .......... 50% 95.0M 18s
266600K .......... .......... .......... .......... .......... 50% 18.9M 18s
266650K .......... .......... .......... .......... .......... 50% 206M 18s
266700K .......... .......... .......... .......... .......... 50% 131M 18s
266750K .......... .......... .......... .......... .......... 50% 197M 18s
266800K .......... .......... .......... .......... .......... 50% 271M 18s
266850K .......... .......... .......... .......... .......... 50% 158M 18s
266900K .......... .......... .......... .......... .......... 50% 198M 18s
266950K .......... .......... .......... .......... .......... 50% 187M 18s
267000K .......... .......... .......... .......... .......... 50% 303M 18s
267050K .......... .......... .......... .......... .......... 50% 289M 18s
267100K .......... .......... .......... .......... .......... 50% 66.7M 18s
267150K .......... .......... .......... .......... .......... 50% 249M 18s
267200K .......... .......... .......... .......... .......... 50% 241M 18s
267250K .......... .......... .......... .......... .......... 50% 210M 18s
267300K .......... .......... .......... .......... .......... 50% 323M 18s
267350K .......... .......... .......... .......... .......... 50% 213M 18s
267400K .......... .......... .......... .......... .......... 50% 265M 18s
267450K .......... .......... .......... .......... .......... 50% 14.2M 18s
267500K .......... .......... .......... .......... .......... 50% 26.0M 18s
267550K .......... .......... .......... .......... .......... 50% 188M 18s
267600K .......... .......... .......... .......... .......... 50% 159M 18s
267650K .......... .......... .......... .......... .......... 50% 28.7M 18s
267700K .......... .......... .......... .......... .......... 50% 166M 18s
267750K .......... .......... .......... .......... .......... 50% 10.5M 18s
267800K .......... .......... .......... .......... .......... 50% 132M 18s
267850K .......... .......... .......... .......... .......... 50% 24.7M 18s
267900K .......... .......... .......... .......... .......... 50% 159M 18s
267950K .......... .......... .......... .......... .......... 50% 144M 18s
268000K .......... .......... .......... .......... .......... 50% 146M 18s
268050K .......... .......... .......... .......... .......... 50% 9.17M 18s
268100K .......... .......... .......... .......... .......... 50% 76.3M 18s
268150K .......... .......... .......... .......... .......... 50% 211M 18s
268200K .......... .......... .......... .......... .......... 50% 184M 18s
268250K .......... .......... .......... .......... .......... 50% 2.69M 18s
268300K .......... .......... .......... .......... .......... 50% 127M 18s
268350K .......... .......... .......... .......... .......... 50% 170M 18s
268400K .......... .......... .......... .......... .......... 50% 148M 18s
268450K .......... .......... .......... .......... .......... 50% 136M 18s
268500K .......... .......... .......... .......... .......... 50% 168M 18s
268550K .......... .......... .......... .......... .......... 50% 155M 18s
268600K .......... .......... .......... .......... .......... 50% 203M 18s
268650K .......... .......... .......... .......... .......... 50% 189M 18s
268700K .......... .......... .......... .......... .......... 50% 184M 18s
268750K .......... .......... .......... .......... .......... 50% 206M 18s
268800K .......... .......... .......... .......... .......... 50% 227M 18s
268850K .......... .......... .......... .......... .......... 50% 187M 18s
268900K .......... .......... .......... .......... .......... 50% 10.0M 18s
268950K .......... .......... .......... .......... .......... 50% 114M 18s
269000K .......... .......... .......... .......... .......... 50% 132M 18s
269050K .......... .......... .......... .......... .......... 50% 92.1M 18s
269100K .......... .......... .......... .......... .......... 50% 101M 18s
269150K .......... .......... .......... .......... .......... 50% 148M 18s
269200K .......... .......... .......... .......... .......... 50% 136M 18s
269250K .......... .......... .......... .......... .......... 50% 7.37M 18s
269300K .......... .......... .......... .......... .......... 50% 950K 18s
269350K .......... .......... .......... .......... .......... 50% 110M 18s
269400K .......... .......... .......... .......... .......... 50% 149M 18s
269450K .......... .......... .......... .......... .......... 50% 86.7M 18s
269500K .......... .......... .......... .......... .......... 50% 133M 18s
269550K .......... .......... .......... .......... .......... 50% 84.5M 18s
269600K .......... .......... .......... .......... .......... 50% 33.1M 18s
269650K .......... .......... .......... .......... .......... 50% 10.8M 18s
269700K .......... .......... .......... .......... .......... 50% 75.0M 18s
269750K .......... .......... .......... .......... .......... 50% 213M 18s
269800K .......... .......... .......... .......... .......... 50% 114M 18s
269850K .......... .......... .......... .......... .......... 50% 158M 18s
269900K .......... .......... .......... .......... .......... 50% 186M 18s
269950K .......... .......... .......... .......... .......... 50% 159M 18s
270000K .......... .......... .......... .......... .......... 50% 139M 18s
270050K .......... .......... .......... .......... .......... 50% 209M 18s
270100K .......... .......... .......... .......... .......... 50% 128M 18s
270150K .......... .......... .......... .......... .......... 50% 28.7M 18s
270200K .......... .......... .......... .......... .......... 50% 92.0M 18s
270250K .......... .......... .......... .......... .......... 50% 50.5M 18s
270300K .......... .......... .......... .......... .......... 50% 7.65M 18s
270350K .......... .......... .......... .......... .......... 50% 59.2M 18s
270400K .......... .......... .......... .......... .......... 50% 40.4M 18s
270450K .......... .......... .......... .......... .......... 50% 164M 18s
270500K .......... .......... .......... .......... .......... 50% 186M 18s
270550K .......... .......... .......... .......... .......... 50% 300M 18s
270600K .......... .......... .......... .......... .......... 50% 213M 18s
270650K .......... .......... .......... .......... .......... 50% 192M 18s
270700K .......... .......... .......... .......... .......... 50% 235M 18s
270750K .......... .......... .......... .......... .......... 50% 111M 18s
270800K .......... .......... .......... .......... .......... 50% 236M 18s
270850K .......... .......... .......... .......... .......... 50% 166M 18s
270900K .......... .......... .......... .......... .......... 50% 188M 18s
270950K .......... .......... .......... .......... .......... 50% 273M 18s
271000K .......... .......... .......... .......... .......... 50% 10.4M 18s
271050K .......... .......... .......... .......... .......... 50% 194M 18s
271100K .......... .......... .......... .......... .......... 50% 103M 18s
271150K .......... .......... .......... .......... .......... 50% 135M 18s
271200K .......... .......... .......... .......... .......... 50% 105M 18s
271250K .......... .......... .......... .......... .......... 50% 168M 18s
271300K .......... .......... .......... .......... .......... 50% 220M 18s
271350K .......... .......... .......... .......... .......... 50% 689K 18s
271400K .......... .......... .......... .......... .......... 50% 118M 18s
271450K .......... .......... .......... .......... .......... 50% 26.5M 18s
271500K .......... .......... .......... .......... .......... 50% 121M 18s
271550K .......... .......... .......... .......... .......... 50% 208M 18s
271600K .......... .......... .......... .......... .......... 50% 123M 18s
271650K .......... .......... .......... .......... .......... 50% 104M 18s
271700K .......... .......... .......... .......... .......... 50% 140M 18s
271750K .......... .......... .......... .......... .......... 50% 153M 18s
271800K .......... .......... .......... .......... .......... 50% 189M 18s
271850K .......... .......... .......... .......... .......... 50% 135M 18s
271900K .......... .......... .......... .......... .......... 51% 28.4M 18s
271950K .......... .......... .......... .......... .......... 51% 140M 18s
272000K .......... .......... .......... .......... .......... 51% 188M 18s
272050K .......... .......... .......... .......... .......... 51% 30.5M 18s
272100K .......... .......... .......... .......... .......... 51% 243M 18s
272150K .......... .......... .......... .......... .......... 51% 264M 18s
272200K .......... .......... .......... .......... .......... 51% 265M 18s
272250K .......... .......... .......... .......... .......... 51% 264M 18s
272300K .......... .......... .......... .......... .......... 51% 279M 18s
272350K .......... .......... .......... .......... .......... 51% 325K 18s
272400K .......... .......... .......... .......... .......... 51% 17.6M 18s
272450K .......... .......... .......... .......... .......... 51% 59.0M 18s
272500K .......... .......... .......... .......... .......... 51% 65.9M 18s
272550K .......... .......... .......... .......... .......... 51% 90.1M 18s
272600K .......... .......... .......... .......... .......... 51% 24.9M 18s
272650K .......... .......... .......... .......... .......... 51% 71.5M 18s
272700K .......... .......... .......... .......... .......... 51% 117M 18s
272750K .......... .......... .......... .......... .......... 51% 124M 18s
272800K .......... .......... .......... .......... .......... 51% 151M 18s
272850K .......... .......... .......... .......... .......... 51% 68.3M 18s
272900K .......... .......... .......... .......... .......... 51% 126M 18s
272950K .......... .......... .......... .......... .......... 51% 108M 18s
273000K .......... .......... .......... .......... .......... 51% 102M 18s
273050K .......... .......... .......... .......... .......... 51% 146M 18s
273100K .......... .......... .......... .......... .......... 51% 159M 18s
273150K .......... .......... .......... .......... .......... 51% 205M 18s
273200K .......... .......... .......... .......... .......... 51% 148M 18s
273250K .......... .......... .......... .......... .......... 51% 163M 18s
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273400K .......... .......... .......... .......... .......... 51% 11.3M 18s
273450K .......... .......... .......... .......... .......... 51% 82.3M 18s
273500K .......... .......... .......... .......... .......... 51% 28.3M 18s
273550K .......... .......... .......... .......... .......... 51% 138M 18s
273600K .......... .......... .......... .......... .......... 51% 128M 18s
273650K .......... .......... .......... .......... .......... 51% 170M 18s
273700K .......... .......... .......... .......... .......... 51% 168M 18s
273750K .......... .......... .......... .......... .......... 51% 178M 18s
273800K .......... .......... .......... .......... .......... 51% 193M 18s
273850K .......... .......... .......... .......... .......... 51% 168M 18s
273900K .......... .......... .......... .......... .......... 51% 9.67M 18s
273950K .......... .......... .......... .......... .......... 51% 79.5M 18s
274000K .......... .......... .......... .......... .......... 51% 83.6M 18s
274050K .......... .......... .......... .......... .......... 51% 78.9M 18s
274100K .......... .......... .......... .......... .......... 51% 159M 18s
274150K .......... .......... .......... .......... .......... 51% 177M 18s
274200K .......... .......... .......... .......... .......... 51% 5.23M 18s
274250K .......... .......... .......... .......... .......... 51% 59.5M 18s
274300K .......... .......... .......... .......... .......... 51% 130M 18s
274350K .......... .......... .......... .......... .......... 51% 128M 18s
274400K .......... .......... .......... .......... .......... 51% 8.71M 18s
274450K .......... .......... .......... .......... .......... 51% 68.1M 18s
274500K .......... .......... .......... .......... .......... 51% 86.0M 18s
274550K .......... .......... .......... .......... .......... 51% 27.7M 18s
274600K .......... .......... .......... .......... .......... 51% 168M 18s
274650K .......... .......... .......... .......... .......... 51% 106M 18s
274700K .......... .......... .......... .......... .......... 51% 133M 18s
274750K .......... .......... .......... .......... .......... 51% 138M 18s
274800K .......... .......... .......... .......... .......... 51% 9.29M 18s
274850K .......... .......... .......... .......... .......... 51% 26.8M 18s
274900K .......... .......... .......... .......... .......... 51% 101M 18s
274950K .......... .......... .......... .......... .......... 51% 164M 18s
275000K .......... .......... .......... .......... .......... 51% 196M 18s
275050K .......... .......... .......... .......... .......... 51% 28.4M 18s
275100K .......... .......... .......... .......... .......... 51% 7.37M 18s
275150K .......... .......... .......... .......... .......... 51% 96.3M 18s
275200K .......... .......... .......... .......... .......... 51% 123M 18s
275250K .......... .......... .......... .......... .......... 51% 171M 18s
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275350K .......... .......... .......... .......... .......... 51% 28.0M 18s
275400K .......... .......... .......... .......... .......... 51% 186M 18s
275450K .......... .......... .......... .......... .......... 51% 570K 18s
275500K .......... .......... .......... .......... .......... 51% 80.4M 18s
275550K .......... .......... .......... .......... .......... 51% 134M 18s
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275650K .......... .......... .......... .......... .......... 51% 89.3M 18s
275700K .......... .......... .......... .......... .......... 51% 130M 18s
275750K .......... .......... .......... .......... .......... 51% 13.4M 18s
275800K .......... .......... .......... .......... .......... 51% 109M 18s
275850K .......... .......... .......... .......... .......... 51% 15.5M 18s
275900K .......... .......... .......... .......... .......... 51% 150M 18s
275950K .......... .......... .......... .......... .......... 51% 154M 18s
276000K .......... .......... .......... .......... .......... 51% 160M 18s
276050K .......... .......... .......... .......... .......... 51% 57.0M 18s
276100K .......... .......... .......... .......... .......... 51% 122M 18s
276150K .......... .......... .......... .......... .......... 51% 132M 18s
276200K .......... .......... .......... .......... .......... 51% 28.4M 18s
276250K .......... .......... .......... .......... .......... 51% 109M 18s
276300K .......... .......... .......... .......... .......... 51% 148M 18s
276350K .......... .......... .......... .......... .......... 51% 27.1M 18s
276400K .......... .......... .......... .......... .......... 51% 86.4M 18s
276450K .......... .......... .......... .......... .......... 51% 91.1M 18s
276500K .......... .......... .......... .......... .......... 51% 25.0M 17s
276550K .......... .......... .......... .......... .......... 51% 80.2M 17s
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276650K .......... .......... .......... .......... .......... 51% 136M 17s
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276750K .......... .......... .......... .......... .......... 51% 117M 17s
276800K .......... .......... .......... .......... .......... 51% 98.2M 17s
276850K .......... .......... .......... .......... .......... 51% 88.3M 17s
276900K .......... .......... .......... .......... .......... 51% 28.5M 17s
276950K .......... .......... .......... .......... .......... 51% 9.65M 17s
277000K .......... .......... .......... .......... .......... 51% 156M 17s
277050K .......... .......... .......... .......... .......... 51% 150M 17s
277100K .......... .......... .......... .......... .......... 51% 97.9M 17s
277150K .......... .......... .......... .......... .......... 51% 166M 17s
277200K .......... .......... .......... .......... .......... 52% 131M 17s
277250K .......... .......... .......... .......... .......... 52% 7.47M 17s
277300K .......... .......... .......... .......... .......... 52% 97.5M 17s
277350K .......... .......... .......... .......... .......... 52% 160M 17s
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277450K .......... .......... .......... .......... .......... 52% 81.5M 17s
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277550K .......... .......... .......... .......... .......... 52% 69.7M 18s
277600K .......... .......... .......... .......... .......... 52% 43.4M 18s
277650K .......... .......... .......... .......... .......... 52% 127M 17s
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278000K .......... .......... .......... .......... .......... 52% 121M 17s
278050K .......... .......... .......... .......... .......... 52% 127M 17s
278100K .......... .......... .......... .......... .......... 52% 109M 17s
278150K .......... .......... .......... .......... .......... 52% 94.6M 17s
278200K .......... .......... .......... .......... .......... 52% 136M 17s
278250K .......... .......... .......... .......... .......... 52% 164M 17s
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278500K .......... .......... .......... .......... .......... 52% 11.2M 17s
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278650K .......... .......... .......... .......... .......... 52% 96.9M 17s
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278800K .......... .......... .......... .......... .......... 52% 76.5M 17s
278850K .......... .......... .......... .......... .......... 52% 96.7M 17s
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278950K .......... .......... .......... .......... .......... 52% 84.6M 17s
279000K .......... .......... .......... .......... .......... 52% 6.76M 17s
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279100K .......... .......... .......... .......... .......... 52% 16.9M 17s
279150K .......... .......... .......... .......... .......... 52% 144M 17s
279200K .......... .......... .......... .......... .......... 52% 135M 17s
279250K .......... .......... .......... .......... .......... 52% 6.52M 17s
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279850K .......... .......... .......... .......... .......... 52% 72.1M 17s
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280000K .......... .......... .......... .......... .......... 52% 186M 17s
280050K .......... .......... .......... .......... .......... 52% 193M 17s
280100K .......... .......... .......... .......... .......... 52% 168M 17s
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280400K .......... .......... .......... .......... .......... 52% 211M 17s
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280550K .......... .......... .......... .......... .......... 52% 454K 17s
280600K .......... .......... .......... .......... .......... 52% 113M 17s
280650K .......... .......... .......... .......... .......... 52% 128M 17s
280700K .......... .......... .......... .......... .......... 52% 121M 17s
280750K .......... .......... .......... .......... .......... 52% 141M 17s
280800K .......... .......... .......... .......... .......... 52% 126M 17s
280850K .......... .......... .......... .......... .......... 52% 107M 17s
280900K .......... .......... .......... .......... .......... 52% 97.5M 17s
280950K .......... .......... .......... .......... .......... 52% 41.9M 17s
281000K .......... .......... .......... .......... .......... 52% 71.1M 17s
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281100K .......... .......... .......... .......... .......... 52% 160M 17s
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281200K .......... .......... .......... .......... .......... 52% 169M 17s
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281300K .......... .......... .......... .......... .......... 52% 231M 17s
281350K .......... .......... .......... .......... .......... 52% 207M 17s
281400K .......... .......... .......... .......... .......... 52% 239M 17s
281450K .......... .......... .......... .......... .......... 52% 198M 17s
281500K .......... .......... .......... .......... .......... 52% 230M 17s
281550K .......... .......... .......... .......... .......... 52% 135M 17s
281600K .......... .......... .......... .......... .......... 52% 12.7M 17s
281650K .......... .......... .......... .......... .......... 52% 203M 17s
281700K .......... .......... .......... .......... .......... 52% 111M 17s
281750K .......... .......... .......... .......... .......... 52% 131M 17s
281800K .......... .......... .......... .......... .......... 52% 117M 17s
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281900K .......... .......... .......... .......... .......... 52% 163M 17s
281950K .......... .......... .......... .......... .......... 52% 175M 17s
282000K .......... .......... .......... .......... .......... 52% 170M 17s
282050K .......... .......... .......... .......... .......... 52% 8.81M 17s
282100K .......... .......... .......... .......... .......... 52% 150M 17s
282150K .......... .......... .......... .......... .......... 52% 172M 17s
282200K .......... .......... .......... .......... .......... 52% 175M 17s
282250K .......... .......... .......... .......... .......... 52% 213M 17s
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282350K .......... .......... .......... .......... .......... 52% 20.7M 17s
282400K .......... .......... .......... .......... .......... 52% 65.3M 17s
282450K .......... .......... .......... .......... .......... 52% 4.61M 17s
282500K .......... .......... .......... .......... .......... 52% 37.2M 17s
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282600K .......... .......... .......... .......... .......... 53% 1.62M 17s
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282800K .......... .......... .......... .......... .......... 53% 111M 17s
282850K .......... .......... .......... .......... .......... 53% 90.3M 17s
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282950K .......... .......... .......... .......... .......... 53% 164M 17s
283000K .......... .......... .......... .......... .......... 53% 167M 17s
283050K .......... .......... .......... .......... .......... 53% 30.4M 17s
283100K .......... .......... .......... .......... .......... 53% 220M 17s
283150K .......... .......... .......... .......... .......... 53% 294M 17s
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283250K .......... .......... .......... .......... .......... 53% 242M 17s
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283600K .......... .......... .......... .......... .......... 53% 28.5M 17s
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283800K .......... .......... .......... .......... .......... 53% 25.0M 17s
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283900K .......... .......... .......... .......... .......... 53% 237M 17s
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284000K .......... .......... .......... .......... .......... 53% 38.8M 17s
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284100K .......... .......... .......... .......... .......... 53% 134M 17s
284150K .......... .......... .......... .......... .......... 53% 185M 17s
284200K .......... .......... .......... .......... .......... 53% 14.1M 17s
284250K .......... .......... .......... .......... .......... 53% 162M 17s
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284350K .......... .......... .......... .......... .......... 53% 7.42M 17s
284400K .......... .......... .......... .......... .......... 53% 131M 17s
284450K .......... .......... .......... .......... .......... 53% 28.1M 17s
284500K .......... .......... .......... .......... .......... 53% 28.5M 17s
284550K .......... .......... .......... .......... .......... 53% 120M 17s
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284650K .......... .......... .......... .......... .......... 53% 91.6M 17s
284700K .......... .......... .......... .......... .......... 53% 45.8M 17s
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285000K .......... .......... .......... .......... .......... 53% 8.85M 17s
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285100K .......... .......... .......... .......... .......... 53% 95.7M 17s
285150K .......... .......... .......... .......... .......... 53% 173M 17s
285200K .......... .......... .......... .......... .......... 53% 182M 17s
285250K .......... .......... .......... .......... .......... 53% 2.93M 17s
285300K .......... .......... .......... .......... .......... 53% 24.6M 17s
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285400K .......... .......... .......... .......... .......... 53% 11.0M 17s
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285550K .......... .......... .......... .......... .......... 53% 27.7M 17s
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285650K .......... .......... .......... .......... .......... 53% 24.8M 17s
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285750K .......... .......... .......... .......... .......... 53% 71.9M 17s
285800K .......... .......... .......... .......... .......... 53% 92.5M 17s
285850K .......... .......... .......... .......... .......... 53% 67.7M 17s
285900K .......... .......... .......... .......... .......... 53% 195M 17s
285950K .......... .......... .......... .......... .......... 53% 84.8M 17s
286000K .......... .......... .......... .......... .......... 53% 118M 17s
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286100K .......... .......... .......... .......... .......... 53% 138M 17s
286150K .......... .......... .......... .......... .......... 53% 92.8M 17s
286200K .......... .......... .......... .......... .......... 53% 75.1M 17s
286250K .......... .......... .......... .......... .......... 53% 95.6M 17s
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286350K .......... .......... .......... .......... .......... 53% 63.2M 17s
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286550K .......... .......... .......... .......... .......... 53% 91.8M 17s
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286750K .......... .......... .......... .......... .......... 53% 26.7M 17s
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286850K .......... .......... .......... .......... .......... 53% 17.9M 17s
286900K .......... .......... .......... .......... .......... 53% 66.1M 17s
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287000K .......... .......... .......... .......... .......... 53% 102M 17s
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287100K .......... .......... .......... .......... .......... 53% 88.0M 17s
287150K .......... .......... .......... .......... .......... 53% 203M 17s
287200K .......... .......... .......... .......... .......... 53% 24.0M 17s
287250K .......... .......... .......... .......... .......... 53% 6.66M 17s
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288000K .......... .......... .......... .......... .......... 54% 136M 17s
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288100K .......... .......... .......... .......... .......... 54% 109M 17s
288150K .......... .......... .......... .......... .......... 54% 5.63M 17s
288200K .......... .......... .......... .......... .......... 54% 149M 17s
288250K .......... .......... .......... .......... .......... 54% 136M 17s
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288550K .......... .......... .......... .......... .......... 54% 8.35M 17s
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288850K .......... .......... .......... .......... .......... 54% 75.0M 17s
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289000K .......... .......... .......... .......... .......... 54% 116M 17s
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289100K .......... .......... .......... .......... .......... 54% 132M 17s
289150K .......... .......... .......... .......... .......... 54% 133M 17s
289200K .......... .......... .......... .......... .......... 54% 136M 17s
289250K .......... .......... .......... .......... .......... 54% 210M 17s
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290900K .......... .......... .......... .......... .......... 54% 87.8M 16s
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291000K .......... .......... .......... .......... .......... 54% 126M 16s
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291500K .......... .......... .......... .......... .......... 54% 210M 16s
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291800K .......... .......... .......... .......... .......... 54% 160M 16s
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291900K .......... .......... .......... .......... .......... 54% 207M 16s
291950K .......... .......... .......... .......... .......... 54% 179M 16s
292000K .......... .......... .......... .......... .......... 54% 14.2M 16s
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292100K .......... .......... .......... .......... .......... 54% 135M 16s
292150K .......... .......... .......... .......... .......... 54% 203M 16s
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292250K .......... .......... .......... .......... .......... 54% 220M 16s
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292800K .......... .......... .......... .......... .......... 54% 216M 16s
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293000K .......... .......... .......... .......... .......... 54% 119M 16s
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293100K .......... .......... .......... .......... .......... 54% 72.6M 16s
293150K .......... .......... .......... .......... .......... 54% 223M 16s
293200K .......... .......... .......... .......... .......... 55% 196M 16s
293250K .......... .......... .......... .......... .......... 55% 226M 16s
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293700K .......... .......... .......... .......... .......... 55% 9.54M 16s
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293900K .......... .......... .......... .......... .......... 55% 65.4M 16s
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294000K .......... .......... .......... .......... .......... 55% 159M 16s
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294100K .......... .......... .......... .......... .......... 55% 79.9M 16s
294150K .......... .......... .......... .......... .......... 55% 175M 16s
294200K .......... .......... .......... .......... .......... 55% 162M 16s
294250K .......... .......... .......... .......... .......... 55% 194M 16s
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294450K .......... .......... .......... .......... .......... 55% 82.9M 16s
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294900K .......... .......... .......... .......... .......... 55% 8.23M 16s
294950K .......... .......... .......... .......... .......... 55% 97.5M 16s
295000K .......... .......... .......... .......... .......... 55% 138M 16s
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295100K .......... .......... .......... .......... .......... 55% 154M 16s
295150K .......... .......... .......... .......... .......... 55% 158M 16s
295200K .......... .......... .......... .......... .......... 55% 144M 16s
295250K .......... .......... .......... .......... .......... 55% 154M 16s
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295400K .......... .......... .......... .......... .......... 55% 3.60M 16s
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295750K .......... .......... .......... .......... .......... 55% 5.76M 16s
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296000K .......... .......... .......... .......... .......... 55% 126M 16s
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296100K .......... .......... .......... .......... .......... 55% 38.3M 16s
296150K .......... .......... .......... .......... .......... 55% 150M 16s
296200K .......... .......... .......... .......... .......... 55% 94.6M 16s
296250K .......... .......... .......... .......... .......... 55% 129M 16s
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296350K .......... .......... .......... .......... .......... 55% 68.1M 16s
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297000K .......... .......... .......... .......... .......... 55% 4.69M 16s
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297100K .......... .......... .......... .......... .......... 55% 137M 16s
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297200K .......... .......... .......... .......... .......... 55% 106M 16s
297250K .......... .......... .......... .......... .......... 55% 93.5M 16s
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300050K .......... .......... .......... .......... .......... 56% 77.6M 16s
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311150K .......... .......... .......... .......... .......... 58% 138M 15s
311200K .......... .......... .......... .......... .......... 58% 180M 15s
311250K .......... .......... .......... .......... .......... 58% 171M 15s
311300K .......... .......... .......... .......... .......... 58% 7.37M 15s
311350K .......... .......... .......... .......... .......... 58% 148M 15s
311400K .......... .......... .......... .......... .......... 58% 191M 15s
311450K .......... .......... .......... .......... .......... 58% 137M 15s
311500K .......... .......... .......... .......... .......... 58% 188M 15s
311550K .......... .......... .......... .......... .......... 58% 148M 15s
311600K .......... .......... .......... .......... .......... 58% 3.80M 15s
311650K .......... .......... .......... .......... .......... 58% 121M 15s
311700K .......... .......... .......... .......... .......... 58% 98.8M 15s
311750K .......... .......... .......... .......... .......... 58% 150M 15s
311800K .......... .......... .......... .......... .......... 58% 176M 15s
311850K .......... .......... .......... .......... .......... 58% 144M 15s
311900K .......... .......... .......... .......... .......... 58% 83.5M 15s
311950K .......... .......... .......... .......... .......... 58% 6.17M 15s
312000K .......... .......... .......... .......... .......... 58% 135M 15s
312050K .......... .......... .......... .......... .......... 58% 205M 15s
312100K .......... .......... .......... .......... .......... 58% 203M 15s
312150K .......... .......... .......... .......... .......... 58% 108M 15s
312200K .......... .......... .......... .......... .......... 58% 198M 15s
312250K .......... .......... .......... .......... .......... 58% 197M 15s
312300K .......... .......... .......... .......... .......... 58% 5.03M 15s
312350K .......... .......... .......... .......... .......... 58% 152M 15s
312400K .......... .......... .......... .......... .......... 58% 156M 15s
312450K .......... .......... .......... .......... .......... 58% 188M 15s
312500K .......... .......... .......... .......... .......... 58% 250M 15s
312550K .......... .......... .......... .......... .......... 58% 184M 15s
312600K .......... .......... .......... .......... .......... 58% 127M 15s
312650K .......... .......... .......... .......... .......... 58% 5.80M 15s
312700K .......... .......... .......... .......... .......... 58% 120M 15s
312750K .......... .......... .......... .......... .......... 58% 138M 15s
312800K .......... .......... .......... .......... .......... 58% 182M 15s
312850K .......... .......... .......... .......... .......... 58% 212M 15s
312900K .......... .......... .......... .......... .......... 58% 191M 15s
312950K .......... .......... .......... .......... .......... 58% 173M 15s
313000K .......... .......... .......... .......... .......... 58% 6.98M 15s
313050K .......... .......... .......... .......... .......... 58% 168M 15s
313100K .......... .......... .......... .......... .......... 58% 171M 15s
313150K .......... .......... .......... .......... .......... 58% 138M 15s
313200K .......... .......... .......... .......... .......... 58% 150M 15s
313250K .......... .......... .......... .......... .......... 58% 180M 15s
313300K .......... .......... .......... .......... .......... 58% 180M 14s
313350K .......... .......... .......... .......... .......... 58% 604K 15s
313400K .......... .......... .......... .......... .......... 58% 187M 15s
313450K .......... .......... .......... .......... .......... 58% 113M 15s
313500K .......... .......... .......... .......... .......... 58% 122M 15s
313550K .......... .......... .......... .......... .......... 58% 62.9M 15s
313600K .......... .......... .......... .......... .......... 58% 126M 15s
313650K .......... .......... .......... .......... .......... 58% 123M 15s
313700K .......... .......... .......... .......... .......... 58% 152M 15s
313750K .......... .......... .......... .......... .......... 58% 116M 15s
313800K .......... .......... .......... .......... .......... 58% 111M 15s
313850K .......... .......... .......... .......... .......... 58% 104M 14s
313900K .......... .......... .......... .......... .......... 58% 162M 14s
313950K .......... .......... .......... .......... .......... 58% 111M 14s
314000K .......... .......... .......... .......... .......... 58% 70.9M 14s
314050K .......... .......... .......... .......... .......... 58% 142M 14s
314100K .......... .......... .......... .......... .......... 58% 236M 14s
314150K .......... .......... .......... .......... .......... 58% 247M 14s
314200K .......... .......... .......... .......... .......... 58% 244M 14s
314250K .......... .......... .......... .......... .......... 58% 237M 14s
314300K .......... .......... .......... .......... .......... 58% 260M 14s
314350K .......... .......... .......... .......... .......... 58% 173M 14s
314400K .......... .......... .......... .......... .......... 58% 214M 14s
314450K .......... .......... .......... .......... .......... 58% 210M 14s
314500K .......... .......... .......... .......... .......... 58% 166M 14s
314550K .......... .......... .......... .......... .......... 59% 9.63M 14s
314600K .......... .......... .......... .......... .......... 59% 107M 14s
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314700K .......... .......... .......... .......... .......... 59% 140M 14s
314750K .......... .......... .......... .......... .......... 59% 138M 14s
314800K .......... .......... .......... .......... .......... 59% 160M 14s
314850K .......... .......... .......... .......... .......... 59% 5.37M 14s
314900K .......... .......... .......... .......... .......... 59% 156M 14s
314950K .......... .......... .......... .......... .......... 59% 221M 14s
315000K .......... .......... .......... .......... .......... 59% 212M 14s
315050K .......... .......... .......... .......... .......... 59% 147M 14s
315100K .......... .......... .......... .......... .......... 59% 97.1M 14s
315150K .......... .......... .......... .......... .......... 59% 115M 14s
315200K .......... .......... .......... .......... .......... 59% 149M 14s
315250K .......... .......... .......... .......... .......... 59% 8.70M 14s
315300K .......... .......... .......... .......... .......... 59% 128M 14s
315350K .......... .......... .......... .......... .......... 59% 1.08M 14s
315400K .......... .......... .......... .......... .......... 59% 105M 14s
315450K .......... .......... .......... .......... .......... 59% 142M 14s
315500K .......... .......... .......... .......... .......... 59% 175M 14s
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315600K .......... .......... .......... .......... .......... 59% 117M 14s
315650K .......... .......... .......... .......... .......... 59% 125M 14s
315700K .......... .......... .......... .......... .......... 59% 102M 14s
315750K .......... .......... .......... .......... .......... 59% 150M 14s
315800K .......... .......... .......... .......... .......... 59% 127M 14s
315850K .......... .......... .......... .......... .......... 59% 114M 14s
315900K .......... .......... .......... .......... .......... 59% 132M 14s
315950K .......... .......... .......... .......... .......... 59% 100M 14s
316000K .......... .......... .......... .......... .......... 59% 148M 14s
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316100K .......... .......... .......... .......... .......... 59% 111M 14s
316150K .......... .......... .......... .......... .......... 59% 153M 14s
316200K .......... .......... .......... .......... .......... 59% 151M 14s
316250K .......... .......... .......... .......... .......... 59% 185M 14s
316300K .......... .......... .......... .......... .......... 59% 178M 14s
316350K .......... .......... .......... .......... .......... 59% 167M 14s
316400K .......... .......... .......... .......... .......... 59% 10.9M 14s
316450K .......... .......... .......... .......... .......... 59% 101M 14s
316500K .......... .......... .......... .......... .......... 59% 158M 14s
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316600K .......... .......... .......... .......... .......... 59% 112M 14s
316650K .......... .......... .......... .......... .......... 59% 185M 14s
316700K .......... .......... .......... .......... .......... 59% 136M 14s
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316800K .......... .......... .......... .......... .......... 59% 195M 14s
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316900K .......... .......... .......... .......... .......... 59% 6.38M 14s
316950K .......... .......... .......... .......... .......... 59% 126M 14s
317000K .......... .......... .......... .......... .......... 59% 191M 14s
317050K .......... .......... .......... .......... .......... 59% 110M 14s
317100K .......... .......... .......... .......... .......... 59% 177M 14s
317150K .......... .......... .......... .......... .......... 59% 155M 14s
317200K .......... .......... .......... .......... .......... 59% 134M 14s
317250K .......... .......... .......... .......... .......... 59% 6.91M 14s
317300K .......... .......... .......... .......... .......... 59% 158M 14s
317350K .......... .......... .......... .......... .......... 59% 178M 14s
317400K .......... .......... .......... .......... .......... 59% 454K 14s
317450K .......... .......... .......... .......... .......... 59% 128M 14s
317500K .......... .......... .......... .......... .......... 59% 193M 14s
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317600K .......... .......... .......... .......... .......... 59% 103M 14s
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317700K .......... .......... .......... .......... .......... 59% 105M 14s
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317800K .......... .......... .......... .......... .......... 59% 107M 14s
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317900K .......... .......... .......... .......... .......... 59% 148M 14s
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318000K .......... .......... .......... .......... .......... 59% 164M 14s
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318100K .......... .......... .......... .......... .......... 59% 70.7M 14s
318150K .......... .......... .......... .......... .......... 59% 78.3M 14s
318200K .......... .......... .......... .......... .......... 59% 134M 14s
318250K .......... .......... .......... .......... .......... 59% 205M 14s
318300K .......... .......... .......... .......... .......... 59% 161M 14s
318350K .......... .......... .......... .......... .......... 59% 112M 14s
318400K .......... .......... .......... .......... .......... 59% 171M 14s
318450K .......... .......... .......... .......... .......... 59% 10.1M 14s
318500K .......... .......... .......... .......... .......... 59% 109M 14s
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318600K .......... .......... .......... .......... .......... 59% 132M 14s
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318700K .......... .......... .......... .......... .......... 59% 166M 14s
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318800K .......... .......... .......... .......... .......... 59% 157M 14s
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318900K .......... .......... .......... .......... .......... 59% 178M 14s
318950K .......... .......... .......... .......... .......... 59% 5.97M 14s
319000K .......... .......... .......... .......... .......... 59% 178M 14s
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319100K .......... .......... .......... .......... .......... 59% 143M 14s
319150K .......... .......... .......... .......... .......... 59% 147M 14s
319200K .......... .......... .......... .......... .......... 59% 133M 14s
319250K .......... .......... .......... .......... .......... 59% 148M 14s
319300K .......... .......... .......... .......... .......... 59% 6.56M 14s
319350K .......... .......... .......... .......... .......... 59% 111M 14s
319400K .......... .......... .......... .......... .......... 59% 217M 14s
319450K .......... .......... .......... .......... .......... 59% 798K 14s
319500K .......... .......... .......... .......... .......... 59% 198M 14s
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319600K .......... .......... .......... .......... .......... 59% 79.4M 14s
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319700K .......... .......... .......... .......... .......... 59% 141M 14s
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319800K .......... .......... .......... .......... .......... 59% 96.7M 14s
319850K .......... .......... .......... .......... .......... 60% 122M 14s
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320000K .......... .......... .......... .......... .......... 60% 184M 14s
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320500K .......... .......... .......... .......... .......... 60% 5.80M 14s
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320700K .......... .......... .......... .......... .......... 60% 236M 14s
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320800K .......... .......... .......... .......... .......... 60% 198M 14s
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321000K .......... .......... .......... .......... .......... 60% 3.23M 14s
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321100K .......... .......... .......... .......... .......... 60% 163M 14s
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321200K .......... .......... .......... .......... .......... 60% 187M 14s
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321350K .......... .......... .......... .......... .......... 60% 8.28M 14s
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321500K .......... .......... .......... .......... .......... 60% 2.51M 14s
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321900K .......... .......... .......... .......... .......... 60% 195M 14s
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322000K .......... .......... .......... .......... .......... 60% 202M 14s
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322100K .......... .......... .......... .......... .......... 60% 94.1M 14s
322150K .......... .......... .......... .......... .......... 60% 147M 14s
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322250K .......... .......... .......... .......... .......... 60% 237M 14s
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323000K .......... .......... .......... .......... .......... 60% 134M 14s
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323100K .......... .......... .......... .......... .......... 60% 173M 14s
323150K .......... .......... .......... .......... .......... 60% 205M 14s
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323250K .......... .......... .......... .......... .......... 60% 228M 14s
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323600K .......... .......... .......... .......... .......... 60% 89.1M 14s
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323700K .......... .......... .......... .......... .......... 60% 73.9M 14s
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323850K .......... .......... .......... .......... .......... 60% 94.1M 14s
323900K .......... .......... .......... .......... .......... 60% 94.6M 14s
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324000K .......... .......... .......... .......... .......... 60% 212M 14s
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324600K .......... .......... .......... .......... .......... 60% 11.3M 14s
324650K .......... .......... .......... .......... .......... 60% 75.7M 14s
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324800K .......... .......... .......... .......... .......... 60% 9.15M 14s
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325000K .......... .......... .......... .......... .......... 60% 180M 14s
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325100K .......... .......... .......... .......... .......... 60% 140M 14s
325150K .......... .......... .......... .......... .......... 60% 173M 14s
325200K .......... .......... .......... .......... .......... 61% 8.79M 14s
325250K .......... .......... .......... .......... .......... 61% 151M 14s
325300K .......... .......... .......... .......... .......... 61% 175M 14s
325350K .......... .......... .......... .......... .......... 61% 163M 14s
325400K .......... .......... .......... .......... .......... 61% 136M 14s
325450K .......... .......... .......... .......... .......... 61% 3.57M 14s
325500K .......... .......... .......... .......... .......... 61% 201M 14s
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325600K .......... .......... .......... .......... .......... 61% 4.33M 14s
325650K .......... .......... .......... .......... .......... 61% 125M 14s
325700K .......... .......... .......... .......... .......... 61% 163M 14s
325750K .......... .......... .......... .......... .......... 61% 140M 14s
325800K .......... .......... .......... .......... .......... 61% 162M 14s
325850K .......... .......... .......... .......... .......... 61% 163M 14s
325900K .......... .......... .......... .......... .......... 61% 142M 14s
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326000K .......... .......... .......... .......... .......... 61% 176M 14s
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326100K .......... .......... .......... .......... .......... 61% 165M 14s
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326200K .......... .......... .......... .......... .......... 61% 115M 14s
326250K .......... .......... .......... .......... .......... 61% 178M 14s
326300K .......... .......... .......... .......... .......... 61% 189M 14s
326350K .......... .......... .......... .......... .......... 61% 7.17M 14s
326400K .......... .......... .......... .......... .......... 61% 126M 14s
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326500K .......... .......... .......... .......... .......... 61% 171M 14s
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326600K .......... .......... .......... .......... .......... 61% 91.8M 14s
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327100K .......... .......... .......... .......... .......... 61% 116M 13s
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330700K .......... .......... .......... .......... .......... 62% 150M 13s
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330800K .......... .......... .......... .......... .......... 62% 117M 13s
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330900K .......... .......... .......... .......... .......... 62% 154M 13s
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331500K .......... .......... .......... .......... .......... 62% 181M 13s
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331600K .......... .......... .......... .......... .......... 62% 87.8M 13s
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331800K .......... .......... .......... .......... .......... 62% 98.6M 13s
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332000K .......... .......... .......... .......... .......... 62% 131M 13s
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332100K .......... .......... .......... .......... .......... 62% 86.9M 13s
332150K .......... .......... .......... .......... .......... 62% 105M 13s
332200K .......... .......... .......... .......... .......... 62% 87.7M 13s
332250K .......... .......... .......... .......... .......... 62% 160M 13s
332300K .......... .......... .......... .......... .......... 62% 138M 13s
332350K .......... .......... .......... .......... .......... 62% 107M 13s
332400K .......... .......... .......... .......... .......... 62% 109M 13s
332450K .......... .......... .......... .......... .......... 62% 141M 13s
332500K .......... .......... .......... .......... .......... 62% 146M 13s
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332900K .......... .......... .......... .......... .......... 62% 152M 13s
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338250K .......... .......... .......... .......... .......... 63% 139M 13s
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340000K .......... .......... .......... .......... .......... 63% 95.0M 13s
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340100K .......... .......... .......... .......... .......... 63% 75.7M 13s
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340200K .......... .......... .......... .......... .......... 63% 109M 13s
340250K .......... .......... .......... .......... .......... 63% 95.0M 13s
340300K .......... .......... .......... .......... .......... 63% 104M 13s
340350K .......... .......... .......... .......... .......... 63% 109M 13s
340400K .......... .......... .......... .......... .......... 63% 182M 13s
340450K .......... .......... .......... .......... .......... 63% 107M 13s
340500K .......... .......... .......... .......... .......... 63% 155M 13s
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340650K .......... .......... .......... .......... .......... 63% 3.86M 13s
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341300K .......... .......... .......... .......... .......... 64% 168M 13s
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341400K .......... .......... .......... .......... .......... 64% 59.6M 13s
341450K .......... .......... .......... .......... .......... 64% 252M 13s
341500K .......... .......... .......... .......... .......... 64% 289M 13s
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341600K .......... .......... .......... .......... .......... 64% 252M 13s
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342150K .......... .......... .......... .......... .......... 64% 119M 12s
342200K .......... .......... .......... .......... .......... 64% 11.5M 12s
342250K .......... .......... .......... .......... .......... 64% 151M 12s
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342500K .......... .......... .......... .......... .......... 64% 4.32M 12s
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342750K .......... .......... .......... .......... .......... 64% 96.3M 12s
342800K .......... .......... .......... .......... .......... 64% 183M 12s
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342900K .......... .......... .......... .......... .......... 64% 4.96M 12s
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343000K .......... .......... .......... .......... .......... 64% 318K 13s
343050K .......... .......... .......... .......... .......... 64% 92.8M 13s
343100K .......... .......... .......... .......... .......... 64% 180M 13s
343150K .......... .......... .......... .......... .......... 64% 186M 13s
343200K .......... .......... .......... .......... .......... 64% 122M 12s
343250K .......... .......... .......... .......... .......... 64% 133M 12s
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344000K .......... .......... .......... .......... .......... 64% 175M 12s
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345000K .......... .......... .......... .......... .......... 64% 171M 12s
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345100K .......... .......... .......... .......... .......... 64% 148M 12s
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345250K .......... .......... .......... .......... .......... 64% 298M 12s
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345350K .......... .......... .......... .......... .......... 64% 75.9M 12s
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346000K .......... .......... .......... .......... .......... 64% 192M 12s
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346100K .......... .......... .......... .......... .......... 64% 300K 12s
346150K .......... .......... .......... .......... .......... 64% 48.8M 12s
346200K .......... .......... .......... .......... .......... 64% 69.8M 12s
346250K .......... .......... .......... .......... .......... 64% 56.1M 12s
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347000K .......... .......... .......... .......... .......... 65% 125M 12s
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347100K .......... .......... .......... .......... .......... 65% 14.7M 12s
347150K .......... .......... .......... .......... .......... 65% 39.0M 12s
347200K .......... .......... .......... .......... .......... 65% 100M 12s
347250K .......... .......... .......... .......... .......... 65% 100M 12s
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347350K .......... .......... .......... .......... .......... 65% 74.7M 12s
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348150K .......... .......... .......... .......... .......... 65% 2.48M 12s
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352000K .......... .......... .......... .......... .......... 66% 157M 12s
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352150K .......... .......... .......... .......... .......... 66% 121M 12s
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353000K .......... .......... .......... .......... .......... 66% 8.68M 12s
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353150K .......... .......... .......... .......... .......... 66% 167M 12s
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353750K .......... .......... .......... .......... .......... 66% 97.3M 12s
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355900K .......... .......... .......... .......... .......... 66% 146M 11s
355950K .......... .......... .......... .......... .......... 66% 6.20M 11s
356000K .......... .......... .......... .......... .......... 66% 102M 11s
356050K .......... .......... .......... .......... .......... 66% 173M 11s
356100K .......... .......... .......... .......... .......... 66% 88.1M 11s
356150K .......... .......... .......... .......... .......... 66% 25.2M 11s
356200K .......... .......... .......... .......... .......... 66% 105M 11s
356250K .......... .......... .......... .......... .......... 66% 12.2M 11s
356300K .......... .......... .......... .......... .......... 66% 24.6M 11s
356350K .......... .......... .......... .......... .......... 66% 1.57M 11s
356400K .......... .......... .......... .......... .......... 66% 119M 11s
356450K .......... .......... .......... .......... .......... 66% 115M 11s
356500K .......... .......... .......... .......... .......... 66% 144M 11s
356550K .......... .......... .......... .......... .......... 66% 109M 11s
356600K .......... .......... .......... .......... .......... 66% 106M 11s
356650K .......... .......... .......... .......... .......... 66% 26.7M 11s
356700K .......... .......... .......... .......... .......... 66% 112M 11s
356750K .......... .......... .......... .......... .......... 66% 204M 11s
356800K .......... .......... .......... .......... .......... 66% 189M 11s
356850K .......... .......... .......... .......... .......... 66% 164M 11s
356900K .......... .......... .......... .......... .......... 66% 184M 11s
356950K .......... .......... .......... .......... .......... 66% 27.4M 11s
357000K .......... .......... .......... .......... .......... 66% 136M 11s
357050K .......... .......... .......... .......... .......... 66% 101M 11s
357100K .......... .......... .......... .......... .......... 66% 84.8M 11s
357150K .......... .......... .......... .......... .......... 66% 165M 11s
357200K .......... .......... .......... .......... .......... 67% 110M 11s
357250K .......... .......... .......... .......... .......... 67% 24.8M 11s
357300K .......... .......... .......... .......... .......... 67% 101M 11s
357350K .......... .......... .......... .......... .......... 67% 972K 11s
357400K .......... .......... .......... .......... .......... 67% 115M 11s
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357600K .......... .......... .......... .......... .......... 67% 94.3M 11s
357650K .......... .......... .......... .......... .......... 67% 115M 11s
357700K .......... .......... .......... .......... .......... 67% 99.4M 11s
357750K .......... .......... .......... .......... .......... 67% 139M 11s
357800K .......... .......... .......... .......... .......... 67% 81.1M 11s
357850K .......... .......... .......... .......... .......... 67% 25.3M 11s
357900K .......... .......... .......... .......... .......... 67% 102M 11s
357950K .......... .......... .......... .......... .......... 67% 189M 11s
358000K .......... .......... .......... .......... .......... 67% 168M 11s
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358100K .......... .......... .......... .......... .......... 67% 200M 11s
358150K .......... .......... .......... .......... .......... 67% 315M 11s
358200K .......... .......... .......... .......... .......... 67% 213M 11s
358250K .......... .......... .......... .......... .......... 67% 253M 11s
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358350K .......... .......... .......... .......... .......... 67% 95.6M 11s
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358450K .......... .......... .......... .......... .......... 67% 93.9M 11s
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358700K .......... .......... .......... .......... .......... 67% 86.4M 11s
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358850K .......... .......... .......... .......... .......... 67% 6.14M 11s
358900K .......... .......... .......... .......... .......... 67% 66.2M 11s
358950K .......... .......... .......... .......... .......... 67% 69.0M 11s
359000K .......... .......... .......... .......... .......... 67% 67.9M 11s
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359100K .......... .......... .......... .......... .......... 67% 73.3M 11s
359150K .......... .......... .......... .......... .......... 67% 5.13M 11s
359200K .......... .......... .......... .......... .......... 67% 76.8M 11s
359250K .......... .......... .......... .......... .......... 67% 106M 11s
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359350K .......... .......... .......... .......... .......... 67% 89.1M 11s
359400K .......... .......... .......... .......... .......... 67% 773K 11s
359450K .......... .......... .......... .......... .......... 67% 44.5M 11s
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360000K .......... .......... .......... .......... .......... 67% 46.9M 11s
360050K .......... .......... .......... .......... .......... 67% 53.6M 11s
360100K .......... .......... .......... .......... .......... 67% 31.9M 11s
360150K .......... .......... .......... .......... .......... 67% 6.39M 11s
360200K .......... .......... .......... .......... .......... 67% 10.7M 11s
360250K .......... .......... .......... .......... .......... 67% 113M 11s
360300K .......... .......... .......... .......... .......... 67% 13.9M 11s
360350K .......... .......... .......... .......... .......... 67% 82.3M 11s
360400K .......... .......... .......... .......... .......... 67% 118M 11s
360450K .......... .......... .......... .......... .......... 67% 10.4M 11s
360500K .......... .......... .......... .......... .......... 67% 66.5M 11s
360550K .......... .......... .......... .......... .......... 67% 142M 11s
360600K .......... .......... .......... .......... .......... 67% 80.4M 11s
360650K .......... .......... .......... .......... .......... 67% 117M 11s
360700K .......... .......... .......... .......... .......... 67% 114M 11s
360750K .......... .......... .......... .......... .......... 67% 151M 11s
360800K .......... .......... .......... .......... .......... 67% 186M 11s
360850K .......... .......... .......... .......... .......... 67% 160M 11s
360900K .......... .......... .......... .......... .......... 67% 26.9M 11s
360950K .......... .......... .......... .......... .......... 67% 162M 11s
361000K .......... .......... .......... .......... .......... 67% 166M 11s
361050K .......... .......... .......... .......... .......... 67% 88.5M 11s
361100K .......... .......... .......... .......... .......... 67% 81.7M 11s
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361200K .......... .......... .......... .......... .......... 67% 88.8M 11s
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361450K .......... .......... .......... .......... .......... 67% 7.40M 11s
361500K .......... .......... .......... .......... .......... 67% 174M 11s
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361600K .......... .......... .......... .......... .......... 67% 97.5M 11s
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361700K .......... .......... .......... .......... .......... 67% 83.3M 11s
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361800K .......... .......... .......... .......... .......... 67% 96.1M 11s
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361950K .......... .......... .......... .......... .......... 67% 12.4M 11s
362000K .......... .......... .......... .......... .......... 67% 113M 11s
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362150K .......... .......... .......... .......... .......... 67% 292M 11s
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362250K .......... .......... .......... .......... .......... 67% 111M 11s
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362500K .......... .......... .......... .......... .......... 68% 74.5M 11s
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363000K .......... .......... .......... .......... .......... 68% 189M 11s
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364300K .......... .......... .......... .......... .......... 68% 194M 11s
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365000K .......... .......... .......... .......... .......... 68% 5.51M 11s
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368000K .......... .......... .......... .......... .......... 69% 213M 11s
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369100K .......... .......... .......... .......... .......... 69% 4.48M 11s
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369200K .......... .......... .......... .......... .......... 69% 194M 11s
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370000K .......... .......... .......... .......... .......... 69% 155M 11s
370050K .......... .......... .......... .......... .......... 69% 227M 11s
370100K .......... .......... .......... .......... .......... 69% 112M 11s
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370200K .......... .......... .......... .......... .......... 69% 104M 11s
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370950K .......... .......... .......... .......... .......... 69% 38.5M 11s
371000K .......... .......... .......... .......... .......... 69% 172M 11s
371050K .......... .......... .......... .......... .......... 69% 140M 11s
371100K .......... .......... .......... .......... .......... 69% 179M 11s
371150K .......... .......... .......... .......... .......... 69% 143M 11s
371200K .......... .......... .......... .......... .......... 69% 151M 11s
371250K .......... .......... .......... .......... .......... 69% 223M 11s
371300K .......... .......... .......... .......... .......... 69% 224M 11s
371350K .......... .......... .......... .......... .......... 69% 195M 11s
371400K .......... .......... .......... .......... .......... 69% 161M 11s
371450K .......... .......... .......... .......... .......... 69% 156M 11s
371500K .......... .......... .......... .......... .......... 69% 277M 11s
371550K .......... .......... .......... .......... .......... 69% 294M 11s
371600K .......... .......... .......... .......... .......... 69% 188M 11s
371650K .......... .......... .......... .......... .......... 69% 271M 11s
371700K .......... .......... .......... .......... .......... 69% 4.18M 11s
371750K .......... .......... .......... .......... .......... 69% 176M 11s
371800K .......... .......... .......... .......... .......... 69% 189M 11s
371850K .......... .......... .......... .......... .......... 69% 130M 11s
371900K .......... .......... .......... .......... .......... 69% 173M 11s
371950K .......... .......... .......... .......... .......... 69% 72.2M 11s
372000K .......... .......... .......... .......... .......... 69% 66.5M 11s
372050K .......... .......... .......... .......... .......... 69% 52.7M 11s
372100K .......... .......... .......... .......... .......... 69% 60.1M 11s
372150K .......... .......... .......... .......... .......... 69% 88.5M 11s
372200K .......... .......... .......... .......... .......... 69% 6.57M 11s
372250K .......... .......... .......... .......... .......... 69% 202M 11s
372300K .......... .......... .......... .......... .......... 69% 105M 11s
372350K .......... .......... .......... .......... .......... 69% 103M 11s
372400K .......... .......... .......... .......... .......... 69% 162M 11s
372450K .......... .......... .......... .......... .......... 69% 186M 11s
372500K .......... .......... .......... .......... .......... 69% 4.44M 11s
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372650K .......... .......... .......... .......... .......... 69% 142M 11s
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372750K .......... .......... .......... .......... .......... 69% 19.5M 11s
372800K .......... .......... .......... .......... .......... 69% 111M 11s
372850K .......... .......... .......... .......... .......... 69% 96.5M 11s
372900K .......... .......... .......... .......... .......... 69% 93.2M 11s
372950K .......... .......... .......... .......... .......... 69% 148M 11s
373000K .......... .......... .......... .......... .......... 69% 63.4M 11s
373050K .......... .......... .......... .......... .......... 69% 145M 11s
373100K .......... .......... .......... .......... .......... 69% 64.0M 11s
373150K .......... .......... .......... .......... .......... 69% 86.3M 11s
373200K .......... .......... .......... .......... .......... 70% 127M 11s
373250K .......... .......... .......... .......... .......... 70% 144M 11s
373300K .......... .......... .......... .......... .......... 70% 206M 11s
373350K .......... .......... .......... .......... .......... 70% 93.7M 11s
373400K .......... .......... .......... .......... .......... 70% 125M 11s
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373550K .......... .......... .......... .......... .......... 70% 305M 10s
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373750K .......... .......... .......... .......... .......... 70% 6.61M 10s
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373900K .......... .......... .......... .......... .......... 70% 208M 10s
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374000K .......... .......... .......... .......... .......... 70% 128M 10s
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374100K .......... .......... .......... .......... .......... 70% 118M 10s
374150K .......... .......... .......... .......... .......... 70% 136M 10s
374200K .......... .......... .......... .......... .......... 70% 147M 10s
374250K .......... .......... .......... .......... .......... 70% 2.57M 10s
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374800K .......... .......... .......... .......... .......... 70% 115M 10s
374850K .......... .......... .......... .......... .......... 70% 23.6M 10s
374900K .......... .......... .......... .......... .......... 70% 63.4M 10s
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375000K .......... .......... .......... .......... .......... 70% 56.0M 10s
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375100K .......... .......... .......... .......... .......... 70% 53.3M 10s
375150K .......... .......... .......... .......... .......... 70% 164M 10s
375200K .......... .......... .......... .......... .......... 70% 80.2M 10s
375250K .......... .......... .......... .......... .......... 70% 125M 10s
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375350K .......... .......... .......... .......... .......... 70% 120M 10s
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375450K .......... .......... .......... .......... .......... 70% 99.2M 10s
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375650K .......... .......... .......... .......... .......... 70% 91.6M 10s
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375850K .......... .......... .......... .......... .......... 70% 51.4M 10s
375900K .......... .......... .......... .......... .......... 70% 69.3M 10s
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376000K .......... .......... .......... .......... .......... 70% 78.0M 10s
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376100K .......... .......... .......... .......... .......... 70% 118M 10s
376150K .......... .......... .......... .......... .......... 70% 171M 10s
376200K .......... .......... .......... .......... .......... 70% 121M 10s
376250K .......... .......... .......... .......... .......... 70% 124M 10s
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376750K .......... .......... .......... .......... .......... 70% 207M 10s
376800K .......... .......... .......... .......... .......... 70% 9.39M 10s
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376950K .......... .......... .......... .......... .......... 70% 70.1M 10s
377000K .......... .......... .......... .......... .......... 70% 3.70M 10s
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377100K .......... .......... .......... .......... .......... 70% 17.9M 10s
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377200K .......... .......... .......... .......... .......... 70% 68.4M 10s
377250K .......... .......... .......... .......... .......... 70% 80.7M 10s
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377400K .......... .......... .......... .......... .......... 70% 40.1M 10s
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378000K .......... .......... .......... .......... .......... 70% 122M 10s
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378100K .......... .......... .......... .......... .......... 70% 135M 10s
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378200K .......... .......... .......... .......... .......... 70% 10.1M 10s
378250K .......... .......... .......... .......... .......... 70% 163M 10s
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378450K .......... .......... .......... .......... .......... 70% 5.60M 10s
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378550K .......... .......... .......... .......... .......... 71% 65.9M 10s
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378850K .......... .......... .......... .......... .......... 71% 35.9K 11s
378900K .......... .......... .......... .......... .......... 71% 97.3M 11s
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379100K .......... .......... .......... .......... .......... 71% 74.5M 11s
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380000K .......... .......... .......... .......... .......... 71% 162M 11s
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380200K .......... .......... .......... .......... .......... 71% 98.4M 11s
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380300K .......... .......... .......... .......... .......... 71% 95.2M 11s
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380600K .......... .......... .......... .......... .......... 71% 27.4M 11s
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380750K .......... .......... .......... .......... .......... 71% 225M 11s
380800K .......... .......... .......... .......... .......... 71% 176M 11s
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381100K .......... .......... .......... .......... .......... 71% 132M 11s
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381500K .......... .......... .......... .......... .......... 71% 152M 11s
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381800K .......... .......... .......... .......... .......... 71% 101M 11s
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382000K .......... .......... .......... .......... .......... 71% 60.4M 11s
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382150K .......... .......... .......... .......... .......... 71% 145M 10s
382200K .......... .......... .......... .......... .......... 71% 17.5M 10s
382250K .......... .......... .......... .......... .......... 71% 161M 10s
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382800K .......... .......... .......... .......... .......... 71% 152M 10s
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382950K .......... .......... .......... .......... .......... 71% 16.6M 10s
383000K .......... .......... .......... .......... .......... 71% 136M 10s
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383100K .......... .......... .......... .......... .......... 71% 126M 10s
383150K .......... .......... .......... .......... .......... 71% 183M 10s
383200K .......... .......... .......... .......... .......... 71% 25.3M 10s
383250K .......... .......... .......... .......... .......... 71% 165M 10s
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383900K .......... .......... .......... .......... .......... 72% 50.2M 10s
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384000K .......... .......... .......... .......... .......... 72% 1.29M 10s
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384100K .......... .......... .......... .......... .......... 72% 72.8M 10s
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384250K .......... .......... .......... .......... .......... 72% 112M 10s
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384500K .......... .......... .......... .......... .......... 72% 68.6M 10s
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384700K .......... .......... .......... .......... .......... 72% 98.2M 10s
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384900K .......... .......... .......... .......... .......... 72% 161M 10s
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385000K .......... .......... .......... .......... .......... 72% 716K 10s
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385100K .......... .......... .......... .......... .......... 72% 67.7M 10s
385150K .......... .......... .......... .......... .......... 72% 21.1M 10s
385200K .......... .......... .......... .......... .......... 72% 113M 10s
385250K .......... .......... .......... .......... .......... 72% 26.6M 10s
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385400K .......... .......... .......... .......... .......... 72% 104M 10s
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385500K .......... .......... .......... .......... .......... 72% 52.6M 10s
385550K .......... .......... .......... .......... .......... 72% 129M 10s
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385750K .......... .......... .......... .......... .......... 72% 27.7M 10s
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385900K .......... .......... .......... .......... .......... 72% 86.0M 10s
385950K .......... .......... .......... .......... .......... 72% 83.9M 10s
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400600K .......... .......... .......... .......... .......... 75% 95.7M 9s
400650K .......... .......... .......... .......... .......... 75% 6.31M 9s
400700K .......... .......... .......... .......... .......... 75% 105M 9s
400750K .......... .......... .......... .......... .......... 75% 99.9M 9s
400800K .......... .......... .......... .......... .......... 75% 7.62M 9s
400850K .......... .......... .......... .......... .......... 75% 106M 9s
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400950K .......... .......... .......... .......... .......... 75% 7.40M 9s
401000K .......... .......... .......... .......... .......... 75% 25.1M 9s
401050K .......... .......... .......... .......... .......... 75% 226M 9s
401100K .......... .......... .......... .......... .......... 75% 140M 9s
401150K .......... .......... .......... .......... .......... 75% 6.65M 9s
401200K .......... .......... .......... .......... .......... 75% 119M 9s
401250K .......... .......... .......... .......... .......... 75% 121M 9s
401300K .......... .......... .......... .......... .......... 75% 4.00M 9s
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401400K .......... .......... .......... .......... .......... 75% 1.58M 9s
401450K .......... .......... .......... .......... .......... 75% 20.4K 10s
401500K .......... .......... .......... .......... .......... 75% 57.6M 10s
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401800K .......... .......... .......... .......... .......... 75% 22.1M 10s
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402800K .......... .......... .......... .......... .......... 75% 108M 10s
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403000K .......... .......... .......... .......... .......... 75% 66.3M 10s
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403700K .......... .......... .......... .......... .......... 75% 63.9M 10s
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406300K .......... .......... .......... .......... .......... 76% 195M 9s
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415350K .......... .......... .......... .......... .......... 77% 81.8M 9s
415400K .......... .......... .......... .......... .......... 77% 4.25M 9s
415450K .......... .......... .......... .......... .......... 77% 110M 9s
415500K .......... .......... .......... .......... .......... 77% 80.2M 9s
415550K .......... .......... .......... .......... .......... 77% 118M 9s
415600K .......... .......... .......... .......... .......... 77% 113M 9s
415650K .......... .......... .......... .......... .......... 77% 4.37M 9s
415700K .......... .......... .......... .......... .......... 77% 93.4M 9s
415750K .......... .......... .......... .......... .......... 77% 39.5M 9s
415800K .......... .......... .......... .......... .......... 77% 67.3M 9s
415850K .......... .......... .......... .......... .......... 78% 28.7M 9s
415900K .......... .......... .......... .......... .......... 78% 4.80M 9s
415950K .......... .......... .......... .......... .......... 78% 41.7M 9s
416000K .......... .......... .......... .......... .......... 78% 83.9M 9s
416050K .......... .......... .......... .......... .......... 78% 52.2M 9s
416100K .......... .......... .......... .......... .......... 78% 5.76M 9s
416150K .......... .......... .......... .......... .......... 78% 24.2M 9s
416200K .......... .......... .......... .......... .......... 78% 50.2M 9s
416250K .......... .......... .......... .......... .......... 78% 73.6M 9s
416300K .......... .......... .......... .......... .......... 78% 92.1M 9s
416350K .......... .......... .......... .......... .......... 78% 6.04M 9s
416400K .......... .......... .......... .......... .......... 78% 152M 9s
416450K .......... .......... .......... .......... .......... 78% 95.9M 9s
416500K .......... .......... .......... .......... .......... 78% 115M 9s
416550K .......... .......... .......... .......... .......... 78% 6.33M 9s
416600K .......... .......... .......... .......... .......... 78% 140M 9s
416650K .......... .......... .......... .......... .......... 78% 94.6M 9s
416700K .......... .......... .......... .......... .......... 78% 129M 9s
416750K .......... .......... .......... .......... .......... 78% 130M 9s
416800K .......... .......... .......... .......... .......... 78% 607K 9s
416850K .......... .......... .......... .......... .......... 78% 25.2M 9s
416900K .......... .......... .......... .......... .......... 78% 219M 9s
416950K .......... .......... .......... .......... .......... 78% 105M 9s
417000K .......... .......... .......... .......... .......... 78% 200M 9s
417050K .......... .......... .......... .......... .......... 78% 5.24M 9s
417100K .......... .......... .......... .......... .......... 78% 164M 9s
417150K .......... .......... .......... .......... .......... 78% 186M 9s
417200K .......... .......... .......... .......... .......... 78% 121M 9s
417250K .......... .......... .......... .......... .......... 78% 4.48M 9s
417300K .......... .......... .......... .......... .......... 78% 72.2M 9s
417350K .......... .......... .......... .......... .......... 78% 90.9M 9s
417400K .......... .......... .......... .......... .......... 78% 75.2M 9s
417450K .......... .......... .......... .......... .......... 78% 115M 9s
417500K .......... .......... .......... .......... .......... 78% 6.57M 9s
417550K .......... .......... .......... .......... .......... 78% 90.1M 9s
417600K .......... .......... .......... .......... .......... 78% 183M 9s
417650K .......... .......... .......... .......... .......... 78% 186M 9s
417700K .......... .......... .......... .......... .......... 78% 5.28M 9s
417750K .......... .......... .......... .......... .......... 78% 113M 9s
417800K .......... .......... .......... .......... .......... 78% 118M 9s
417850K .......... .......... .......... .......... .......... 78% 67.8M 9s
417900K .......... .......... .......... .......... .......... 78% 60.9M 9s
417950K .......... .......... .......... .......... .......... 78% 5.72M 9s
418000K .......... .......... .......... .......... .......... 78% 94.3M 9s
418050K .......... .......... .......... .......... .......... 78% 84.8M 9s
418100K .......... .......... .......... .......... .......... 78% 103M 9s
418150K .......... .......... .......... .......... .......... 78% 111M 9s
418200K .......... .......... .......... .......... .......... 78% 6.20M 9s
418250K .......... .......... .......... .......... .......... 78% 116M 9s
418300K .......... .......... .......... .......... .......... 78% 108M 9s
418350K .......... .......... .......... .......... .......... 78% 131M 9s
418400K .......... .......... .......... .......... .......... 78% 106M 9s
418450K .......... .......... .......... .......... .......... 78% 5.65M 9s
418500K .......... .......... .......... .......... .......... 78% 130M 9s
418550K .......... .......... .......... .......... .......... 78% 148M 9s
418600K .......... .......... .......... .......... .......... 78% 128M 9s
418650K .......... .......... .......... .......... .......... 78% 9.40M 9s
418700K .......... .......... .......... .......... .......... 78% 51.1M 9s
418750K .......... .......... .......... .......... .......... 78% 102M 9s
418800K .......... .......... .......... .......... .......... 78% 146M 9s
418850K .......... .......... .......... .......... .......... 78% 1.08M 9s
418900K .......... .......... .......... .......... .......... 78% 37.4M 9s
418950K .......... .......... .......... .......... .......... 78% 18.2M 9s
419000K .......... .......... .......... .......... .......... 78% 138M 9s
419050K .......... .......... .......... .......... .......... 78% 174M 9s
419100K .......... .......... .......... .......... .......... 78% 77.1M 9s
419150K .......... .......... .......... .......... .......... 78% 173M 8s
419200K .......... .......... .......... .......... .......... 78% 120M 8s
419250K .......... .......... .......... .......... .......... 78% 38.3M 8s
419300K .......... .......... .......... .......... .......... 78% 202M 8s
419350K .......... .......... .......... .......... .......... 78% 5.29M 8s
419400K .......... .......... .......... .......... .......... 78% 173M 8s
419450K .......... .......... .......... .......... .......... 78% 196M 8s
419500K .......... .......... .......... .......... .......... 78% 7.33M 8s
419550K .......... .......... .......... .......... .......... 78% 15.3M 8s
419600K .......... .......... .......... .......... .......... 78% 134M 8s
419650K .......... .......... .......... .......... .......... 78% 115K 9s
419700K .......... .......... .......... .......... .......... 78% 183M 9s
419750K .......... .......... .......... .......... .......... 78% 195M 9s
419800K .......... .......... .......... .......... .......... 78% 83.6M 9s
419850K .......... .......... .......... .......... .......... 78% 9.26M 9s
419900K .......... .......... .......... .......... .......... 78% 128M 9s
419950K .......... .......... .......... .......... .......... 78% 172M 9s
420000K .......... .......... .......... .......... .......... 78% 54.9M 9s
420050K .......... .......... .......... .......... .......... 78% 223M 9s
420100K .......... .......... .......... .......... .......... 78% 169M 9s
420150K .......... .......... .......... .......... .......... 78% 124M 9s
420200K .......... .......... .......... .......... .......... 78% 101M 9s
420250K .......... .......... .......... .......... .......... 78% 228M 9s
420300K .......... .......... .......... .......... .......... 78% 102M 9s
420350K .......... .......... .......... .......... .......... 78% 138M 9s
420400K .......... .......... .......... .......... .......... 78% 70.3M 9s
420450K .......... .......... .......... .......... .......... 78% 126M 8s
420500K .......... .......... .......... .......... .......... 78% 128M 8s
420550K .......... .......... .......... .......... .......... 78% 82.2M 8s
420600K .......... .......... .......... .......... .......... 78% 86.4M 8s
420650K .......... .......... .......... .......... .......... 78% 93.7M 8s
420700K .......... .......... .......... .......... .......... 78% 141M 8s
420750K .......... .......... .......... .......... .......... 78% 102M 8s
420800K .......... .......... .......... .......... .......... 78% 96.9M 8s
420850K .......... .......... .......... .......... .......... 78% 133M 8s
420900K .......... .......... .......... .......... .......... 78% 114M 8s
420950K .......... .......... .......... .......... .......... 78% 26.9M 8s
421000K .......... .......... .......... .......... .......... 78% 91.1M 8s
421050K .......... .......... .......... .......... .......... 78% 6.55M 8s
421100K .......... .......... .......... .......... .......... 78% 118M 8s
421150K .......... .......... .......... .......... .......... 79% 72.6M 8s
421200K .......... .......... .......... .......... .......... 79% 58.9M 8s
421250K .......... .......... .......... .......... .......... 79% 4.26M 8s
421300K .......... .......... .......... .......... .......... 79% 191M 8s
421350K .......... .......... .......... .......... .......... 79% 35.4M 8s
421400K .......... .......... .......... .......... .......... 79% 146M 8s
421450K .......... .......... .......... .......... .......... 79% 58.1M 8s
421500K .......... .......... .......... .......... .......... 79% 8.30M 8s
421550K .......... .......... .......... .......... .......... 79% 66.3M 8s
421600K .......... .......... .......... .......... .......... 79% 117M 8s
421650K .......... .......... .......... .......... .......... 79% 199M 8s
421700K .......... .......... .......... .......... .......... 79% 164M 8s
421750K .......... .......... .......... .......... .......... 79% 5.11M 8s
421800K .......... .......... .......... .......... .......... 79% 137M 8s
421850K .......... .......... .......... .......... .......... 79% 12.6M 8s
421900K .......... .......... .......... .......... .......... 79% 18.7M 8s
421950K .......... .......... .......... .......... .......... 79% 128M 8s
422000K .......... .......... .......... .......... .......... 79% 118M 8s
422050K .......... .......... .......... .......... .......... 79% 18.7M 8s
422100K .......... .......... .......... .......... .......... 79% 11.8M 8s
422150K .......... .......... .......... .......... .......... 79% 131M 8s
422200K .......... .......... .......... .......... .......... 79% 124M 8s
422250K .......... .......... .......... .......... .......... 79% 48.4M 8s
422300K .......... .......... .......... .......... .......... 79% 7.05M 8s
422350K .......... .......... .......... .......... .......... 79% 25.5M 8s
422400K .......... .......... .......... .......... .......... 79% 132M 8s
422450K .......... .......... .......... .......... .......... 79% 2.10M 8s
422500K .......... .......... .......... .......... .......... 79% 111M 8s
422550K .......... .......... .......... .......... .......... 79% 93.9M 8s
422600K .......... .......... .......... .......... .......... 79% 29.0M 8s
422650K .......... .......... .......... .......... .......... 79% 72.4M 8s
422700K .......... .......... .......... .......... .......... 79% 8.46M 8s
422750K .......... .......... .......... .......... .......... 79% 4.29M 8s
422800K .......... .......... .......... .......... .......... 79% 124M 8s
422850K .......... .......... .......... .......... .......... 79% 137M 8s
422900K .......... .......... .......... .......... .......... 79% 42.3M 8s
422950K .......... .......... .......... .......... .......... 79% 5.13M 8s
423000K .......... .......... .......... .......... .......... 79% 23.3M 8s
423050K .......... .......... .......... .......... .......... 79% 36.5M 8s
423100K .......... .......... .......... .......... .......... 79% 36.8M 8s
423150K .......... .......... .......... .......... .......... 79% 148M 8s
423200K .......... .......... .......... .......... .......... 79% 151M 8s
423250K .......... .......... .......... .......... .......... 79% 191M 8s
423300K .......... .......... .......... .......... .......... 79% 120M 8s
423350K .......... .......... .......... .......... .......... 79% 74.8M 8s
423400K .......... .......... .......... .......... .......... 79% 118M 8s
423450K .......... .......... .......... .......... .......... 79% 131M 8s
423500K .......... .......... .......... .......... .......... 79% 100M 8s
423550K .......... .......... .......... .......... .......... 79% 146M 8s
423600K .......... .......... .......... .......... .......... 79% 135M 8s
423650K .......... .......... .......... .......... .......... 79% 174M 8s
423700K .......... .......... .......... .......... .......... 79% 60.3M 8s
423750K .......... .......... .......... .......... .......... 79% 198M 8s
423800K .......... .......... .......... .......... .......... 79% 204M 8s
423850K .......... .......... .......... .......... .......... 79% 130M 8s
423900K .......... .......... .......... .......... .......... 79% 161M 8s
423950K .......... .......... .......... .......... .......... 79% 5.88M 8s
424000K .......... .......... .......... .......... .......... 79% 63.4M 8s
424050K .......... .......... .......... .......... .......... 79% 170M 8s
424100K .......... .......... .......... .......... .......... 79% 138M 8s
424150K .......... .......... .......... .......... .......... 79% 217M 8s
424200K .......... .......... .......... .......... .......... 79% 160M 8s
424250K .......... .......... .......... .......... .......... 79% 119M 8s
424300K .......... .......... .......... .......... .......... 79% 7.86M 8s
424350K .......... .......... .......... .......... .......... 79% 73.3M 8s
424400K .......... .......... .......... .......... .......... 79% 84.6M 8s
424450K .......... .......... .......... .......... .......... 79% 111M 8s
424500K .......... .......... .......... .......... .......... 79% 42.4M 8s
424550K .......... .......... .......... .......... .......... 79% 6.18M 8s
424600K .......... .......... .......... .......... .......... 79% 115M 8s
424650K .......... .......... .......... .......... .......... 79% 110M 8s
424700K .......... .......... .......... .......... .......... 79% 187M 8s
424750K .......... .......... .......... .......... .......... 79% 53.4M 8s
424800K .......... .......... .......... .......... .......... 79% 4.13M 8s
424850K .......... .......... .......... .......... .......... 79% 72.7M 8s
424900K .......... .......... .......... .......... .......... 79% 120M 8s
424950K .......... .......... .......... .......... .......... 79% 180M 8s
425000K .......... .......... .......... .......... .......... 79% 8.77M 8s
425050K .......... .......... .......... .......... .......... 79% 169M 8s
425100K .......... .......... .......... .......... .......... 79% 189M 8s
425150K .......... .......... .......... .......... .......... 79% 221M 8s
425200K .......... .......... .......... .......... .......... 79% 157M 8s
425250K .......... .......... .......... .......... .......... 79% 222M 8s
425300K .......... .......... .......... .......... .......... 79% 4.24M 8s
425350K .......... .......... .......... .......... .......... 79% 26.7M 8s
425400K .......... .......... .......... .......... .......... 79% 2.58M 8s
425450K .......... .......... .......... .......... .......... 79% 2.73M 8s
425500K .......... .......... .......... .......... .......... 79% 2.61M 8s
425550K .......... .......... .......... .......... .......... 79% 2.90M 8s
425600K .......... .......... .......... .......... .......... 79% 5.65M 8s
425650K .......... .......... .......... .......... .......... 79% 4.10M 8s
425700K .......... .......... .......... .......... .......... 79% 9.95M 8s
425750K .......... .......... .......... .......... .......... 79% 38.3M 8s
425800K .......... .......... .......... .......... .......... 79% 4.09M 8s
425850K .......... .......... .......... .......... .......... 79% 27.9M 8s
425900K .......... .......... .......... .......... .......... 79% 26.1M 8s
425950K .......... .......... .......... .......... .......... 79% 17.7M 8s
426000K .......... .......... .......... .......... .......... 79% 52.7M 8s
426050K .......... .......... .......... .......... .......... 79% 85.8M 8s
426100K .......... .......... .......... .......... .......... 79% 25.4M 8s
426150K .......... .......... .......... .......... .......... 79% 104M 8s
426200K .......... .......... .......... .......... .......... 79% 29.2M 8s
426250K .......... .......... .......... .......... .......... 79% 3.53M 8s
426300K .......... .......... .......... .......... .......... 79% 3.06M 8s
426350K .......... .......... .......... .......... .......... 79% 17.7M 8s
426400K .......... .......... .......... .......... .......... 79% 9.34M 8s
426450K .......... .......... .......... .......... .......... 79% 4.99M 8s
426500K .......... .......... .......... .......... .......... 80% 78.9M 8s
426550K .......... .......... .......... .......... .......... 80% 24.9M 8s
426600K .......... .......... .......... .......... .......... 80% 3.04M 8s
426650K .......... .......... .......... .......... .......... 80% 9.14M 8s
426700K .......... .......... .......... .......... .......... 80% 19.7M 8s
426750K .......... .......... .......... .......... .......... 80% 44.4M 8s
426800K .......... .......... .......... .......... .......... 80% 73.6M 8s
426850K .......... .......... .......... .......... .......... 80% 17.8M 8s
426900K .......... .......... .......... .......... .......... 80% 16.9M 8s
426950K .......... .......... .......... .......... .......... 80% 2.05M 8s
427000K .......... .......... .......... .......... .......... 80% 2.02M 8s
427050K .......... .......... .......... .......... .......... 80% 3.68M 8s
427100K .......... .......... .......... .......... .......... 80% 3.45M 8s
427150K .......... .......... .......... .......... .......... 80% 53.8M 8s
427200K .......... .......... .......... .......... .......... 80% 5.68M 8s
427250K .......... .......... .......... .......... .......... 80% 108M 8s
427300K .......... .......... .......... .......... .......... 80% 52.9M 8s
427350K .......... .......... .......... .......... .......... 80% 50.2M 8s
427400K .......... .......... .......... .......... .......... 80% 1.30M 8s
427450K .......... .......... .......... .......... .......... 80% 1.82M 8s
427500K .......... .......... .......... .......... .......... 80% 29.8M 8s
427550K .......... .......... .......... .......... .......... 80% 4.22M 8s
427600K .......... .......... .......... .......... .......... 80% 8.25M 8s
427650K .......... .......... .......... .......... .......... 80% 42.8M 8s
427700K .......... .......... .......... .......... .......... 80% 61.9M 8s
427750K .......... .......... .......... .......... .......... 80% 20.8M 8s
427800K .......... .......... .......... .......... .......... 80% 93.4M 8s
427850K .......... .......... .......... .......... .......... 80% 47.0M 8s
427900K .......... .......... .......... .......... .......... 80% 18.0M 8s
427950K .......... .......... .......... .......... .......... 80% 11.4M 8s
428000K .......... .......... .......... .......... .......... 80% 67.0M 8s
428050K .......... .......... .......... .......... .......... 80% 4.29M 8s
428100K .......... .......... .......... .......... .......... 80% 30.7M 8s
428150K .......... .......... .......... .......... .......... 80% 137M 8s
428200K .......... .......... .......... .......... .......... 80% 114M 8s
428250K .......... .......... .......... .......... .......... 80% 110M 8s
428300K .......... .......... .......... .......... .......... 80% 41.3M 8s
428350K .......... .......... .......... .......... .......... 80% 22.1M 8s
428400K .......... .......... .......... .......... .......... 80% 41.1M 8s
428450K .......... .......... .......... .......... .......... 80% 104M 8s
428500K .......... .......... .......... .......... .......... 80% 26.2M 8s
428550K .......... .......... .......... .......... .......... 80% 122M 8s
428600K .......... .......... .......... .......... .......... 80% 110M 8s
428650K .......... .......... .......... .......... .......... 80% 33.0M 8s
428700K .......... .......... .......... .......... .......... 80% 24.8M 8s
428750K .......... .......... .......... .......... .......... 80% 154M 8s
428800K .......... .......... .......... .......... .......... 80% 30.6M 8s
428850K .......... .......... .......... .......... .......... 80% 32.6M 8s
428900K .......... .......... .......... .......... .......... 80% 155M 8s
428950K .......... .......... .......... .......... .......... 80% 135M 8s
429000K .......... .......... .......... .......... .......... 80% 176M 8s
429050K .......... .......... .......... .......... .......... 80% 200M 8s
429100K .......... .......... .......... .......... .......... 80% 6.49M 8s
429150K .......... .......... .......... .......... .......... 80% 142M 8s
429200K .......... .......... .......... .......... .......... 80% 133M 8s
429250K .......... .......... .......... .......... .......... 80% 42.9M 8s
429300K .......... .......... .......... .......... .......... 80% 30.2M 8s
429350K .......... .......... .......... .......... .......... 80% 154M 8s
429400K .......... .......... .......... .......... .......... 80% 31.8M 8s
429450K .......... .......... .......... .......... .......... 80% 26.9M 8s
429500K .......... .......... .......... .......... .......... 80% 2.51M 8s
429550K .......... .......... .......... .......... .......... 80% 2.50M 8s
429600K .......... .......... .......... .......... .......... 80% 16.3M 8s
429650K .......... .......... .......... .......... .......... 80% 4.15M 8s
429700K .......... .......... .......... .......... .......... 80% 1.42M 8s
429750K .......... .......... .......... .......... .......... 80% 139M 8s
429800K .......... .......... .......... .......... .......... 80% 1.28M 8s
429850K .......... .......... .......... .......... .......... 80% 6.88M 8s
429900K .......... .......... .......... .......... .......... 80% 1.95M 8s
429950K .......... .......... .......... .......... .......... 80% 15.6M 8s
430000K .......... .......... .......... .......... .......... 80% 17.9M 8s
430050K .......... .......... .......... .......... .......... 80% 1.31M 8s
430100K .......... .......... .......... .......... .......... 80% 4.59M 8s
430150K .......... .......... .......... .......... .......... 80% 3.95M 8s
430200K .......... .......... .......... .......... .......... 80% 823K 8s
430250K .......... .......... .......... .......... .......... 80% 7.57M 8s
430300K .......... .......... .......... .......... .......... 80% 13.7M 8s
430350K .......... .......... .......... .......... .......... 80% 13.3M 8s
430400K .......... .......... .......... .......... .......... 80% 15.4M 8s
430450K .......... .......... .......... .......... .......... 80% 13.0M 8s
430500K .......... .......... .......... .......... .......... 80% 4.20M 8s
430550K .......... .......... .......... .......... .......... 80% 6.66M 8s
430600K .......... .......... .......... .......... .......... 80% 80.8M 8s
430650K .......... .......... .......... .......... .......... 80% 144M 8s
430700K .......... .......... .......... .......... .......... 80% 74.8M 8s
430750K .......... .......... .......... .......... .......... 80% 153M 8s
430800K .......... .......... .......... .......... .......... 80% 149M 8s
430850K .......... .......... .......... .......... .......... 80% 33.0M 8s
430900K .......... .......... .......... .......... .......... 80% 182M 8s
430950K .......... .......... .......... .......... .......... 80% 132M 8s
431000K .......... .......... .......... .......... .......... 80% 8.65M 8s
431050K .......... .......... .......... .......... .......... 80% 3.96M 8s
431100K .......... .......... .......... .......... .......... 80% 50.0M 8s
431150K .......... .......... .......... .......... .......... 80% 14.8M 8s
431200K .......... .......... .......... .......... .......... 80% 22.6M 8s
431250K .......... .......... .......... .......... .......... 80% 173M 8s
431300K .......... .......... .......... .......... .......... 80% 127M 8s
431350K .......... .......... .......... .......... .......... 80% 968K 8s
431400K .......... .......... .......... .......... .......... 80% 77.3M 8s
431450K .......... .......... .......... .......... .......... 80% 47.3M 8s
431500K .......... .......... .......... .......... .......... 80% 170M 8s
431550K .......... .......... .......... .......... .......... 80% 174M 8s
431600K .......... .......... .......... .......... .......... 80% 33.8M 8s
431650K .......... .......... .......... .......... .......... 80% 47.6M 8s
431700K .......... .......... .......... .......... .......... 80% 155M 8s
431750K .......... .......... .......... .......... .......... 80% 171M 8s
431800K .......... .......... .......... .......... .......... 80% 156M 8s
431850K .......... .......... .......... .......... .......... 81% 164M 8s
431900K .......... .......... .......... .......... .......... 81% 165M 8s
431950K .......... .......... .......... .......... .......... 81% 58.5M 8s
432000K .......... .......... .......... .......... .......... 81% 182M 8s
432050K .......... .......... .......... .......... .......... 81% 49.6M 8s
432100K .......... .......... .......... .......... .......... 81% 34.6M 8s
432150K .......... .......... .......... .......... .......... 81% 1.18M 8s
432200K .......... .......... .......... .......... .......... 81% 178M 8s
432250K .......... .......... .......... .......... .......... 81% 120M 8s
432300K .......... .......... .......... .......... .......... 81% 167M 8s
432350K .......... .......... .......... .......... .......... 81% 99.2M 8s
432400K .......... .......... .......... .......... .......... 81% 121M 8s
432450K .......... .......... .......... .......... .......... 81% 81.4M 8s
432500K .......... .......... .......... .......... .......... 81% 103M 8s
432550K .......... .......... .......... .......... .......... 81% 40.8M 8s
432600K .......... .......... .......... .......... .......... 81% 135M 8s
432650K .......... .......... .......... .......... .......... 81% 140M 8s
432700K .......... .......... .......... .......... .......... 81% 81.4M 8s
432750K .......... .......... .......... .......... .......... 81% 115M 8s
432800K .......... .......... .......... .......... .......... 81% 144M 8s
432850K .......... .......... .......... .......... .......... 81% 157M 8s
432900K .......... .......... .......... .......... .......... 81% 193M 8s
432950K .......... .......... .......... .......... .......... 81% 103M 8s
433000K .......... .......... .......... .......... .......... 81% 140M 8s
433050K .......... .......... .......... .......... .......... 81% 182M 8s
433100K .......... .......... .......... .......... .......... 81% 114M 8s
433150K .......... .......... .......... .......... .......... 81% 186M 8s
433200K .......... .......... .......... .......... .......... 81% 109M 8s
433250K .......... .......... .......... .......... .......... 81% 152M 8s
433300K .......... .......... .......... .......... .......... 81% 167M 8s
433350K .......... .......... .......... .......... .......... 81% 174M 8s
433400K .......... .......... .......... .......... .......... 81% 11.4M 8s
433450K .......... .......... .......... .......... .......... 81% 121M 8s
433500K .......... .......... .......... .......... .......... 81% 124M 8s
433550K .......... .......... .......... .......... .......... 81% 133M 8s
433600K .......... .......... .......... .......... .......... 81% 99.6M 8s
433650K .......... .......... .......... .......... .......... 81% 6.51M 8s
433700K .......... .......... .......... .......... .......... 81% 95.0M 8s
433750K .......... .......... .......... .......... .......... 81% 96.9M 8s
433800K .......... .......... .......... .......... .......... 81% 123M 8s
433850K .......... .......... .......... .......... .......... 81% 106M 8s
433900K .......... .......... .......... .......... .......... 81% 6.57M 8s
433950K .......... .......... .......... .......... .......... 81% 153M 8s
434000K .......... .......... .......... .......... .......... 81% 224M 8s
434050K .......... .......... .......... .......... .......... 81% 225M 7s
434100K .......... .......... .......... .......... .......... 81% 161M 7s
434150K .......... .......... .......... .......... .......... 81% 5.80M 7s
434200K .......... .......... .......... .......... .......... 81% 82.2M 7s
434250K .......... .......... .......... .......... .......... 81% 62.0M 7s
434300K .......... .......... .......... .......... .......... 81% 234M 7s
434350K .......... .......... .......... .......... .......... 81% 195M 7s
434400K .......... .......... .......... .......... .......... 81% 5.32M 7s
434450K .......... .......... .......... .......... .......... 81% 145M 7s
434500K .......... .......... .......... .......... .......... 81% 169M 7s
434550K .......... .......... .......... .......... .......... 81% 107M 7s
434600K .......... .......... .......... .......... .......... 81% 124M 7s
434650K .......... .......... .......... .......... .......... 81% 6.90M 7s
434700K .......... .......... .......... .......... .......... 81% 64.2M 7s
434750K .......... .......... .......... .......... .......... 81% 195M 7s
434800K .......... .......... .......... .......... .......... 81% 81.2M 7s
434850K .......... .......... .......... .......... .......... 81% 81.1M 7s
434900K .......... .......... .......... .......... .......... 81% 120M 7s
434950K .......... .......... .......... .......... .......... 81% 4.11M 7s
435000K .......... .......... .......... .......... .......... 81% 89.8M 7s
435050K .......... .......... .......... .......... .......... 81% 209M 7s
435100K .......... .......... .......... .......... .......... 81% 106M 7s
435150K .......... .......... .......... .......... .......... 81% 91.8M 7s
435200K .......... .......... .......... .......... .......... 81% 7.31M 7s
435250K .......... .......... .......... .......... .......... 81% 1.49M 7s
435300K .......... .......... .......... .......... .......... 81% 159M 7s
435350K .......... .......... .......... .......... .......... 81% 12.0M 7s
435400K .......... .......... .......... .......... .......... 81% 136M 7s
435450K .......... .......... .......... .......... .......... 81% 20.0M 7s
435500K .......... .......... .......... .......... .......... 81% 249M 7s
435550K .......... .......... .......... .......... .......... 81% 268M 7s
435600K .......... .......... .......... .......... .......... 81% 25.9M 7s
435650K .......... .......... .......... .......... .......... 81% 90.4M 7s
435700K .......... .......... .......... .......... .......... 81% 161M 7s
435750K .......... .......... .......... .......... .......... 81% 167M 7s
435800K .......... .......... .......... .......... .......... 81% 146M 7s
435850K .......... .......... .......... .......... .......... 81% 143M 7s
435900K .......... .......... .......... .......... .......... 81% 181M 7s
435950K .......... .......... .......... .......... .......... 81% 118M 7s
436000K .......... .......... .......... .......... .......... 81% 18.6M 7s
436050K .......... .......... .......... .......... .......... 81% 124M 7s
436100K .......... .......... .......... .......... .......... 81% 150M 7s
436150K .......... .......... .......... .......... .......... 81% 16.2M 7s
436200K .......... .......... .......... .......... .......... 81% 23.1M 7s
436250K .......... .......... .......... .......... .......... 81% 126M 7s
436300K .......... .......... .......... .......... .......... 81% 205M 7s
436350K .......... .......... .......... .......... .......... 81% 192M 7s
436400K .......... .......... .......... .......... .......... 81% 150M 7s
436450K .......... .......... .......... .......... .......... 81% 55.4M 7s
436500K .......... .......... .......... .......... .......... 81% 28.3M 7s
436550K .......... .......... .......... .......... .......... 81% 14.4M 7s
436600K .......... .......... .......... .......... .......... 81% 17.3M 7s
436650K .......... .......... .......... .......... .......... 81% 22.6M 7s
436700K .......... .......... .......... .......... .......... 81% 38.5M 7s
436750K .......... .......... .......... .......... .......... 81% 27.7M 7s
436800K .......... .......... .......... .......... .......... 81% 214M 7s
436850K .......... .......... .......... .......... .......... 81% 25.4M 7s
436900K .......... .......... .......... .......... .......... 81% 106M 7s
436950K .......... .......... .......... .......... .......... 81% 69.6M 7s
437000K .......... .......... .......... .......... .......... 81% 41.2M 7s
437050K .......... .......... .......... .......... .......... 81% 53.0M 7s
437100K .......... .......... .......... .......... .......... 81% 59.7M 7s
437150K .......... .......... .......... .......... .......... 82% 83.9M 7s
437200K .......... .......... .......... .......... .......... 82% 69.4M 7s
437250K .......... .......... .......... .......... .......... 82% 7.22M 7s
437300K .......... .......... .......... .......... .......... 82% 1007K 7s
437350K .......... .......... .......... .......... .......... 82% 11.3M 7s
437400K .......... .......... .......... .......... .......... 82% 53.9M 7s
437450K .......... .......... .......... .......... .......... 82% 52.9M 7s
437500K .......... .......... .......... .......... .......... 82% 30.2M 7s
437550K .......... .......... .......... .......... .......... 82% 64.2M 7s
437600K .......... .......... .......... .......... .......... 82% 79.7M 7s
437650K .......... .......... .......... .......... .......... 82% 182M 7s
437700K .......... .......... .......... .......... .......... 82% 4.42M 7s
437750K .......... .......... .......... .......... .......... 82% 44.6M 7s
437800K .......... .......... .......... .......... .......... 82% 77.6M 7s
437850K .......... .......... .......... .......... .......... 82% 95.0M 7s
437900K .......... .......... .......... .......... .......... 82% 75.6M 7s
437950K .......... .......... .......... .......... .......... 82% 100M 7s
438000K .......... .......... .......... .......... .......... 82% 24.2M 7s
438050K .......... .......... .......... .......... .......... 82% 159M 7s
438100K .......... .......... .......... .......... .......... 82% 168M 7s
438150K .......... .......... .......... .......... .......... 82% 7.09M 7s
438200K .......... .......... .......... .......... .......... 82% 1.06M 7s
438250K .......... .......... .......... .......... .......... 82% 11.2M 7s
438300K .......... .......... .......... .......... .......... 82% 1.57M 7s
438350K .......... .......... .......... .......... .......... 82% 4.83M 7s
438400K .......... .......... .......... .......... .......... 82% 64.6M 7s
438450K .......... .......... .......... .......... .......... 82% 19.7M 7s
438500K .......... .......... .......... .......... .......... 82% 78.4M 7s
438550K .......... .......... .......... .......... .......... 82% 37.7M 7s
438600K .......... .......... .......... .......... .......... 82% 39.9M 7s
438650K .......... .......... .......... .......... .......... 82% 32.0M 7s
438700K .......... .......... .......... .......... .......... 82% 13.9M 7s
438750K .......... .......... .......... .......... .......... 82% 14.0M 7s
438800K .......... .......... .......... .......... .......... 82% 14.7M 7s
438850K .......... .......... .......... .......... .......... 82% 28.3M 7s
438900K .......... .......... .......... .......... .......... 82% 30.9M 7s
438950K .......... .......... .......... .......... .......... 82% 32.9M 7s
439000K .......... .......... .......... .......... .......... 82% 42.2M 7s
439050K .......... .......... .......... .......... .......... 82% 59.8M 7s
439100K .......... .......... .......... .......... .......... 82% 26.4M 7s
439150K .......... .......... .......... .......... .......... 82% 112M 7s
439200K .......... .......... .......... .......... .......... 82% 58.5M 7s
439250K .......... .......... .......... .......... .......... 82% 153M 7s
439300K .......... .......... .......... .......... .......... 82% 43.9M 7s
439350K .......... .......... .......... .......... .......... 82% 13.8M 7s
439400K .......... .......... .......... .......... .......... 82% 22.1M 7s
439450K .......... .......... .......... .......... .......... 82% 33.6M 7s
439500K .......... .......... .......... .......... .......... 82% 46.1M 7s
439550K .......... .......... .......... .......... .......... 82% 43.9M 7s
439600K .......... .......... .......... .......... .......... 82% 42.7M 7s
439650K .......... .......... .......... .......... .......... 82% 101M 7s
439700K .......... .......... .......... .......... .......... 82% 35.5M 7s
439750K .......... .......... .......... .......... .......... 82% 23.4M 7s
439800K .......... .......... .......... .......... .......... 82% 95.9M 7s
439850K .......... .......... .......... .......... .......... 82% 44.8M 7s
439900K .......... .......... .......... .......... .......... 82% 32.7M 7s
439950K .......... .......... .......... .......... .......... 82% 66.6M 7s
440000K .......... .......... .......... .......... .......... 82% 55.4M 7s
440050K .......... .......... .......... .......... .......... 82% 11.9M 7s
440100K .......... .......... .......... .......... .......... 82% 34.9M 7s
440150K .......... .......... .......... .......... .......... 82% 51.7M 7s
440200K .......... .......... .......... .......... .......... 82% 15.5M 7s
440250K .......... .......... .......... .......... .......... 82% 22.7M 7s
440300K .......... .......... .......... .......... .......... 82% 60.9M 7s
440350K .......... .......... .......... .......... .......... 82% 882K 7s
440400K .......... .......... .......... .......... .......... 82% 31.4M 7s
440450K .......... .......... .......... .......... .......... 82% 57.8M 7s
440500K .......... .......... .......... .......... .......... 82% 27.1M 7s
440550K .......... .......... .......... .......... .......... 82% 21.4M 7s
440600K .......... .......... .......... .......... .......... 82% 120M 7s
440650K .......... .......... .......... .......... .......... 82% 161M 7s
440700K .......... .......... .......... .......... .......... 82% 35.7M 7s
440750K .......... .......... .......... .......... .......... 82% 3.66M 7s
440800K .......... .......... .......... .......... .......... 82% 144M 7s
440850K .......... .......... .......... .......... .......... 82% 20.4M 7s
440900K .......... .......... .......... .......... .......... 82% 18.6M 7s
440950K .......... .......... .......... .......... .......... 82% 27.4M 7s
441000K .......... .......... .......... .......... .......... 82% 115M 7s
441050K .......... .......... .......... .......... .......... 82% 77.5M 7s
441100K .......... .......... .......... .......... .......... 82% 123M 7s
441150K .......... .......... .......... .......... .......... 82% 70.7M 7s
441200K .......... .......... .......... .......... .......... 82% 127M 7s
441250K .......... .......... .......... .......... .......... 82% 120M 7s
441300K .......... .......... .......... .......... .......... 82% 38.5M 7s
441350K .......... .......... .......... .......... .......... 82% 3.26M 7s
441400K .......... .......... .......... .......... .......... 82% 16.2M 7s
441450K .......... .......... .......... .......... .......... 82% 4.05M 7s
441500K .......... .......... .......... .......... .......... 82% 87.0M 7s
441550K .......... .......... .......... .......... .......... 82% 8.82M 7s
441600K .......... .......... .......... .......... .......... 82% 7.26M 7s
441650K .......... .......... .......... .......... .......... 82% 10.4M 7s
441700K .......... .......... .......... .......... .......... 82% 102M 7s
441750K .......... .......... .......... .......... .......... 82% 181M 7s
441800K .......... .......... .......... .......... .......... 82% 168M 7s
441850K .......... .......... .......... .......... .......... 82% 91.4M 7s
441900K .......... .......... .......... .......... .......... 82% 38.2M 7s
441950K .......... .......... .......... .......... .......... 82% 6.93M 7s
442000K .......... .......... .......... .......... .......... 82% 80.0M 7s
442050K .......... .......... .......... .......... .......... 82% 132M 7s
442100K .......... .......... .......... .......... .......... 82% 140M 7s
442150K .......... .......... .......... .......... .......... 82% 221M 7s
442200K .......... .......... .......... .......... .......... 82% 137M 7s
442250K .......... .......... .......... .......... .......... 82% 119M 7s
442300K .......... .......... .......... .......... .......... 82% 127M 7s
442350K .......... .......... .......... .......... .......... 82% 79.7M 7s
442400K .......... .......... .......... .......... .......... 82% 64.2M 7s
442450K .......... .......... .......... .......... .......... 82% 8.40M 7s
442500K .......... .......... .......... .......... .......... 83% 7.79M 7s
442550K .......... .......... .......... .......... .......... 83% 164M 7s
442600K .......... .......... .......... .......... .......... 83% 116M 7s
442650K .......... .......... .......... .......... .......... 83% 120M 7s
442700K .......... .......... .......... .......... .......... 83% 91.8M 7s
442750K .......... .......... .......... .......... .......... 83% 14.3M 7s
442800K .......... .......... .......... .......... .......... 83% 106M 7s
442850K .......... .......... .......... .......... .......... 83% 59.1M 7s
442900K .......... .......... .......... .......... .......... 83% 6.72M 7s
442950K .......... .......... .......... .......... .......... 83% 13.0M 7s
443000K .......... .......... .......... .......... .......... 83% 11.6M 7s
443050K .......... .......... .......... .......... .......... 83% 47.4M 7s
443100K .......... .......... .......... .......... .......... 83% 42.8M 7s
443150K .......... .......... .......... .......... .......... 83% 86.1M 7s
443200K .......... .......... .......... .......... .......... 83% 22.9M 7s
443250K .......... .......... .......... .......... .......... 83% 39.7M 7s
443300K .......... .......... .......... .......... .......... 83% 161M 7s
443350K .......... .......... .......... .......... .......... 83% 14.7M 7s
443400K .......... .......... .......... .......... .......... 83% 3.29M 7s
443450K .......... .......... .......... .......... .......... 83% 9.23M 7s
443500K .......... .......... .......... .......... .......... 83% 149M 7s
443550K .......... .......... .......... .......... .......... 83% 59.9M 7s
443600K .......... .......... .......... .......... .......... 83% 122M 7s
443650K .......... .......... .......... .......... .......... 83% 170M 7s
443700K .......... .......... .......... .......... .......... 83% 55.6M 7s
443750K .......... .......... .......... .......... .......... 83% 22.7M 7s
443800K .......... .......... .......... .......... .......... 83% 67.4M 7s
443850K .......... .......... .......... .......... .......... 83% 47.4M 7s
443900K .......... .......... .......... .......... .......... 83% 67.3M 7s
443950K .......... .......... .......... .......... .......... 83% 55.0M 7s
444000K .......... .......... .......... .......... .......... 83% 131M 7s
444050K .......... .......... .......... .......... .......... 83% 104M 7s
444100K .......... .......... .......... .......... .......... 83% 128M 7s
444150K .......... .......... .......... .......... .......... 83% 128M 7s
444200K .......... .......... .......... .......... .......... 83% 57.4M 7s
444250K .......... .......... .......... .......... .......... 83% 87.3M 7s
444300K .......... .......... .......... .......... .......... 83% 128M 7s
444350K .......... .......... .......... .......... .......... 83% 121M 7s
444400K .......... .......... .......... .......... .......... 83% 76.9M 7s
444450K .......... .......... .......... .......... .......... 83% 5.65M 7s
444500K .......... .......... .......... .......... .......... 83% 200M 7s
444550K .......... .......... .......... .......... .......... 83% 22.9M 7s
444600K .......... .......... .......... .......... .......... 83% 65.4M 7s
444650K .......... .......... .......... .......... .......... 83% 36.7M 7s
444700K .......... .......... .......... .......... .......... 83% 28.3M 7s
444750K .......... .......... .......... .......... .......... 83% 4.81M 7s
444800K .......... .......... .......... .......... .......... 83% 43.9M 7s
444850K .......... .......... .......... .......... .......... 83% 53.2M 7s
444900K .......... .......... .......... .......... .......... 83% 18.6M 7s
444950K .......... .......... .......... .......... .......... 83% 4.67M 7s
445000K .......... .......... .......... .......... .......... 83% 45.9M 7s
445050K .......... .......... .......... .......... .......... 83% 78.5M 7s
445100K .......... .......... .......... .......... .......... 83% 53.0M 7s
445150K .......... .......... .......... .......... .......... 83% 4.85M 7s
445200K .......... .......... .......... .......... .......... 83% 85.1M 7s
445250K .......... .......... .......... .......... .......... 83% 135M 7s
445300K .......... .......... .......... .......... .......... 83% 181M 7s
445350K .......... .......... .......... .......... .......... 83% 26.4M 7s
445400K .......... .......... .......... .......... .......... 83% 4.03M 7s
445450K .......... .......... .......... .......... .......... 83% 18.4M 7s
445500K .......... .......... .......... .......... .......... 83% 44.5M 7s
445550K .......... .......... .......... .......... .......... 83% 25.3M 7s
445600K .......... .......... .......... .......... .......... 83% 4.47M 7s
445650K .......... .......... .......... .......... .......... 83% 141M 7s
445700K .......... .......... .......... .......... .......... 83% 96.9M 7s
445750K .......... .......... .......... .......... .......... 83% 54.7M 7s
445800K .......... .......... .......... .......... .......... 83% 4.54M 7s
445850K .......... .......... .......... .......... .......... 83% 105M 7s
445900K .......... .......... .......... .......... .......... 83% 100M 7s
445950K .......... .......... .......... .......... .......... 83% 47.7M 7s
446000K .......... .......... .......... .......... .......... 83% 36.8M 7s
446050K .......... .......... .......... .......... .......... 83% 5.02M 7s
446100K .......... .......... .......... .......... .......... 83% 48.0M 7s
446150K .......... .......... .......... .......... .......... 83% 39.2M 7s
446200K .......... .......... .......... .......... .......... 83% 12.3M 7s
446250K .......... .......... .......... .......... .......... 83% 4.46M 7s
446300K .......... .......... .......... .......... .......... 83% 98.4M 7s
446350K .......... .......... .......... .......... .......... 83% 19.2M 7s
446400K .......... .......... .......... .......... .......... 83% 134M 7s
446450K .......... .......... .......... .......... .......... 83% 5.49M 7s
446500K .......... .......... .......... .......... .......... 83% 49.7M 7s
446550K .......... .......... .......... .......... .......... 83% 67.7M 7s
446600K .......... .......... .......... .......... .......... 83% 73.9M 7s
446650K .......... .......... .......... .......... .......... 83% 52.8M 7s
446700K .......... .......... .......... .......... .......... 83% 5.04M 6s
446750K .......... .......... .......... .......... .......... 83% 196M 6s
446800K .......... .......... .......... .......... .......... 83% 71.6M 6s
446850K .......... .......... .......... .......... .......... 83% 20.1M 6s
446900K .......... .......... .......... .......... .......... 83% 5.52M 6s
446950K .......... .......... .......... .......... .......... 83% 52.7M 6s
447000K .......... .......... .......... .......... .......... 83% 202M 6s
447050K .......... .......... .......... .......... .......... 83% 175M 6s
447100K .......... .......... .......... .......... .......... 83% 59.7M 6s
447150K .......... .......... .......... .......... .......... 83% 4.55M 6s
447200K .......... .......... .......... .......... .......... 83% 49.1M 6s
447250K .......... .......... .......... .......... .......... 83% 37.7M 6s
447300K .......... .......... .......... .......... .......... 83% 93.0M 6s
447350K .......... .......... .......... .......... .......... 83% 4.14M 6s
447400K .......... .......... .......... .......... .......... 83% 223M 6s
447450K .......... .......... .......... .......... .......... 83% 199M 6s
447500K .......... .......... .......... .......... .......... 83% 77.4M 6s
447550K .......... .......... .......... .......... .......... 83% 56.8M 6s
447600K .......... .......... .......... .......... .......... 83% 4.20M 6s
447650K .......... .......... .......... .......... .......... 83% 92.5M 6s
447700K .......... .......... .......... .......... .......... 83% 189M 6s
447750K .......... .......... .......... .......... .......... 83% 78.6M 6s
447800K .......... .......... .......... .......... .......... 83% 3.85M 6s
447850K .......... .......... .......... .......... .......... 84% 49.7M 6s
447900K .......... .......... .......... .......... .......... 84% 22.3M 6s
447950K .......... .......... .......... .......... .......... 84% 40.8M 6s
448000K .......... .......... .......... .......... .......... 84% 104M 6s
448050K .......... .......... .......... .......... .......... 84% 4.79M 6s
448100K .......... .......... .......... .......... .......... 84% 61.0M 6s
448150K .......... .......... .......... .......... .......... 84% 86.6M 6s
448200K .......... .......... .......... .......... .......... 84% 50.7M 6s
448250K .......... .......... .......... .......... .......... 84% 5.72M 6s
448300K .......... .......... .......... .......... .......... 84% 170M 6s
448350K .......... .......... .......... .......... .......... 84% 83.5M 6s
448400K .......... .......... .......... .......... .......... 84% 89.6M 6s
448450K .......... .......... .......... .......... .......... 84% 111M 6s
448500K .......... .......... .......... .......... .......... 84% 6.00M 6s
448550K .......... .......... .......... .......... .......... 84% 14.9M 6s
448600K .......... .......... .......... .......... .......... 84% 70.1M 6s
448650K .......... .......... .......... .......... .......... 84% 104M 6s
448700K .......... .......... .......... .......... .......... 84% 5.26M 6s
448750K .......... .......... .......... .......... .......... 84% 73.1M 6s
448800K .......... .......... .......... .......... .......... 84% 88.8M 6s
448850K .......... .......... .......... .......... .......... 84% 71.8M 6s
448900K .......... .......... .......... .......... .......... 84% 124M 6s
448950K .......... .......... .......... .......... .......... 84% 4.88M 6s
449000K .......... .......... .......... .......... .......... 84% 191M 6s
449050K .......... .......... .......... .......... .......... 84% 194M 6s
449100K .......... .......... .......... .......... .......... 84% 154M 6s
449150K .......... .......... .......... .......... .......... 84% 4.96M 6s
449200K .......... .......... .......... .......... .......... 84% 172M 6s
449250K .......... .......... .......... .......... .......... 84% 229M 6s
449300K .......... .......... .......... .......... .......... 84% 203M 6s
449350K .......... .......... .......... .......... .......... 84% 182M 6s
449400K .......... .......... .......... .......... .......... 84% 5.58M 6s
449450K .......... .......... .......... .......... .......... 84% 106M 6s
449500K .......... .......... .......... .......... .......... 84% 2.59M 6s
449550K .......... .......... .......... .......... .......... 84% 2.64M 6s
449600K .......... .......... .......... .......... .......... 84% 4.89M 6s
449650K .......... .......... .......... .......... .......... 84% 51.5M 6s
449700K .......... .......... .......... .......... .......... 84% 72.2M 6s
449750K .......... .......... .......... .......... .......... 84% 90.4M 6s
449800K .......... .......... .......... .......... .......... 84% 92.1M 6s
449850K .......... .......... .......... .......... .......... 84% 4.31M 6s
449900K .......... .......... .......... .......... .......... 84% 43.2M 6s
449950K .......... .......... .......... .......... .......... 84% 4.73M 6s
450000K .......... .......... .......... .......... .......... 84% 121M 6s
450050K .......... .......... .......... .......... .......... 84% 116M 6s
450100K .......... .......... .......... .......... .......... 84% 5.12M 6s
450150K .......... .......... .......... .......... .......... 84% 58.0M 6s
450200K .......... .......... .......... .......... .......... 84% 78.3M 6s
450250K .......... .......... .......... .......... .......... 84% 25.0M 6s
450300K .......... .......... .......... .......... .......... 84% 6.44M 6s
450350K .......... .......... .......... .......... .......... 84% 112M 6s
450400K .......... .......... .......... .......... .......... 84% 142M 6s
450450K .......... .......... .......... .......... .......... 84% 140M 6s
450500K .......... .......... .......... .......... .......... 84% 28.8M 6s
450550K .......... .......... .......... .......... .......... 84% 6.24M 6s
450600K .......... .......... .......... .......... .......... 84% 2.37M 6s
450650K .......... .......... .......... .......... .......... 84% 154M 6s
450700K .......... .......... .......... .......... .......... 84% 131M 6s
450750K .......... .......... .......... .......... .......... 84% 24.0M 6s
450800K .......... .......... .......... .......... .......... 84% 5.94M 6s
450850K .......... .......... .......... .......... .......... 84% 103M 6s
450900K .......... .......... .......... .......... .......... 84% 111M 6s
450950K .......... .......... .......... .......... .......... 84% 174M 6s
451000K .......... .......... .......... .......... .......... 84% 6.37M 6s
451050K .......... .......... .......... .......... .......... 84% 101M 6s
451100K .......... .......... .......... .......... .......... 84% 74.0M 6s
451150K .......... .......... .......... .......... .......... 84% 108M 6s
451200K .......... .......... .......... .......... .......... 84% 78.3M 6s
451250K .......... .......... .......... .......... .......... 84% 6.85M 6s
451300K .......... .......... .......... .......... .......... 84% 93.5M 6s
451350K .......... .......... .......... .......... .......... 84% 140M 6s
451400K .......... .......... .......... .......... .......... 84% 120M 6s
451450K .......... .......... .......... .......... .......... 84% 88.6M 6s
451500K .......... .......... .......... .......... .......... 84% 5.99M 6s
451550K .......... .......... .......... .......... .......... 84% 132M 6s
451600K .......... .......... .......... .......... .......... 84% 96.1M 6s
451650K .......... .......... .......... .......... .......... 84% 149M 6s
451700K .......... .......... .......... .......... .......... 84% 6.41M 6s
451750K .......... .......... .......... .......... .......... 84% 167M 6s
451800K .......... .......... .......... .......... .......... 84% 156M 6s
451850K .......... .......... .......... .......... .......... 84% 115M 6s
451900K .......... .......... .......... .......... .......... 84% 123M 6s
451950K .......... .......... .......... .......... .......... 84% 8.38M 6s
452000K .......... .......... .......... .......... .......... 84% 125M 6s
452050K .......... .......... .......... .......... .......... 84% 166M 6s
452100K .......... .......... .......... .......... .......... 84% 126M 6s
452150K .......... .......... .......... .......... .......... 84% 184M 6s
452200K .......... .......... .......... .......... .......... 84% 6.56M 6s
452250K .......... .......... .......... .......... .......... 84% 56.0M 6s
452300K .......... .......... .......... .......... .......... 84% 105M 6s
452350K .......... .......... .......... .......... .......... 84% 72.3M 6s
452400K .......... .......... .......... .......... .......... 84% 154M 6s
452450K .......... .......... .......... .......... .......... 84% 8.84M 6s
452500K .......... .......... .......... .......... .......... 84% 106M 6s
452550K .......... .......... .......... .......... .......... 84% 180M 6s
452600K .......... .......... .......... .......... .......... 84% 174M 6s
452650K .......... .......... .......... .......... .......... 84% 882K 6s
452700K .......... .......... .......... .......... .......... 84% 126M 6s
452750K .......... .......... .......... .......... .......... 84% 138M 6s
452800K .......... .......... .......... .......... .......... 84% 148M 6s
452850K .......... .......... .......... .......... .......... 84% 125M 6s
452900K .......... .......... .......... .......... .......... 84% 80.8M 6s
452950K .......... .......... .......... .......... .......... 84% 76.7M 6s
453000K .......... .......... .......... .......... .......... 84% 97.1M 6s
453050K .......... .......... .......... .......... .......... 84% 138M 6s
453100K .......... .......... .......... .......... .......... 84% 124M 6s
453150K .......... .......... .......... .......... .......... 85% 144M 6s
453200K .......... .......... .......... .......... .......... 85% 204M 6s
453250K .......... .......... .......... .......... .......... 85% 111M 6s
453300K .......... .......... .......... .......... .......... 85% 192M 6s
453350K .......... .......... .......... .......... .......... 85% 233M 6s
453400K .......... .......... .......... .......... .......... 85% 218M 6s
453450K .......... .......... .......... .......... .......... 85% 207M 6s
453500K .......... .......... .......... .......... .......... 85% 326M 6s
453550K .......... .......... .......... .......... .......... 85% 313M 6s
453600K .......... .......... .......... .......... .......... 85% 282M 6s
453650K .......... .......... .......... .......... .......... 85% 245M 6s
453700K .......... .......... .......... .......... .......... 85% 286M 6s
453750K .......... .......... .......... .......... .......... 85% 337M 6s
453800K .......... .......... .......... .......... .......... 85% 339M 6s
453850K .......... .......... .......... .......... .......... 85% 15.7M 6s
453900K .......... .......... .......... .......... .......... 85% 182M 6s
453950K .......... .......... .......... .......... .......... 85% 173M 6s
454000K .......... .......... .......... .......... .......... 85% 199M 6s
454050K .......... .......... .......... .......... .......... 85% 235M 6s
454100K .......... .......... .......... .......... .......... 85% 7.77M 6s
454150K .......... .......... .......... .......... .......... 85% 147M 6s
454200K .......... .......... .......... .......... .......... 85% 30.9M 6s
454250K .......... .......... .......... .......... .......... 85% 75.4M 6s
454300K .......... .......... .......... .......... .......... 85% 112M 6s
454350K .......... .......... .......... .......... .......... 85% 7.62M 6s
454400K .......... .......... .......... .......... .......... 85% 131M 6s
454450K .......... .......... .......... .......... .......... 85% 104M 6s
454500K .......... .......... .......... .......... .......... 85% 198M 6s
454550K .......... .......... .......... .......... .......... 85% 192M 6s
454600K .......... .......... .......... .......... .......... 85% 8.25M 6s
454650K .......... .......... .......... .......... .......... 85% 112M 6s
454700K .......... .......... .......... .......... .......... 85% 1.44M 6s
454750K .......... .......... .......... .......... .......... 85% 118M 6s
454800K .......... .......... .......... .......... .......... 85% 106M 6s
454850K .......... .......... .......... .......... .......... 85% 75.6M 6s
454900K .......... .......... .......... .......... .......... 85% 144M 6s
454950K .......... .......... .......... .......... .......... 85% 127M 6s
455000K .......... .......... .......... .......... .......... 85% 208M 6s
455050K .......... .......... .......... .......... .......... 85% 218M 6s
455100K .......... .......... .......... .......... .......... 85% 116M 6s
455150K .......... .......... .......... .......... .......... 85% 143M 6s
455200K .......... .......... .......... .......... .......... 85% 108M 6s
455250K .......... .......... .......... .......... .......... 85% 138M 6s
455300K .......... .......... .......... .......... .......... 85% 138M 6s
455350K .......... .......... .......... .......... .......... 85% 168M 6s
455400K .......... .......... .......... .......... .......... 85% 203M 6s
455450K .......... .......... .......... .......... .......... 85% 197M 6s
455500K .......... .......... .......... .......... .......... 85% 231M 6s
455550K .......... .......... .......... .......... .......... 85% 238M 6s
455600K .......... .......... .......... .......... .......... 85% 174M 6s
455650K .......... .......... .......... .......... .......... 85% 213M 6s
455700K .......... .......... .......... .......... .......... 85% 10.9M 6s
455750K .......... .......... .......... .......... .......... 85% 193M 6s
455800K .......... .......... .......... .......... .......... 85% 115M 6s
455850K .......... .......... .......... .......... .......... 85% 135M 6s
455900K .......... .......... .......... .......... .......... 85% 44.3M 6s
455950K .......... .......... .......... .......... .......... 85% 105M 6s
456000K .......... .......... .......... .......... .......... 85% 145M 6s
456050K .......... .......... .......... .......... .......... 85% 35.4M 6s
456100K .......... .......... .......... .......... .......... 85% 7.45M 6s
456150K .......... .......... .......... .......... .......... 85% 57.9M 6s
456200K .......... .......... .......... .......... .......... 85% 21.8M 6s
456250K .......... .......... .......... .......... .......... 85% 74.3M 6s
456300K .......... .......... .......... .......... .......... 85% 69.7M 6s
456350K .......... .......... .......... .......... .......... 85% 4.81M 6s
456400K .......... .......... .......... .......... .......... 85% 49.5M 6s
456450K .......... .......... .......... .......... .......... 85% 37.9M 6s
456500K .......... .......... .......... .......... .......... 85% 65.2M 6s
456550K .......... .......... .......... .......... .......... 85% 75.9M 6s
456600K .......... .......... .......... .......... .......... 85% 7.12M 6s
456650K .......... .......... .......... .......... .......... 85% 22.8M 6s
456700K .......... .......... .......... .......... .......... 85% 82.9M 6s
456750K .......... .......... .......... .......... .......... 85% 5.36M 6s
456800K .......... .......... .......... .......... .......... 85% 6.75M 6s
456850K .......... .......... .......... .......... .......... 85% 51.5M 6s
456900K .......... .......... .......... .......... .......... 85% 138M 6s
456950K .......... .......... .......... .......... .......... 85% 83.9M 6s
457000K .......... .......... .......... .......... .......... 85% 99.9M 6s
457050K .......... .......... .......... .......... .......... 85% 113M 6s
457100K .......... .......... .......... .......... .......... 85% 94.4M 6s
457150K .......... .......... .......... .......... .......... 85% 178M 6s
457200K .......... .......... .......... .......... .......... 85% 24.7M 6s
457250K .......... .......... .......... .......... .......... 85% 73.6M 6s
457300K .......... .......... .......... .......... .......... 85% 168M 6s
457350K .......... .......... .......... .......... .......... 85% 55.8M 6s
457400K .......... .......... .......... .......... .......... 85% 21.3M 6s
457450K .......... .......... .......... .......... .......... 85% 63.2M 6s
457500K .......... .......... .......... .......... .......... 85% 76.9M 6s
457550K .......... .......... .......... .......... .......... 85% 78.1M 6s
457600K .......... .......... .......... .......... .......... 85% 3.71M 6s
457650K .......... .......... .......... .......... .......... 85% 81.2M 6s
457700K .......... .......... .......... .......... .......... 85% 20.3M 6s
457750K .......... .......... .......... .......... .......... 85% 619K 6s
457800K .......... .......... .......... .......... .......... 85% 103M 6s
457850K .......... .......... .......... .......... .......... 85% 48.1M 6s
457900K .......... .......... .......... .......... .......... 85% 41.9M 6s
457950K .......... .......... .......... .......... .......... 85% 93.5M 6s
458000K .......... .......... .......... .......... .......... 85% 83.5M 6s
458050K .......... .......... .......... .......... .......... 85% 11.4M 6s
458100K .......... .......... .......... .......... .......... 85% 88.8M 6s
458150K .......... .......... .......... .......... .......... 85% 70.6M 6s
458200K .......... .......... .......... .......... .......... 85% 24.0M 6s
458250K .......... .......... .......... .......... .......... 85% 205M 6s
458300K .......... .......... .......... .......... .......... 85% 162M 6s
458350K .......... .......... .......... .......... .......... 85% 4.04M 6s
458400K .......... .......... .......... .......... .......... 85% 111M 6s
458450K .......... .......... .......... .......... .......... 85% 133M 6s
458500K .......... .......... .......... .......... .......... 86% 27.4M 6s
458550K .......... .......... .......... .......... .......... 86% 29.7M 6s
458600K .......... .......... .......... .......... .......... 86% 45.0M 6s
458650K .......... .......... .......... .......... .......... 86% 156M 6s
458700K .......... .......... .......... .......... .......... 86% 127M 6s
458750K .......... .......... .......... .......... .......... 86% 7.15M 6s
458800K .......... .......... .......... .......... .......... 86% 11.5M 6s
458850K .......... .......... .......... .......... .......... 86% 96.5M 6s
458900K .......... .......... .......... .......... .......... 86% 219M 6s
458950K .......... .......... .......... .......... .......... 86% 22.1M 6s
459000K .......... .......... .......... .......... .......... 86% 12.5M 6s
459050K .......... .......... .......... .......... .......... 86% 54.0M 6s
459100K .......... .......... .......... .......... .......... 86% 25.0M 6s
459150K .......... .......... .......... .......... .......... 86% 90.4M 6s
459200K .......... .......... .......... .......... .......... 86% 986K 6s
459250K .......... .......... .......... .......... .......... 86% 3.96M 6s
459300K .......... .......... .......... .......... .......... 86% 1.65M 6s
459350K .......... .......... .......... .......... .......... 86% 44.8M 6s
459400K .......... .......... .......... .......... .......... 86% 86.7M 6s
459450K .......... .......... .......... .......... .......... 86% 23.7M 6s
459500K .......... .......... .......... .......... .......... 86% 45.2M 6s
459550K .......... .......... .......... .......... .......... 86% 44.8M 6s
459600K .......... .......... .......... .......... .......... 86% 16.6M 6s
459650K .......... .......... .......... .......... .......... 86% 46.9M 5s
459700K .......... .......... .......... .......... .......... 86% 103M 5s
459750K .......... .......... .......... .......... .......... 86% 69.7M 5s
459800K .......... .......... .......... .......... .......... 86% 55.0M 5s
459850K .......... .......... .......... .......... .......... 86% 67.6M 5s
459900K .......... .......... .......... .......... .......... 86% 80.8M 5s
459950K .......... .......... .......... .......... .......... 86% 137M 5s
460000K .......... .......... .......... .......... .......... 86% 78.1M 5s
460050K .......... .......... .......... .......... .......... 86% 144M 5s
460100K .......... .......... .......... .......... .......... 86% 19.7M 5s
460150K .......... .......... .......... .......... .......... 86% 116M 5s
460200K .......... .......... .......... .......... .......... 86% 18.9M 5s
460250K .......... .......... .......... .......... .......... 86% 99.4M 5s
460300K .......... .......... .......... .......... .......... 86% 76.9M 5s
460350K .......... .......... .......... .......... .......... 86% 27.2M 5s
460400K .......... .......... .......... .......... .......... 86% 18.1M 5s
460450K .......... .......... .......... .......... .......... 86% 43.5M 5s
460500K .......... .......... .......... .......... .......... 86% 91.6M 5s
460550K .......... .......... .......... .......... .......... 86% 47.3M 5s
460600K .......... .......... .......... .......... .......... 86% 64.6M 5s
460650K .......... .......... .......... .......... .......... 86% 40.7M 5s
460700K .......... .......... .......... .......... .......... 86% 127M 5s
460750K .......... .......... .......... .......... .......... 86% 20.6M 5s
460800K .......... .......... .......... .......... .......... 86% 63.2M 5s
460850K .......... .......... .......... .......... .......... 86% 631K 5s
460900K .......... .......... .......... .......... .......... 86% 44.7M 5s
460950K .......... .......... .......... .......... .......... 86% 54.8M 5s
461000K .......... .......... .......... .......... .......... 86% 42.9M 5s
461050K .......... .......... .......... .......... .......... 86% 27.6M 5s
461100K .......... .......... .......... .......... .......... 86% 38.0M 5s
461150K .......... .......... .......... .......... .......... 86% 2.72M 5s
461200K .......... .......... .......... .......... .......... 86% 47.5M 5s
461250K .......... .......... .......... .......... .......... 86% 33.2M 5s
461300K .......... .......... .......... .......... .......... 86% 4.78M 5s
461350K .......... .......... .......... .......... .......... 86% 41.6M 5s
461400K .......... .......... .......... .......... .......... 86% 43.1M 5s
461450K .......... .......... .......... .......... .......... 86% 123M 5s
461500K .......... .......... .......... .......... .......... 86% 81.7M 5s
461550K .......... .......... .......... .......... .......... 86% 65.7M 5s
461600K .......... .......... .......... .......... .......... 86% 82.9M 5s
461650K .......... .......... .......... .......... .......... 86% 144M 5s
461700K .......... .......... .......... .......... .......... 86% 102M 5s
461750K .......... .......... .......... .......... .......... 86% 91.1M 5s
461800K .......... .......... .......... .......... .......... 86% 35.3M 5s
461850K .......... .......... .......... .......... .......... 86% 3.29M 5s
461900K .......... .......... .......... .......... .......... 86% 14.4M 5s
461950K .......... .......... .......... .......... .......... 86% 36.9M 5s
462000K .......... .......... .......... .......... .......... 86% 130M 5s
462050K .......... .......... .......... .......... .......... 86% 36.6M 5s
462100K .......... .......... .......... .......... .......... 86% 45.3M 5s
462150K .......... .......... .......... .......... .......... 86% 103M 5s
462200K .......... .......... .......... .......... .......... 86% 113M 5s
462250K .......... .......... .......... .......... .......... 86% 8.52M 5s
462300K .......... .......... .......... .......... .......... 86% 203M 5s
462350K .......... .......... .......... .......... .......... 86% 22.2M 5s
462400K .......... .......... .......... .......... .......... 86% 11.8M 5s
462450K .......... .......... .......... .......... .......... 86% 14.3M 5s
462500K .......... .......... .......... .......... .......... 86% 4.10M 5s
462550K .......... .......... .......... .......... .......... 86% 2.96M 5s
462600K .......... .......... .......... .......... .......... 86% 44.1M 5s
462650K .......... .......... .......... .......... .......... 86% 31.5M 5s
462700K .......... .......... .......... .......... .......... 86% 30.8M 5s
462750K .......... .......... .......... .......... .......... 86% 49.0M 5s
462800K .......... .......... .......... .......... .......... 86% 44.3M 5s
462850K .......... .......... .......... .......... .......... 86% 98.0M 5s
462900K .......... .......... .......... .......... .......... 86% 4.77M 5s
462950K .......... .......... .......... .......... .......... 86% 99.4M 5s
463000K .......... .......... .......... .......... .......... 86% 66.1M 5s
463050K .......... .......... .......... .......... .......... 86% 71.1M 5s
463100K .......... .......... .......... .......... .......... 86% 106M 5s
463150K .......... .......... .......... .......... .......... 86% 146M 5s
463200K .......... .......... .......... .......... .......... 86% 22.4M 5s
463250K .......... .......... .......... .......... .......... 86% 11.8M 5s
463300K .......... .......... .......... .......... .......... 86% 4.66M 5s
463350K .......... .......... .......... .......... .......... 86% 42.8M 5s
463400K .......... .......... .......... .......... .......... 86% 45.4M 5s
463450K .......... .......... .......... .......... .......... 86% 24.1M 5s
463500K .......... .......... .......... .......... .......... 86% 22.1M 5s
463550K .......... .......... .......... .......... .......... 86% 17.8M 5s
463600K .......... .......... .......... .......... .......... 86% 165M 5s
463650K .......... .......... .......... .......... .......... 86% 184M 5s
463700K .......... .......... .......... .......... .......... 86% 168M 5s
463750K .......... .......... .......... .......... .......... 86% 215M 5s
463800K .......... .......... .......... .......... .......... 87% 173M 5s
463850K .......... .......... .......... .......... .......... 87% 136M 5s
463900K .......... .......... .......... .......... .......... 87% 178M 5s
463950K .......... .......... .......... .......... .......... 87% 175M 5s
464000K .......... .......... .......... .......... .......... 87% 168M 5s
464050K .......... .......... .......... .......... .......... 87% 68.2M 5s
464100K .......... .......... .......... .......... .......... 87% 22.4M 5s
464150K .......... .......... .......... .......... .......... 87% 41.0M 5s
464200K .......... .......... .......... .......... .......... 87% 122M 5s
464250K .......... .......... .......... .......... .......... 87% 36.3M 5s
464300K .......... .......... .......... .......... .......... 87% 142M 5s
464350K .......... .......... .......... .......... .......... 87% 109M 5s
464400K .......... .......... .......... .......... .......... 87% 198M 5s
464450K .......... .......... .......... .......... .......... 87% 117M 5s
464500K .......... .......... .......... .......... .......... 87% 205M 5s
464550K .......... .......... .......... .......... .......... 87% 164M 5s
464600K .......... .......... .......... .......... .......... 87% 31.4M 5s
464650K .......... .......... .......... .......... .......... 87% 164M 5s
464700K .......... .......... .......... .......... .......... 87% 49.5M 5s
464750K .......... .......... .......... .......... .......... 87% 77.4M 5s
464800K .......... .......... .......... .......... .......... 87% 61.0M 5s
464850K .......... .......... .......... .......... .......... 87% 164M 5s
464900K .......... .......... .......... .......... .......... 87% 7.18M 5s
464950K .......... .......... .......... .......... .......... 87% 17.5M 5s
465000K .......... .......... .......... .......... .......... 87% 214M 5s
465050K .......... .......... .......... .......... .......... 87% 132M 5s
465100K .......... .......... .......... .......... .......... 87% 147M 5s
465150K .......... .......... .......... .......... .......... 87% 3.17M 5s
465200K .......... .......... .......... .......... .......... 87% 168M 5s
465250K .......... .......... .......... .......... .......... 87% 113M 5s
465300K .......... .......... .......... .......... .......... 87% 205M 5s
465350K .......... .......... .......... .......... .......... 87% 159M 5s
465400K .......... .......... .......... .......... .......... 87% 200M 5s
465450K .......... .......... .......... .......... .......... 87% 104M 5s
465500K .......... .......... .......... .......... .......... 87% 165M 5s
465550K .......... .......... .......... .......... .......... 87% 152M 5s
465600K .......... .......... .......... .......... .......... 87% 43.4M 5s
465650K .......... .......... .......... .......... .......... 87% 15.2M 5s
465700K .......... .......... .......... .......... .......... 87% 113M 5s
465750K .......... .......... .......... .......... .......... 87% 147M 5s
465800K .......... .......... .......... .......... .......... 87% 148M 5s
465850K .......... .......... .......... .......... .......... 87% 19.0M 5s
465900K .......... .......... .......... .......... .......... 87% 7.40M 5s
465950K .......... .......... .......... .......... .......... 87% 13.1M 5s
466000K .......... .......... .......... .......... .......... 87% 81.2M 5s
466050K .......... .......... .......... .......... .......... 87% 87.3M 5s
466100K .......... .......... .......... .......... .......... 87% 154M 5s
466150K .......... .......... .......... .......... .......... 87% 159M 5s
466200K .......... .......... .......... .......... .......... 87% 5.91M 5s
466250K .......... .......... .......... .......... .......... 87% 210M 5s
466300K .......... .......... .......... .......... .......... 87% 91.4M 5s
466350K .......... .......... .......... .......... .......... 87% 97.9M 5s
466400K .......... .......... .......... .......... .......... 87% 196M 5s
466450K .......... .......... .......... .......... .......... 87% 6.73M 5s
466500K .......... .......... .......... .......... .......... 87% 163M 5s
466550K .......... .......... .......... .......... .......... 87% 167M 5s
466600K .......... .......... .......... .......... .......... 87% 140M 5s
466650K .......... .......... .......... .......... .......... 87% 168M 5s
466700K .......... .......... .......... .......... .......... 87% 4.51M 5s
466750K .......... .......... .......... .......... .......... 87% 98.6M 5s
466800K .......... .......... .......... .......... .......... 87% 76.9M 5s
466850K .......... .......... .......... .......... .......... 87% 8.04M 5s
466900K .......... .......... .......... .......... .......... 87% 125M 5s
466950K .......... .......... .......... .......... .......... 87% 15.4M 5s
467000K .......... .......... .......... .......... .......... 87% 4.48M 5s
467050K .......... .......... .......... .......... .......... 87% 57.4M 5s
467100K .......... .......... .......... .......... .......... 87% 44.7M 5s
467150K .......... .......... .......... .......... .......... 87% 24.1M 5s
467200K .......... .......... .......... .......... .......... 87% 22.5M 5s
467250K .......... .......... .......... .......... .......... 87% 258M 5s
467300K .......... .......... .......... .......... .......... 87% 10.5M 5s
467350K .......... .......... .......... .......... .......... 87% 77.3M 5s
467400K .......... .......... .......... .......... .......... 87% 862K 5s
467450K .......... .......... .......... .......... .......... 87% 6.89M 5s
467500K .......... .......... .......... .......... .......... 87% 666K 5s
467550K .......... .......... .......... .......... .......... 87% 140M 5s
467600K .......... .......... .......... .......... .......... 87% 26.8M 5s
467650K .......... .......... .......... .......... .......... 87% 4.36M 5s
467700K .......... .......... .......... .......... .......... 87% 18.2M 5s
467750K .......... .......... .......... .......... .......... 87% 78.8M 5s
467800K .......... .......... .......... .......... .......... 87% 63.1M 5s
467850K .......... .......... .......... .......... .......... 87% 28.4M 5s
467900K .......... .......... .......... .......... .......... 87% 51.3M 5s
467950K .......... .......... .......... .......... .......... 87% 26.5M 5s
468000K .......... .......... .......... .......... .......... 87% 60.4M 5s
468050K .......... .......... .......... .......... .......... 87% 50.5M 5s
468100K .......... .......... .......... .......... .......... 87% 71.4M 5s
468150K .......... .......... .......... .......... .......... 87% 27.6M 5s
468200K .......... .......... .......... .......... .......... 87% 198M 5s
468250K .......... .......... .......... .......... .......... 87% 82.9M 5s
468300K .......... .......... .......... .......... .......... 87% 159M 5s
468350K .......... .......... .......... .......... .......... 87% 51.3M 5s
468400K .......... .......... .......... .......... .......... 87% 69.3M 5s
468450K .......... .......... .......... .......... .......... 87% 61.3M 5s
468500K .......... .......... .......... .......... .......... 87% 22.0M 5s
468550K .......... .......... .......... .......... .......... 87% 2.11M 5s
468600K .......... .......... .......... .......... .......... 87% 16.0M 5s
468650K .......... .......... .......... .......... .......... 87% 115M 5s
468700K .......... .......... .......... .......... .......... 87% 181M 5s
468750K .......... .......... .......... .......... .......... 87% 138M 5s
468800K .......... .......... .......... .......... .......... 87% 173M 5s
468850K .......... .......... .......... .......... .......... 87% 161M 5s
468900K .......... .......... .......... .......... .......... 87% 14.4M 5s
468950K .......... .......... .......... .......... .......... 87% 132M 5s
469000K .......... .......... .......... .......... .......... 87% 131M 5s
469050K .......... .......... .......... .......... .......... 87% 6.91M 5s
469100K .......... .......... .......... .......... .......... 87% 10.0M 5s
469150K .......... .......... .......... .......... .......... 88% 8.39M 5s
469200K .......... .......... .......... .......... .......... 88% 45.5M 5s
469250K .......... .......... .......... .......... .......... 88% 26.0M 5s
469300K .......... .......... .......... .......... .......... 88% 159M 5s
469350K .......... .......... .......... .......... .......... 88% 3.95M 5s
469400K .......... .......... .......... .......... .......... 88% 18.9M 5s
469450K .......... .......... .......... .......... .......... 88% 16.7M 5s
469500K .......... .......... .......... .......... .......... 88% 15.9M 5s
469550K .......... .......... .......... .......... .......... 88% 20.9M 5s
469600K .......... .......... .......... .......... .......... 88% 2.18M 5s
469650K .......... .......... .......... .......... .......... 88% 3.64M 5s
469700K .......... .......... .......... .......... .......... 88% 7.63M 5s
469750K .......... .......... .......... .......... .......... 88% 13.0M 5s
469800K .......... .......... .......... .......... .......... 88% 35.9M 5s
469850K .......... .......... .......... .......... .......... 88% 1.44M 5s
469900K .......... .......... .......... .......... .......... 88% 9.13M 5s
469950K .......... .......... .......... .......... .......... 88% 46.8M 5s
470000K .......... .......... .......... .......... .......... 88% 53.2M 5s
470050K .......... .......... .......... .......... .......... 88% 23.6M 5s
470100K .......... .......... .......... .......... .......... 88% 47.9M 5s
470150K .......... .......... .......... .......... .......... 88% 53.4M 5s
470200K .......... .......... .......... .......... .......... 88% 47.2M 5s
470250K .......... .......... .......... .......... .......... 88% 91.6M 5s
470300K .......... .......... .......... .......... .......... 88% 52.8M 5s
470350K .......... .......... .......... .......... .......... 88% 33.7M 5s
470400K .......... .......... .......... .......... .......... 88% 113M 5s
470450K .......... .......... .......... .......... .......... 88% 4.51M 5s
470500K .......... .......... .......... .......... .......... 88% 3.08M 5s
470550K .......... .......... .......... .......... .......... 88% 56.6M 5s
470600K .......... .......... .......... .......... .......... 88% 44.6M 5s
470650K .......... .......... .......... .......... .......... 88% 65.4M 5s
470700K .......... .......... .......... .......... .......... 88% 43.1M 5s
470750K .......... .......... .......... .......... .......... 88% 69.0M 5s
470800K .......... .......... .......... .......... .......... 88% 34.1M 5s
470850K .......... .......... .......... .......... .......... 88% 61.3M 5s
470900K .......... .......... .......... .......... .......... 88% 94.3M 5s
470950K .......... .......... .......... .......... .......... 88% 52.3M 5s
471000K .......... .......... .......... .......... .......... 88% 53.8M 5s
471050K .......... .......... .......... .......... .......... 88% 13.5M 5s
471100K .......... .......... .......... .......... .......... 88% 79.5M 5s
471150K .......... .......... .......... .......... .......... 88% 98.4M 5s
471200K .......... .......... .......... .......... .......... 88% 36.8M 5s
471250K .......... .......... .......... .......... .......... 88% 134M 5s
471300K .......... .......... .......... .......... .......... 88% 90.3M 5s
471350K .......... .......... .......... .......... .......... 88% 47.5M 5s
471400K .......... .......... .......... .......... .......... 88% 122M 5s
471450K .......... .......... .......... .......... .......... 88% 69.9M 5s
471500K .......... .......... .......... .......... .......... 88% 25.2M 5s
471550K .......... .......... .......... .......... .......... 88% 80.7M 5s
471600K .......... .......... .......... .......... .......... 88% 75.5M 5s
471650K .......... .......... .......... .......... .......... 88% 149M 5s
471700K .......... .......... .......... .......... .......... 88% 85.7M 5s
471750K .......... .......... .......... .......... .......... 88% 87.3M 5s
471800K .......... .......... .......... .......... .......... 88% 75.4M 5s
471850K .......... .......... .......... .......... .......... 88% 551K 5s
471900K .......... .......... .......... .......... .......... 88% 9.86M 5s
471950K .......... .......... .......... .......... .......... 88% 43.8M 5s
472000K .......... .......... .......... .......... .......... 88% 176M 5s
472050K .......... .......... .......... .......... .......... 88% 77.5M 5s
472100K .......... .......... .......... .......... .......... 88% 34.2M 5s
472150K .......... .......... .......... .......... .......... 88% 34.0M 5s
472200K .......... .......... .......... .......... .......... 88% 56.7M 5s
472250K .......... .......... .......... .......... .......... 88% 5.60M 5s
472300K .......... .......... .......... .......... .......... 88% 80.4M 5s
472350K .......... .......... .......... .......... .......... 88% 81.7M 5s
472400K .......... .......... .......... .......... .......... 88% 125M 5s
472450K .......... .......... .......... .......... .......... 88% 102M 5s
472500K .......... .......... .......... .......... .......... 88% 48.8M 5s
472550K .......... .......... .......... .......... .......... 88% 18.3M 5s
472600K .......... .......... .......... .......... .......... 88% 60.6M 5s
472650K .......... .......... .......... .......... .......... 88% 60.2M 5s
472700K .......... .......... .......... .......... .......... 88% 30.0M 5s
472750K .......... .......... .......... .......... .......... 88% 11.1M 5s
472800K .......... .......... .......... .......... .......... 88% 20.0M 5s
472850K .......... .......... .......... .......... .......... 88% 45.2M 4s
472900K .......... .......... .......... .......... .......... 88% 94.4M 4s
472950K .......... .......... .......... .......... .......... 88% 108M 4s
473000K .......... .......... .......... .......... .......... 88% 164M 4s
473050K .......... .......... .......... .......... .......... 88% 137M 4s
473100K .......... .......... .......... .......... .......... 88% 2.08M 4s
473150K .......... .......... .......... .......... .......... 88% 64.2M 4s
473200K .......... .......... .......... .......... .......... 88% 158M 4s
473250K .......... .......... .......... .......... .......... 88% 18.2M 4s
473300K .......... .......... .......... .......... .......... 88% 94.3M 4s
473350K .......... .......... .......... .......... .......... 88% 116M 4s
473400K .......... .......... .......... .......... .......... 88% 137M 4s
473450K .......... .......... .......... .......... .......... 88% 167M 4s
473500K .......... .......... .......... .......... .......... 88% 198M 4s
473550K .......... .......... .......... .......... .......... 88% 126M 4s
473600K .......... .......... .......... .......... .......... 88% 82.6M 4s
473650K .......... .......... .......... .......... .......... 88% 123M 4s
473700K .......... .......... .......... .......... .......... 88% 156M 4s
473750K .......... .......... .......... .......... .......... 88% 206M 4s
473800K .......... .......... .......... .......... .......... 88% 192M 4s
473850K .......... .......... .......... .......... .......... 88% 121M 4s
473900K .......... .......... .......... .......... .......... 88% 130M 4s
473950K .......... .......... .......... .......... .......... 88% 191M 4s
474000K .......... .......... .......... .......... .......... 88% 117M 4s
474050K .......... .......... .......... .......... .......... 88% 121M 4s
474100K .......... .......... .......... .......... .......... 88% 139M 4s
474150K .......... .......... .......... .......... .......... 88% 158M 4s
474200K .......... .......... .......... .......... .......... 88% 111M 4s
474250K .......... .......... .......... .......... .......... 88% 170M 4s
474300K .......... .......... .......... .......... .......... 88% 180M 4s
474350K .......... .......... .......... .......... .......... 88% 136M 4s
474400K .......... .......... .......... .......... .......... 88% 204M 4s
474450K .......... .......... .......... .......... .......... 88% 8.33M 4s
474500K .......... .......... .......... .......... .......... 89% 196M 4s
474550K .......... .......... .......... .......... .......... 89% 184M 4s
474600K .......... .......... .......... .......... .......... 89% 111M 4s
474650K .......... .......... .......... .......... .......... 89% 92.8M 4s
474700K .......... .......... .......... .......... .......... 89% 5.79M 4s
474750K .......... .......... .......... .......... .......... 89% 186M 4s
474800K .......... .......... .......... .......... .......... 89% 88.8M 4s
474850K .......... .......... .......... .......... .......... 89% 152M 4s
474900K .......... .......... .......... .......... .......... 89% 65.1M 4s
474950K .......... .......... .......... .......... .......... 89% 7.73M 4s
475000K .......... .......... .......... .......... .......... 89% 129M 4s
475050K .......... .......... .......... .......... .......... 89% 138M 4s
475100K .......... .......... .......... .......... .......... 89% 130M 4s
475150K .......... .......... .......... .......... .......... 89% 1.35M 4s
475200K .......... .......... .......... .......... .......... 89% 132M 4s
475250K .......... .......... .......... .......... .......... 89% 137M 4s
475300K .......... .......... .......... .......... .......... 89% 36.1M 4s
475350K .......... .......... .......... .......... .......... 89% 135M 4s
475400K .......... .......... .......... .......... .......... 89% 167M 4s
475450K .......... .......... .......... .......... .......... 89% 154M 4s
475500K .......... .......... .......... .......... .......... 89% 174M 4s
475550K .......... .......... .......... .......... .......... 89% 161M 4s
475600K .......... .......... .......... .......... .......... 89% 157M 4s
475650K .......... .......... .......... .......... .......... 89% 188M 4s
475700K .......... .......... .......... .......... .......... 89% 162M 4s
475750K .......... .......... .......... .......... .......... 89% 180M 4s
475800K .......... .......... .......... .......... .......... 89% 180M 4s
475850K .......... .......... .......... .......... .......... 89% 152M 4s
475900K .......... .......... .......... .......... .......... 89% 174M 4s
475950K .......... .......... .......... .......... .......... 89% 153M 4s
476000K .......... .......... .......... .......... .......... 89% 172M 4s
476050K .......... .......... .......... .......... .......... 89% 161M 4s
476100K .......... .......... .......... .......... .......... 89% 160M 4s
476150K .......... .......... .......... .......... .......... 89% 184M 4s
476200K .......... .......... .......... .......... .......... 89% 119M 4s
476250K .......... .......... .......... .......... .......... 89% 167M 4s
476300K .......... .......... .......... .......... .......... 89% 242M 4s
476350K .......... .......... .......... .......... .......... 89% 8.20M 4s
476400K .......... .......... .......... .......... .......... 89% 106M 4s
476450K .......... .......... .......... .......... .......... 89% 8.64M 4s
476500K .......... .......... .......... .......... .......... 89% 179M 4s
476550K .......... .......... .......... .......... .......... 89% 209M 4s
476600K .......... .......... .......... .......... .......... 89% 9.06M 4s
476650K .......... .......... .......... .......... .......... 89% 115M 4s
476700K .......... .......... .......... .......... .......... 89% 155M 4s
476750K .......... .......... .......... .......... .......... 89% 10.5M 4s
476800K .......... .......... .......... .......... .......... 89% 209M 4s
476850K .......... .......... .......... .......... .......... 89% 12.3M 4s
476900K .......... .......... .......... .......... .......... 89% 210M 4s
476950K .......... .......... .......... .......... .......... 89% 206M 4s
477000K .......... .......... .......... .......... .......... 89% 169M 4s
477050K .......... .......... .......... .......... .......... 89% 3.37M 4s
477100K .......... .......... .......... .......... .......... 89% 198M 4s
477150K .......... .......... .......... .......... .......... 89% 191M 4s
477200K .......... .......... .......... .......... .......... 89% 7.35M 4s
477250K .......... .......... .......... .......... .......... 89% 115M 4s
477300K .......... .......... .......... .......... .......... 89% 146M 4s
477350K .......... .......... .......... .......... .......... 89% 123M 4s
477400K .......... .......... .......... .......... .......... 89% 113M 4s
477450K .......... .......... .......... .......... .......... 89% 110M 4s
477500K .......... .......... .......... .......... .......... 89% 253M 4s
477550K .......... .......... .......... .......... .......... 89% 155M 4s
477600K .......... .......... .......... .......... .......... 89% 6.72M 4s
477650K .......... .......... .......... .......... .......... 89% 132M 4s
477700K .......... .......... .......... .......... .......... 89% 180M 4s
477750K .......... .......... .......... .......... .......... 89% 216M 4s
477800K .......... .......... .......... .......... .......... 89% 210M 4s
477850K .......... .......... .......... .......... .......... 89% 6.68M 4s
477900K .......... .......... .......... .......... .......... 89% 143M 4s
477950K .......... .......... .......... .......... .......... 89% 147M 4s
478000K .......... .......... .......... .......... .......... 89% 105M 4s
478050K .......... .......... .......... .......... .......... 89% 199M 4s
478100K .......... .......... .......... .......... .......... 89% 7.74M 4s
478150K .......... .......... .......... .......... .......... 89% 146M 4s
478200K .......... .......... .......... .......... .......... 89% 178M 4s
478250K .......... .......... .......... .......... .......... 89% 152M 4s
478300K .......... .......... .......... .......... .......... 89% 213M 4s
478350K .......... .......... .......... .......... .......... 89% 7.00M 4s
478400K .......... .......... .......... .......... .......... 89% 176M 4s
478450K .......... .......... .......... .......... .......... 89% 125M 4s
478500K .......... .......... .......... .......... .......... 89% 200M 4s
478550K .......... .......... .......... .......... .......... 89% 194M 4s
478600K .......... .......... .......... .......... .......... 89% 180M 4s
478650K .......... .......... .......... .......... .......... 89% 7.23M 4s
478700K .......... .......... .......... .......... .......... 89% 160M 4s
478750K .......... .......... .......... .......... .......... 89% 167M 4s
478800K .......... .......... .......... .......... .......... 89% 186M 4s
478850K .......... .......... .......... .......... .......... 89% 161M 4s
478900K .......... .......... .......... .......... .......... 89% 7.12M 4s
478950K .......... .......... .......... .......... .......... 89% 139M 4s
479000K .......... .......... .......... .......... .......... 89% 97.9M 4s
479050K .......... .......... .......... .......... .......... 89% 215M 4s
479100K .......... .......... .......... .......... .......... 89% 197M 4s
479150K .......... .......... .......... .......... .......... 89% 184M 4s
479200K .......... .......... .......... .......... .......... 89% 7.94M 4s
479250K .......... .......... .......... .......... .......... 89% 6.04M 4s
479300K .......... .......... .......... .......... .......... 89% 83.2M 4s
479350K .......... .......... .......... .......... .......... 89% 84.0M 4s
479400K .......... .......... .......... .......... .......... 89% 168M 4s
479450K .......... .......... .......... .......... .......... 89% 11.3M 4s
479500K .......... .......... .......... .......... .......... 89% 115M 4s
479550K .......... .......... .......... .......... .......... 89% 48.8M 4s
479600K .......... .......... .......... .......... .......... 89% 63.6M 4s
479650K .......... .......... .......... .......... .......... 89% 26.1M 4s
479700K .......... .......... .......... .......... .......... 89% 35.1M 4s
479750K .......... .......... .......... .......... .......... 89% 7.50M 4s
479800K .......... .......... .......... .......... .......... 90% 45.6M 4s
479850K .......... .......... .......... .......... .......... 90% 52.4M 4s
479900K .......... .......... .......... .......... .......... 90% 59.8M 4s
479950K .......... .......... .......... .......... .......... 90% 134M 4s
480000K .......... .......... .......... .......... .......... 90% 168M 4s
480050K .......... .......... .......... .......... .......... 90% 9.33M 4s
480100K .......... .......... .......... .......... .......... 90% 46.1M 4s
480150K .......... .......... .......... .......... .......... 90% 51.8M 4s
480200K .......... .......... .......... .......... .......... 90% 112M 4s
480250K .......... .......... .......... .......... .......... 90% 53.8M 4s
480300K .......... .......... .......... .......... .......... 90% 513K 4s
480350K .......... .......... .......... .......... .......... 90% 184M 4s
480400K .......... .......... .......... .......... .......... 90% 160M 4s
480450K .......... .......... .......... .......... .......... 90% 50.9M 4s
480500K .......... .......... .......... .......... .......... 90% 154M 4s
480550K .......... .......... .......... .......... .......... 90% 109M 4s
480600K .......... .......... .......... .......... .......... 90% 57.2M 4s
480650K .......... .......... .......... .......... .......... 90% 95.2M 4s
480700K .......... .......... .......... .......... .......... 90% 24.7M 4s
480750K .......... .......... .......... .......... .......... 90% 48.4M 4s
480800K .......... .......... .......... .......... .......... 90% 171M 4s
480850K .......... .......... .......... .......... .......... 90% 149M 4s
480900K .......... .......... .......... .......... .......... 90% 155M 4s
480950K .......... .......... .......... .......... .......... 90% 52.2M 4s
481000K .......... .......... .......... .......... .......... 90% 27.0M 4s
481050K .......... .......... .......... .......... .......... 90% 109M 4s
481100K .......... .......... .......... .......... .......... 90% 37.4M 4s
481150K .......... .......... .......... .......... .......... 90% 131M 4s
481200K .......... .......... .......... .......... .......... 90% 142M 4s
481250K .......... .......... .......... .......... .......... 90% 54.9M 4s
481300K .......... .......... .......... .......... .......... 90% 43.3M 4s
481350K .......... .......... .......... .......... .......... 90% 75.9M 4s
481400K .......... .......... .......... .......... .......... 90% 76.9M 4s
481450K .......... .......... .......... .......... .......... 90% 69.7M 4s
481500K .......... .......... .......... .......... .......... 90% 109M 4s
481550K .......... .......... .......... .......... .......... 90% 87.2M 4s
481600K .......... .......... .......... .......... .......... 90% 110M 4s
481650K .......... .......... .......... .......... .......... 90% 49.4M 4s
481700K .......... .......... .......... .......... .......... 90% 72.9M 4s
481750K .......... .......... .......... .......... .......... 90% 24.1M 4s
481800K .......... .......... .......... .......... .......... 90% 45.0M 4s
481850K .......... .......... .......... .......... .......... 90% 42.4M 4s
481900K .......... .......... .......... .......... .......... 90% 60.7M 4s
481950K .......... .......... .......... .......... .......... 90% 16.3M 4s
482000K .......... .......... .......... .......... .......... 90% 31.5M 4s
482050K .......... .......... .......... .......... .......... 90% 130M 4s
482100K .......... .......... .......... .......... .......... 90% 6.16M 4s
482150K .......... .......... .......... .......... .......... 90% 49.0M 4s
482200K .......... .......... .......... .......... .......... 90% 59.8M 4s
482250K .......... .......... .......... .......... .......... 90% 17.8M 4s
482300K .......... .......... .......... .......... .......... 90% 83.3M 4s
482350K .......... .......... .......... .......... .......... 90% 2.77M 4s
482400K .......... .......... .......... .......... .......... 90% 78.8M 4s
482450K .......... .......... .......... .......... .......... 90% 92.7M 4s
482500K .......... .......... .......... .......... .......... 90% 140M 4s
482550K .......... .......... .......... .......... .......... 90% 21.9M 4s
482600K .......... .......... .......... .......... .......... 90% 130M 4s
482650K .......... .......... .......... .......... .......... 90% 148M 4s
482700K .......... .......... .......... .......... .......... 90% 123M 4s
482750K .......... .......... .......... .......... .......... 90% 24.6M 4s
482800K .......... .......... .......... .......... .......... 90% 132M 4s
482850K .......... .......... .......... .......... .......... 90% 35.2M 4s
482900K .......... .......... .......... .......... .......... 90% 131M 4s
482950K .......... .......... .......... .......... .......... 90% 135M 4s
483000K .......... .......... .......... .......... .......... 90% 78.4M 4s
483050K .......... .......... .......... .......... .......... 90% 168M 4s
483100K .......... .......... .......... .......... .......... 90% 24.9M 4s
483150K .......... .......... .......... .......... .......... 90% 87.2M 4s
483200K .......... .......... .......... .......... .......... 90% 114M 4s
483250K .......... .......... .......... .......... .......... 90% 10.1M 4s
483300K .......... .......... .......... .......... .......... 90% 129M 4s
483350K .......... .......... .......... .......... .......... 90% 15.1M 4s
483400K .......... .......... .......... .......... .......... 90% 23.6M 4s
483450K .......... .......... .......... .......... .......... 90% 30.3M 4s
483500K .......... .......... .......... .......... .......... 90% 49.0M 4s
483550K .......... .......... .......... .......... .......... 90% 6.43M 4s
483600K .......... .......... .......... .......... .......... 90% 14.2M 4s
483650K .......... .......... .......... .......... .......... 90% 17.1M 4s
483700K .......... .......... .......... .......... .......... 90% 23.7M 4s
483750K .......... .......... .......... .......... .......... 90% 62.6M 4s
483800K .......... .......... .......... .......... .......... 90% 83.9M 4s
483850K .......... .......... .......... .......... .......... 90% 68.5M 4s
483900K .......... .......... .......... .......... .......... 90% 111M 4s
483950K .......... .......... .......... .......... .......... 90% 94.4M 4s
484000K .......... .......... .......... .......... .......... 90% 73.3M 4s
484050K .......... .......... .......... .......... .......... 90% 99.6M 4s
484100K .......... .......... .......... .......... .......... 90% 2.49M 4s
484150K .......... .......... .......... .......... .......... 90% 12.4M 4s
484200K .......... .......... .......... .......... .......... 90% 14.7M 4s
484250K .......... .......... .......... .......... .......... 90% 148M 4s
484300K .......... .......... .......... .......... .......... 90% 116M 4s
484350K .......... .......... .......... .......... .......... 90% 154M 4s
484400K .......... .......... .......... .......... .......... 90% 161M 4s
484450K .......... .......... .......... .......... .......... 90% 12.3M 4s
484500K .......... .......... .......... .......... .......... 90% 84.3M 4s
484550K .......... .......... .......... .......... .......... 90% 2.04M 4s
484600K .......... .......... .......... .......... .......... 90% 9.15M 4s
484650K .......... .......... .......... .......... .......... 90% 23.7M 4s
484700K .......... .......... .......... .......... .......... 90% 15.8M 4s
484750K .......... .......... .......... .......... .......... 90% 79.8M 4s
484800K .......... .......... .......... .......... .......... 90% 91.8M 4s
484850K .......... .......... .......... .......... .......... 90% 47.2M 4s
484900K .......... .......... .......... .......... .......... 90% 66.9M 4s
484950K .......... .......... .......... .......... .......... 90% 47.7M 4s
485000K .......... .......... .......... .......... .......... 90% 61.2M 4s
485050K .......... .......... .......... .......... .......... 90% 95.0M 4s
485100K .......... .......... .......... .......... .......... 90% 185M 4s
485150K .......... .......... .......... .......... .......... 91% 198M 4s
485200K .......... .......... .......... .......... .......... 91% 219M 4s
485250K .......... .......... .......... .......... .......... 91% 237M 4s
485300K .......... .......... .......... .......... .......... 91% 209M 4s
485350K .......... .......... .......... .......... .......... 91% 9.53M 4s
485400K .......... .......... .......... .......... .......... 91% 4.30M 4s
485450K .......... .......... .......... .......... .......... 91% 6.78M 4s
485500K .......... .......... .......... .......... .......... 91% 7.27M 4s
485550K .......... .......... .......... .......... .......... 91% 1.53M 4s
485600K .......... .......... .......... .......... .......... 91% 114M 4s
485650K .......... .......... .......... .......... .......... 91% 10.8M 4s
485700K .......... .......... .......... .......... .......... 91% 8.18M 4s
485750K .......... .......... .......... .......... .......... 91% 95.7M 4s
485800K .......... .......... .......... .......... .......... 91% 5.48M 3s
485850K .......... .......... .......... .......... .......... 91% 93.7M 3s
485900K .......... .......... .......... .......... .......... 91% 153M 3s
485950K .......... .......... .......... .......... .......... 91% 61.7M 3s
486000K .......... .......... .......... .......... .......... 91% 32.9M 3s
486050K .......... .......... .......... .......... .......... 91% 45.0M 3s
486100K .......... .......... .......... .......... .......... 91% 34.7M 3s
486150K .......... .......... .......... .......... .......... 91% 144M 3s
486200K .......... .......... .......... .......... .......... 91% 11.9M 3s
486250K .......... .......... .......... .......... .......... 91% 103M 3s
486300K .......... .......... .......... .......... .......... 91% 111M 3s
486350K .......... .......... .......... .......... .......... 91% 6.19M 3s
486400K .......... .......... .......... .......... .......... 91% 42.7M 3s
486450K .......... .......... .......... .......... .......... 91% 30.2M 3s
486500K .......... .......... .......... .......... .......... 91% 3.68M 3s
486550K .......... .......... .......... .......... .......... 91% 41.5M 3s
486600K .......... .......... .......... .......... .......... 91% 36.8M 3s
486650K .......... .......... .......... .......... .......... 91% 40.1M 3s
486700K .......... .......... .......... .......... .......... 91% 6.71M 3s
486750K .......... .......... .......... .......... .......... 91% 90.4M 3s
486800K .......... .......... .......... .......... .......... 91% 37.3M 3s
486850K .......... .......... .......... .......... .......... 91% 7.44M 3s
486900K .......... .......... .......... .......... .......... 91% 43.6M 3s
486950K .......... .......... .......... .......... .......... 91% 20.2M 3s
487000K .......... .......... .......... .......... .......... 91% 6.31M 3s
487050K .......... .......... .......... .......... .......... 91% 131M 3s
487100K .......... .......... .......... .......... .......... 91% 34.5M 3s
487150K .......... .......... .......... .......... .......... 91% 21.5M 3s
487200K .......... .......... .......... .......... .......... 91% 6.87M 3s
487250K .......... .......... .......... .......... .......... 91% 213M 3s
487300K .......... .......... .......... .......... .......... 91% 75.5M 3s
487350K .......... .......... .......... .......... .......... 91% 7.43M 3s
487400K .......... .......... .......... .......... .......... 91% 24.5M 3s
487450K .......... .......... .......... .......... .......... 91% 38.8M 3s
487500K .......... .......... .......... .......... .......... 91% 6.77M 3s
487550K .......... .......... .......... .......... .......... 91% 75.7M 3s
487600K .......... .......... .......... .......... .......... 91% 60.9M 3s
487650K .......... .......... .......... .......... .......... 91% 35.7M 3s
487700K .......... .......... .......... .......... .......... 91% 5.15M 3s
487750K .......... .......... .......... .......... .......... 91% 16.4M 3s
487800K .......... .......... .......... .......... .......... 91% 90.1M 3s
487850K .......... .......... .......... .......... .......... 91% 6.18M 3s
487900K .......... .......... .......... .......... .......... 91% 113M 3s
487950K .......... .......... .......... .......... .......... 91% 55.6M 3s
488000K .......... .......... .......... .......... .......... 91% 5.22M 3s
488050K .......... .......... .......... .......... .......... 91% 191M 3s
488100K .......... .......... .......... .......... .......... 91% 70.4M 3s
488150K .......... .......... .......... .......... .......... 91% 89.9M 3s
488200K .......... .......... .......... .......... .......... 91% 5.71M 3s
488250K .......... .......... .......... .......... .......... 91% 94.8M 3s
488300K .......... .......... .......... .......... .......... 91% 196M 3s
488350K .......... .......... .......... .......... .......... 91% 6.85M 3s
488400K .......... .......... .......... .......... .......... 91% 58.4M 3s
488450K .......... .......... .......... .......... .......... 91% 129M 3s
488500K .......... .......... .......... .......... .......... 91% 4.38M 3s
488550K .......... .......... .......... .......... .......... 91% 182M 3s
488600K .......... .......... .......... .......... .......... 91% 194M 3s
488650K .......... .......... .......... .......... .......... 91% 208M 3s
488700K .......... .......... .......... .......... .......... 91% 5.45M 3s
488750K .......... .......... .......... .......... .......... 91% 198M 3s
488800K .......... .......... .......... .......... .......... 91% 208M 3s
488850K .......... .......... .......... .......... .......... 91% 6.67M 3s
488900K .......... .......... .......... .......... .......... 91% 131M 3s
488950K .......... .......... .......... .......... .......... 91% 66.8M 3s
489000K .......... .......... .......... .......... .......... 91% 103M 3s
489050K .......... .......... .......... .......... .......... 91% 5.73M 3s
489100K .......... .......... .......... .......... .......... 91% 81.8M 3s
489150K .......... .......... .......... .......... .......... 91% 212M 3s
489200K .......... .......... .......... .......... .......... 91% 5.82M 3s
489250K .......... .......... .......... .......... .......... 91% 39.0M 3s
489300K .......... .......... .......... .......... .......... 91% 81.1M 3s
489350K .......... .......... .......... .......... .......... 91% 24.1M 3s
489400K .......... .......... .......... .......... .......... 91% 6.34M 3s
489450K .......... .......... .......... .......... .......... 91% 128M 3s
489500K .......... .......... .......... .......... .......... 91% 36.1M 3s
489550K .......... .......... .......... .......... .......... 91% 6.44M 3s
489600K .......... .......... .......... .......... .......... 91% 71.6M 3s
489650K .......... .......... .......... .......... .......... 91% 83.6M 3s
489700K .......... .......... .......... .......... .......... 91% 40.6M 3s
489750K .......... .......... .......... .......... .......... 91% 6.39M 3s
489800K .......... .......... .......... .......... .......... 91% 50.4M 3s
489850K .......... .......... .......... .......... .......... 91% 38.2M 3s
489900K .......... .......... .......... .......... .......... 91% 6.23M 3s
489950K .......... .......... .......... .......... .......... 91% 89.4M 3s
490000K .......... .......... .......... .......... .......... 91% 73.5M 3s
490050K .......... .......... .......... .......... .......... 91% 18.1M 3s
490100K .......... .......... .......... .......... .......... 91% 6.37M 3s
490150K .......... .......... .......... .......... .......... 91% 35.8M 3s
490200K .......... .......... .......... .......... .......... 91% 24.4M 3s
490250K .......... .......... .......... .......... .......... 91% 5.89M 3s
490300K .......... .......... .......... .......... .......... 91% 104M 3s
490350K .......... .......... .......... .......... .......... 91% 35.5M 3s
490400K .......... .......... .......... .......... .......... 91% 61.0M 3s
490450K .......... .......... .......... .......... .......... 91% 5.65M 3s
490500K .......... .......... .......... .......... .......... 92% 104M 3s
490550K .......... .......... .......... .......... .......... 92% 49.6M 3s
490600K .......... .......... .......... .......... .......... 92% 6.65M 3s
490650K .......... .......... .......... .......... .......... 92% 52.2M 3s
490700K .......... .......... .......... .......... .......... 92% 43.1M 3s
490750K .......... .......... .......... .......... .......... 92% 85.8M 3s
490800K .......... .......... .......... .......... .......... 92% 6.32M 3s
490850K .......... .......... .......... .......... .......... 92% 99.2M 3s
490900K .......... .......... .......... .......... .......... 92% 186M 3s
490950K .......... .......... .......... .......... .......... 92% 147M 3s
491000K .......... .......... .......... .......... .......... 92% 6.31M 3s
491050K .......... .......... .......... .......... .......... 92% 86.6M 3s
491100K .......... .......... .......... .......... .......... 92% 88.8M 3s
491150K .......... .......... .......... .......... .......... 92% 7.23M 3s
491200K .......... .......... .......... .......... .......... 92% 143M 3s
491250K .......... .......... .......... .......... .......... 92% 200M 3s
491300K .......... .......... .......... .......... .......... 92% 186M 3s
491350K .......... .......... .......... .......... .......... 92% 6.73M 3s
491400K .......... .......... .......... .......... .......... 92% 63.7M 3s
491450K .......... .......... .......... .......... .......... 92% 97.7M 3s
491500K .......... .......... .......... .......... .......... 92% 62.5M 3s
491550K .......... .......... .......... .......... .......... 92% 7.34M 3s
491600K .......... .......... .......... .......... .......... 92% 93.5M 3s
491650K .......... .......... .......... .......... .......... 92% 127M 3s
491700K .......... .......... .......... .......... .......... 92% 6.66M 3s
491750K .......... .......... .......... .......... .......... 92% 47.4M 3s
491800K .......... .......... .......... .......... .......... 92% 75.5M 3s
491850K .......... .......... .......... .......... .......... 92% 3.57M 3s
491900K .......... .......... .......... .......... .......... 92% 2.47M 3s
491950K .......... .......... .......... .......... .......... 92% 62.7M 3s
492000K .......... .......... .......... .......... .......... 92% 43.5M 3s
492050K .......... .......... .......... .......... .......... 92% 63.2M 3s
492100K .......... .......... .......... .......... .......... 92% 5.81M 3s
492150K .......... .......... .......... .......... .......... 92% 66.3M 3s
492200K .......... .......... .......... .......... .......... 92% 28.6M 3s
492250K .......... .......... .......... .......... .......... 92% 5.83M 3s
492300K .......... .......... .......... .......... .......... 92% 10.5M 3s
492350K .......... .......... .......... .......... .......... 92% 15.2M 3s
492400K .......... .......... .......... .......... .......... 92% 43.6M 3s
492450K .......... .......... .......... .......... .......... 92% 5.51M 3s
492500K .......... .......... .......... .......... .......... 92% 15.2M 3s
492550K .......... .......... .......... .......... .......... 92% 97.1M 3s
492600K .......... .......... .......... .......... .......... 92% 59.3M 3s
492650K .......... .......... .......... .......... .......... 92% 5.75M 3s
492700K .......... .......... .......... .......... .......... 92% 46.2M 3s
492750K .......... .......... .......... .......... .......... 92% 59.3M 3s
492800K .......... .......... .......... .......... .......... 92% 51.2M 3s
492850K .......... .......... .......... .......... .......... 92% 5.93M 3s
492900K .......... .......... .......... .......... .......... 92% 53.7M 3s
492950K .......... .......... .......... .......... .......... 92% 52.6M 3s
493000K .......... .......... .......... .......... .......... 92% 6.00M 3s
493050K .......... .......... .......... .......... .......... 92% 60.7M 3s
493100K .......... .......... .......... .......... .......... 92% 47.0M 3s
493150K .......... .......... .......... .......... .......... 92% 23.8M 3s
493200K .......... .......... .......... .......... .......... 92% 6.12M 3s
493250K .......... .......... .......... .......... .......... 92% 105M 3s
493300K .......... .......... .......... .......... .......... 92% 104M 3s
493350K .......... .......... .......... .......... .......... 92% 105M 3s
493400K .......... .......... .......... .......... .......... 92% 5.81M 3s
493450K .......... .......... .......... .......... .......... 92% 119M 3s
493500K .......... .......... .......... .......... .......... 92% 103M 3s
493550K .......... .......... .......... .......... .......... 92% 119M 3s
493600K .......... .......... .......... .......... .......... 92% 462K 3s
493650K .......... .......... .......... .......... .......... 92% 135M 3s
493700K .......... .......... .......... .......... .......... 92% 94.6M 3s
493750K .......... .......... .......... .......... .......... 92% 48.4M 3s
493800K .......... .......... .......... .......... .......... 92% 5.98M 3s
493850K .......... .......... .......... .......... .......... 92% 82.1M 3s
493900K .......... .......... .......... .......... .......... 92% 130M 3s
493950K .......... .......... .......... .......... .......... 92% 95.7M 3s
494000K .......... .......... .......... .......... .......... 92% 9.30M 3s
494050K .......... .......... .......... .......... .......... 92% 210M 3s
494100K .......... .......... .......... .......... .......... 92% 53.6M 3s
494150K .......... .......... .......... .......... .......... 92% 67.5M 3s
494200K .......... .......... .......... .......... .......... 92% 6.14M 3s
494250K .......... .......... .......... .......... .......... 92% 107M 3s
494300K .......... .......... .......... .......... .......... 92% 100M 3s
494350K .......... .......... .......... .......... .......... 92% 74.4M 3s
494400K .......... .......... .......... .......... .......... 92% 5.30M 3s
494450K .......... .......... .......... .......... .......... 92% 96.1M 3s
494500K .......... .......... .......... .......... .......... 92% 138M 3s
494550K .......... .......... .......... .......... .......... 92% 77.5M 3s
494600K .......... .......... .......... .......... .......... 92% 6.31M 3s
494650K .......... .......... .......... .......... .......... 92% 77.8M 3s
494700K .......... .......... .......... .......... .......... 92% 70.9M 3s
494750K .......... .......... .......... .......... .......... 92% 6.43M 3s
494800K .......... .......... .......... .......... .......... 92% 178M 3s
494850K .......... .......... .......... .......... .......... 92% 180M 3s
494900K .......... .......... .......... .......... .......... 92% 173M 3s
494950K .......... .......... .......... .......... .......... 92% 5.84M 3s
495000K .......... .......... .......... .......... .......... 92% 44.2M 3s
495050K .......... .......... .......... .......... .......... 92% 206M 3s
495100K .......... .......... .......... .......... .......... 92% 158M 3s
495150K .......... .......... .......... .......... .......... 92% 6.62M 3s
495200K .......... .......... .......... .......... .......... 92% 77.5M 3s
495250K .......... .......... .......... .......... .......... 92% 137M 3s
495300K .......... .......... .......... .......... .......... 92% 203M 3s
495350K .......... .......... .......... .......... .......... 92% 3.96M 3s
495400K .......... .......... .......... .......... .......... 92% 139M 3s
495450K .......... .......... .......... .......... .......... 92% 82.9M 3s
495500K .......... .......... .......... .......... .......... 92% 108M 3s
495550K .......... .......... .......... .......... .......... 92% 6.52M 3s
495600K .......... .......... .......... .......... .......... 92% 65.6M 3s
495650K .......... .......... .......... .......... .......... 92% 66.0M 3s
495700K .......... .......... .......... .......... .......... 92% 23.0M 3s
495750K .......... .......... .......... .......... .......... 92% 5.96M 3s
495800K .......... .......... .......... .......... .......... 93% 202M 3s
495850K .......... .......... .......... .......... .......... 93% 36.5M 3s
495900K .......... .......... .......... .......... .......... 93% 120M 3s
495950K .......... .......... .......... .......... .......... 93% 6.54M 3s
496000K .......... .......... .......... .......... .......... 93% 47.7M 3s
496050K .......... .......... .......... .......... .......... 93% 194M 3s
496100K .......... .......... .......... .......... .......... 93% 185M 3s
496150K .......... .......... .......... .......... .......... 93% 7.08M 3s
496200K .......... .......... .......... .......... .......... 93% 109M 3s
496250K .......... .......... .......... .......... .......... 93% 117M 3s
496300K .......... .......... .......... .......... .......... 93% 95.9M 3s
496350K .......... .......... .......... .......... .......... 93% 7.02M 3s
496400K .......... .......... .......... .......... .......... 93% 202M 3s
496450K .......... .......... .......... .......... .......... 93% 108M 3s
496500K .......... .......... .......... .......... .......... 93% 108M 3s
496550K .......... .......... .......... .......... .......... 93% 6.84M 3s
496600K .......... .......... .......... .......... .......... 93% 60.7M 3s
496650K .......... .......... .......... .......... .......... 93% 1.31M 3s
496700K .......... .......... .......... .......... .......... 93% 90.9M 3s
496750K .......... .......... .......... .......... .......... 93% 190M 3s
496800K .......... .......... .......... .......... .......... 93% 6.10M 3s
496850K .......... .......... .......... .......... .......... 93% 207M 3s
496900K .......... .......... .......... .......... .......... 93% 215M 3s
496950K .......... .......... .......... .......... .......... 93% 213M 3s
497000K .......... .......... .......... .......... .......... 93% 6.84M 3s
497050K .......... .......... .......... .......... .......... 93% 192M 3s
497100K .......... .......... .......... .......... .......... 93% 144M 3s
497150K .......... .......... .......... .......... .......... 93% 105M 3s
497200K .......... .......... .......... .......... .......... 93% 5.01M 3s
497250K .......... .......... .......... .......... .......... 93% 230M 3s
497300K .......... .......... .......... .......... .......... 93% 197M 3s
497350K .......... .......... .......... .......... .......... 93% 206M 3s
497400K .......... .......... .......... .......... .......... 93% 6.95M 3s
497450K .......... .......... .......... .......... .......... 93% 208M 3s
497500K .......... .......... .......... .......... .......... 93% 241M 3s
497550K .......... .......... .......... .......... .......... 93% 243M 3s
497600K .......... .......... .......... .......... .......... 93% 5.88M 3s
497650K .......... .......... .......... .......... .......... 93% 291M 3s
497700K .......... .......... .......... .......... .......... 93% 162M 3s
497750K .......... .......... .......... .......... .......... 93% 305M 3s
497800K .......... .......... .......... .......... .......... 93% 5.49M 3s
497850K .......... .......... .......... .......... .......... 93% 123M 3s
497900K .......... .......... .......... .......... .......... 93% 215M 3s
497950K .......... .......... .......... .......... .......... 93% 110M 3s
498000K .......... .......... .......... .......... .......... 93% 7.66M 3s
498050K .......... .......... .......... .......... .......... 93% 169M 3s
498100K .......... .......... .......... .......... .......... 93% 75.7M 3s
498150K .......... .......... .......... .......... .......... 93% 162M 3s
498200K .......... .......... .......... .......... .......... 93% 6.56M 3s
498250K .......... .......... .......... .......... .......... 93% 182M 3s
498300K .......... .......... .......... .......... .......... 93% 164M 3s
498350K .......... .......... .......... .......... .......... 93% 118M 3s
498400K .......... .......... .......... .......... .......... 93% 106M 3s
498450K .......... .......... .......... .......... .......... 93% 5.96M 3s
498500K .......... .......... .......... .......... .......... 93% 98.4M 3s
498550K .......... .......... .......... .......... .......... 93% 129M 3s
498600K .......... .......... .......... .......... .......... 93% 116M 3s
498650K .......... .......... .......... .......... .......... 93% 5.65M 3s
498700K .......... .......... .......... .......... .......... 93% 46.0M 3s
498750K .......... .......... .......... .......... .......... 93% 37.8M 3s
498800K .......... .......... .......... .......... .......... 93% 161M 3s
498850K .......... .......... .......... .......... .......... 93% 5.90M 3s
498900K .......... .......... .......... .......... .......... 93% 136M 3s
498950K .......... .......... .......... .......... .......... 93% 67.1M 3s
499000K .......... .......... .......... .......... .......... 93% 35.2M 3s
499050K .......... .......... .......... .......... .......... 93% 4.89M 3s
499100K .......... .......... .......... .......... .......... 93% 116M 3s
499150K .......... .......... .......... .......... .......... 93% 186M 3s
499200K .......... .......... .......... .......... .......... 93% 124M 2s
499250K .......... .......... .......... .......... .......... 93% 203M 2s
499300K .......... .......... .......... .......... .......... 93% 6.59M 2s
499350K .......... .......... .......... .......... .......... 93% 146M 2s
499400K .......... .......... .......... .......... .......... 93% 110M 2s
499450K .......... .......... .......... .......... .......... 93% 171M 2s
499500K .......... .......... .......... .......... .......... 93% 6.94M 2s
499550K .......... .......... .......... .......... .......... 93% 209M 2s
499600K .......... .......... .......... .......... .......... 93% 185M 2s
499650K .......... .......... .......... .......... .......... 93% 233M 2s
499700K .......... .......... .......... .......... .......... 93% 6.01M 2s
499750K .......... .......... .......... .......... .......... 93% 89.1M 2s
499800K .......... .......... .......... .......... .......... 93% 97.9M 2s
499850K .......... .......... .......... .......... .......... 93% 150M 2s
499900K .......... .......... .......... .......... .......... 93% 6.77M 2s
499950K .......... .......... .......... .......... .......... 93% 142M 2s
500000K .......... .......... .......... .......... .......... 93% 116M 2s
500050K .......... .......... .......... .......... .......... 93% 155M 2s
500100K .......... .......... .......... .......... .......... 93% 104M 2s
500150K .......... .......... .......... .......... .......... 93% 6.00M 2s
500200K .......... .......... .......... .......... .......... 93% 197M 2s
500250K .......... .......... .......... .......... .......... 93% 101M 2s
500300K .......... .......... .......... .......... .......... 93% 126M 2s
500350K .......... .......... .......... .......... .......... 93% 6.53M 2s
500400K .......... .......... .......... .......... .......... 93% 92.3M 2s
500450K .......... .......... .......... .......... .......... 93% 139M 2s
500500K .......... .......... .......... .......... .......... 93% 104M 2s
500550K .......... .......... .......... .......... .......... 93% 6.68M 2s
500600K .......... .......... .......... .......... .......... 93% 109M 2s
500650K .......... .......... .......... .......... .......... 93% 135M 2s
500700K .......... .......... .......... .......... .......... 93% 81.9M 2s
500750K .......... .......... .......... .......... .......... 93% 2.08M 2s
500800K .......... .......... .......... .......... .......... 93% 4.71M 2s
500850K .......... .......... .......... .......... .......... 93% 92.7M 2s
500900K .......... .......... .......... .......... .......... 93% 91.4M 2s
500950K .......... .......... .......... .......... .......... 93% 76.3M 2s
501000K .......... .......... .......... .......... .......... 93% 6.02M 2s
501050K .......... .......... .......... .......... .......... 93% 111M 2s
501100K .......... .......... .......... .......... .......... 93% 183M 2s
501150K .......... .......... .......... .......... .......... 94% 207M 2s
501200K .......... .......... .......... .......... .......... 94% 6.94M 2s
501250K .......... .......... .......... .......... .......... 94% 252M 2s
501300K .......... .......... .......... .......... .......... 94% 212M 2s
501350K .......... .......... .......... .......... .......... 94% 174M 2s
501400K .......... .......... .......... .......... .......... 94% 191M 2s
501450K .......... .......... .......... .......... .......... 94% 6.96M 2s
501500K .......... .......... .......... .......... .......... 94% 207M 2s
501550K .......... .......... .......... .......... .......... 94% 218M 2s
501600K .......... .......... .......... .......... .......... 94% 182M 2s
501650K .......... .......... .......... .......... .......... 94% 5.87M 2s
501700K .......... .......... .......... .......... .......... 94% 129M 2s
501750K .......... .......... .......... .......... .......... 94% 117M 2s
501800K .......... .......... .......... .......... .......... 94% 106M 2s
501850K .......... .......... .......... .......... .......... 94% 52.3M 2s
501900K .......... .......... .......... .......... .......... 94% 5.35M 2s
501950K .......... .......... .......... .......... .......... 94% 116M 2s
502000K .......... .......... .......... .......... .......... 94% 151M 2s
502050K .......... .......... .......... .......... .......... 94% 110M 2s
502100K .......... .......... .......... .......... .......... 94% 5.33M 2s
502150K .......... .......... .......... .......... .......... 94% 134M 2s
502200K .......... .......... .......... .......... .......... 94% 129M 2s
502250K .......... .......... .......... .......... .......... 94% 114M 2s
502300K .......... .......... .......... .......... .......... 94% 164M 2s
502350K .......... .......... .......... .......... .......... 94% 7.07M 2s
502400K .......... .......... .......... .......... .......... 94% 201M 2s
502450K .......... .......... .......... .......... .......... 94% 86.9M 2s
502500K .......... .......... .......... .......... .......... 94% 72.3M 2s
502550K .......... .......... .......... .......... .......... 94% 6.64M 2s
502600K .......... .......... .......... .......... .......... 94% 179M 2s
502650K .......... .......... .......... .......... .......... 94% 222M 2s
502700K .......... .......... .......... .......... .......... 94% 127M 2s
502750K .......... .......... .......... .......... .......... 94% 177M 2s
502800K .......... .......... .......... .......... .......... 94% 5.91M 2s
502850K .......... .......... .......... .......... .......... 94% 74.5M 2s
502900K .......... .......... .......... .......... .......... 94% 70.7M 2s
502950K .......... .......... .......... .......... .......... 94% 59.5M 2s
503000K .......... .......... .......... .......... .......... 94% 5.92M 2s
503050K .......... .......... .......... .......... .......... 94% 158M 2s
503100K .......... .......... .......... .......... .......... 94% 124M 2s
503150K .......... .......... .......... .......... .......... 94% 167M 2s
503200K .......... .......... .......... .......... .......... 94% 142M 2s
503250K .......... .......... .......... .......... .......... 94% 4.85M 2s
503300K .......... .......... .......... .......... .......... 94% 198M 2s
503350K .......... .......... .......... .......... .......... 94% 151M 2s
503400K .......... .......... .......... .......... .......... 94% 158M 2s
503450K .......... .......... .......... .......... .......... 94% 4.07M 2s
503500K .......... .......... .......... .......... .......... 94% 120M 2s
503550K .......... .......... .......... .......... .......... 94% 141M 2s
503600K .......... .......... .......... .......... .......... 94% 162M 2s
503650K .......... .......... .......... .......... .......... 94% 162M 2s
503700K .......... .......... .......... .......... .......... 94% 3.85M 2s
503750K .......... .......... .......... .......... .......... 94% 184M 2s
503800K .......... .......... .......... .......... .......... 94% 140M 2s
503850K .......... .......... .......... .......... .......... 94% 75.7M 2s
503900K .......... .......... .......... .......... .......... 94% 4.65M 2s
503950K .......... .......... .......... .......... .......... 94% 109M 2s
504000K .......... .......... .......... .......... .......... 94% 129M 2s
504050K .......... .......... .......... .......... .......... 94% 132M 2s
504100K .......... .......... .......... .......... .......... 94% 77.5M 2s
504150K .......... .......... .......... .......... .......... 94% 5.35M 2s
504200K .......... .......... .......... .......... .......... 94% 67.5M 2s
504250K .......... .......... .......... .......... .......... 94% 139M 2s
504300K .......... .......... .......... .......... .......... 94% 108M 2s
504350K .......... .......... .......... .......... .......... 94% 6.12M 2s
504400K .......... .......... .......... .......... .......... 94% 92.1M 2s
504450K .......... .......... .......... .......... .......... 94% 144M 2s
504500K .......... .......... .......... .......... .......... 94% 64.4M 2s
504550K .......... .......... .......... .......... .......... 94% 133M 2s
504600K .......... .......... .......... .......... .......... 94% 5.71M 2s
504650K .......... .......... .......... .......... .......... 94% 201M 2s
504700K .......... .......... .......... .......... .......... 94% 56.1M 2s
504750K .......... .......... .......... .......... .......... 94% 78.8M 2s
504800K .......... .......... .......... .......... .......... 94% 45.6M 2s
504850K .......... .......... .......... .......... .......... 94% 1.13M 2s
504900K .......... .......... .......... .......... .......... 94% 200M 2s
504950K .......... .......... .......... .......... .......... 94% 37.5M 2s
505000K .......... .......... .......... .......... .......... 94% 167M 2s
505050K .......... .......... .......... .......... .......... 94% 5.20M 2s
505100K .......... .......... .......... .......... .......... 94% 150M 2s
505150K .......... .......... .......... .......... .......... 94% 176M 2s
505200K .......... .......... .......... .......... .......... 94% 210M 2s
505250K .......... .......... .......... .......... .......... 94% 162M 2s
505300K .......... .......... .......... .......... .......... 94% 4.49M 2s
505350K .......... .......... .......... .......... .......... 94% 184M 2s
505400K .......... .......... .......... .......... .......... 94% 138M 2s
505450K .......... .......... .......... .......... .......... 94% 169M 2s
505500K .......... .......... .......... .......... .......... 94% 163M 2s
505550K .......... .......... .......... .......... .......... 94% 4.95M 2s
505600K .......... .......... .......... .......... .......... 94% 171M 2s
505650K .......... .......... .......... .......... .......... 94% 166M 2s
505700K .......... .......... .......... .......... .......... 94% 189M 2s
505750K .......... .......... .......... .......... .......... 94% 5.34M 2s
505800K .......... .......... .......... .......... .......... 94% 112M 2s
505850K .......... .......... .......... .......... .......... 94% 99.0M 2s
505900K .......... .......... .......... .......... .......... 94% 6.30M 2s
505950K .......... .......... .......... .......... .......... 94% 152M 2s
506000K .......... .......... .......... .......... .......... 94% 126M 2s
506050K .......... .......... .......... .......... .......... 94% 135M 2s
506100K .......... .......... .......... .......... .......... 94% 100M 2s
506150K .......... .......... .......... .......... .......... 94% 155M 2s
506200K .......... .......... .......... .......... .......... 94% 135M 2s
506250K .......... .......... .......... .......... .......... 94% 5.49M 2s
506300K .......... .......... .......... .......... .......... 94% 130M 2s
506350K .......... .......... .......... .......... .......... 94% 90.4M 2s
506400K .......... .......... .......... .......... .......... 94% 142M 2s
506450K .......... .......... .......... .......... .......... 94% 93.7M 2s
506500K .......... .......... .......... .......... .......... 95% 6.75M 2s
506550K .......... .......... .......... .......... .......... 95% 5.92M 2s
506600K .......... .......... .......... .......... .......... 95% 34.4M 2s
506650K .......... .......... .......... .......... .......... 95% 92.8M 2s
506700K .......... .......... .......... .......... .......... 95% 104M 2s
506750K .......... .......... .......... .......... .......... 95% 131M 2s
506800K .......... .......... .......... .......... .......... 95% 92.8M 2s
506850K .......... .......... .......... .......... .......... 95% 109M 2s
506900K .......... .......... .......... .......... .......... 95% 78.4M 2s
506950K .......... .......... .......... .......... .......... 95% 12.5M 2s
507000K .......... .......... .......... .......... .......... 95% 168M 2s
507050K .......... .......... .......... .......... .......... 95% 137M 2s
507100K .......... .......... .......... .......... .......... 95% 102M 2s
507150K .......... .......... .......... .......... .......... 95% 54.7M 2s
507200K .......... .......... .......... .......... .......... 95% 5.23M 2s
507250K .......... .......... .......... .......... .......... 95% 66.9M 2s
507300K .......... .......... .......... .......... .......... 95% 76.5M 2s
507350K .......... .......... .......... .......... .......... 95% 64.2M 2s
507400K .......... .......... .......... .......... .......... 95% 101M 2s
507450K .......... .......... .......... .......... .......... 95% 7.85M 2s
507500K .......... .......... .......... .......... .......... 95% 76.8M 2s
507550K .......... .......... .......... .......... .......... 95% 109M 2s
507600K .......... .......... .......... .......... .......... 95% 65.5M 2s
507650K .......... .......... .......... .......... .......... 95% 4.94M 2s
507700K .......... .......... .......... .......... .......... 95% 77.5M 2s
507750K .......... .......... .......... .......... .......... 95% 69.9M 2s
507800K .......... .......... .......... .......... .......... 95% 113M 2s
507850K .......... .......... .......... .......... .......... 95% 99.0M 2s
507900K .......... .......... .......... .......... .......... 95% 6.39M 2s
507950K .......... .......... .......... .......... .......... 95% 2.88M 2s
508000K .......... .......... .......... .......... .......... 95% 7.13M 2s
508050K .......... .......... .......... .......... .......... 95% 62.0M 2s
508100K .......... .......... .......... .......... .......... 95% 86.6M 2s
508150K .......... .......... .......... .......... .......... 95% 95.4M 2s
508200K .......... .......... .......... .......... .......... 95% 15.9M 2s
508250K .......... .......... .......... .......... .......... 95% 176M 2s
508300K .......... .......... .......... .......... .......... 95% 211M 2s
508350K .......... .......... .......... .......... .......... 95% 72.7M 2s
508400K .......... .......... .......... .......... .......... 95% 99.2M 2s
508450K .......... .......... .......... .......... .......... 95% 178M 2s
508500K .......... .......... .......... .......... .......... 95% 205M 2s
508550K .......... .......... .......... .......... .......... 95% 161M 2s
508600K .......... .......... .......... .......... .......... 95% 111M 2s
508650K .......... .......... .......... .......... .......... 95% 178M 2s
508700K .......... .......... .......... .......... .......... 95% 139M 2s
508750K .......... .......... .......... .......... .......... 95% 142M 2s
508800K .......... .......... .......... .......... .......... 95% 106M 2s
508850K .......... .......... .......... .......... .......... 95% 133M 2s
508900K .......... .......... .......... .......... .......... 95% 30.3M 2s
508950K .......... .......... .......... .......... .......... 95% 11.6M 2s
509000K .......... .......... .......... .......... .......... 95% 76.1M 2s
509050K .......... .......... .......... .......... .......... 95% 177M 2s
509100K .......... .......... .......... .......... .......... 95% 4.69M 2s
509150K .......... .......... .......... .......... .......... 95% 115M 2s
509200K .......... .......... .......... .......... .......... 95% 89.1M 2s
509250K .......... .......... .......... .......... .......... 95% 188M 2s
509300K .......... .......... .......... .......... .......... 95% 166M 2s
509350K .......... .......... .......... .......... .......... 95% 6.82M 2s
509400K .......... .......... .......... .......... .......... 95% 183M 2s
509450K .......... .......... .......... .......... .......... 95% 133M 2s
509500K .......... .......... .......... .......... .......... 95% 192M 2s
509550K .......... .......... .......... .......... .......... 95% 87.2M 2s
509600K .......... .......... .......... .......... .......... 95% 4.99M 2s
509650K .......... .......... .......... .......... .......... 95% 187M 2s
509700K .......... .......... .......... .......... .......... 95% 140M 2s
509750K .......... .......... .......... .......... .......... 95% 186M 2s
509800K .......... .......... .......... .......... .......... 95% 189M 2s
509850K .......... .......... .......... .......... .......... 95% 6.06M 2s
509900K .......... .......... .......... .......... .......... 95% 146M 2s
509950K .......... .......... .......... .......... .......... 95% 87.5M 2s
510000K .......... .......... .......... .......... .......... 95% 4.62M 2s
510050K .......... .......... .......... .......... .......... 95% 199M 2s
510100K .......... .......... .......... .......... .......... 95% 90.6M 2s
510150K .......... .......... .......... .......... .......... 95% 142M 2s
510200K .......... .......... .......... .......... .......... 95% 187M 2s
510250K .......... .......... .......... .......... .......... 95% 7.52M 2s
510300K .......... .......... .......... .......... .......... 95% 37.4M 2s
510350K .......... .......... .......... .......... .......... 95% 109M 2s
510400K .......... .......... .......... .......... .......... 95% 195M 2s
510450K .......... .......... .......... .......... .......... 95% 129M 2s
510500K .......... .......... .......... .......... .......... 95% 214M 2s
510550K .......... .......... .......... .......... .......... 95% 137M 2s
510600K .......... .......... .......... .......... .......... 95% 8.15M 2s
510650K .......... .......... .......... .......... .......... 95% 99.9M 2s
510700K .......... .......... .......... .......... .......... 95% 92.0M 2s
510750K .......... .......... .......... .......... .......... 95% 96.5M 2s
510800K .......... .......... .......... .......... .......... 95% 7.07M 2s
510850K .......... .......... .......... .......... .......... 95% 79.0M 2s
510900K .......... .......... .......... .......... .......... 95% 137M 2s
510950K .......... .......... .......... .......... .......... 95% 120M 2s
511000K .......... .......... .......... .......... .......... 95% 60.7M 2s
511050K .......... .......... .......... .......... .......... 95% 7.53M 2s
511100K .......... .......... .......... .......... .......... 95% 54.5M 2s
511150K .......... .......... .......... .......... .......... 95% 70.8M 2s
511200K .......... .......... .......... .......... .......... 95% 47.7M 2s
511250K .......... .......... .......... .......... .......... 95% 77.9M 2s
511300K .......... .......... .......... .......... .......... 95% 4.75M 2s
511350K .......... .......... .......... .......... .......... 95% 64.8M 2s
511400K .......... .......... .......... .......... .......... 95% 132M 2s
511450K .......... .......... .......... .......... .......... 95% 189M 2s
511500K .......... .......... .......... .......... .......... 95% 178M 2s
511550K .......... .......... .......... .......... .......... 95% 6.89M 2s
511600K .......... .......... .......... .......... .......... 95% 155M 2s
511650K .......... .......... .......... .......... .......... 95% 161M 2s
511700K .......... .......... .......... .......... .......... 95% 108M 2s
511750K .......... .......... .......... .......... .......... 95% 159M 2s
511800K .......... .......... .......... .......... .......... 96% 5.58M 2s
511850K .......... .......... .......... .......... .......... 96% 195M 2s
511900K .......... .......... .......... .......... .......... 96% 176M 2s
511950K .......... .......... .......... .......... .......... 96% 137M 2s
512000K .......... .......... .......... .......... .......... 96% 164M 2s
512050K .......... .......... .......... .......... .......... 96% 7.62M 2s
512100K .......... .......... .......... .......... .......... 96% 147M 2s
512150K .......... .......... .......... .......... .......... 96% 194M 2s
512200K .......... .......... .......... .......... .......... 96% 112M 2s
512250K .......... .......... .......... .......... .......... 96% 212M 2s
512300K .......... .......... .......... .......... .......... 96% 4.75M 2s
512350K .......... .......... .......... .......... .......... 96% 98.4M 2s
512400K .......... .......... .......... .......... .......... 96% 105M 2s
512450K .......... .......... .......... .......... .......... 96% 98.4M 2s
512500K .......... .......... .......... .......... .......... 96% 221M 2s
512550K .......... .......... .......... .......... .......... 96% 9.30M 2s
512600K .......... .......... .......... .......... .......... 96% 59.9M 1s
512650K .......... .......... .......... .......... .......... 96% 106M 1s
512700K .......... .......... .......... .......... .......... 96% 110M 1s
512750K .......... .......... .......... .......... .......... 96% 148M 1s
512800K .......... .......... .......... .......... .......... 96% 7.35M 1s
512850K .......... .......... .......... .......... .......... 96% 44.9M 1s
512900K .......... .......... .......... .......... .......... 96% 248M 1s
512950K .......... .......... .......... .......... .......... 96% 199M 1s
513000K .......... .......... .......... .......... .......... 96% 153M 1s
513050K .......... .......... .......... .......... .......... 96% 8.15M 1s
513100K .......... .......... .......... .......... .......... 96% 100M 1s
513150K .......... .......... .......... .......... .......... 96% 90.3M 1s
513200K .......... .......... .......... .......... .......... 96% 91.6M 1s
513250K .......... .......... .......... .......... .......... 96% 115M 1s
513300K .......... .......... .......... .......... .......... 96% 4.24M 1s
513350K .......... .......... .......... .......... .......... 96% 110M 1s
513400K .......... .......... .......... .......... .......... 96% 130M 1s
513450K .......... .......... .......... .......... .......... 96% 109M 1s
513500K .......... .......... .......... .......... .......... 96% 109M 1s
513550K .......... .......... .......... .......... .......... 96% 6.53M 1s
513600K .......... .......... .......... .......... .......... 96% 84.6M 1s
513650K .......... .......... .......... .......... .......... 96% 132M 1s
513700K .......... .......... .......... .......... .......... 96% 137M 1s
513750K .......... .......... .......... .......... .......... 96% 184M 1s
513800K .......... .......... .......... .......... .......... 96% 6.40M 1s
513850K .......... .......... .......... .......... .......... 96% 83.0M 1s
513900K .......... .......... .......... .......... .......... 96% 90.8M 1s
513950K .......... .......... .......... .......... .......... 96% 118M 1s
514000K .......... .......... .......... .......... .......... 96% 94.1M 1s
514050K .......... .......... .......... .......... .......... 96% 5.49M 1s
514100K .......... .......... .......... .......... .......... 96% 29.4M 1s
514150K .......... .......... .......... .......... .......... 96% 88.6M 1s
514200K .......... .......... .......... .......... .......... 96% 108M 1s
514250K .......... .......... .......... .......... .......... 96% 149M 1s
514300K .......... .......... .......... .......... .......... 96% 7.05M 1s
514350K .......... .......... .......... .......... .......... 96% 92.5M 1s
514400K .......... .......... .......... .......... .......... 96% 129M 1s
514450K .......... .......... .......... .......... .......... 96% 109M 1s
514500K .......... .......... .......... .......... .......... 96% 85.2M 1s
514550K .......... .......... .......... .......... .......... 96% 4.60M 1s
514600K .......... .......... .......... .......... .......... 96% 137M 1s
514650K .......... .......... .......... .......... .......... 96% 188M 1s
514700K .......... .......... .......... .......... .......... 96% 110M 1s
514750K .......... .......... .......... .......... .......... 96% 234M 1s
514800K .......... .......... .......... .......... .......... 96% 7.78M 1s
514850K .......... .......... .......... .......... .......... 96% 83.2M 1s
514900K .......... .......... .......... .......... .......... 96% 86.0M 1s
514950K .......... .......... .......... .......... .......... 96% 101M 1s
515000K .......... .......... .......... .......... .......... 96% 115M 1s
515050K .......... .......... .......... .......... .......... 96% 95.6M 1s
515100K .......... .......... .......... .......... .......... 96% 1007K 1s
515150K .......... .......... .......... .......... .......... 96% 91.6M 1s
515200K .......... .......... .......... .......... .......... 96% 68.9M 1s
515250K .......... .......... .......... .......... .......... 96% 133M 1s
515300K .......... .......... .......... .......... .......... 96% 132M 1s
515350K .......... .......... .......... .......... .......... 96% 57.4M 1s
515400K .......... .......... .......... .......... .......... 96% 112M 1s
515450K .......... .......... .......... .......... .......... 96% 119M 1s
515500K .......... .......... .......... .......... .......... 96% 109M 1s
515550K .......... .......... .......... .......... .......... 96% 203M 1s
515600K .......... .......... .......... .......... .......... 96% 138M 1s
515650K .......... .......... .......... .......... .......... 96% 130M 1s
515700K .......... .......... .......... .......... .......... 96% 141M 1s
515750K .......... .......... .......... .......... .......... 96% 147M 1s
515800K .......... .......... .......... .......... .......... 96% 134M 1s
515850K .......... .......... .......... .......... .......... 96% 167M 1s
515900K .......... .......... .......... .......... .......... 96% 163M 1s
515950K .......... .......... .......... .......... .......... 96% 125M 1s
516000K .......... .......... .......... .......... .......... 96% 112M 1s
516050K .......... .......... .......... .......... .......... 96% 78.5M 1s
516100K .......... .......... .......... .......... .......... 96% 9.36M 1s
516150K .......... .......... .......... .......... .......... 96% 122M 1s
516200K .......... .......... .......... .......... .......... 96% 105M 1s
516250K .......... .......... .......... .......... .......... 96% 113M 1s
516300K .......... .......... .......... .......... .......... 96% 30.9M 1s
516350K .......... .......... .......... .......... .......... 96% 118M 1s
516400K .......... .......... .......... .......... .......... 96% 161M 1s
516450K .......... .......... .......... .......... .......... 96% 121M 1s
516500K .......... .......... .......... .......... .......... 96% 154M 1s
516550K .......... .......... .......... .......... .......... 96% 154M 1s
516600K .......... .......... .......... .......... .......... 96% 14.8M 1s
516650K .......... .......... .......... .......... .......... 96% 123M 1s
516700K .......... .......... .......... .......... .......... 96% 142M 1s
516750K .......... .......... .......... .......... .......... 96% 132M 1s
516800K .......... .......... .......... .......... .......... 96% 16.2M 1s
516850K .......... .......... .......... .......... .......... 96% 7.22M 1s
516900K .......... .......... .......... .......... .......... 96% 153M 1s
516950K .......... .......... .......... .......... .......... 96% 53.8M 1s
517000K .......... .......... .......... .......... .......... 96% 115M 1s
517050K .......... .......... .......... .......... .......... 96% 26.5M 1s
517100K .......... .......... .......... .......... .......... 96% 4.49M 1s
517150K .......... .......... .......... .......... .......... 97% 12.6M 1s
517200K .......... .......... .......... .......... .......... 97% 57.0M 1s
517250K .......... .......... .......... .......... .......... 97% 144M 1s
517300K .......... .......... .......... .......... .......... 97% 77.1M 1s
517350K .......... .......... .......... .......... .......... 97% 13.7M 1s
517400K .......... .......... .......... .......... .......... 97% 73.8M 1s
517450K .......... .......... .......... .......... .......... 97% 5.14M 1s
517500K .......... .......... .......... .......... .......... 97% 72.7M 1s
517550K .......... .......... .......... .......... .......... 97% 51.2M 1s
517600K .......... .......... .......... .......... .......... 97% 66.4M 1s
517650K .......... .......... .......... .......... .......... 97% 103M 1s
517700K .......... .......... .......... .......... .......... 97% 88.6M 1s
517750K .......... .......... .......... .......... .......... 97% 12.1M 1s
517800K .......... .......... .......... .......... .......... 97% 62.8M 1s
517850K .......... .......... .......... .......... .......... 97% 72.4M 1s
517900K .......... .......... .......... .......... .......... 97% 75.8M 1s
517950K .......... .......... .......... .......... .......... 97% 87.3M 1s
518000K .......... .......... .......... .......... .......... 97% 76.1M 1s
518050K .......... .......... .......... .......... .......... 97% 8.95M 1s
518100K .......... .......... .......... .......... .......... 97% 69.6M 1s
518150K .......... .......... .......... .......... .......... 97% 80.3M 1s
518200K .......... .......... .......... .......... .......... 97% 14.1M 1s
518250K .......... .......... .......... .......... .......... 97% 5.40M 1s
518300K .......... .......... .......... .......... .......... 97% 50.3M 1s
518350K .......... .......... .......... .......... .......... 97% 51.0M 1s
518400K .......... .......... .......... .......... .......... 97% 37.0M 1s
518450K .......... .......... .......... .......... .......... 97% 4.98M 1s
518500K .......... .......... .......... .......... .......... 97% 73.1M 1s
518550K .......... .......... .......... .......... .......... 97% 47.1M 1s
518600K .......... .......... .......... .......... .......... 97% 5.21M 1s
518650K .......... .......... .......... .......... .......... 97% 55.7M 1s
518700K .......... .......... .......... .......... .......... 97% 70.2M 1s
518750K .......... .......... .......... .......... .......... 97% 112M 1s
518800K .......... .......... .......... .......... .......... 97% 6.20M 1s
518850K .......... .......... .......... .......... .......... 97% 89.6M 1s
518900K .......... .......... .......... .......... .......... 97% 130M 1s
518950K .......... .......... .......... .......... .......... 97% 110M 1s
519000K .......... .......... .......... .......... .......... 97% 5.38M 1s
519050K .......... .......... .......... .......... .......... 97% 32.1M 1s
519100K .......... .......... .......... .......... .......... 97% 65.3M 1s
519150K .......... .......... .......... .......... .......... 97% 31.0M 1s
519200K .......... .......... .......... .......... .......... 97% 1.15M 1s
519250K .......... .......... .......... .......... .......... 97% 93.5M 1s
519300K .......... .......... .......... .......... .......... 97% 132M 1s
519350K .......... .......... .......... .......... .......... 97% 52.6M 1s
519400K .......... .......... .......... .......... .......... 97% 6.92M 1s
519450K .......... .......... .......... .......... .......... 97% 41.6M 1s
519500K .......... .......... .......... .......... .......... 97% 87.2M 1s
519550K .......... .......... .......... .......... .......... 97% 29.7M 1s
519600K .......... .......... .......... .......... .......... 97% 5.34M 1s
519650K .......... .......... .......... .......... .......... 97% 64.8M 1s
519700K .......... .......... .......... .......... .......... 97% 68.0M 1s
519750K .......... .......... .......... .......... .......... 97% 7.59M 1s
519800K .......... .......... .......... .......... .......... 97% 105M 1s
519850K .......... .......... .......... .......... .......... 97% 62.9M 1s
519900K .......... .......... .......... .......... .......... 97% 118M 1s
519950K .......... .......... .......... .......... .......... 97% 4.14M 1s
520000K .......... .......... .......... .......... .......... 97% 153M 1s
520050K .......... .......... .......... .......... .......... 97% 176M 1s
520100K .......... .......... .......... .......... .......... 97% 92.5M 1s
520150K .......... .......... .......... .......... .......... 97% 6.68M 1s
520200K .......... .......... .......... .......... .......... 97% 93.5M 1s
520250K .......... .......... .......... .......... .......... 97% 137M 1s
520300K .......... .......... .......... .......... .......... 97% 122M 1s
520350K .......... .......... .......... .......... .......... 97% 7.16M 1s
520400K .......... .......... .......... .......... .......... 97% 198M 1s
520450K .......... .......... .......... .......... .......... 97% 196M 1s
520500K .......... .......... .......... .......... .......... 97% 178M 1s
520550K .......... .......... .......... .......... .......... 97% 6.84M 1s
520600K .......... .......... .......... .......... .......... 97% 135M 1s
520650K .......... .......... .......... .......... .......... 97% 101M 1s
520700K .......... .......... .......... .......... .......... 97% 175M 1s
520750K .......... .......... .......... .......... .......... 97% 5.48M 1s
520800K .......... .......... .......... .......... .......... 97% 194M 1s
520850K .......... .......... .......... .......... .......... 97% 182M 1s
520900K .......... .......... .......... .......... .......... 97% 22.9M 1s
520950K .......... .......... .......... .......... .......... 97% 6.89M 1s
521000K .......... .......... .......... .......... .......... 97% 88.3M 1s
521050K .......... .......... .......... .......... .......... 97% 127M 1s
521100K .......... .......... .......... .......... .......... 97% 79.4M 1s
521150K .......... .......... .......... .......... .......... 97% 4.32M 1s
521200K .......... .......... .......... .......... .......... 97% 114M 1s
521250K .......... .......... .......... .......... .......... 97% 61.3M 1s
521300K .......... .......... .......... .......... .......... 97% 208M 1s
521350K .......... .......... .......... .......... .......... 97% 6.87M 1s
521400K .......... .......... .......... .......... .......... 97% 139M 1s
521450K .......... .......... .......... .......... .......... 97% 166M 1s
521500K .......... .......... .......... .......... .......... 97% 157M 1s
521550K .......... .......... .......... .......... .......... 97% 6.92M 1s
521600K .......... .......... .......... .......... .......... 97% 96.9M 1s
521650K .......... .......... .......... .......... .......... 97% 143M 1s
521700K .......... .......... .......... .......... .......... 97% 127M 1s
521750K .......... .......... .......... .......... .......... 97% 6.77M 1s
521800K .......... .......... .......... .......... .......... 97% 122M 1s
521850K .......... .......... .......... .......... .......... 97% 152M 1s
521900K .......... .......... .......... .......... .......... 97% 102M 1s
521950K .......... .......... .......... .......... .......... 97% 6.89M 1s
522000K .......... .......... .......... .......... .......... 97% 116M 1s
522050K .......... .......... .......... .......... .......... 97% 95.0M 1s
522100K .......... .......... .......... .......... .......... 97% 107M 1s
522150K .......... .......... .......... .......... .......... 97% 6.89M 1s
522200K .......... .......... .......... .......... .......... 97% 137M 1s
522250K .......... .......... .......... .......... .......... 97% 87.0M 1s
522300K .......... .......... .......... .......... .......... 97% 155M 1s
522350K .......... .......... .......... .......... .......... 97% 7.11M 1s
522400K .......... .......... .......... .......... .......... 97% 83.2M 1s
522450K .......... .......... .......... .......... .......... 98% 73.5M 1s
522500K .......... .......... .......... .......... .......... 98% 115M 1s
522550K .......... .......... .......... .......... .......... 98% 7.52M 1s
522600K .......... .......... .......... .......... .......... 98% 121M 1s
522650K .......... .......... .......... .......... .......... 98% 154M 1s
522700K .......... .......... .......... .......... .......... 98% 95.2M 1s
522750K .......... .......... .......... .......... .......... 98% 7.08M 1s
522800K .......... .......... .......... .......... .......... 98% 126M 1s
522850K .......... .......... .......... .......... .......... 98% 98.0M 1s
522900K .......... .......... .......... .......... .......... 98% 117M 1s
522950K .......... .......... .......... .......... .......... 98% 81.1M 1s
523000K .......... .......... .......... .......... .......... 98% 6.38M 1s
523050K .......... .......... .......... .......... .......... 98% 84.0M 1s
523100K .......... .......... .......... .......... .......... 98% 104M 1s
523150K .......... .......... .......... .......... .......... 98% 54.9M 1s
523200K .......... .......... .......... .......... .......... 98% 4.59M 1s
523250K .......... .......... .......... .......... .......... 98% 82.3M 1s
523300K .......... .......... .......... .......... .......... 98% 50.0M 1s
523350K .......... .......... .......... .......... .......... 98% 29.4M 1s
523400K .......... .......... .......... .......... .......... 98% 1.99M 1s
523450K .......... .......... .......... .......... .......... 98% 177M 1s
523500K .......... .......... .......... .......... .......... 98% 8.96M 1s
523550K .......... .......... .......... .......... .......... 98% 189M 1s
523600K .......... .......... .......... .......... .......... 98% 5.61M 1s
523650K .......... .......... .......... .......... .......... 98% 150M 1s
523700K .......... .......... .......... .......... .......... 98% 74.3M 1s
523750K .......... .......... .......... .......... .......... 98% 120M 1s
523800K .......... .......... .......... .......... .......... 98% 5.63M 1s
523850K .......... .......... .......... .......... .......... 98% 153M 1s
523900K .......... .......... .......... .......... .......... 98% 210M 1s
523950K .......... .......... .......... .......... .......... 98% 163M 1s
524000K .......... .......... .......... .......... .......... 98% 5.59M 1s
524050K .......... .......... .......... .......... .......... 98% 119M 1s
524100K .......... .......... .......... .......... .......... 98% 55.4M 1s
524150K .......... .......... .......... .......... .......... 98% 158M 1s
524200K .......... .......... .......... .......... .......... 98% 83.5M 1s
524250K .......... .......... .......... .......... .......... 98% 3.52M 1s
524300K .......... .......... .......... .......... .......... 98% 4.19M 1s
524350K .......... .......... .......... .......... .......... 98% 112M 1s
524400K .......... .......... .......... .......... .......... 98% 132M 1s
524450K .......... .......... .......... .......... .......... 98% 2.35M 1s
524500K .......... .......... .......... .......... .......... 98% 201M 1s
524550K .......... .......... .......... .......... .......... 98% 197M 1s
524600K .......... .......... .......... .......... .......... 98% 150M 1s
524650K .......... .......... .......... .......... .......... 98% 7.17M 1s
524700K .......... .......... .......... .......... .......... 98% 102M 1s
524750K .......... .......... .......... .......... .......... 98% 114M 1s
524800K .......... .......... .......... .......... .......... 98% 99.0M 1s
524850K .......... .......... .......... .......... .......... 98% 7.50M 1s
524900K .......... .......... .......... .......... .......... 98% 199M 1s
524950K .......... .......... .......... .......... .......... 98% 136M 1s
525000K .......... .......... .......... .......... .......... 98% 117M 1s
525050K .......... .......... .......... .......... .......... 98% 155M 1s
525100K .......... .......... .......... .......... .......... 98% 7.32M 1s
525150K .......... .......... .......... .......... .......... 98% 206M 1s
525200K .......... .......... .......... .......... .......... 98% 133M 1s
525250K .......... .......... .......... .......... .......... 98% 171M 1s
525300K .......... .......... .......... .......... .......... 98% 7.39M 1s
525350K .......... .......... .......... .......... .......... 98% 3.90M 1s
525400K .......... .......... .......... .......... .......... 98% 207M 1s
525450K .......... .......... .......... .......... .......... 98% 116M 1s
525500K .......... .......... .......... .......... .......... 98% 5.88M 1s
525550K .......... .......... .......... .......... .......... 98% 203M 1s
525600K .......... .......... .......... .......... .......... 98% 178M 1s
525650K .......... .......... .......... .......... .......... 98% 148M 1s
525700K .......... .......... .......... .......... .......... 98% 6.50M 1s
525750K .......... .......... .......... .......... .......... 98% 133M 1s
525800K .......... .......... .......... .......... .......... 98% 96.7M 1s
525850K .......... .......... .......... .......... .......... 98% 115M 1s
525900K .......... .......... .......... .......... .......... 98% 214M 1s
525950K .......... .......... .......... .......... .......... 98% 6.62M 1s
526000K .......... .......... .......... .......... .......... 98% 106M 1s
526050K .......... .......... .......... .......... .......... 98% 193M 1s
526100K .......... .......... .......... .......... .......... 98% 180M 1s
526150K .......... .......... .......... .......... .......... 98% 8.24M 1s
526200K .......... .......... .......... .......... .......... 98% 184M 1s
526250K .......... .......... .......... .......... .......... 98% 116M 0s
526300K .......... .......... .......... .......... .......... 98% 200M 0s
526350K .......... .......... .......... .......... .......... 98% 6.01M 0s
526400K .......... .......... .......... .......... .......... 98% 145M 0s
526450K .......... .......... .......... .......... .......... 98% 115M 0s
526500K .......... .......... .......... .......... .......... 98% 177M 0s
526550K .......... .......... .......... .......... .......... 98% 171M 0s
526600K .......... .......... .......... .......... .......... 98% 6.88M 0s
526650K .......... .......... .......... .......... .......... 98% 190M 0s
526700K .......... .......... .......... .......... .......... 98% 127M 0s
526750K .......... .......... .......... .......... .......... 98% 176M 0s
526800K .......... .......... .......... .......... .......... 98% 8.19M 0s
526850K .......... .......... .......... .......... .......... 98% 181M 0s
526900K .......... .......... .......... .......... .......... 98% 119M 0s
526950K .......... .......... .......... .......... .......... 98% 113M 0s
527000K .......... .......... .......... .......... .......... 98% 96.9M 0s
527050K .......... .......... .......... .......... .......... 98% 6.76M 0s
527100K .......... .......... .......... .......... .......... 98% 131M 0s
527150K .......... .......... .......... .......... .......... 98% 118M 0s
527200K .......... .......... .......... .......... .......... 98% 73.8M 0s
527250K .......... .......... .......... .......... .......... 98% 8.01M 0s
527300K .......... .......... .......... .......... .......... 98% 149M 0s
527350K .......... .......... .......... .......... .......... 98% 167M 0s
527400K .......... .......... .......... .......... .......... 98% 102M 0s
527450K .......... .......... .......... .......... .......... 98% 7.44M 0s
527500K .......... .......... .......... .......... .......... 98% 141M 0s
527550K .......... .......... .......... .......... .......... 98% 112M 0s
527600K .......... .......... .......... .......... .......... 98% 86.7M 0s
527650K .......... .......... .......... .......... .......... 98% 127M 0s
527700K .......... .......... .......... .......... .......... 98% 6.78M 0s
527750K .......... .......... .......... .......... .......... 98% 97.9M 0s
527800K .......... .......... .......... .......... .......... 99% 71.7M 0s
527850K .......... .......... .......... .......... .......... 99% 98.6M 0s
527900K .......... .......... .......... .......... .......... 99% 7.06M 0s
527950K .......... .......... .......... .......... .......... 99% 91.8M 0s
528000K .......... .......... .......... .......... .......... 99% 219M 0s
528050K .......... .......... .......... .......... .......... 99% 130M 0s
528100K .......... .......... .......... .......... .......... 99% 126M 0s
528150K .......... .......... .......... .......... .......... 99% 5.26M 0s
528200K .......... .......... .......... .......... .......... 99% 169M 0s
528250K .......... .......... .......... .......... .......... 99% 204M 0s
528300K .......... .......... .......... .......... .......... 99% 164M 0s
528350K .......... .......... .......... .......... .......... 99% 6.95M 0s
528400K .......... .......... .......... .......... .......... 99% 81.9M 0s
528450K .......... .......... .......... .......... .......... 99% 110M 0s
528500K .......... .......... .......... .......... .......... 99% 140M 0s
528550K .......... .......... .......... .......... .......... 99% 142M 0s
528600K .......... .......... .......... .......... .......... 99% 6.75M 0s
528650K .......... .......... .......... .......... .......... 99% 164M 0s
528700K .......... .......... .......... .......... .......... 99% 112M 0s
528750K .......... .......... .......... .......... .......... 99% 115M 0s
528800K .......... .......... .......... .......... .......... 99% 6.55M 0s
528850K .......... .......... .......... .......... .......... 99% 135M 0s
528900K .......... .......... .......... .......... .......... 99% 94.3M 0s
528950K .......... .......... .......... .......... .......... 99% 152M 0s
529000K .......... .......... .......... .......... .......... 99% 128M 0s
529050K .......... .......... .......... .......... .......... 99% 6.60M 0s
529100K .......... .......... .......... .......... .......... 99% 98.4M 0s
529150K .......... .......... .......... .......... .......... 99% 132M 0s
529200K .......... .......... .......... .......... .......... 99% 104M 0s
529250K .......... .......... .......... .......... .......... 99% 115M 0s
529300K .......... .......... .......... .......... .......... 99% 7.53M 0s
529350K .......... .......... .......... .......... .......... 99% 147M 0s
529400K .......... .......... .......... .......... .......... 99% 132M 0s
529450K .......... .......... .......... .......... .......... 99% 79.0M 0s
529500K .......... .......... .......... .......... .......... 99% 7.13M 0s
529550K .......... .......... .......... .......... .......... 99% 136M 0s
529600K .......... .......... .......... .......... .......... 99% 125M 0s
529650K .......... .......... .......... .......... .......... 99% 105M 0s
529700K .......... .......... .......... .......... .......... 99% 111M 0s
529750K .......... .......... .......... .......... .......... 99% 5.69M 0s
529800K .......... .......... .......... .......... .......... 99% 86.1M 0s
529850K .......... .......... .......... .......... .......... 99% 124M 0s
529900K .......... .......... .......... .......... .......... 99% 120M 0s
529950K .......... .......... .......... .......... .......... 99% 5.25M 0s
530000K .......... .......... .......... .......... .......... 99% 133M 0s
530050K .......... .......... .......... .......... .......... 99% 66.4M 0s
530100K .......... .......... .......... .......... .......... 99% 58.9M 0s
530150K .......... .......... .......... .......... .......... 99% 84.6M 0s
530200K .......... .......... .......... .......... .......... 99% 5.40M 0s
530250K .......... .......... .......... .......... .......... 99% 98.4M 0s
530300K .......... .......... .......... .......... .......... 99% 122M 0s
530350K .......... .......... .......... .......... .......... 99% 78.5M 0s
530400K .......... .......... .......... .......... .......... 99% 88.3M 0s
530450K .......... .......... .......... .......... .......... 99% 312K 0s
530500K .......... .......... .......... .......... .......... 99% 84.5M 0s
530550K .......... .......... .......... .......... .......... 99% 189M 0s
530600K .......... .......... .......... .......... .......... 99% 153M 0s
530650K .......... .......... .......... .......... .......... 99% 140M 0s
530700K .......... .......... .......... .......... .......... 99% 69.7M 0s
530750K .......... .......... .......... .......... .......... 99% 170M 0s
530800K .......... .......... .......... .......... .......... 99% 136M 0s
530850K .......... .......... .......... .......... .......... 99% 76.1M 0s
530900K .......... .......... .......... .......... .......... 99% 124M 0s
530950K .......... .......... .......... .......... .......... 99% 93.5M 0s
531000K .......... .......... .......... .......... .......... 99% 148M 0s
531050K .......... .......... .......... .......... .......... 99% 139M 0s
531100K .......... .......... .......... .......... .......... 99% 78.3M 0s
531150K .......... .......... .......... .......... .......... 99% 169M 0s
531200K .......... .......... .......... .......... .......... 99% 177M 0s
531250K .......... .......... .......... .......... .......... 99% 53.7M 0s
531300K .......... .......... .......... .......... .......... 99% 187M 0s
531350K .......... .......... .......... .......... .......... 99% 199M 0s
531400K .......... .......... .......... .......... .......... 99% 203M 0s
531450K .......... .......... .......... .......... .......... 99% 188M 0s
531500K .......... .......... .......... .......... .......... 99% 17.4M 0s
531550K .......... .......... .......... .......... .......... 99% 139M 0s
531600K .......... .......... .......... .......... .......... 99% 135M 0s
531650K .......... .......... .......... .......... .......... 99% 69.6M 0s
531700K .......... .......... .......... .......... .......... 99% 94.8M 0s
531750K .......... .......... .......... .......... .......... 99% 199M 0s
531800K .......... .......... .......... .......... .......... 99% 233M 0s
531850K .......... .......... .......... .......... .......... 99% 166M 0s
531900K .......... .......... .......... .......... .......... 99% 17.4M 0s
531950K .......... .......... .......... .......... .......... 99% 146M 0s
532000K .......... .......... .......... .......... .......... 99% 150M 0s
532050K .......... .......... .......... .......... .......... 99% 188M 0s
532100K .......... .......... .......... .......... .......... 99% 26.8M 0s
532150K .......... .......... .......... .......... .......... 99% 7.80M 0s
532200K .......... .......... .......... .......... .......... 99% 59.4M 0s
532250K .......... .......... .......... .......... .......... 99% 133M 0s
532300K .......... .......... .......... .......... .......... 99% 157M 0s
532350K .......... .......... .......... .......... .......... 99% 116M 0s
532400K .......... .......... .......... .......... .......... 99% 6.10M 0s
532450K .......... .......... .......... .......... .......... 99% 87.7M 0s
532500K .......... .......... .......... .......... .......... 99% 560K 0s
532550K .......... .......... .......... .......... .......... 99% 136M 0s
532600K .......... .......... .......... .......... .......... 99% 117M 0s
532650K .......... .......... .......... .......... .......... 99% 114M 0s
532700K .......... .......... .......... .......... .......... 99% 153M 0s
532750K .......... .......... .......... .......... .......... 99% 85.4M 0s
532800K .......... .......... .......... .......... .......... 99% 113M 0s
532850K .......... .......... .......... .......... .......... 99% 109M 0s
532900K .......... .......... .......... .......... .......... 99% 48.2M 0s
532950K .......... .......... .......... .......... .......... 99% 82.9M 0s
533000K .......... .......... .......... .......... .......... 99% 178M 0s
533050K .......... .......... .......... .......... .......... 99% 126M 0s
533100K .......... .......... .......... .......... .......... 99% 135M 0s
533150K ......... 100% 162M=39s
2024-07-28 00:47:09 (13.5 MB/s) - ‘ESP126-macos-x86_64.tgz’ saved [545954930/545954930]
+ tar -xf ESP126-macos-x86_64.tgz
+ cd ESP126
+ rm -rf /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Slugs
++ 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* ]]
+ ./setup.command
Custom icon assigned to '/Users/jenkins/Desktop/ESP126.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/esp_logo.png'.
Custom icon assigned to '/Users/jenkins/Desktop/runESP126.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/esp_logo.png'.
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/idle3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pyftsubset'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_op4'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/ttx'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/wingproj'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_op2'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pip3'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/imageio_remove_bin'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/undill'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/run_om_test'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/f90nml'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/webview'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/fonttools'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/openmdao'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pyNastranGUI'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/f2py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pydoc3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/2to3-3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/imageio_download_bin'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pip3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_pynastrangui'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/numba'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/normalizer'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/virtualenv'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/reset_notebook'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/abaqus_to_nastran'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/get_gprof'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/format_converter'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pyftmerge'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python3.11-config'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/f06'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/get_objgraph'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/config-3.11-darwin/Makefile'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/config-3.11-darwin/python-config.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/pkgconfig/python-3.11-embed.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/pkgconfig/python-3.11.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/_sysconfigdata__darwin_darwin.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages/mpi4py/mpi.cfg'
Patching 'bin/mpirun_esp'
Patching 'bin/ompi_info'
Patching 'bin/pmix_info'
Patching 'bin/prte_info'
Patching 'lib/libmpi.40.dylib'
Patching 'lib/libopen-pal.80.dylib'
Patching 'lib/libpmix.2.dylib'
Patching 'lib/libprrte.3.dylib'
Patching 'lib/openmpi/mca_io_romio341.so'
Patching 'lib/prte/prte_mca_schizo_ompi.so'
Patching 'include/pmix/src/include/pmix_config.h'
Patching 'lib/pkgconfig/ompi-c.pc'
Patching 'lib/pkgconfig/ompi-cxx.pc'
Patching 'lib/pkgconfig/ompi-fort.pc'
Patching 'lib/pkgconfig/ompi.pc'
Patching 'lib/pkgconfig/pmix.pc'
Patching 'share/openmpi/mpic++-wrapper-data.txt'
Patching 'share/openmpi/mpicc-wrapper-data.txt'
Patching 'share/openmpi/mpifort-wrapper-data.txt'
Patching 'share/pmix/pmixcc-wrapper-data.txt'
+ rm -rf /Users/jenkins/Desktop/ESP126.command /Users/jenkins/Desktop/runESP126.command
+ source /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN64
++ ESP_ARCH=DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad
++ export CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/OpenCASCADE-7.8.1
++ CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/OpenCASCADE-7.8.1
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ '[' -z /Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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-v8.0.1/bin ']'
++ export PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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-v8.0.1/bin
++ PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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-v8.0.1/bin
++ export PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/include/python3.11
++ PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib -lpython3.11'
++ '[' -z /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin ']'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.1/bin
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/ESP-localhost7681.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/ESP-localhost7681.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/wvClient/wv.html'
+ which python
/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python
+ python --version
Python 3.11.9
+ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/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_bPreBuilt/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
==> serveESP completed successfully with no verification data
real 0m4.315s
user 0m0.033s
sys 0m0.021s
+ set +x
=============================================
ESP verification case 01 passed (as expected)
=============================================
+ expectSuccess 02 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.245s
user 0m0.291s
sys 0m0.038s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/verify_7.8.1/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m2.813s
user 0m4.145s
sys 0m0.762s
+ set +x
=============================================
ESP verification case 03 passed (as expected)
=============================================
+ expectSuccess 04 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.693s
user 0m0.769s
sys 0m0.045s
+ set +x
=============================================
ESP verification case 04 passed (as expected)
=============================================
+ expectSuccess 05 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.648s
user 0m0.878s
sys 0m0.064s
+ set +x
=============================================
ESP verification case 05 passed (as expected)
=============================================
+ expectSuccess 06 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/verify_7.8.1/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.716s
user 0m0.912s
sys 0m0.064s
+ set +x
=============================================
ESP verification case 06 passed (as expected)
=============================================
+ expectSuccess 07 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/verify_7.8.1/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m3.784s
user 0m5.594s
sys 0m0.427s
+ set +x
=============================================
ESP verification case 07 passed (as expected)
=============================================
+ expectSuccess 08 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/CAPS/verify_7.8.1/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data
real 0m35.664s
user 0m49.219s
sys 0m2.054s
+ set +x
=============================================
ESP verification case 08 passed (as expected)
=============================================
+ expectSuccess 09 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/verify_7.8.1/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.665s
user 0m0.812s
sys 0m0.034s
+ set +x
=============================================
ESP verification case 09 passed (as expected)
=============================================
+ expectSuccess 10 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data
real 0m42.765s
user 1m12.680s
sys 0m5.177s
+ set +x
=============================================
ESP verification case 10 passed (as expected)
=============================================
+ expectSuccess 11 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: could not find mapping for iedge=10
WARNING:: could not find mapping for iedge=14
WARNING:: could not find mapping for iedge=7
WARNING:: could not find mapping for iedge=11
==> serveESP completed successfully with 4 warnings and no verification data
real 0m0.512s
user 0m0.280s
sys 0m0.037s
+ set +x
=============================================
ESP verification case 11 passed (as expected)
=============================================
+ expectSuccess 12 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.527s
user 0m0.780s
sys 0m0.026s
+ set +x
=============================================
ESP verification case 12 passed (as expected)
=============================================
+ expectSuccess 13 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.172s
user 0m0.211s
sys 0m0.021s
+ set +x
=============================================
ESP verification case 13 passed (as expected)
=============================================
+ expectSuccess 14 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/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 0m0.437s
user 0m0.497s
sys 0m0.029s
+ set +x
=============================================
ESP verification case 14 passed (as expected)
=============================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
...................................................... PCurve Map: 48 (alloc 48)!
Surface Map: 12 (alloc 24)!
Curve Map: 28 (alloc 28)!
Writing PCurves...
Writing Curves...
Writing Surfaces...
Writing 16 Nodes...
Writing 28 Edges...
Writing 12 Loops...
Writing 12 Faces...
Writing 1 Shells...
EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 73 tests in 2.864s
OK
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m8.450s
user 0m11.251s
sys 0m0.312s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
..Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 143
Number of elements = 282
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 282
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 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 40.745s
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_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.032 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4283 6322
AFLR2 GG : Nodes, Faces = 6128 10012
AFLR2 GG : Nodes, Faces = 7863 13482
AFLR2 GG : Nodes, Faces = 9464 16684
AFLR2 GG : Nodes, Faces = 10948 19652
AFLR2 GG : Nodes, Faces = 12322 22400
AFLR2 GG : Nodes, Faces = 13619 24994
AFLR2 GG : Nodes, Faces = 14829 27414
AFLR2 GG : Nodes, Faces = 15981 29718
AFLR2 GG : Nodes, Faces = 17082 31920
AFLR2 GG : Nodes, Faces = 18110 33976
AFLR2 GG : Nodes, Faces = 19081 35918
AFLR2 GG : Nodes, Faces = 20014 37784
AFLR2 GG : Nodes, Faces = 20924 39604
AFLR2 GG : Nodes, Faces = 21782 41320
AFLR2 GG : Nodes, Faces = 22595 42946
AFLR2 GG : Nodes, Faces = 23377 44510
AFLR2 GG : Nodes, Faces = 24129 46014
AFLR2 GG : Nodes, Faces = 24840 47436
AFLR2 GG : Nodes, Faces = 25522 48800
AFLR2 GG : Nodes, Faces = 26170 50096
AFLR2 GG : Nodes, Faces = 26793 51342
AFLR2 GG : Nodes, Faces = 27346 52448
AFLR2 GG : Nodes, Faces = 27846 53448
AFLR2 GG : Nodes, Faces = 28280 54316
AFLR2 GG : Nodes, Faces = 28652 55060
AFLR2 GG : Nodes, Faces = 28920 55596
AFLR2 GG : Nodes, Faces = 29143 56042
AFLR2 GG : Nodes, Faces = 29358 56472
AFLR2 GG : Nodes, Faces = 29550 56856
AFLR2 GG : Nodes, Faces = 29693 57142
AFLR2 GG : Nodes, Faces = 29805 57366
AFLR2 GG : Nodes, Faces = 29875 57506
AFLR2 GG : Nodes, Faces = 29895 57546
AFLR2 GG : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.090 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.010 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2224 0
AFLR2 : CPU Time = 0.001 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 = 0.049 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 = 0.147 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.009 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.033 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4283 6322
AFLR2 GG : Nodes, Faces = 6128 10012
AFLR2 GG : Nodes, Faces = 7863 13482
AFLR2 GG : Nodes, Faces = 9464 16684
AFLR2 GG : Nodes, Faces = 10948 19652
AFLR2 GG : Nodes, Faces = 12322 22400
AFLR2 GG : Nodes, Faces = 13619 24994
AFLR2 GG : Nodes, Faces = 14829 27414
AFLR2 GG : Nodes, Faces = 15981 29718
AFLR2 GG : Nodes, Faces = 17082 31920
AFLR2 GG : Nodes, Faces = 18110 33976
AFLR2 GG : Nodes, Faces = 19081 35918
AFLR2 GG : Nodes, Faces = 20014 37784
AFLR2 GG : Nodes, Faces = 20924 39604
AFLR2 GG : Nodes, Faces = 21782 41320
AFLR2 GG : Nodes, Faces = 22595 42946
AFLR2 GG : Nodes, Faces = 23377 44510
AFLR2 GG : Nodes, Faces = 24129 46014
AFLR2 GG : Nodes, Faces = 24840 47436
AFLR2 GG : Nodes, Faces = 25522 48800
AFLR2 GG : Nodes, Faces = 26170 50096
AFLR2 GG : Nodes, Faces = 26793 51342
AFLR2 GG : Nodes, Faces = 27346 52448
AFLR2 GG : Nodes, Faces = 27846 53448
AFLR2 GG : Nodes, Faces = 28280 54316
AFLR2 GG : Nodes, Faces = 28652 55060
AFLR2 GG : Nodes, Faces = 28920 55596
AFLR2 GG : Nodes, Faces = 29143 56042
AFLR2 GG : Nodes, Faces = 29358 56472
AFLR2 GG : Nodes, Faces = 29550 56856
AFLR2 GG : Nodes, Faces = 29693 57142
AFLR2 GG : Nodes, Faces = 29805 57366
AFLR2 GG : Nodes, Faces = 29875 57506
AFLR2 GG : Nodes, Faces = 29895 57546
AFLR2 GG : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.138 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.013 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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 = 0.030 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 = 0.091 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.009 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.032 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4283 6322
AFLR2 GG : Nodes, Faces = 6128 10012
AFLR2 GG : Nodes, Faces = 7863 13482
AFLR2 GG : Nodes, Faces = 9464 16684
AFLR2 GG : Nodes, Faces = 10948 19652
AFLR2 GG : Nodes, Faces = 12322 22400
AFLR2 GG : Nodes, Faces = 13619 24994
AFLR2 GG : Nodes, Faces = 14829 27414
AFLR2 GG : Nodes, Faces = 15981 29718
AFLR2 GG : Nodes, Faces = 17082 31920
AFLR2 GG : Nodes, Faces = 18110 33976
AFLR2 GG : Nodes, Faces = 19081 35918
AFLR2 GG : Nodes, Faces = 20014 37784
AFLR2 GG : Nodes, Faces = 20924 39604
AFLR2 GG : Nodes, Faces = 21782 41320
AFLR2 GG : Nodes, Faces = 22595 42946
AFLR2 GG : Nodes, Faces = 23377 44510
AFLR2 GG : Nodes, Faces = 24129 46014
AFLR2 GG : Nodes, Faces = 24840 47436
AFLR2 GG : Nodes, Faces = 25522 48800
AFLR2 GG : Nodes, Faces = 26170 50096
AFLR2 GG : Nodes, Faces = 26793 51342
AFLR2 GG : Nodes, Faces = 27346 52448
AFLR2 GG : Nodes, Faces = 27846 53448
AFLR2 GG : Nodes, Faces = 28280 54316
AFLR2 GG : Nodes, Faces = 28652 55060
AFLR2 GG : Nodes, Faces = 28920 55596
AFLR2 GG : Nodes, Faces = 29143 56042
AFLR2 GG : Nodes, Faces = 29358 56472
AFLR2 GG : Nodes, Faces = 29550 56856
AFLR2 GG : Nodes, Faces = 29693 57142
AFLR2 GG : Nodes, Faces = 29805 57366
AFLR2 GG : Nodes, Faces = 29875 57506
AFLR2 GG : Nodes, Faces = 29895 57546
AFLR2 GG : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.086 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.008 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 = 0.001 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 = 0.001 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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 = 0.009 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.001 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.059 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 = 0.015 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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 = 0.045 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 = 0.012 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:63376)
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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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:63376)
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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 17441
Number of elements = 99306
Number of triangles = 8306
Number of quadrilatarals = 0
Number of tetrahedrals = 91000
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1494
Number of elements = 7708
Number of triangles = 1988
Number of quadrilatarals = 0
Number of tetrahedrals = 5720
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1558
Number of elements = 7832
Number of triangles = 2112
Number of quadrilatarals = 0
Number of tetrahedrals = 5720
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1151
Number of elements = 6028
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4720
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 363
Number of elements = 1645
Number of triangles = 720
Number of quadrilatarals = 0
Number of tetrahedrals = 925
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 20671
Number of elements = 119572
Number of triangles = 5446
Number of quadrilatarals = 0
Number of tetrahedrals = 114126
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18912
Number of elements = 109307
Number of triangles = 5256
Number of quadrilatarals = 0
Number of tetrahedrals = 104051
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 20671
Number of elements = 119572
Number of triangles = 5446
Number of quadrilatarals = 0
Number of tetrahedrals = 114126
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18912
Number of elements = 109307
Number of triangles = 5256
Number of quadrilatarals = 0
Number of tetrahedrals = 104051
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 20671
Number of elements = 119572
Number of triangles = 5446
Number of quadrilatarals = 0
Number of tetrahedrals = 114126
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18912
Number of elements = 109307
Number of triangles = 5256
Number of quadrilatarals = 0
Number of tetrahedrals = 104051
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_quad (test_aflr3.TestAFLR3.test_quad) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 28583
Number of elements = 129179
Number of triangles = 410
Number of quadrilatarals = 3218
Number of tetrahedrals = 118367
Number of pyramids = 0
Number of prisms = 748
Number of hexahedrals = 6436
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk 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_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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 21315
Number of elements = 123546
Number of triangles = 5542
Number of quadrilatarals = 0
Number of tetrahedrals = 118004
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 20272
Number of elements = 117350
Number of triangles = 5384
Number of quadrilatarals = 0
Number of tetrahedrals = 111966
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 41690
Number of elements = 240892
Number of triangles = 11826
Number of quadrilatarals = 0
Number of tetrahedrals = 229066
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 45515
Number of elements = 263531
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 251835
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 41690
Number of elements = 240762
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 229066
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
test_Edge_scaleFactor (test_aflr4.TestAFLR4.test_Edge_scaleFactor) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - trailingEdge
Done getting mesh sizing parameters
ok
test_Face_scaleFactor (test_aflr4.TestAFLR4.test_Face_scaleFactor) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - leftWing
Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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_erw (test_aflr4.TestAFLR4.test_erw) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - leftWing
Done getting mesh sizing parameters
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_ff_cdfr (test_aflr4.TestAFLR4.test_ff_cdfr) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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:63376)
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:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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:63376)
ok
test_max_min_scale (test_aflr4.TestAFLR4.test_max_min_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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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_proximity (test_aflr4.TestAFLR4.test_proximity) ... 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 - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
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 - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
ok
test_quad (test_aflr4.TestAFLR4.test_quad) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk 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_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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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_regions (test_aflr4.TestAFLR4.test_regions) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: box
2: cut
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) ... ok
test_skin (test_aflr4.TestAFLR4.test_skin) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Ribs
2: Skin
3: Spar1
4: Rib_Root
5: Spar2
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_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Rib_Root, index = 1
Name = Skin, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 46
Number of elements = 44
Number of triangle elements = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes = 47
Total number of elements = 44
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 46
Number of elements = 44
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 44
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 47
Combined Number of elements = 45
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 44
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 3
Surface 2: Number of points found for aero-spline = 6
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
8 automatic connections were made for capsConnect Rib_Root (node id 1)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
ok
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice control surface data
VLM control surface name - Elevator
VLM control surface name - LeftAileron
VLM control surface name - RightAileron
VLM control surface name - Rudder
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... skipped 'No flowCart executable'
test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable'
test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable'
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable'
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable'
test_Output_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = riteWing, index = 1
Name = leftWing, index = 2
Name = trailingEdge, index = 3
Writing FAST file ....
Finished writing FAST file
Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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:63376)
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
110333E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
110333E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000AC77000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000AC77000 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
110333E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
70000AC77000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000AC77000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
110333E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, 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
70000AC77000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
70000AC77000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000AC77000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000AC77000 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
70000AC77000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
70000AC77000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
110333E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
110333E00 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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:63376)
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:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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:63376)
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:63376)
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:63376)
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:63376)
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 6751
Number of elements = 13498
Number of triangle elements = 13498
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 4919
Number of elements = 9834
Number of triangle elements = 9834
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 196
Number of elements = 388
Number of triangle elements = 388
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 11866
Total number of elements = 23720
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 - 11866, elements - 23720
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.138613
Creating surface mesh ...
Surface mesh seconds: 0.034878
Recovering boundaries...
Boundary recovery seconds: 0.135883
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.055207
Recovering Delaunayness...
Delaunay recovery seconds: 0.067403
Refining mesh...
15817 insertions, added 8076 points, 516596 tetrahedra in queue.
5267 insertions, added 1612 points, 522415 tetrahedra in queue.
7020 insertions, added 1839 points, 496219 tetrahedra in queue.
9358 insertions, added 1649 points, 350840 tetrahedra in queue.
12474 insertions, added 1188 points, 9687 tetrahedra in queue.
16628 insertions, added 1422 points, 5458 tetrahedra in queue.
Refinement seconds: 8.9361
Smoothing vertices...
Mesh smoothing seconds: 1.92933
Improving mesh...
Mesh improvement seconds: 0.051271
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.018509
Total running seconds: 11.3685
Statistics:
Input points: 11866
Input facets: 23720
Input segments: 35580
Input holes: 2
Input regions: 0
Mesh points: 28105
Mesh tetrahedra: 135725
Mesh faces: 283310
Mesh faces on exterior boundary: 23720
Mesh faces on input facets: 23720
Mesh edges on input segments: 35580
Steiner points inside domain: 16239
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 = 6751
Number of elements = 13498
Number of triangle elements = 13498
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 4919
Number of elements = 9834
Number of triangle elements = 9834
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 196
Number of elements = 388
Number of triangle elements = 388
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 11866
Total number of elements = 23720
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 - 11866, elements - 23720
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.129669
Creating surface mesh ...
Surface mesh seconds: 0.037522
Recovering boundaries...
Boundary recovery seconds: 0.129756
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.054077
Recovering Delaunayness...
Delaunay recovery seconds: 0.062532
Refining mesh...
15817 insertions, added 8076 points, 516596 tetrahedra in queue.
5267 insertions, added 1612 points, 522415 tetrahedra in queue.
7020 insertions, added 1839 points, 496219 tetrahedra in queue.
9358 insertions, added 1649 points, 350840 tetrahedra in queue.
12474 insertions, added 1188 points, 9687 tetrahedra in queue.
16628 insertions, added 1422 points, 5458 tetrahedra in queue.
Refinement seconds: 8.37202
Smoothing vertices...
Mesh smoothing seconds: 2.14625
Improving mesh...
Mesh improvement seconds: 0.037577
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.016446
Total running seconds: 10.9872
Statistics:
Input points: 11866
Input facets: 23720
Input segments: 35580
Input holes: 2
Input regions: 0
Mesh points: 28105
Mesh tetrahedra: 135725
Mesh faces: 283310
Mesh faces on exterior boundary: 23720
Mesh faces on input facets: 23720
Mesh edges on input segments: 35580
Steiner points inside domain: 16239
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_bPreBuilt/ESP126/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_bPreBuilt/ESP126/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_bPreBuilt/ESP126/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 - 1208, elements - 2404
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 - 1208, elements - 2404
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 - 11866, elements - 23720
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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1665
Number of elements = 9143
Number of triangles = 1216
Number of quadrilatarals = 0
Number of tetrahedrals = 7927
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2600
Number of elements = 13864
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1071
Number of elements = 5705
Number of triangles = 998
Number of quadrilatarals = 0
Number of tetrahedrals = 4707
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 20272
Number of elements = 117350
Number of triangles = 5384
Number of quadrilatarals = 0
Number of tetrahedrals = 111966
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1665
Number of elements = 9143
Number of triangles = 1216
Number of quadrilatarals = 0
Number of tetrahedrals = 7927
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 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 438
Number of elements = 2179
Number of triangles = 644
Number of quadrilatarals = 0
Number of tetrahedrals = 1535
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 936
Number of elements = 4999
Number of triangles = 758
Number of quadrilatarals = 0
Number of tetrahedrals = 4241
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 3 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 8 Faces
EGADS : Body 0 has 15 Edges
EGADS : Body 0 has 8 Loops
EGADS : Body 0 has 9 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 8 Faces
EGADS : Body 1 has 15 Edges
EGADS : Body 1 has 8 Loops
EGADS : Body 1 has 9 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 2 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 2 Loops
EGADS : Body 2 has 2 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 4 5
EGADS : 2 Yes 0 0 1 1 1 1 3 4 6
EGADS : 3 Yes 0 0 1 1 1 1 2 4 7
EGADS : 4 Yes 0 0 1 1 1 1 2 3
EGADS : 5 Yes 0 0 1 1 1 1 6 7 8
EGADS : 6 Yes 0 0 1 1 1 2 5 7 8
EGADS : 7 Yes 0 0 1 1 1 3 5 6 8
EGADS : 8 Yes 0 0 1 1 1 5 6 7
EGADS : 9 Yes 1 0 1 0 10 10 11 12 13
EGADS : 10 Yes 1 0 1 0 10 9 11 12 14
EGADS : 11 Yes 1 0 1 0 10 9 10 12 15
EGADS : 12 Yes 1 0 1 0 10 9 10 11
EGADS : 13 Yes 1 0 1 0 10 9 14 15 16
EGADS : 14 Yes 1 0 1 0 10 10 13 15 16
EGADS : 15 Yes 1 0 1 0 10 11 13 14 16
EGADS : 16 Yes 1 0 1 0 10 13 14 15
EGADS : 17 Yes 2 0 1 NA NA 18
EGADS : 18 Yes 2 0 1 NA NA 17
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 4 -3 -2
EGADS : 2 3 7 -6 -5
EGADS : 3 6 9 -1 -8
EGADS : 4 -4 -9 -7
EGADS : 5 -10 2 11 -12
EGADS : 6 -11 5 13 -14
EGADS : 7 -13 8 10 -15
EGADS : 8 12 14 15
EGADS : 9 16 19 -18 -17
EGADS : 10 18 22 -21 -20
EGADS : 11 21 24 -16 -23
EGADS : 12 -19 -24 -22
EGADS : 13 -25 17 26 -27
EGADS : 14 -26 20 28 -29
EGADS : 15 -28 23 25 -30
EGADS : 16 27 29 30
EGADS : 17 -31 -32 33 34
EGADS : 18 -35 -34 36 32
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 4 -3 -2
EGADS : 2 Yes 3 7 -6 -5
EGADS : 3 Yes 6 9 -1 -8
EGADS : 4 Yes -4 -9 -7
EGADS : 5 Yes -10 2 11 -12
EGADS : 6 Yes -11 5 13 -14
EGADS : 7 Yes -13 8 10 -15
EGADS : 8 Yes 12 14 15
EGADS : 9 Yes 16 19 -18 -17
EGADS : 10 Yes 18 22 -21 -20
EGADS : 11 Yes 21 24 -16 -23
EGADS : 12 Yes -19 -24 -22
EGADS : 13 Yes -25 17 26 -27
EGADS : 14 Yes -26 20 28 -29
EGADS : 15 Yes -28 23 25 -30
EGADS : 16 Yes 27 29 30
EGADS : 17 Yes -31 -32 33 34
EGADS : 18 Yes -35 -34 36 32
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 5
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 4
EGADS : 5 0 Yes 3 5 1 2 6
EGADS : 6 0 Yes 5 6 1 2 3
EGADS : 7 0 Yes 4 6 1 2 4
EGADS : 8 0 Yes 5 1 1 3 7
EGADS : 9 0 Yes 6 2 1 3 4
EGADS : 10 0 Yes 1 7 1 5 7
EGADS : 11 0 Yes 3 8 1 5 6
EGADS : 12 0 Yes 7 8 1 5 8
EGADS : 13 0 Yes 5 9 1 6 7
EGADS : 14 0 Yes 8 9 1 6 8
EGADS : 15 0 Yes 9 7 1 7 8
EGADS : 16 1 Yes 10 11 1 9 11
EGADS : 17 1 Yes 10 12 1 9 13
EGADS : 18 1 Yes 12 13 1 9 10
EGADS : 19 1 Yes 11 13 1 9 12
EGADS : 20 1 Yes 12 14 1 10 14
EGADS : 21 1 Yes 14 15 1 10 11
EGADS : 22 1 Yes 13 15 1 10 12
EGADS : 23 1 Yes 14 10 1 11 15
EGADS : 24 1 Yes 15 11 1 11 12
EGADS : 25 1 Yes 10 16 1 13 15
EGADS : 26 1 Yes 12 17 1 13 14
EGADS : 27 1 Yes 16 17 1 13 16
EGADS : 28 1 Yes 14 18 1 14 15
EGADS : 29 1 Yes 17 18 1 14 16
EGADS : 30 1 Yes 18 16 1 15 16
EGADS : 31 2 DEGEN 19 19 - 17
EGADS : 32 2 Yes 20 19 NA 17 18
EGADS : 33 2 DEGEN 20 20 - 17
EGADS : 34 2 Yes 20 19 NA 17 18
EGADS : 35 2 DEGEN 19 19 - 18
EGADS : 36 2 DEGEN 20 20 - 18
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 3.77246052 0 0.00459131419
EGADS : 2 Yes 5.90487498 7.07106781 0
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 4.0824829 7.07106781 0.123425948
EGADS : 5 Yes 3.77001182 0 0
EGADS : 6 Yes 5.90282524 7.07106781 0
EGADS : 7 Yes 5.90487498 0 0
EGADS : 8 Yes 4.0824829 0 0.123425948
EGADS : 9 Yes 5.90282524 0 0
EGADS : 10 Yes 15.2802204 0 0.00183652568
EGADS : 11 Yes 16.1331862 2.82842712 0
EGADS : 12 Yes 13.7712362 0 0
EGADS : 13 Yes 15.4042293 2.82842712 0.0493703791
EGADS : 14 Yes 15.2792409 0 0
EGADS : 15 Yes 16.1323663 2.82842712 0
EGADS : 16 Yes 16.1331862 0 0
EGADS : 17 Yes 15.4042293 0 0.0493703791
EGADS : 18 Yes 16.1323663 0 0
EGADS : 19 Yes 0 0 80
EGADS : 20 Yes 0 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 160
AFLR4 : Min Bounding Box Length = 160
AFLR4 : Max Ref Bounding Box Length = 16.1372
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 0.890888
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 14.7419
AFLR4 : Abs Min Surf Spacing = 0.00222722
AFLR4 : Min Surf Spacing = 0.00445444
AFLR4 : Max Surf Spacing = 0.0890888
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 STD
AFLR4 : 12 CAD geometry 0 STD
AFLR4 : 13 CAD geometry 0 STD
AFLR4 : 14 CAD geometry 0 STD
AFLR4 : 15 CAD geometry 0 STD
AFLR4 : 16 CAD geometry 0 STD
AFLR4 : 17 CAD geometry 0 FARFIELD
AFLR4 : 18 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 11696
AFLR43 : Nodes = 5854
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 5854 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 Solid
UG3 : 12 Solid
UG3 : 13 Solid
UG3 : 14 Solid
UG3 : 15 Solid
UG3 : 16 Solid
UG3 : 17 FarField
UG3 : 18 FarField
AFLR3 : CPU Time = 0.016 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 5854 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1172 6979
AFLR3 IG : Nodes, Elements = 2344 15144
AFLR3 IG : Nodes, Elements = 3516 23433
AFLR3 IG : Nodes, Elements = 4688 31724
AFLR3 IG : Nodes, Elements = 5860 39971
AFLR3 IG : Nodes, Elements = 5861 39980
AFLR3 IG : Nodes, Elements = 5861 39927
AFLR3 IG : Nodes, Elements = 5861 39954
AFLR3 IG : Nodes, Elements = 5861 39928
AFLR3 IG : Nodes, Elements = 5854 23732
AFLR3 IG : Nodes, Elements = 5854 23747
AFLR3 IG : Nodes, Elements = 5854 19617
AFLR3 IG : Nodes, Elements = 5854 17611
AFLR3 : CPU Time = 0.165 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 5854 17611
AFLR3 GG : Nodes, Elements = 8532 25853
AFLR3 GG : Nodes, Elements = 8532 37006
AFLR3 GG : Nodes, Elements = 8532 34255
AFLR3 GG : Nodes, Elements = 8532 32797
AFLR3 GG : Nodes, Elements = 10906 40277
AFLR3 GG : Nodes, Elements = 10906 50546
AFLR3 GG : Nodes, Elements = 10906 47482
AFLR3 GG : Nodes, Elements = 10906 46581
AFLR3 GG : Nodes, Elements = 13450 54531
AFLR3 GG : Nodes, Elements = 13450 65541
AFLR3 GG : Nodes, Elements = 13450 62498
AFLR3 GG : Nodes, Elements = 13450 61609
AFLR3 GG : Nodes, Elements = 16238 70196
AFLR3 GG : Nodes, Elements = 16238 82337
AFLR3 GG : Nodes, Elements = 16238 78892
AFLR3 GG : Nodes, Elements = 16238 78137
AFLR3 GG : Nodes, Elements = 19188 87158
AFLR3 GG : Nodes, Elements = 19188 99776
AFLR3 GG : Nodes, Elements = 19188 96365
AFLR3 GG : Nodes, Elements = 19188 95572
AFLR3 GG : Nodes, Elements = 22304 105061
AFLR3 GG : Nodes, Elements = 22304 118271
AFLR3 GG : Nodes, Elements = 22304 114811
AFLR3 GG : Nodes, Elements = 22304 114030
AFLR3 GG : Nodes, Elements = 25475 123681
AFLR3 GG : Nodes, Elements = 25475 137067
AFLR3 GG : Nodes, Elements = 25475 133537
AFLR3 GG : Nodes, Elements = 25475 132780
AFLR3 GG : Nodes, Elements = 28675 142487
AFLR3 GG : Nodes, Elements = 28675 156012
AFLR3 GG : Nodes, Elements = 28675 152457
AFLR3 GG : Nodes, Elements = 28675 151739
AFLR3 GG : Nodes, Elements = 31934 161625
AFLR3 GG : Nodes, Elements = 31934 175349
AFLR3 GG : Nodes, Elements = 31934 171839
AFLR3 GG : Nodes, Elements = 31934 171106
AFLR3 GG : Nodes, Elements = 35163 180863
AFLR3 GG : Nodes, Elements = 35163 194576
AFLR3 GG : Nodes, Elements = 35163 190963
AFLR3 GG : Nodes, Elements = 35163 190274
AFLR3 GG : Nodes, Elements = 38336 199857
AFLR3 GG : Nodes, Elements = 38336 213429
AFLR3 GG : Nodes, Elements = 38336 209909
AFLR3 GG : Nodes, Elements = 38336 209231
AFLR3 GG : Nodes, Elements = 41434 218581
AFLR3 GG : Nodes, Elements = 41434 231715
AFLR3 GG : Nodes, Elements = 41434 228240
AFLR3 GG : Nodes, Elements = 41434 227631
AFLR3 GG : Nodes, Elements = 44440 236679
AFLR3 GG : Nodes, Elements = 44440 249363
AFLR3 GG : Nodes, Elements = 44440 246132
AFLR3 GG : Nodes, Elements = 44440 245533
AFLR3 GG : Nodes, Elements = 47347 254281
AFLR3 GG : Nodes, Elements = 47347 266689
AFLR3 GG : Nodes, Elements = 47347 263399
AFLR3 GG : Nodes, Elements = 47347 262800
AFLR3 GG : Nodes, Elements = 50173 271299
AFLR3 GG : Nodes, Elements = 50173 283107
AFLR3 GG : Nodes, Elements = 50173 280170
AFLR3 GG : Nodes, Elements = 50173 279671
AFLR3 GG : Nodes, Elements = 52815 287608
AFLR3 GG : Nodes, Elements = 52815 298804
AFLR3 GG : Nodes, Elements = 52815 295916
AFLR3 GG : Nodes, Elements = 52815 295442
AFLR3 GG : Nodes, Elements = 55304 302914
AFLR3 GG : Nodes, Elements = 55304 313461
AFLR3 GG : Nodes, Elements = 55304 310793
AFLR3 GG : Nodes, Elements = 55304 310363
AFLR3 GG : Nodes, Elements = 57635 317360
AFLR3 GG : Nodes, Elements = 57635 327233
AFLR3 GG : Nodes, Elements = 57635 324637
AFLR3 GG : Nodes, Elements = 57635 324280
AFLR3 GG : Nodes, Elements = 59724 330549
AFLR3 GG : Nodes, Elements = 59724 339298
AFLR3 GG : Nodes, Elements = 59724 337038
AFLR3 GG : Nodes, Elements = 59724 336752
AFLR3 GG : Nodes, Elements = 61562 342268
AFLR3 GG : Nodes, Elements = 61562 349934
AFLR3 GG : Nodes, Elements = 61562 347979
AFLR3 GG : Nodes, Elements = 61562 347773
AFLR3 GG : Nodes, Elements = 63109 352415
AFLR3 GG : Nodes, Elements = 63109 359035
AFLR3 GG : Nodes, Elements = 63109 357272
AFLR3 GG : Nodes, Elements = 63109 357093
AFLR3 GG : Nodes, Elements = 64355 360832
AFLR3 GG : Nodes, Elements = 64355 366080
AFLR3 GG : Nodes, Elements = 64355 364756
AFLR3 GG : Nodes, Elements = 64355 364628
AFLR3 GG : Nodes, Elements = 65290 367433
AFLR3 GG : Nodes, Elements = 65290 371353
AFLR3 GG : Nodes, Elements = 65290 370306
AFLR3 GG : Nodes, Elements = 65290 370196
AFLR3 GG : Nodes, Elements = 65976 372254
AFLR3 GG : Nodes, Elements = 65976 375192
AFLR3 GG : Nodes, Elements = 65976 374355
AFLR3 GG : Nodes, Elements = 65976 374298
AFLR3 GG : Nodes, Elements = 66420 375633
AFLR3 GG : Nodes, Elements = 66420 377500
AFLR3 GG : Nodes, Elements = 66420 376965
AFLR3 GG : Nodes, Elements = 66420 376924
AFLR3 GG : Nodes, Elements = 66661 377647
AFLR3 GG : Nodes, Elements = 66661 378639
AFLR3 GG : Nodes, Elements = 66661 378364
AFLR3 GG : Nodes, Elements = 66661 378356
AFLR3 GG : Nodes, Elements = 66797 378764
AFLR3 GG : Nodes, Elements = 66797 379340
AFLR3 GG : Nodes, Elements = 66797 379179
AFLR3 GG : Nodes, Elements = 66797 379161
AFLR3 GG : Nodes, Elements = 66849 379317
AFLR3 GG : Nodes, Elements = 66849 379528
AFLR3 GG : Nodes, Elements = 66849 379462
AFLR3 GG : Nodes, Elements = 66849 379457
AFLR3 GG : Nodes, Elements = 66871 379523
AFLR3 GG : Nodes, Elements = 66871 379611
AFLR3 GG : Nodes, Elements = 66871 379589
AFLR3 GG : Nodes, Elements = 66871 379590
AFLR3 GG : Nodes, Elements = 66876 379605
AFLR3 GG : Nodes, Elements = 66876 379619
AFLR3 GG : Nodes, Elements = 66876 379616
AFLR3 GG : Nodes, Elements = 66877 379619
AFLR3 GG : Nodes, Elements = 66877 379623
AFLR3 GG : Nodes, Elements = 66877 379622
AFLR3 GG : Nodes, Elements = 66916 379739
AFLR3 GG : Nodes, Elements = 66916 379896
AFLR3 GG : Nodes, Elements = 66916 379848
AFLR3 GG : Nodes, Elements = 66916 379839
AFLR3 GG : Nodes, Elements = 66927 379872
AFLR3 GG : Nodes, Elements = 66927 379912
AFLR3 GG : Nodes, Elements = 66927 379900
AFLR3 GG : Nodes, Elements = 66930 379909
AFLR3 GG : Nodes, Elements = 66930 379922
AFLR3 GG : Nodes, Elements = 66930 379916
AFLR3 GG : Nodes, Elements = 66933 379925
AFLR3 GG : Nodes, Elements = 66933 379935
AFLR3 GG : Nodes, Elements = 66933 379933
AFLR3 GG : Nodes, Elements = 66936 379942
AFLR3 GG : Nodes, Elements = 66936 379954
AFLR3 GG : Nodes, Elements = 66936 379950
AFLR3 GG : Nodes, Elements = 66937 379953
AFLR3 GG : Nodes, Elements = 66937 379956
AFLR3 GG : Nodes, Elements = 66937 379955
AFLR3 : CPU Time = 6.356 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 66937 379955
AFLR3 QI : Nodes, Elements = 65603 372405
AFLR3 QI : Nodes, Elements = 65393 371215
AFLR3 QI : Nodes, Elements = 65367 371065
AFLR3 QI : Nodes, Elements = 65361 371028
AFLR3 QI : Nodes, Elements = 65360 371022
AFLR3 QI : Nodes, Elements = 65360 374533
AFLR3 QI : Nodes, Elements = 65360 370824
AFLR3 QI : Nodes, Elements = 65360 370404
AFLR3 QI : Nodes, Elements = 65360 372792
AFLR3 QI : Nodes, Elements = 65360 370439
AFLR3 QI : Nodes, Elements = 65360 370349
AFLR3 QI : Nodes, Elements = 65360 372662
AFLR3 QI : Nodes, Elements = 65360 370400
AFLR3 QI : Nodes, Elements = 65360 370340
AFLR3 QI : Nodes, Elements = 65360 372613
AFLR3 QI : Nodes, Elements = 65360 370385
AFLR3 QI : Nodes, Elements = 65360 370331
AFLR3 QI : Nodes, Elements = 65360 372584
AFLR3 QI : Nodes, Elements = 65360 370375
AFLR3 QI : Nodes, Elements = 65360 370325
AFLR3 QI : Nodes, Elements = 65370 370371
AFLR3 QI : Nodes, Elements = 65370 372641
AFLR3 QI : Nodes, Elements = 65370 370426
AFLR3 QI : Nodes, Elements = 65370 370384
AFLR3 QI : Nodes, Elements = 65370 372133
AFLR3 QI : Nodes, Elements = 65370 370386
AFLR3 QI : Nodes, Elements = 65370 370317
AFLR3 QI : Nodes, Elements = 65370 370371
AFLR3 : CPU Time = 3.054 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 65370 370371
AFLR3 QRG: Nodes, Elements = 65396 370514
AFLR3 QRG: Nodes, Elements = 65401 370544
AFLR3 QRG: Nodes, Elements = 65401 370543
AFLR3 QRG: Nodes, Elements = 65400 370538
AFLR3 QRG: Nodes, Elements = 65402 370551
AFLR3 : CPU Time = 0.077 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 370551
UG3 : Min, Max Ang = 0.928 177.4
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 154
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 370551
UG3 : Min Vol = 6.85e-10
UG3 : Average Vol = 5.73
UG3 : Total-Tet-Vol = 2.12e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 370551
UG3 : Min, Max Q = 0.0696 1
UG3 : Average Q = 0.846
UG3 : No. Q< 0.1 = 32
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 10.334 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 370551
UG3 : Min, Max Ang = 0.928 177.4
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 154
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 370551
UG3 : Min Vol = 6.85e-10
UG3 : Average Vol = 5.73
UG3 : Total-Tet-Vol = 2.12e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 370551
UG3 : Min, Max Q = 0.0986 1
UG3 : Average Q = 0.838
UG3 : No. Q< 0.1 = 1
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
Number of nodes = 65402
Number of elements = 382247
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 370551
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 65402
Number of elements = 382247
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 370551
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 65402
Number of elements = 382247
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 370551
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 1
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
ok
test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 65402
Number of elements = 382247
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 370551
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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)
110333E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
110333E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000AC77000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000AC77000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes = 294
Number of elements = 584
Number of triangle elements = 584
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes = 2048
Number of elements = 4096
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes = 152
Number of elements = 300
Number of triangle elements = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes = 624
Number of elements = 1248
Number of triangle elements = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4192
Total number of elements = 8364
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 294, elements - 584
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 294, elements - 584
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4192, elements - 8364
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 374
Number of elements = 744
Number of triangle elements = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 472
Total number of elements = 936
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 386
Number of elements = 768
Number of triangle elements = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 351
Number of elements = 698
Number of triangle elements = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 491
Total number of elements = 970
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 376
Number of elements = 748
Number of triangle elements = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 454
Total number of elements = 896
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 126
Number of elements = 252
Number of triangle elements = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 109
Number of elements = 214
Number of triangle elements = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 48
Number of elements = 96
Number of triangle elements = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 12
Number of elements = 20
Number of triangle elements = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 169
Total number of elements = 330
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 536
Number of elements = 1072
Number of triangle elements = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 544
Number of elements = 1084
Number of triangle elements = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes = 1351
Number of elements = 2682
Number of triangle elements = 2682
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 288
Number of elements = 572
Number of triangle elements = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 174
Number of elements = 344
Number of triangle elements = 344
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 26
Number of elements = 48
Number of triangle elements = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 482
Number of elements = 960
Number of triangle elements = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 174, elements - 344
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 174, elements - 344
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 444
Number of elements = 884
Number of triangle elements = 884
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 522
Number of elements = 1044
Number of triangle elements = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 966
Total number of elements = 1928
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 444, elements - 884
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 444, elements - 884
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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!
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 = 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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!
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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!
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 - 5924, elements - 11840
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 7173
Number of elements = 14338
Number of triangle elements = 14338
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7173
Total number of elements = 14338
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!
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 - 7173, elements - 14338
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_Cl (test_xfoil.Testxfoil_Parsec.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Parsec.test_alpha_custom_increment) ... ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1220
Number of elements = 2680
Number of triangle elements = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1221
Total number of elements = 2680
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1220
Number of elements = 2680
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 2680
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 1221
Combined Number of elements = 2681
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 2680
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 6
Property name - Rib_Root
Property name - Rib_Root_Point
Property name - Ribs
Property name - Skin
Property name - Spar1
Property name - Spar2
Done getting FEA properties
Updating mesh element types based on properties input
'Smart_Restart' is ON
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting vortex lattice control surface data
VLM control surface name - CntrlLE
VLM control surface name - CntrlTE
Done getting vortex lattice control surface data
Getting FEA vortex lattice mesh
Getting ZAERO UAIC Configurations.......
Number of UAIC Configurations - 2
UAIC Configuration: climb, id = 1
- Mach Number : 0.200000
- Reduced Freq: [0.020000, ... , 0.250000]
UAIC Configuration: cruise, id = 2
- Mach Number : 0.700000
- Reduced Freq: [0.040000, ... , 0.350000]
Getting ZAERO Analysis Subcases.......
Number of Analysis Subcases - 2
Analysis Subcase: FlutterCruise, id = 1
- Discipline : flutter
- UAIC : cruise
Analysis Subcase: Trim, id = 2
- Discipline : Trim
- UAIC : climb
Getting ZAERO Trim Variables.......
Number of Trim Variables - 2
Trim Variable: ANGLEA
- Label : ALPHA
- Value : free
Trim Variable: URDD3
- Label : NZ
- Value : 1.0
Updating StaticAeroelastic subcase: Trim
- vectorToCG -> [0.345898, 1.652951, -0.041403]
- weight -> 476456.149985
- weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813290, 6179.981375, 19723.152207, 370546.335523]
ok
----------------------------------------------------------------------
Ran 154 tests in 951.081s
OK (skipped=15)
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest
+ ./execute_CTestRegression.sh
No options provided...defaulting to ALL
Running.... MINIMAL c-Tests
Running.... LINEARAERO c-Tests
=================================================
+ echo './avlTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./avlTest test;
+ ./avlTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
Attention: avlTest is hard coded to look for ../csmData/avlWingTail.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
VLM control surface name - WingRightLE
VLM control surface name - WingRightTE
VLM control surface name - Tail
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vertical_Tail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Writing surface - Vertical_Tail (ID = 1)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Running AVL!
Value of Cltot = 0.619913
StripForces
Wing = {"Xle":[1.565221892029e+00,1.512117367810e+00,1.409527304938e+00,1.264443046659e+00,1.086751845411e+00,8.885630629098e-01,6.833829371601e-01,4.851941546545e-01,3.075029533974e-01,1.624186951053e-01,5.982863221714e-02,6.724107980270e-03,6.724107971058e-03,5.982863219013e-02,1.624186950623e-01,3.075029533414e-01,4.851941545893e-01,6.833829370902e-01,8.885630628399e-01,1.086751845346e+00,1.264443046603e+00,1.409527304895e+00,1.512117367783e+00,1.565221892020e+00],"Yle":[-3.856416046770e+00,-3.725576361740e+00,-3.472813499993e+00,-3.115352832843e+00,-2.677554714026e+00,-2.189254361841e+00,-1.683728638332e+00,-1.195428286135e+00,-7.576301672945e-01,-4.001695001132e-01,-1.474066383261e-01,-1.656695325269e-02,1.656695322999e-02,1.474066382596e-01,4.001695000074e-01,7.576301671565e-01,1.195428285974e+00,1.683728638159e+00,2.189254361668e+00,2.677554713865e+00,3.115352832706e+00,3.472813499887e+00,3.725576361674e+00,3.856416046747e+00],"Zle":[2.486597711706e-01,2.402232939480e-01,2.239252714835e-01,2.008763870743e-01,1.726473841027e-01,1.411620224705e-01,1.085659775407e-01,7.708061590764e-02,4.885161293456e-02,2.580272852328e-02,9.504706056265e-03,1.068228830823e-03,1.068228829360e-03,9.504706051974e-03,2.580272851645e-02,4.885161292566e-02,7.708061589728e-02,1.085659775295e-01,1.411620224593e-01,1.726473840924e-01,2.008763870654e-01,2.239252714767e-01,2.402232939437e-01,2.486597711692e-01],"Chord":[9.710071581587e-01,9.928137666999e-01,1.034940899447e+00,1.094517661923e+00,1.167483996219e+00,1.248867367237e+00,1.333121632734e+00,1.414505003754e+00,1.487471338054e+00,1.547048100535e+00,1.589175233289e+00,1.610981841837e+00,1.610981841841e+00,1.589175233300e+00,1.547048100553e+00,1.487471338077e+00,1.414505003781e+00,1.333121632763e+00,1.248867367266e+00,1.167483996246e+00,1.094517661946e+00,1.034940899465e+00,9.928137667110e-01,9.710071581625e-01],"Area":[6.420432739224e-02,1.924649501823e-01,3.191588402418e-01,4.398794051499e-01,5.463997379092e-01,6.272332670617e-01,6.695492724342e-01,6.620092145623e-01,5.978048871833e-01,4.770843222898e-01,3.080744268775e-01,1.065203328294e-01,1.065203327570e-01,3.080744268129e-01,4.770843222394e-01,5.978048871514e-01,6.620092145502e-01,6.695492724407e-01,6.272332670835e-01,5.463997379421e-01,4.398794051895e-01,3.191588402846e-01,1.924649502262e-01,6.420432743628e-02],"c_cl":[1.751976980131e-01,4.816388142980e-01,7.134545983425e-01,8.955798774854e-01,1.045275116632e+00,1.165642609066e+00,1.251488483106e+00,1.294909342036e+00,1.290147495293e+00,1.237589733955e+00,1.147354354590e+00,1.069716379938e+00,1.027204841580e+00,9.123069911140e-01,8.271224835189e-01,7.465072383829e-01,6.622506856527e-01,5.718077594720e-01,4.773770050905e-01,3.839108464455e-01,2.965810831880e-01,2.166269422082e-01,1.372747954618e-01,4.847522879861e-02],"ai":[2.423376448062e-01,1.891573605670e-01,1.387726073610e-01,1.136377561111e-01,1.056109957988e-01,1.077519869781e-01,1.163918473304e-01,1.297918603655e-01,1.465983278745e-01,1.624995174599e-01,1.707158095744e-01,1.656351191924e-01,-7.833998870069e-02,-4.190817556549e-02,-1.699095118252e-02,-7.589503463268e-04,7.958849673323e-03,1.019416065192e-02,8.688915578662e-03,6.053380335362e-03,5.120395027030e-03,9.296755297867e-03,2.004804046071e-02,3.330492577589e-02],"cl_norm":[2.044051829732e-01,5.494672225944e-01,7.808579037671e-01,9.268407130709e-01,1.014078158136e+00,1.057019341176e+00,1.062951411332e+00,1.036333388588e+00,9.816462634657e-01,9.051794884122e-01,8.167547094734e-01,7.499676468301e-01,7.211772113982e-01,6.503467495440e-01,6.057660560789e-01,5.686988847409e-01,5.305932247986e-01,4.861412346272e-01,4.332732553839e-01,3.727603475171e-01,3.071901673660e-01,2.373206031159e-01,1.568074209169e-01,5.666485024198e-02],"cl":[1.803741931756e-01,4.848688546459e-01,6.890559834545e-01,8.178762563197e-01,8.948575908404e-01,9.327503738523e-01,9.379850374388e-01,9.144963748400e-01,8.662385668551e-01,7.987616435483e-01,7.207325646090e-01,6.617973538495e-01,6.363916792640e-01,5.738884333905e-01,5.345488897546e-01,5.018395375447e-01,4.682137871232e-01,4.289878157188e-01,3.823352848870e-01,3.289366049983e-01,2.710752133784e-01,2.094198967381e-01,1.383722840117e-01,5.000302093687e-02],"cd":[4.708816796028e-03,1.893013552461e-02,2.388458719217e-02,2.809788812561e-02,3.450496926232e-02,4.310977683936e-02,5.296690620750e-02,6.273588035908e-02,7.092746653695e-02,7.623132904850e-02,7.793919402374e-02,1.330641046361e-01,7.642533954139e-02,1.575280561795e-02,1.020926164300e-02,5.734996040044e-03,2.453990236882e-03,7.034156944392e-05,-1.681061755697e-03,-2.904871637688e-03,-3.696799546922e-03,-4.291551637882e-03,-4.755989795808e-03,-4.178738547375e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-6.175122770636e-02,-1.541367450249e-01,-1.990020049078e-01,-2.179523703798e-01,-2.259241556000e-01,-2.291785023832e-01,-2.301045091168e-01,-2.293937884749e-01,-2.266765134794e-01,-2.205756980543e-01,-2.089282623641e-01,-1.947906406100e-01,-1.847119741766e-01,-1.559354818193e-01,-1.355315131375e-01,-1.232795365876e-01,-1.170486694971e-01,-1.141869860843e-01,-1.128288355904e-01,-1.117855412669e-01,-1.094863434133e-01,-1.016126232940e-01,-7.889656776611e-02,-3.215621313961e-02],"cm_LE":[-9.907391078332e-02,-2.553625521061e-01,-3.443180862961e-01,-3.917771248736e-01,-4.170475207536e-01,-4.288879437378e-01,-4.309998082914e-01,-4.249313258859e-01,-4.112512348868e-01,-3.899661415022e-01,-3.610798550199e-01,-3.345295675168e-01,-3.190696575594e-01,-2.776668920570e-01,-2.496150543393e-01,-2.306580335187e-01,-2.170714278267e-01,-2.053105443164e-01,-1.932221818518e-01,-1.798625218874e-01,-1.643057066258e-01,-1.427050164900e-01,-1.051753523064e-01,-4.137433282282e-02],"C.P.x/c":[5.923506801011e-01,5.678936810397e-01,5.388038268097e-01,5.164857534324e-01,5.024693961503e-01,4.957018606561e-01,4.953178888067e-01,5.008416597223e-01,5.116790825907e-01,5.261470832205e-01,5.398832002650e-01,5.443357803971e-01,5.402488831882e-01,5.217174153486e-01,5.035437183300e-01,4.956552889212e-01,4.999897967897e-01,5.161776906017e-01,5.451044281036e-01,5.898391652626e-01,6.538965497759e-01,7.352099770687e-01,8.201760893058e-01,8.930854083838e-01]}
Vertical_Tail = {"Xle":[5.481142821257e+00,5.457739875756e+00,5.413224828118e+00,5.351955121359e+00,5.279928261269e+00,5.204194738752e+00,5.132167878660e+00,5.070898171897e+00,5.026383124254e+00,5.002980178746e+00],"Yle":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"Zle":[1.462285642514e+00,1.415479751513e+00,1.326449656236e+00,1.203910242719e+00,1.059856522538e+00,9.083894775049e-01,7.643357573198e-01,6.417963437947e-01,5.527662485071e-01,5.059603574925e-01],"Chord":[7.291641787429e-01,7.525671242437e-01,7.970821718820e-01,8.583518786405e-01,9.303787387310e-01,1.006112261248e+00,1.078139121340e+00,1.139408828103e+00,1.183923875746e+00,1.207326821254e+00],"Area":[1.727730179136e-02,5.174997687051e-02,8.537019049526e-02,1.158415604078e-01,1.391867381176e-01,1.505166423044e-01,1.455036346588e-01,1.220345306258e-01,8.141205112924e-02,2.860720599220e-02],"c_cl":[4.143502484418e-02,1.146121890397e-01,1.669674480704e-01,2.000258625574e-01,2.165069436647e-01,2.173612378313e-01,2.020982864238e-01,1.687203348324e-01,1.143884794128e-01,4.073751989356e-02],"ai":[2.065296924524e-01,1.849180223915e-01,1.591285664757e-01,1.456224964407e-01,1.435231644006e-01,1.506386553619e-01,1.666466052405e-01,1.914179167692e-01,2.193221173426e-01,2.365321328628e-01],"cl_norm":[6.579957348175e-02,1.763463053600e-01,2.425545992661e-01,2.698370559984e-01,2.694590983036e-01,2.501591871286e-01,2.170544160378e-01,1.714623014102e-01,1.118766125248e-01,3.907064104103e-02],"cl":[5.682537081788e-02,1.522949719002e-01,2.094733190132e-01,2.330348048801e-01,2.327083956798e-01,2.160407403860e-01,1.874510278160e-01,1.480770823176e-01,9.661810337317e-02,3.374191575671e-02],"cd":[4.670566079259e-03,1.374698956983e-02,1.845844898550e-02,2.032218684722e-02,2.072187092669e-02,2.023884851594e-02,1.896705322928e-02,1.657142171116e-02,1.222733795464e-02,5.106244760906e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-3.303465544546e-02,-8.761746958841e-02,-1.194746602282e-01,-1.341488123562e-01,-1.380350789961e-01,-1.339349413679e-01,-1.218867053323e-01,-1.002593790934e-01,-6.716156843018e-02,-2.373448304332e-02],"cm_LE":[-4.232877133358e-02,-1.126299441676e-01,-1.539951982649e-01,-1.724118490115e-01,-1.757829360722e-01,-1.683239687782e-01,-1.510824211715e-01,-1.228726806386e-01,-8.171902803714e-02,-2.878672165371e-02],"C.P.x/c":[8.313363814436e-01,8.253142634666e-01,8.203574125382e-01,8.256599853196e-01,8.431675932571e-01,8.699522420103e-01,9.002322593393e-01,9.270755982235e-01,9.451240614896e-01,9.534124326092e-01]}
real 0m0.719s
user 0m0.401s
sys 0m0.211s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./avlTest passed (as expected)
=============================================
=================================================
+ echo './msesTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./msesTest test;
+ ./msesTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm
Value of CL = 0.276892
real 0m2.056s
user 0m1.833s
sys 0m0.146s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./msesTest passed (as expected)
=============================================
=================================================
+ echo './frictionTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./frictionTest test;
+ ./frictionTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
Attention: frictionTest is hard coded to look for ../csmData/frictionWingTailFuselage.csm
To not make system calls to the friction executable the second command line option may be supplied - 0 = no analysis , >0 run analysis (default).
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Running FRICTION!
Value of CDfric = 0.009900
Value of CDfric = 0.009190
real 0m0.514s
user 0m0.138s
sys 0m0.067s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./frictionTest passed (as expected)
=============================================
Running.... MESH c-Tests
Running.... CFD c-Tests
=================================================
+ echo './fun3dAFLR2Test test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dAFLR2Test test;
+ ./fun3dAFLR2Test 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
Attention: fun3dAFLR2Test is hard coded to look for ../csmData/cfd2D.csm
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)
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mquad = 1
UG PARAM : mpp = 3
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 841 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 841 841
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 168 338
AFLR2 IG : Nodes, Faces = 336 674
AFLR2 IG : Nodes, Faces = 504 1010
AFLR2 IG : Nodes, Faces = 617 1236
AFLR2 IG : Nodes, Faces = 672 1346
AFLR2 IG : Nodes, Faces = 741 1484
AFLR2 IG : Nodes, Faces = 803 1608
AFLR2 IG : Nodes, Faces = 840 1682
AFLR2 IG : Nodes, Faces = 841 1684
AFLR2 IG : Nodes, Faces = 845 1684
AFLR2 IG : Nodes, Faces = 841 841
AFLR2 : CPU Time = 0.006 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 841 841
AFLR2 GGp: Nodes, Faces = 1648 2455
AFLR2 GGp: Nodes, Faces = 2446 4051
AFLR2 GGp: Nodes, Faces = 3257 5673
AFLR2 GGp: Nodes, Faces = 4054 7267
AFLR2 GGp: Nodes, Faces = 4821 8801
AFLR2 GGp: Nodes, Faces = 5577 10313
AFLR2 GGp: Nodes, Faces = 6325 11809
AFLR2 GGp: Nodes, Faces = 7053 13265
AFLR2 GGp: Nodes, Faces = 7732 14623
AFLR2 GGp: Nodes, Faces = 8394 15947
AFLR2 GGp: Nodes, Faces = 9022 17203
AFLR2 GGp: Nodes, Faces = 9620 18399
AFLR2 GGp: Nodes, Faces = 10176 19511
AFLR2 GGp: Nodes, Faces = 10689 20537
AFLR2 GGp: Nodes, Faces = 11181 21521
AFLR2 GGp: Nodes, Faces = 11646 22451
AFLR2 GGp: Nodes, Faces = 12098 23355
AFLR2 GGp: Nodes, Faces = 12529 24217
AFLR2 GGp: Nodes, Faces = 12943 25045
AFLR2 GGp: Nodes, Faces = 13331 25821
AFLR2 GGp: Nodes, Faces = 13710 26579
AFLR2 GGp: Nodes, Faces = 14061 27281
AFLR2 GGp: Nodes, Faces = 14424 28007
AFLR2 GGp: Nodes, Faces = 14774 28707
AFLR2 GGp: Nodes, Faces = 15107 29373
AFLR2 GGp: Nodes, Faces = 15422 30003
AFLR2 GGp: Nodes, Faces = 15707 30573
AFLR2 GGp: Nodes, Faces = 15982 31123
AFLR2 GGp: Nodes, Faces = 16233 31625
AFLR2 GGp: Nodes, Faces = 16473 32105
AFLR2 GGp: Nodes, Faces = 16685 32529
AFLR2 GGp: Nodes, Faces = 16898 32955
AFLR2 GGp: Nodes, Faces = 17104 33367
AFLR2 GGp: Nodes, Faces = 17291 33741
AFLR2 GGp: Nodes, Faces = 17468 34095
AFLR2 GGp: Nodes, Faces = 17627 34413
AFLR2 GGp: Nodes, Faces = 17781 34721
AFLR2 GGp: Nodes, Faces = 17929 35017
AFLR2 GGp: Nodes, Faces = 18060 35279
AFLR2 GGp: Nodes, Faces = 18186 35531
AFLR2 GGp: Nodes, Faces = 18292 35743
AFLR2 GGp: Nodes, Faces = 18403 35965
AFLR2 GGp: Nodes, Faces = 18499 36157
AFLR2 GGp: Nodes, Faces = 18568 36295
AFLR2 GGp: Nodes, Faces = 18603 36365
AFLR2 GGp: Nodes, Faces = 18615 36389
AFLR2 : CPU Time = 0.077 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 18615 36389
AFLR2 QI : Nodes, Faces = 18608 1893
AFLR2 QI : Nodes, Faces = 18608 17241
AFLR2 QI : Nodes, Faces = 18608 36375
AFLR2 QI : Nodes, Faces = 18606 1789
AFLR2 QI : Nodes, Faces = 18606 17291
AFLR2 QI : Nodes, Faces = 18606 36371
AFLR2 QI : Nodes, Faces = 18604 1971
AFLR2 QI : Nodes, Faces = 18604 17198
AFLR2 QI : Nodes, Faces = 18604 36367
AFLR2 QI : Nodes, Faces = 18604 2161
AFLR2 QI : Nodes, Faces = 18604 17103
AFLR2 QI : Nodes, Faces = 18604 36367
AFLR2 QI : Nodes, Faces = 18604 2149
AFLR2 QI : Nodes, Faces = 18604 17109
AFLR2 QI : Nodes, Faces = 18604 2149
AFLR2 QI : Nodes, Faces = 18604 17109
AFLR2 : CPU Time = 0.037 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 18604
Number of elements = 20099
Number of tris = 2149
Number of quad = 17109
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - TunnelWall
Boundary condition name - InFlow
Boundary condition name - OutFlow
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Creating a 3D volume mesh from a 2D surface
Number of Nodes = 37208
Number of Prisms = 2149
Number of Hexahedral = 17109
Writing AFLR3 file ....
Finished writing AFLR3 file
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.
NOT Running fun3d!
real 0m1.321s
user 0m1.132s
sys 0m0.327s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./fun3dAFLR2Test passed (as expected)
=============================================
=================================================
+ echo './fun3dTetgenTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dTetgenTest test;
+ ./fun3dTetgenTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
Attention: fun3dTetgenTest is hard coded to look for ../csmData/cfdMultiBody.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 9618
Number of elements = 19232
Number of triangle elements = 19232
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 6142
Number of elements = 12280
Number of triangle elements = 12280
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 267
Number of elements = 530
Number of triangle elements = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 16027
Total number of elements = 32042
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 - 16027, elements - 32042
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.185406
Creating surface mesh ...
Surface mesh seconds: 0.046354
Recovering boundaries...
Boundary recovery seconds: 0.150763
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.059195
Recovering Delaunayness...
Delaunay recovery seconds: 0.082325
Refining mesh...
21363 insertions, added 16942 points, 799712 tetrahedra in queue.
7113 insertions, added 2754 points, 343153 tetrahedra in queue.
Refinement seconds: 2.27313
Smoothing vertices...
Mesh smoothing seconds: 2.94536
Improving mesh...
Mesh improvement seconds: 0.071305
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.030612
Total running seconds: 5.84557
Statistics:
Input points: 16027
Input facets: 32042
Input segments: 48063
Input holes: 2
Input regions: 0
Mesh points: 37108
Mesh tetrahedra: 179009
Mesh faces: 374039
Mesh faces on exterior boundary: 32042
Mesh faces on input facets: 32042
Mesh edges on input segments: 48063
Steiner points inside domain: 21081
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Wing1
Boundary condition name - Wing2
Boundary condition name - Farfield
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.
NOT Running fun3d!
real 0m9.490s
user 0m10.066s
sys 0m0.564s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./fun3dTetgenTest passed (as expected)
=============================================
Running.... STRUCTURE c-Tests
=================================================
+ echo './interferenceTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./interferenceTest test;
+ ./interferenceTest
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
Note: interferenceTest uses ../csmData/interference.csm
classifyClouds: EG_generalBoolean = -7!
classifyClouds: EG_generalBoolean = -7!
classifyClouds: EG_generalBoolean = -7!
classifyClouds: EG_generalBoolean = -7!
1: 1.000000e+00 Box
2: 5.849417e-01 Sphere
3: 7.191810e-01 Cylinder
4: 4.000000e+01 OuterBox
0.000000e+00 -2.685383e-02 0.000000e+00 0.000000e+00
-2.685383e-02 0.000000e+00 0.000000e+00 -2.592150e-02
0.000000e+00 0.000000e+00 0.000000e+00 0.000000e+00
0.000000e+00 -2.592150e-02 0.000000e+00 1.000000e+00
classifyClouds: EG_generalBoolean = -7!
classifyClouds: EG_generalBoolean = -7!
1: 1.000000e+00 Box
2: 5.886880e-01 Sphere
3: 7.235323e-01 Cylinder
0.000000e+00 -2.035193e-02 0.000000e+00
-2.035193e-02 0.000000e+00 0.000000e+00
0.000000e+00 0.000000e+00 0.000000e+00
real 0m3.600s
user 0m6.378s
sys 0m0.154s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./interferenceTest passed (as expected)
=============================================
=================================================
+ echo './hsmCantileverPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmCantileverPlateTest test;
+ ./hsmCantileverPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
Attention: hsmCantileverPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 51
Elemental Tria3 = 0
Elemental Quad4 = 27
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
No "material" specified for Property tuple plate, defaulting to an index of 1
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1313
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.07 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00)
3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.03 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.07 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00)
8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.10 0.00)
9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.10 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
iter dr dd dp rlx max
11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.10 0.00)
11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00)
12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00)
13* 0.335E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00)
15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00)
16 0.573E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00)
17 0.179E-15 0.693E-15 0.745E-15 1.000 dps @ ( 0.78 0.00 0.00)
Converging n vectors ...
it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 )
it = 2 dn = 0.516E-15 rlx = 1.000 ( 13 )
Converging e1,e2 vectors ...
it = 1 de = 0.285E+01 rlx = 0.351 ( 24 )
it = 2 de = 0.269E+01 rlx = 0.372 ( 37 )
it = 3 de = 0.249E+01 rlx = 0.402 ( 21 )
it = 4 de = 0.179E+01 rlx = 0.559 ( 21 )
it = 5 de = 0.954E+00 rlx = 1.000 ( 21 )
it = 6 de = 0.152E+00 rlx = 1.000 ( 21 )
it = 7 de = 0.887E-03 rlx = 1.000 ( 21 )
it = 8 de = 0.177E-09 rlx = 1.000 ( 21 )
it = 9 de = 0.876E-16 rlx = 1.000 ( 28 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat
real 0m0.592s
user 0m0.342s
sys 0m0.071s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected)
=============================================
=================================================
+ echo './hsmSimplePlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmSimplePlateTest test;
+ ./hsmSimplePlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
Attention: hsmTest2 is hard coded to look for ../csmData/feaSimplePlate.csm
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Number of nodal coordinates = 100
Number of elements = 198
Elemental Tria3 = 162
Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
No "material" specified for Property tuple plate, defaulting to an index of 1
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 7
MaxDim = 36, numBCEdge = 0, numBCNode = 36, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 36
->HSMSOL
Matrix Non-zero Entries = 8026
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.609E+00 0.519E+01 0.260E+01 0.096 ddy @ ( 0.28 0.25 0.00)
1* 0.571E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00)
1* 0.159E-01 0.000E+00 0.000E+00 1.000 drz @ ( 0.17 0.11 0.00)
1* 0.254E-02 0.000E+00 0.000E+00 1.000 drz @ ( 0.11 0.14 0.00)
1* 0.838E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.14 0.00)
2 0.768E-02 0.754E+00 0.102E+01 0.492 dps @ ( 0.00 0.00 0.00)
2* 0.336E-03 0.000E+00 0.000E+00 1.000 drx @ ( 0.06 0.06 0.00)
2* 0.690E-06 0.000E+00 0.000E+00 1.000 drz @ ( 0.06 0.08 0.00)
3 0.252E-02 0.204E+00 0.299E+00 1.000 dps @ ( 0.50 0.03 0.00)
3* 0.181E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.39 0.11 0.00)
3* 0.675E-06 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.03 0.00)
4 0.108E-03 0.157E-01 0.567E-01 1.000 dps @ ( 0.39 0.14 0.00)
4* 0.249E-05 0.000E+00 0.000E+00 1.000 drx @ ( 0.44 0.22 0.00)
5 0.103E-05 0.374E-03 0.159E-02 1.000 dps @ ( 0.06 0.06 0.00)
6 0.139E-08 0.994E-07 0.421E-06 1.000 dps @ ( 0.50 0.00 0.00)
7 0.106E-15 0.467E-13 0.133E-12 1.000 dps @ ( 0.50 0.00 0.00)
Converging n vectors ...
it = 1 dn = 0.117E+01 rlx = 1.000 ( 66 )
it = 2 dn = 0.327E-15 rlx = 1.000 ( 81 )
Converging e1,e2 vectors ...
it = 1 de = 0.357E+00 rlx = 1.000 ( 94 )
it = 2 de = 0.167E+00 rlx = 1.000 ( 67 )
it = 3 de = 0.245E-01 rlx = 1.000 ( 76 )
it = 4 de = 0.567E-02 rlx = 1.000 ( 59 )
it = 5 de = 0.192E-02 rlx = 1.000 ( 59 )
it = 6 de = 0.648E-03 rlx = 1.000 ( 59 )
it = 7 de = 0.219E-03 rlx = 1.000 ( 59 )
it = 8 de = 0.740E-04 rlx = 1.000 ( 59 )
it = 9 de = 0.250E-04 rlx = 1.000 ( 59 )
it = 10 de = 0.845E-05 rlx = 1.000 ( 59 )
it = 11 de = 0.286E-05 rlx = 1.000 ( 59 )
it = 12 de = 0.965E-06 rlx = 1.000 ( 59 )
it = 13 de = 0.326E-06 rlx = 1.000 ( 59 )
it = 14 de = 0.110E-06 rlx = 1.000 ( 59 )
it = 15 de = 0.372E-07 rlx = 1.000 ( 59 )
it = 16 de = 0.126E-07 rlx = 1.000 ( 59 )
it = 17 de = 0.425E-08 rlx = 1.000 ( 59 )
it = 18 de = 0.144E-08 rlx = 1.000 ( 59 )
it = 19 de = 0.485E-09 rlx = 1.000 ( 59 )
it = 20 de = 0.164E-09 rlx = 1.000 ( 59 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat
real 0m0.911s
user 0m0.772s
sys 0m0.077s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected)
=============================================
=================================================
+ echo './hsmJoinedPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmJoinedPlateTest test;
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
+ ./hsmJoinedPlateTest 0
Attention: hsmJoinedPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 56
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
No "material" specified for Property tuple plate, defaulting to an index of 1
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 16
MaxDim = 13, numBCEdge = 2, numBCNode = 4, numJoint = 13
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1242
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
1* 0.325E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.05 0.00)
1* 0.434E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2 0.274E+01 0.521E+01 0.118E-07 0.096 ddx @ ( 1.00 0.05 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
2* 0.772E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
3 0.202E+01 0.439E+01 0.107E-06 0.114 ddz @ ( 1.00 0.05 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
3* 0.622E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
3* 0.162E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.05 0.00)
3* 0.163E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4 0.192E+01 0.476E+01 0.147E-07 0.105 ddz @ ( 1.00 0.05 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.448E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.395E+01 0.296E-07 0.127 ddz @ ( 1.00 0.05 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5* 0.636E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
6 0.156E+01 0.301E+01 0.131E-06 0.166 ddx @ ( 1.00 0.05 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.191E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.265E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7 0.103E+01 0.323E+01 0.408E-07 0.155 ddx @ ( 1.00 0.05 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.432E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8 0.757E+00 0.260E+01 0.162E-07 0.192 ddx @ ( 1.00 0.05 0.00)
8* 0.296E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.351E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8* 0.586E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
9 0.680E+00 0.181E+01 0.753E-07 0.276 ddx @ ( 0.88 0.00 0.00)
9* 0.329E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.452E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
9* 0.159E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
9* 0.238E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10 0.457E+00 0.172E+01 0.586E-07 0.290 ddz @ ( 1.00 0.10 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.392E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
iter dr dd dp rlx max
11 0.258E+00 0.122E+01 0.666E-08 0.411 ddz @ ( 1.00 0.10 0.00)
11* 0.207E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.284E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.486E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12 0.135E+00 0.660E+00 0.377E-08 0.758 ddz @ ( 0.88 0.00 0.00)
12* 0.242E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.368E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.869E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13 0.430E-01 0.257E+00 0.505E-07 1.000 ddx @ ( 1.00 0.05 0.00)
13* 0.395E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
13* 0.128E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13* 0.196E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
14 0.656E-03 0.680E-02 0.885E-07 1.000 ddx @ ( 1.00 0.00 0.00)
15 0.156E-05 0.177E-05 0.268E-10 1.000 ddx @ ( 1.00 0.10 0.00)
16 0.273E-09 0.106E-08 0.893E-11 1.000 ddx @ ( 0.50 0.05 0.00)
17 0.138E-15 0.353E-15 0.907E-15 1.000 dps @ ( 0.38 0.10 0.00)
Converging n vectors ...
it = 1 dn = 0.197E+01 rlx = 1.000 ( 17 )
it = 2 dn = 0.866E-15 rlx = 1.000 ( 18 )
Converging e1,e2 vectors ...
it = 1 de = 0.753E+01 rlx = 0.133 ( 1 )
it = 2 de = 0.309E+01 rlx = 0.324 ( 20 )
it = 3 de = 0.324E+01 rlx = 0.309 ( 2 )
it = 4 de = 0.226E+01 rlx = 0.443 ( 2 )
it = 5 de = 0.140E+01 rlx = 0.716 ( 4 )
it = 6 de = 0.660E+00 rlx = 1.000 ( 2 )
it = 7 de = 0.860E-01 rlx = 1.000 ( 4 )
it = 8 de = 0.228E-03 rlx = 1.000 ( 2 )
it = 9 de = 0.428E-11 rlx = 1.000 ( 4 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat
real 0m0.418s
user 0m0.286s
sys 0m0.077s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmJoinedPlateTest passed (as expected)
=============================================
Running.... AEROELASTIC c-Tests
=================================================
Did not run examples for:
awave
pointwise
Mystran
=================================================
All tests pass!
=================================================
=================================================
+ ./execute_PyTestRegression.sh
=================================================
Using python : /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python
=================================================
No options provided...defaulting to ALL
Running.... LINEARAERO PyTests
avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/avl
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
CXtot 0.0006119078685748102
CYtot -6.295467348382128e-15
CZtot -0.3012861394885953
Cltot -4.784258926526785e-14
Cmtot -0.1945055953450382
Cntot -2.338191252215186e-15
Cl'tot -4.787610967125373e-14
Cn'tot -1.502866821492718e-15
CLtot 0.3012509314150635
CDtot 0.004646353488232475
CDvis 0.0
CLff 0.3009503023520388
CYff -7.723329422293541e-15
CDind 0.004646353488232475
CDff 0.004968969500907922
e 0.9669902146157789
StripForces
Wing cl = [0.02994790451347, 0.08555545178933, 0.1329003532587, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.3101221284189, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805664, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996427, 0.2453427152623, 0.2100182422921, 0.17330251928, 0.1329003532723, 0.08555545180787, 0.0299479045408]
Wing cd = [-0.004234137763162, -0.004494543653192, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946409, 0.000511459807839, 0.0021191472861, 0.004145189908974, 0.006609094404181, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.006609094404439, 0.00414518990926, 0.002119147286384, 0.0005114598080993, -0.0007386538944077, -0.001762021024096, -0.002739626801367, -0.003752887372445, -0.004494543653162, -0.004234137764545]
real 0m1.447s
user 0m0.987s
sys 0m0.569s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_AutoSpan_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_AutoSpan_PyTest.py test;
+ python -u avl_AutoSpan_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wing3, index = 3
Getting vortex lattice surface data
VLM surface name - Wing1
VLM surface name - Wing2
VLM surface name - Wing3
Done getting vortex lattice surface data
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Writing surface - Wing1 (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Wing2 (ID = 1)
Section 1 of 7 (ID = 0)
Section 2 of 7 (ID = 1)
Section 3 of 7 (ID = 2)
Section 4 of 7 (ID = 3)
Section 5 of 7 (ID = 4)
Section 6 of 7 (ID = 5)
Section 7 of 7 (ID = 6)
Writing surface - Wing3 (ID = 2)
Section 1 of 7 (ID = 0)
Section 2 of 7 (ID = 3)
Control surface 1 of 1
Section 3 of 7 (ID = 4)
Control surface 1 of 1
Section 4 of 7 (ID = 1)
Section 5 of 7 (ID = 5)
Control surface 1 of 1
Section 6 of 7 (ID = 6)
Control surface 1 of 1
Section 7 of 7 (ID = 2)
CXtot -0.04120015370850767
CYtot -2.245617010841538e-10
CZtot -1.125018809209926
Cltot -1.249787598356312e-09
Cmtot -1.954741267455616
Cntot 1.914701795830442e-10
Cl'tot -1.246255634256898e-09
Cn'tot 2.132528188740779e-10
CLtot 1.124128421568333
CDtot 0.06082816423346078
CDvis 0.0
CLff 1.123105443194628
CYff -2.724471052441854e-10
CDind 0.06082816423346078
CDff -0.2032091360675605
e -0.3293037505974324
real 0m15.417s
user 0m15.516s
sys 0m3.255s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_AutoSpan_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_DesignSweep_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_DesignSweep_PyTest.py test;
+ python -u avl_DesignSweep_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002572533601556616
Cl = 0.2009337808875886
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002586364230247675
Cl = 0.2015191856817219
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002609799718822078
Cl = 0.2025075296435699
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002643444008430607
Cl = 0.2039185811661163
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002688200921004275
Cl = 0.2057816377792995
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002745342060022128
Cl = 0.2081373840562387
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002816610334305089
Cl = 0.2110406736708028
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002904376657741203
Cl = 0.2145646488018499
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003011879793049438
Cl = 0.2188068842337489
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003143602034593163
Cl = 0.2238987294818322
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003305877285459588
Cl = 0.2300199286489811
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003507917885480122
Cl = 0.237422386029936
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003763643677267996
Cl = 0.2464707142747725
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004095167898235787
Cl = 0.2577158067750623
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004540047408144598
Cl = 0.2720394012166634
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.005168237926862041
Cl = 0.290970150746647
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.006128930715340515
Cl = 0.3174875485939014
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.00781835905128463
Cl = 0.3586078919922491
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.01186220444375424
Cl = 0.4382638635248127
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002572533601556616
Cl = 0.2009337808875886
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002586364230247675
Cl = 0.2015191856817219
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002609799718822078
Cl = 0.2025075296435699
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002643444008430607
Cl = 0.2039185811661163
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002688200921004275
Cl = 0.2057816377792995
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002745342060022128
Cl = 0.2081373840562387
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002816610334305089
Cl = 0.2110406736708028
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002904376657741203
Cl = 0.2145646488018499
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003011879793049438
Cl = 0.2188068842337489
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003143602034593163
Cl = 0.2238987294818322
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003305877285459588
Cl = 0.2300199286489811
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003507917885480122
Cl = 0.237422386029936
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003763643677267996
Cl = 0.2464707142747725
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004095167898235787
Cl = 0.2577158067750623
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004540047408144598
Cl = 0.2720394012166634
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.005168237926862041
Cl = 0.290970150746647
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.006128930715340515
Cl = 0.3174875485939014
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.00781835905128463
Cl = 0.3586078919922491
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.01186220444375424
Cl = 0.4382638635248127
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002572533601556616
Cl = 0.2009337808875886
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002586364230247675
Cl = 0.2015191856817219
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002609799718822078
Cl = 0.2025075296435699
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002643444008430607
Cl = 0.2039185811661163
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002688200921004275
Cl = 0.2057816377792995
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002745342060022128
Cl = 0.2081373840562387
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002816610334305089
Cl = 0.2110406736708028
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.002904376657741203
Cl = 0.2145646488018499
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003011879793049438
Cl = 0.2188068842337489
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003143602034593163
Cl = 0.2238987294818322
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003305877285459588
Cl = 0.2300199286489811
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003507917885480122
Cl = 0.237422386029936
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.003763643677267996
Cl = 0.2464707142747725
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004095167898235787
Cl = 0.2577158067750623
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.004540047408144598
Cl = 0.2720394012166634
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.005168237926862041
Cl = 0.290970150746647
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.006128930715340515
Cl = 0.3174875485939014
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.00781835905128463
Cl = 0.3586078919922491
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Cd = 0.01186220444375424
Cl = 0.4382638635248127
Cl[0] = 0.2009337808875886
Cd[0] = 0.002572533601556616
real 0m54.736s
user 0m23.284s
sys 0m27.698s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_ControlSurf_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_ControlSurf_PyTest.py test;
+ python -u avl_ControlSurf_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting design parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
VLM control surface name - Tail
VLM control surface name - WingRightLE
VLM control surface name - WingRightTE
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Vertical_Tail
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 WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
Writing surface - Wing (ID = 1)
Section 1 of 3 (ID = 1)
Control surface 1 of 2
Control surface 2 of 2
Section 2 of 3 (ID = 0)
Control surface 1 of 4
Control surface 2 of 4
Control surface 3 of 4
Control surface 4 of 4
Section 3 of 3 (ID = 2)
Control surface 1 of 2
Control surface 2 of 2
Alpha 1.0
Beta 0.0
Mach 0.5
pb/2V -0.0
qc/2V 0.0
rb/2V -0.0
p'b/2V -0.0
r'b/2V -0.0
CXtot -0.01911479917643664
CYtot 0.03828770401119252
CZtot -0.6203123021542157
Cltot 0.0580302054292887
Cmtot -0.3649415791577237
Cntot -0.02051317548235195
Cl'tot 0.05766336287208888
Cn'tot -0.0215228179571592
CLtot 0.6198842263418534
CDtot 0.02993783031517985
CDvis 0.0
CLff 0.6192452092597066
CYff 0.0328707962584744
CDind 0.02993783031517985
CDff 0.02861019822661097
e 0.7130586920544685
real 0m1.809s
user 0m1.212s
sys 0m0.701s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_EigenValue_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_EigenValue_PyTest.py test;
+ python -u avl_EigenValue_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
EigenValues {'case 1': [[0.48252996, 1.0092579], [0.48252996, -1.0092579], [-6.42569, 0.0], [-1.2733929, 0.0], [-0.0011487329, 0.0], [-1.2380479, 0.49321593], [-1.2380479, -0.49321593], [0.77888703, 0.0]]}
real 0m1.490s
user 0m0.963s
sys 0m0.577s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_EigenValue_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'avl_OpenMDAO_3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_OpenMDAO_3_PyTest.py test;
+ python -u avl_OpenMDAO_3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
[macys-VM:40749] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/387973120/sm_segment.macys-VM.502.17200000.0 could be created.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Alpha [2.] Beta [3.] Cmtot2 [0.04166298]
Alpha [2.] Beta [3.] Cmtot2 [0.04166298]
Cmtot2_Alpha [[0.68007176]]
Cmtot2_Beta [[0.0008466]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 2 M = 10
At X0 0 variables are exactly at the bounds
At iterate 0 f= 4.16630D-02 |proj g|= 6.80072D-01
Alpha [1.31992824] Beta [2.9991534] Cmtot2 [0.03401795]
Cmtot2_Alpha [[0.60837327]]
Cmtot2_Beta [[0.0015253]]
At iterate 1 f= 3.40180D-02 |proj g|= 6.08373D-01
Alpha [-4.45133036] Beta [2.92288326] Cmtot2 [0.00071304]
Cmtot2_Alpha [[0.07860089]]
Cmtot2_Beta [[0.00107544]]
At iterate 2 f= 7.13044D-04 |proj g|= 7.86009D-02
Alpha [-5.30773219] Beta [2.90057802] Cmtot2 [2.43104345e-05]
Cmtot2_Alpha [[0.01420175]]
Cmtot2_Beta [[0.00021881]]
At iterate 3 f= 2.43104D-05 |proj g|= 1.42017D-02
Alpha [-5.49659696] Beta [2.89526135] Cmtot2 [3.72334447e-08]
Cmtot2_Alpha [[0.00055304]]
Cmtot2_Beta [[8.7325759e-06]]
At iterate 4 f= 3.72334D-08 |proj g|= 5.53036D-04
Alpha [-5.50424967] Beta [2.89504288] Cmtot2 [2.19764579e-12]
Cmtot2_Alpha [[4.24793143e-06]]
Cmtot2_Beta [[6.71418674e-08]]
At iterate 5 f= 2.19765D-12 |proj g|= 4.24793D-06
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
2 5 6 5 0 0 4.248D-06 2.198D-12
F = 2.1976457892812188E-012
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
Optimized values: [-5.50424967] [2.89504288]
real 0m32.999s
user 0m8.112s
sys 0m2.974s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected)
=================================================
friction: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/friction
=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
real 0m1.144s
user 0m0.956s
sys 0m0.312s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
tsfoil2: /Users/jenkins/util/tsfoil/tsfoil2
=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go. Other input will terminate the job.
Cl = 0.933417
Cd = 0.000284
Cd Wave = 0.0
Cm = -0.203436
Cp _Critcal = -1.303869
real 0m1.196s
user 0m0.954s
sys 0m0.278s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/mses
=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = 0.37837932402995744
Cd = 0.0077758580442312715
Cm = 0.005262576090327783
real 0m4.329s
user 0m3.899s
sys 0m0.462s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'mses_OpenMDAO_3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_OpenMDAO_3_PyTest.py test;
+ python -u mses_OpenMDAO_3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
[macys-VM:40878] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/3571384320/sm_segment.macys-VM.502.d4df0000.0 could be created.
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - camber
Done getting CFD design variables
camber [0.1] CD [0.01326534]
camber [0.1] CD [0.01326534]
CD_camber [[0.17647556]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 1 M = 10
At X0 1 variables are exactly at the bounds
At iterate 0 f= 1.32653D-02 |proj g|= 1.76476D-01
camber [-0.07647556] CD [0.01022329]
CD_camber [[-0.08760106]]
At iterate 1 f= 1.02233D-02 |proj g|= 8.76011D-02
camber [-0.01793405] CD [0.00770371]
CD_camber [[-0.01328824]]
At iterate 2 f= 7.70371D-03 |proj g|= 1.32882D-02
camber [-0.00746595] CD [0.00760241]
CD_camber [[-0.00542349]]
At iterate 3 f= 7.60241D-03 |proj g|= 5.42349D-03
camber [-0.00024721] CD [0.00758207]
CD_camber [[-0.00011833]]
At iterate 4 f= 7.58207D-03 |proj g|= 1.18327D-04
camber [-8.62005111e-05] CD [0.00758208]
CD_camber [[-3.2293282e-06]]
camber [-0.00022068] CD [0.00758207]
CD_camber [[-0.00010202]]
At iterate 5 f= 7.58207D-03 |proj g|= 1.02022D-04
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
1 5 7 5 0 0 1.020D-04 7.582D-03
F = 7.5820696804286096E-003
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
Optimized values: [-0.00022068]
real 0m29.013s
user 0m27.369s
sys 0m1.741s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected)
=================================================
xfoil: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/xfoil
=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = [1.05475230553347, 1.36488869373699, 1.5660721427216, 2.03059709348412, 1.97271083121139, 1.87307153172667, 1.7605047576018]
Cd = [0.0131991208677172, 0.0166540240605863, 0.0200551482562954, 0.0458671341943513, 0.07542560093961, 0.099446917447585, 0.127479430989108]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.496044115314418, 0.46137773204142, 0.442376568201556, 0.361251636297643, 0.276104140853528, 0.214381239319783, 0.132988264746104]
real 0m5.379s
user 0m5.129s
sys 0m0.339s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
Running.... MESH PyTests
=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting mesh sizing parameters
Mesh sizing name - LeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes = 3793
Number of elements = 4001
Number of triangle elements = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 76
Number of elements = 55
Number of triangle elements = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes = 100
Number of elements = 73
Number of triangle elements = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes = 3970
Total number of elements = 4129
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m9.176s
user 0m15.854s
sys 0m1.882s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_Box_Quad_Pytest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Box_Quad_Pytest.py test;
+ python -u egadsTess_Box_Quad_Pytest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = box1, index = 1
Name = box2, index = 2
Name = box3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 3 TFI quading disabled with attribute .qParams
Face 4 TFI quading disabled with attribute .qParams
TFI quading on all faces disabled with .qParams attribute on the body
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 = 602
Number of elements = 600
Number of triangle elements = 0
Number of quadrilateral elements = 600
Body 2 (of 3)
Number of nodes = 537
Number of elements = 535
Number of triangle elements = 0
Number of quadrilateral elements = 535
Body 3 (of 3)
Number of nodes = 1356
Number of elements = 1354
Number of triangle elements = 0
Number of quadrilateral elements = 1354
----------------------------
Total number of nodes = 2495
Total number of elements = 2489
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m5.235s
user 0m5.868s
sys 0m0.223s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_Box_Quad_Pytest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_Spheres_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Spheres_Quad_PyTest.py test;
+ python -u egadsTess_Spheres_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Spheres, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 4 has a degenerate edge - no TFI quading
Face 5 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 6276
Number of elements = 6274
Number of triangle elements = 0
Number of quadrilateral elements = 6274
----------------------------
Total number of nodes = 6276
Total number of elements = 6274
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m8.145s
user 0m11.184s
sys 0m0.318s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_Spheres_Quad_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_Nose_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Nose_Quad_PyTest.py test;
+ python -u egadsTess_Nose_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = nose, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 2 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
EG_getSidepoint: LineSearch Failed (0.000000 0.973785)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (1.013231 0.966690)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (1.046938 0.962477)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (1.035914 0.957483)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (1.015407 0.966058)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (0.856444 0.971910)!
EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
EG_getSidepoint: LineSearch Failed (0.813517 0.972994)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
Body 1 (of 1)
Number of nodes = 1480
Number of elements = 1478
Number of triangle elements = 0
Number of quadrilateral elements = 1478
----------------------------
Total number of nodes = 1480
Total number of elements = 1478
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m4.424s
user 0m4.738s
sys 0m0.317s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_Nose_Quad_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 316 634
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 681 1018
AFLR2 GGp: Nodes, Faces = 1013 1682
AFLR2 GGp: Nodes, Faces = 1339 2334
AFLR2 GGp: Nodes, Faces = 1652 2960
AFLR2 GGp: Nodes, Faces = 1957 3570
AFLR2 GGp: Nodes, Faces = 2252 4160
AFLR2 GGp: Nodes, Faces = 2526 4708
AFLR2 GGp: Nodes, Faces = 2809 5274
AFLR2 GGp: Nodes, Faces = 3083 5822
AFLR2 GGp: Nodes, Faces = 3327 6310
AFLR2 GGp: Nodes, Faces = 3564 6784
AFLR2 GGp: Nodes, Faces = 3788 7232
AFLR2 GGp: Nodes, Faces = 3995 7646
AFLR2 GGp: Nodes, Faces = 4194 8044
AFLR2 GGp: Nodes, Faces = 4394 8444
AFLR2 GGp: Nodes, Faces = 4585 8826
AFLR2 GGp: Nodes, Faces = 4772 9200
AFLR2 GGp: Nodes, Faces = 4943 9542
AFLR2 GGp: Nodes, Faces = 5129 9914
AFLR2 GGp: Nodes, Faces = 5293 10242
AFLR2 GGp: Nodes, Faces = 5447 10550
AFLR2 GGp: Nodes, Faces = 5594 10844
AFLR2 GGp: Nodes, Faces = 5716 11088
AFLR2 GGp: Nodes, Faces = 5830 11316
AFLR2 GGp: Nodes, Faces = 5909 11474
AFLR2 GGp: Nodes, Faces = 5964 11584
AFLR2 GGp: Nodes, Faces = 6006 11668
AFLR2 GGp: Nodes, Faces = 6025 11706
AFLR2 GGp: Nodes, Faces = 6034 11724
AFLR2 : CPU Time = 0.021 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 6034 11724
AFLR2 QI : Nodes, Faces = 6033 454
AFLR2 QI : Nodes, Faces = 6033 5634
AFLR2 QI : Nodes, Faces = 6033 11722
AFLR2 QI : Nodes, Faces = 6032 462
AFLR2 QI : Nodes, Faces = 6032 5629
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 456
AFLR2 QI : Nodes, Faces = 6032 5632
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 474
AFLR2 QI : Nodes, Faces = 6032 5623
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6031 486
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 QI : Nodes, Faces = 6031 488
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 : CPU Time = 0.011 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
real 0m1.335s
user 0m1.251s
sys 0m0.390s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_PyTest.py test;
+ python -u aflr4_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m3.270s
user 0m2.826s
sys 0m0.504s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_Symmetry_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_Symmetry_PyTest.py test;
+ python -u aflr4_Symmetry_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Farfield, index = 1
Name = Symmetry, index = 2
Name = Wing1, index = 3
Name = Wing2, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = Symmetry, index = 2
Name = Wing1, index = 3
Name = Wing2, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - Symmetry
Done getting mesh sizing parameters
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m3.375s
user 0m3.058s
sys 0m0.555s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_Symmetry_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_Generic_Missile.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_Generic_Missile.py test;
+ python -u aflr4_Generic_Missile.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = MissileOML, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m8.219s
user 0m10.618s
sys 0m0.787s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_Generic_Missile.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_TipTreat_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_TipTreat_PyTest.py test;
+ python -u aflr4_TipTreat_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m10.002s
user 0m9.267s
sys 0m0.754s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_TipTreat_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 150173
Number of elements = 449915
Number of triangles = 14380
Number of quadrilatarals = 0
Number of tetrahedrals = 214483
Number of pyramids = 425
Number of prisms = 220627
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m18.986s
user 0m17.788s
sys 0m1.008s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_Symmetry_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_Symmetry_PyTest.py test;
+ python -u aflr4_and_aflr3_Symmetry_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Farfield, index = 1
Name = Symmetry, index = 2
Name = Wing1, index = 3
Name = Wing2, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = Symmetry, index = 2
Name = Wing1, index = 3
Name = Wing2, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - Symmetry
Done getting mesh sizing parameters
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 = Farfield, index = 1
Name = Symmetry, index = 2
Name = Wing1, index = 3
Name = Wing2, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Farfield, index = 1
Name = Symmetry, index = 2
Name = Wing1, index = 3
Name = Wing2, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 332982
Number of elements = 1068590
Number of triangles = 44340
Number of quadrilatarals = 1613
Number of tetrahedrals = 573242
Number of pyramids = 327
Number of prisms = 449068
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m36.572s
user 0m34.162s
sys 0m1.651s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_Symmetry_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_QuadMesh_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_QuadMesh_PyTest.py test;
+ python -u aflr4_QuadMesh_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m9.913s
user 0m16.535s
sys 0m1.772s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_QuadMesh_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_Tetgen_PyTest.py test;
+ python -u aflr4_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 30045, elements - 60078
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing Tecplot file ....
Finished writing Tecplot file
real 0m15.953s
user 0m14.626s
sys 0m1.086s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_Tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_tetgen_Regions_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_tetgen_Regions_PyTest.py test;
+ python -u aflr4_tetgen_Regions_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SheetBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 11 Faces
EGADS : Body 0 has 20 Edges
EGADS : Body 0 has 11 Loops
EGADS : Body 0 has 12 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 6 8 10 11
EGADS : 2 Yes 0 0 1 0 1 1 3 7 9 11
EGADS : 3 Yes 0 0 1 0 1 2 4 6 9 11
EGADS : 4 Yes 0 0 1 0 1 3 5 7 9 11
EGADS : 5 Yes 0 0 1 0 1 4 6 8 10 11
EGADS : 6 Yes 0 0 1 0 1 1 3 5 10 11
EGADS : 7 Yes 0 0 1 0 1 2 4 8 9 11
EGADS : 8 Yes 0 0 1 0 1 1 5 7 10 11
EGADS : 9 Yes 0 0 1 0 1 2 3 4 7
EGADS : 10 Yes 0 0 1 0 1 1 5 6 8
EGADS : 11 Yes 0 0 1 0 1 1 2 3 4 5 6 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 6 7 -2
EGADS : 3 8 5 9 -10
EGADS : 4 10 11 -12 -13
EGADS : 5 14 15 -16 -11
EGADS : 6 1 -17 -14 -9
EGADS : 7 -18 12 -19 -7
EGADS : 8 16 20 -3 19
EGADS : 9 13 18 -6 -8
EGADS : 10 -15 17 4 -20
EGADS : 11 11 -19 -2 9
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 6 7 -2
EGADS : 3 Yes 8 5 9 -10
EGADS : 4 Yes 10 11 -12 -13
EGADS : 5 Yes 14 15 -16 -11
EGADS : 6 Yes 1 -17 -14 -9
EGADS : 7 Yes -18 12 -19 -7
EGADS : 8 Yes 16 20 -3 19
EGADS : 9 Yes 13 18 -6 -8
EGADS : 10 Yes -15 17 4 -20
EGADS : 11 Yes 11 -19 -2 9
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 6
EGADS : 2 0 Yes 1 3 1 1 2 11
EGADS : 3 0 Yes 3 4 1 1 8
EGADS : 4 0 Yes 2 4 1 1 10
EGADS : 5 0 Yes 5 1 1 2 3
EGADS : 6 0 Yes 5 6 1 2 9
EGADS : 7 0 Yes 6 3 1 2 7
EGADS : 8 0 Yes 7 5 1 3 9
EGADS : 9 0 Yes 1 8 1 3 6 11
EGADS : 10 0 Yes 7 8 1 3 4
EGADS : 11 0 Yes 8 9 1 4 5 11
EGADS : 12 0 Yes 10 9 1 4 7
EGADS : 13 0 Yes 7 10 1 4 9
EGADS : 14 0 Yes 8 11 1 5 6
EGADS : 15 0 Yes 11 12 1 5 10
EGADS : 16 0 Yes 9 12 1 5 8
EGADS : 17 0 Yes 11 2 1 6 10
EGADS : 18 0 Yes 10 6 1 7 9
EGADS : 19 0 Yes 3 9 1 7 8 11
EGADS : 20 0 Yes 12 4 1 8 10
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 1 0 0
EGADS : 2 Yes 1 0 2
EGADS : 3 Yes 1 1 1
EGADS : 4 Yes 1 1 2
EGADS : 5 Yes 1 0 0
EGADS : 6 Yes 1 1 0
EGADS : 7 Yes 0 0 0
EGADS : 8 Yes 0 0 0
EGADS : 9 Yes 0 1 1
EGADS : 10 Yes 0 1 0
EGADS : 11 Yes 0 0 2
EGADS : 12 Yes 0 1 2
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 4
AFLR4 : Min Bounding Box Length = 2
AFLR4 : Max Ref Bounding Box Length = 4
AFLR4 : Min Ref Bounding Box Length = 2
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.01
AFLR4 : Max Surf Spacing = 0.2
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 TRANSP
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 137 228 0
AFLR4 : Nodes, Trias,Quads= 131 216 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 137 228 0
AFLR4 : Nodes, Trias,Quads= 132 218 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 76 120 0
AFLR4 : Nodes, Trias,Quads= 72 112 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 137 228 0
AFLR4 : Nodes, Trias,Quads= 132 218 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 137 228 0
AFLR4 : Nodes, Trias,Quads= 131 216 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 196 340 0
AFLR4 : Nodes, Trias,Quads= 192 332 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 196 340 0
AFLR4 : Nodes, Trias,Quads= 192 332 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 76 120 0
AFLR4 : Nodes, Trias,Quads= 72 112 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 134 226 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 135 228 0
AFLR4 : Nodes, Trias,Quads= 131 220 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 184 318 0
AFLR4 : Nodes, Trias,Quads= 178 306 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1231 2504 464
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1231 2504
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 140 234 0
AFLR4 : Nodes, Trias,Quads= 134 222 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 140 234 0
AFLR4 : Nodes, Trias,Quads= 133 220 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 76 120 0
AFLR4 : Nodes, Trias,Quads= 72 112 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 140 234 0
AFLR4 : Nodes, Trias,Quads= 133 220 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 141 236 0
AFLR4 : Nodes, Trias,Quads= 133 220 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 207 362 0
AFLR4 : Nodes, Trias,Quads= 193 334 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 203 354 0
AFLR4 : Nodes, Trias,Quads= 193 334 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 76 120 0
AFLR4 : Nodes, Trias,Quads= 72 112 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 193 336 0
AFLR4 : Nodes, Trias,Quads= 183 316 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1246 2534 464
OVERALL : CPU Time = 0.115 seconds
Body 1 (of 1)
Number of nodes = 1246
Number of elements = 2534
Number of triangle elements = 2534
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1246
Total number of elements = 2534
Total number of triangle elements = 2534
Total number of quadrilateral elements = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Number of surface: nodes - 1246, elements - 2534
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.009396
Creating surface mesh ...
Surface mesh seconds: 0.002742
Recovering boundaries...
Boundary recovery seconds: 0.006752
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.000881
Recovering Delaunayness...
Delaunay recovery seconds: 0.002417
Refining mesh...
Refinement seconds: 0.014135
Smoothing vertices...
Mesh smoothing seconds: 0.015614
Improving mesh...
Mesh improvement seconds: 0.001269
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000675
Total running seconds: 0.054111
Statistics:
Input points: 1246
Input facets: 2534
Input segments: 3777
Input holes: 0
Input regions: 2
Mesh points: 1455
Mesh tetrahedra: 5105
Mesh faces: 11319
Mesh faces on exterior boundary: 2218
Mesh faces on input facets: 2534
Mesh edges on input segments: 3777
Steiner points inside domain: 209
Done meshing using TetGen!
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Tecplot file ....
Finished writing Tecplot file
real 0m1.074s
user 0m0.943s
sys 0m0.267s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_tetgen_Regions_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 2236
Number of elements = 4468
Number of triangle elements = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 636
Number of elements = 1268
Number of triangle elements = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 267
Number of elements = 530
Number of triangle elements = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3139
Total number of elements = 6266
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 3139, elements - 6266
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.027769
Creating surface mesh ...
Surface mesh seconds: 0.007518
Recovering boundaries...
Boundary recovery seconds: 0.09405
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.008772
Suppressing Steiner points ...
Steiner suppression seconds: 4.8e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.014866
Refining mesh...
4188 insertions, added 2137 points, 127272 tetrahedra in queue.
1394 insertions, added 414 points, 131442 tetrahedra in queue.
1858 insertions, added 464 points, 129858 tetrahedra in queue.
2477 insertions, added 450 points, 111812 tetrahedra in queue.
3302 insertions, added 490 points, 67833 tetrahedra in queue.
4401 insertions, added 401 points, 112 tetrahedra in queue.
Refinement seconds: 0.932153
Smoothing vertices...
Mesh smoothing seconds: 0.480195
Improving mesh...
Mesh improvement seconds: 0.009557
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00311
Total running seconds: 1.57858
Statistics:
Input points: 3139
Input facets: 6266
Input segments: 9399
Input holes: 2
Input regions: 0
Mesh points: 7895
Mesh tetrahedra: 38676
Mesh faces: 80485
Mesh faces on exterior boundary: 6266
Mesh faces on input facets: 6266
Mesh edges on input segments: 9399
Steiner points inside domain: 4756
Done meshing using TetGen!
Writing Tecplot file ....
Finished writing Tecplot file
real 0m6.815s
user 0m5.913s
sys 0m0.445s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_Holes_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_Holes_PyTest.py test;
+ python -u tetgen_Holes_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 8995
Number of elements = 18112
Number of triangle elements = 18112
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 8995
Total number of elements = 18112
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: box
2: cut
Finished writing vtk file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Number of surface: nodes - 8995, elements - 18112
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.214476
Creating surface mesh ...
Surface mesh seconds: 0.019752
Recovering boundaries...
Boundary recovery seconds: 0.111954
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.018024
Recovering Delaunayness...
Delaunay recovery seconds: 0.053802
Refining mesh...
Refinement seconds: 0.268236
Smoothing vertices...
Mesh smoothing seconds: 0.327353
Improving mesh...
Mesh improvement seconds: 0.011403
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.005069
Total running seconds: 1.03115
Statistics:
Input points: 8995
Input facets: 18112
Input segments: 27104
Input holes: 1
Input regions: 0
Mesh points: 7140
Mesh tetrahedra: 27881
Mesh faces: 60802
Mesh faces on exterior boundary: 10080
Mesh faces on input facets: 10080
Mesh edges on input segments: 15120
Steiner points inside domain: 2098
Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
real 0m2.648s
user 0m2.427s
sys 0m0.322s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_Holes_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_Regions_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_Regions_PyTest.py test;
+ python -u tetgen_Regions_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 8995
Number of elements = 18112
Number of triangle elements = 18112
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 8995
Total number of elements = 18112
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: box
2: cut
Finished writing vtk file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Number of surface: nodes - 8995, elements - 18112
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.202696
Creating surface mesh ...
Surface mesh seconds: 0.020815
Recovering boundaries...
Boundary recovery seconds: 0.101866
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.00932
Recovering Delaunayness...
Delaunay recovery seconds: 0.094623
Refining mesh...
Refinement seconds: 0.488791
Smoothing vertices...
Mesh smoothing seconds: 0.609855
Improving mesh...
Mesh improvement seconds: 0.016306
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.006347
Total running seconds: 1.5517
Statistics:
Input points: 8995
Input facets: 18112
Input segments: 27104
Input holes: 0
Input regions: 2
Mesh points: 13181
Mesh tetrahedra: 55765
Mesh faces: 119562
Mesh faces on exterior boundary: 16064
Mesh faces on input facets: 18112
Mesh edges on input segments: 27104
Steiner points inside domain: 4186
Done meshing using TetGen!
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
real 0m3.313s
user 0m3.019s
sys 0m0.340s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_Regions_PyTest.py passed (as expected)
=================================================
delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo
=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Getting mesh sizing parameters
Mesh sizing name - Airfoil
Mesh sizing name - AirfoilTE
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m1.380s
user 0m1.075s
sys 0m0.450s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================
Running.... CFD PyTests
=================================================
+ echo 'su2_and_AFLR2_NodeDist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_NodeDist_PyTest.py test;
+ python -u su2_and_AFLR2_NodeDist_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 224 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 224 224
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 46 94
AFLR2 IG : Nodes, Faces = 92 186
AFLR2 IG : Nodes, Faces = 138 278
AFLR2 IG : Nodes, Faces = 184 370
AFLR2 IG : Nodes, Faces = 196 394
AFLR2 IG : Nodes, Faces = 224 450
AFLR2 IG : Nodes, Faces = 228 450
AFLR2 IG : Nodes, Faces = 224 224
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 224 224
AFLR2 GG : Nodes, Faces = 440 656
AFLR2 GG : Nodes, Faces = 649 1074
AFLR2 GG : Nodes, Faces = 853 1482
AFLR2 GG : Nodes, Faces = 1050 1876
AFLR2 GG : Nodes, Faces = 1238 2252
AFLR2 GG : Nodes, Faces = 1421 2618
AFLR2 GG : Nodes, Faces = 1594 2964
AFLR2 GG : Nodes, Faces = 1760 3296
AFLR2 GG : Nodes, Faces = 1915 3606
AFLR2 GG : Nodes, Faces = 2063 3902
AFLR2 GG : Nodes, Faces = 2202 4180
AFLR2 GG : Nodes, Faces = 2314 4404
AFLR2 GG : Nodes, Faces = 2423 4622
AFLR2 GG : Nodes, Faces = 2528 4832
AFLR2 GG : Nodes, Faces = 2634 5044
AFLR2 GG : Nodes, Faces = 2732 5240
AFLR2 GG : Nodes, Faces = 2831 5438
AFLR2 GG : Nodes, Faces = 2927 5630
AFLR2 GG : Nodes, Faces = 3018 5812
AFLR2 GG : Nodes, Faces = 3109 5994
AFLR2 GG : Nodes, Faces = 3202 6180
AFLR2 GG : Nodes, Faces = 3295 6366
AFLR2 GG : Nodes, Faces = 3386 6548
AFLR2 GG : Nodes, Faces = 3464 6704
AFLR2 GG : Nodes, Faces = 3535 6846
AFLR2 GG : Nodes, Faces = 3594 6964
AFLR2 GG : Nodes, Faces = 3639 7054
AFLR2 GG : Nodes, Faces = 3671 7118
AFLR2 GG : Nodes, Faces = 3691 7158
AFLR2 GG : Nodes, Faces = 3705 7186
AFLR2 GG : Nodes, Faces = 3712 7200
AFLR2 GG : Nodes, Faces = 3715 7206
AFLR2 : CPU Time = 0.010 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 3715 7206
AFLR2 : CPU Time = 0.002 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 3715
Number of elements = 7430
Number of tris = 7206
Number of quad = 0
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_SU2_aflr2.
Volume file name: flow_pyCAPS_SU2_aflr2.
Restart file name: restart_flow_pyCAPS_SU2_aflr2.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
3715 grid points.
7206 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
78 boundary elements in index 3 (Marker = BC_5).
7206 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 7206 TRIANGLE volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 177.06. Mean K: 1.97231. Standard deviation K: 13.0434.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 63.4343| 90|
| CV Face Area Aspect Ratio| 1| 5.23543|
| CV Sub-Volume Ratio| 1| 3.11804|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 3715| 1/1.00| 10|
| 1| 1048| 1/3.54| 7.96696|
| 2| 298| 1/3.52| 6.37252|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06136 m.
Area projection in the x-plane = 0.178383 m, y-plane = 0.994925 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138389 m.
Min. coordinate in the x-direction = -0.000250564 m, y-direction = -0.0151999 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 4.3736e-02| -0.385358| 2.453598| 1.625650| 5.369499| 0.360138|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.3382e-02| -0.512634| 2.087781| 1.374671| 4.973554| 1.183036|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.1902e-02| -0.792582| 1.733529| 1.142729| 4.657622| 3.896320|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 4.2154e-02| -0.880738| 1.486539| 1.023158| 4.334759| 14.592265|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.2485e-02| -0.987528| 1.351478| 0.932491| 4.191092| 111.166022|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 4.2055e-02| -1.104038| 1.188715| 0.874764| 3.951825| -483.924340|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 4.1293e-02| -1.178622| 1.124587| 0.844310| 3.820426| 127.331200|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 4.1202e-02| -1.243517| 1.097463| 0.824869| 3.768858| 40.162273|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 4.1067e-02| -1.287932| 1.075843| 0.810639| 3.733440| 25.154653|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 4.0784e-02| -1.300689| 1.046363| 0.775886| 3.684245| 21.097801|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.30069| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_SU2_aflr2.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|CSV file |surface_flow_pyCAPS_SU2_aflr2.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|Tecplot binary |flow_pyCAPS_SU2_aflr2.szplt |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|Tecplot binary surface |surface_flow_pyCAPS_SU2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 352 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.650457 Cd = 0.030831
Cmz = 0.373226
Cx = 0.030831 Cy = 0.650457
Pressure Contribution
Cl_p = 0.650457 Cd_p = 0.030831
Cmz_p = 0.373226
Cx_p = 0.030831 Cy_p = 0.650457
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m3.609s
user 0m1.730s
sys 0m0.764s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_NodeDist_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 545 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 545 545
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 110 222
AFLR2 IG : Nodes, Faces = 220 442
AFLR2 IG : Nodes, Faces = 330 662
AFLR2 IG : Nodes, Faces = 440 882
AFLR2 IG : Nodes, Faces = 517 1036
AFLR2 IG : Nodes, Faces = 545 1092
AFLR2 IG : Nodes, Faces = 549 1092
AFLR2 IG : Nodes, Faces = 545 545
AFLR2 : CPU Time = 0.002 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 545 545
AFLR2 GGp: Nodes, Faces = 1083 1621
AFLR2 GGp: Nodes, Faces = 1616 2687
AFLR2 GGp: Nodes, Faces = 2144 3743
AFLR2 GGp: Nodes, Faces = 2661 4777
AFLR2 GGp: Nodes, Faces = 3171 5797
AFLR2 GGp: Nodes, Faces = 3672 6799
AFLR2 GGp: Nodes, Faces = 4158 7771
AFLR2 GGp: Nodes, Faces = 4653 8761
AFLR2 GGp: Nodes, Faces = 5142 9739
AFLR2 GGp: Nodes, Faces = 5608 10671
AFLR2 GGp: Nodes, Faces = 6055 11565
AFLR2 GGp: Nodes, Faces = 6482 12419
AFLR2 GGp: Nodes, Faces = 6880 13215
AFLR2 GGp: Nodes, Faces = 7257 13969
AFLR2 GGp: Nodes, Faces = 7614 14683
AFLR2 GGp: Nodes, Faces = 7947 15349
AFLR2 GGp: Nodes, Faces = 8276 16007
AFLR2 GGp: Nodes, Faces = 8575 16605
AFLR2 GGp: Nodes, Faces = 8869 17193
AFLR2 GGp: Nodes, Faces = 9140 17735
AFLR2 GGp: Nodes, Faces = 9401 18257
AFLR2 GGp: Nodes, Faces = 9654 18763
AFLR2 GGp: Nodes, Faces = 9887 19229
AFLR2 GGp: Nodes, Faces = 10110 19675
AFLR2 GGp: Nodes, Faces = 10315 20085
AFLR2 GGp: Nodes, Faces = 10497 20449
AFLR2 GGp: Nodes, Faces = 10656 20767
AFLR2 GGp: Nodes, Faces = 10791 21037
AFLR2 GGp: Nodes, Faces = 10919 21293
AFLR2 GGp: Nodes, Faces = 11022 21499
AFLR2 GGp: Nodes, Faces = 11092 21639
AFLR2 GGp: Nodes, Faces = 11145 21745
AFLR2 GGp: Nodes, Faces = 11156 21767
AFLR2 : CPU Time = 0.049 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 11156 21767
AFLR2 QI : Nodes, Faces = 11155 819
AFLR2 QI : Nodes, Faces = 11155 10473
AFLR2 QI : Nodes, Faces = 11155 21765
AFLR2 QI : Nodes, Faces = 11154 811
AFLR2 QI : Nodes, Faces = 11154 10476
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11154 805
AFLR2 QI : Nodes, Faces = 11154 10479
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11154 911
AFLR2 QI : Nodes, Faces = 11154 10426
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11153 915
AFLR2 QI : Nodes, Faces = 11153 10423
AFLR2 QI : Nodes, Faces = 11153 917
AFLR2 QI : Nodes, Faces = 11153 10423
AFLR2 : CPU Time = 0.019 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 49.3184| 90|
| CV Face Area Aspect Ratio| 1.00035| 33.4982|
| CV Sub-Volume Ratio| 1.00001| 7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11153| 1/1.00| 10|
| 1| 2702| 1/4.13| 7.38309|
| 2| 549| 1/4.92| 4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.2100e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.1628e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.1540e-01| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.1681e-01| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.1336e-01| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.1140e-01| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.0959e-01| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.0732e-01| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.0639e-01| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.0562e-01| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.22124| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file |surface_flow_pyCAPS_su2_aflr2.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary |flow_pyCAPS_su2_aflr2.szplt |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.072253 Cd = -0.01151
Cmz = 0.070975
Cx = -0.01151 Cy = 0.072253
Pressure Contribution
Cl_p = 0.072253 Cd_p = -0.01151
Cmz_p = 0.070975
Cx_p = -0.01151 Cy_p = 0.072253
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m3.466s
user 0m2.966s
sys 0m0.822s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR4_AFLR3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR4_AFLR3_PyTest.py test;
+ python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
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 volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 39568
Number of elements = 228433
Number of triangles = 12446
Number of quadrilatarals = 0
Number of tetrahedrals = 215987
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wake
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_1 (0, 0, 0).
- BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| PARAVIEW| 250|
| SURFACE_PARAVIEW| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
| | BC_2|
+-----------------------------------------------------------------------+
| Far-field| BC_4|
+-----------------------------------------------------------------------+
| Internal boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
39568 grid points.
215987 volume elements.
4 surface markers.
6594 boundary elements in index 0 (Marker = BC_1).
5358 boundary elements in index 1 (Marker = BC_2).
74 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
215987 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 4873.1. Mean K: 61.8682. Standard deviation K: 266.942.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 19.6996| 84.6456|
| CV Face Area Aspect Ratio| 1.0296| 17700.2|
| CV Sub-Volume Ratio| 1.04044| 328478|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 39568| 1/1.00| 10|
| 1| 6515| 1/6.07| 8.22144|
| 2| 1004| 1/6.49| 6.61169|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.038 m^2.
Area projection in the x-plane = 11.1419 m^2, y-plane = 4.96714 m^2, z-plane = 55.4182 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.582636 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 226952| 1| m^2/s^2| 226952|
| Velocity-X| 200.779| 1| m/s| 200.779|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 3.50461| 1| m/s| 3.50461|
| Velocity Magnitude| 200.809| 1| m/s| 200.809|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.2934e+00| -0.065995| 2.296266| 2.031890| 5.424900| 1.969324|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.2312e+00| -0.000146| 2.503192| 2.184653| 5.504433| 2.669994|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.2095e+00| 0.022836| 2.578793| 2.419949| 5.523561| 4.081575|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.2240e+00| -0.041097| 2.580097| 2.548191| 5.445039| 6.003651|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.2060e+00| -0.101756| 2.566392| 2.598258| 5.370190| 7.692754|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.2069e+00| -0.114949| 2.558251| 2.609841| 5.363328| 8.911043|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.2114e+00| -0.124738| 2.541827| 2.614192| 5.362516| 9.794574|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.2151e+00| -0.166905| 2.494151| 2.620861| 5.317920| 10.317284|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.2167e+00| -0.223036| 2.429312| 2.616363| 5.252496| 10.445731|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.2194e+00| -0.269524| 2.392168| 2.592960| 5.200595| 10.271172|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -0.269524| < -8| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_su2AFLRTest.dat |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file |surface_flow_su2AFLRTest.csv |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview |flow_su2AFLRTest.vtu |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface |surface_flow_su2AFLRTest.vtu |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.793167 Cd = 0.077223
Cmx = 4.2e-05 Cmy = -0.202205 Cmz = -7.7e-05
Cx = 0.063368 Cy = 0.000296 Cz = 0.794394
Pressure Contribution
Cl_p = 0.793167 Cd_p = 0.077223
Cmx_p = 4.2e-05 Cmy_p = -0.202205 Cmz_p = -7.7e-05
Cx_p = 0.063368 Cy_p = 0.000296 Cz_p = 0.794394
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmx_v = 0.0 Cmy_v = 0.0 Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0 Cz_v = 0.0
real 0m40.413s
user 0m38.451s
sys 0m1.589s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_Morph_PyTest.py test;
+ python -u su2_Morph_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
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 volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 56157
Number of elements = 325507
Number of triangles = 15872
Number of quadrilatarals = 0
Number of tetrahedrals = 309635
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wake
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing SU2 surface file
Writing SU2 Motion File - su2AFLRTest_motion.dat
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 15
- bcProps.surfaceProp[2].surfaceType = 1
- bcProps.surfaceProp[3].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_1 (0, 0, 0).
- BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Surface(s) affected by the design variables: BC_1, BC_2.
Input mesh file name: ../volumeMesh/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| PARAVIEW| 250|
| SURFACE_PARAVIEW| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
| | BC_2|
+-----------------------------------------------------------------------+
| Far-field| BC_4|
+-----------------------------------------------------------------------+
| Internal boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
56157 grid points.
309635 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
309635 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 5523.74. Mean K: 58.8177. Standard deviation K: 282.533.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 22.8021| 84.7788|
| CV Face Area Aspect Ratio| 1.00879| 391253|
| CV Sub-Volume Ratio| 1.03553| 1.49697e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 56157| 1/1.00| 10|
| 1| 9189| 1/6.11| 8.20439|
| 2| 1395| 1/6.59| 6.56507|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 96.2324 m^2.
Area projection in the x-plane = 7.65774 m^2, y-plane = 4.21853 m^2, z-plane = 45.5887 m^2.
Max. coordinate in the x-direction = 12.3872 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.0650201 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 226952| 1| m^2/s^2| 226952|
| Velocity-X| 200.779| 1| m/s| 200.779|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 3.50461| 1| m/s| 3.50461|
| Velocity Magnitude| 200.809| 1| m/s| 200.809|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.9005e+00| -0.458238| 1.872911| 1.656342| 5.032658| 0.747356|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.8286e+00| -0.474495| 2.012416| 1.722531| 5.023251| 1.417645|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.8110e+00| -0.411436| 2.112682| 1.938918| 5.080139| 3.206640|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.8040e+00| -0.401624| 2.160654| 2.076942| 5.079456| 6.873640|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.8004e+00| -0.411670| 2.180863| 2.151230| 5.057111| 12.470424|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.8001e+00| -0.425533| 2.184395| 2.189878| 5.041713| 19.530915|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.7823e+00| -0.436222| 2.170558| 2.217712| 5.036784| 27.444937|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.7673e+00| -0.438251| 2.130034| 2.242936| 5.037249| 32.489152|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.7569e+00| -0.443916| 2.073807| 2.259407| 5.025917| 31.208484|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.7500e+00| -0.475232| 2.015341| 2.254570| 4.986738| 26.459437|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -0.475232| < -8| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_su2AFLRTest.dat |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file |surface_flow_su2AFLRTest.csv |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview |flow_su2AFLRTest.vtu |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface |surface_flow_su2AFLRTest.vtu |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.521992 Cd = 0.019728
Projecting tessellation 1 (of 4) on to new body
Projecting tessellation 2 (of 4) on to new body
Projecting tessellation 3 (of 4) on to new body
Projecting tessellation 4 (of 4) on to new body
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wake
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing SU2 surface file
Writing SU2 Motion File - su2AFLRTest_motion.dat
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 15
- bcProps.surfaceProp[2].surfaceType = 1
- bcProps.surfaceProp[3].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Mesh Morphing......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
| | BC_2|
+-----------------------------------------------------------------------+
| Far-field| BC_4|
+-----------------------------------------------------------------------+
| Internal boundary| BC_3|
+-----------------------------------------------------------------------+
Three dimensional problem.
56157 grid points.
309635 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
309635 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 2.08667e+06.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Ignoring Convergence Field(s): RMS_DENSITY
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 10.819008 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Paraview |volume_deformed.vtu |
|Paraview surface |surface_deformed.vtu |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_1 (0, 0, 0).
- BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Surface(s) affected by the design variables: BC_1, BC_2.
Input mesh file name: aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| PARAVIEW| 250|
| SURFACE_PARAVIEW| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
| | BC_2|
+-----------------------------------------------------------------------+
| Far-field| BC_4|
+-----------------------------------------------------------------------+
| Internal boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
56157 grid points.
309635 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
309635 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 5523.56. Mean K: 58.7619. Standard deviation K: 282.437.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 22.4386| 85.0504|
| CV Face Area Aspect Ratio| 1.03872| 385864|
| CV Sub-Volume Ratio| 1.04173| 1.51643e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 56157| 1/1.00| 10|
| 1| 9189| 1/6.11| 8.20439|
| 2| 1395| 1/6.59| 6.56507|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 95.6308 m^2.
Area projection in the x-plane = 9.17945 m^2, y-plane = 4.04295 m^2, z-plane = 44.962 m^2.
Max. coordinate in the x-direction = 12.3585 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.400127 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 226952| 1| m^2/s^2| 226952|
| Velocity-X| 200.779| 1| m/s| 200.779|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 3.50461| 1| m/s| 3.50461|
| Velocity Magnitude| 200.809| 1| m/s| 200.809|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.0214e+00| -0.397716| 1.978508| 1.645118| 5.093179| 1.915087|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.0393e+00| -0.257369| 2.241094| 1.916257| 5.249805| 2.557622|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.9455e+00| -0.191638| 2.350399| 2.185809| 5.310465| 3.925162|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.9101e+00| -0.217261| 2.380880| 2.338313| 5.269941| 5.872036|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.8770e+00| -0.261506| 2.381321| 2.406007| 5.209923| 7.749274|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.8426e+00| -0.289071| 2.378299| 2.432486| 5.189120| 9.267784|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.8160e+00| -0.307559| 2.365345| 2.449297| 5.186812| 10.504429|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.8870e+00| -0.325707| 2.326921| 2.468701| 5.171814| 11.399364|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.8700e+00| -0.348872| 2.267332| 2.478078| 5.139102| 11.874957|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.8522e+00| -0.386484| 2.208640| 2.465734| 5.091093| 11.956189|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -0.386484| < -8| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_su2AFLRTest.dat |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file |surface_flow_su2AFLRTest.csv |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview |flow_su2AFLRTest.vtu |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface |surface_flow_su2AFLRTest.vtu |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.884829 Cd = 0.074006
real 1m21.871s
user 1m14.392s
sys 0m6.297s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_Morph_PyTest.py passed (as expected)
=================================================
delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo
=================================================
+ echo 'su2_and_Delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_Delaundo_PyTest.py test;
+ python -u su2_and_Delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
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
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 edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Warning: No boundary condition specified for capsGroup 2DSlice!
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../delaundo/delaundo_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2_CAPS.dat.
Surface file name: surface_flow_su2_CAPS.
Volume file name: flow_su2_CAPS.
Restart file name: restart_flow_su2_CAPS.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
6320 grid points.
12346 volume elements.
5 surface markers.
24 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_2).
24 boundary elements in index 3 (Marker = BC_4).
198 boundary elements in index 4 (Marker = BC_5).
12346 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
There has been a re-orientation of 294 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 45.3524| 89.3051|
| CV Face Area Aspect Ratio| 1.0235| 15.7138|
| CV Sub-Volume Ratio| 1| 7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 6320| 1/1.00| 10|
| 1| 1790| 1/3.53| 7.98287|
| 2| 504| 1/3.55| 6.35388|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 8.1224e-02| -1.163171| 1.073770| 1.341444| 4.312165| 0.062120|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 7.3536e-02| -1.561828| 0.808636| 0.967487| 3.922716| 0.139775|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 7.2965e-02| -1.601698| 0.943793| 1.009036| 3.876382| 0.373708|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 7.4475e-02| -1.659374| 1.008221| 1.015635| 3.799753| 0.952935|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 7.2689e-02| -1.663585| 1.011627| 0.956487| 3.788246| 2.344781|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 7.3104e-02| -1.633451| 0.991734| 0.872954| 3.829708| 6.259549|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 7.1609e-02| -1.626398| 0.990123| 0.847075| 3.843511| 26.349556|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 7.1390e-02| -1.643439| 1.009125| 0.895796| 3.825758| -56.104876|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 7.2176e-02| -1.659565| 1.020774| 0.939260| 3.804303| -24.431167|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 7.1876e-02| -1.676757| 1.012633| 0.938320| 3.783310| -21.456835|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.67676| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_su2_CAPS.dat |
Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
|CSV file |surface_flow_su2_CAPS.csv |
Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
|Tecplot binary |flow_su2_CAPS.szplt |
Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
|Tecplot binary surface |surface_flow_su2_CAPS.szplt |
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 492 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.805231 Cd = -0.037528
Cmz = 0.414714
Cx = -0.037528 Cy = 0.805231
Pressure Contribution
Cl_p = 0.805231 Cd_p = -0.037528
Cmz_p = 0.414714
Cx_p = -0.037528 Cy_p = 0.805231
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m2.690s
user 0m2.246s
sys 0m0.798s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ python -u su2_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 2236
Number of elements = 4468
Number of triangle elements = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 636
Number of elements = 1268
Number of triangle elements = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 267
Number of elements = 530
Number of triangle elements = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3139
Total number of elements = 6266
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 3139, elements - 6266
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.024792
Creating surface mesh ...
Surface mesh seconds: 0.007348
Recovering boundaries...
Boundary recovery seconds: 0.079275
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.00869
Suppressing Steiner points ...
Steiner suppression seconds: 5.6e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.013606
Refining mesh...
4189 insertions, added 2138 points, 127097 tetrahedra in queue.
1394 insertions, added 409 points, 130640 tetrahedra in queue.
1859 insertions, added 449 points, 127916 tetrahedra in queue.
2478 insertions, added 473 points, 111923 tetrahedra in queue.
3303 insertions, added 484 points, 65315 tetrahedra in queue.
4403 insertions, added 433 points, 571 tetrahedra in queue.
Refinement seconds: 0.737348
Smoothing vertices...
Mesh smoothing seconds: 0.495537
Improving mesh...
Mesh improvement seconds: 0.012613
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00308
Total running seconds: 1.38291
Statistics:
Input points: 3139
Input facets: 6266
Input segments: 9399
Input holes: 2
Input regions: 0
Mesh points: 8039
Mesh tetrahedra: 39668
Mesh faces: 82470
Mesh faces on exterior boundary: 6268
Mesh faces on input facets: 6268
Mesh edges on input segments: 9400
Steiner points on input segments: 1
Steiner points inside domain: 4899
Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_1 (0, 0, 0).
- BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../myMesh/tetgen_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| PARAVIEW| 250|
| SURFACE_PARAVIEW| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_Tetgen.dat.
Surface file name: surface_flow_pyCAPS_SU2_Tetgen.
Volume file name: flow_pyCAPS_SU2_Tetgen.
Restart file name: restart_flow_pyCAPS_SU2_Tetgen.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
| | BC_2|
+-----------------------------------------------------------------------+
| Far-field| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
8039 grid points.
39668 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
530 boundary elements in index 2 (Marker = BC_3).
39668 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08934e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 414.134. Mean K: 30.561. Standard deviation K: 37.5336.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.83144| 84.8022|
| CV Face Area Aspect Ratio| 1.55015| 7101.39|
| CV Sub-Volume Ratio| 1.05639| 198266|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 8039| 1/1.00| 10|
| 1| 1338| 1/6.01| 8.25105|
| 2| 214| 1/6.25| 6.7182|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 120.046 m^2.
Area projection in the x-plane = 10.7914 m^2, y-plane = 4.58502 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 226952| 1| m^2/s^2| 226952|
| Velocity-X| 200.779| 1| m/s| 200.779|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 3.50461| 1| m/s| 3.50461|
| Velocity Magnitude| 200.809| 1| m/s| 200.809|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.2532e-01| 0.619384| 3.051344| 2.094590| 6.110279| 1.812161|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.1195e-01| 0.785542| 3.264371| 2.974872| 6.285549| 2.181906|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.0889e-01| 0.724139| 3.334285| 3.249736| 6.229534| 3.226648|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.0490e-01| 0.621976| 3.305627| 3.334988| 6.113861| 4.648342|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.0609e-01| 0.625390| 3.207240| 3.303991| 6.098630| 5.785533|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 0.62539| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_SU2_Tetgen.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|CSV file |surface_flow_pyCAPS_SU2_Tetgen.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview |flow_pyCAPS_SU2_Tetgen.vtu |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview surface |surface_flow_pyCAPS_SU2_Tetgen.vtu |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.759441 Cd = 0.131266
Cmx = 0.001646 Cmy = -0.215157 Cmz = 0.000487
Cx = 0.117991 Cy = 0.00137 Cz = 0.761616
real 1m2.728s
user 1m1.817s
sys 0m1.123s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_X43a_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = fuselage, index = 1
Name = verticalCS, index = 2
Name = fuselage_base, index = 3
Name = horizontalCS, index = 4
Name = inlet, index = 5
Name = hollowInlet, index = 6
Name = Farfield, index = 7
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 = 3808
Number of elements = 7616
Number of triangle elements = 7616
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 5654
Number of elements = 11304
Number of triangle elements = 11304
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9462
Total number of elements = 18920
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = fuselage, index = 1
Name = verticalCS, index = 2
Name = fuselage_base, index = 3
Name = horizontalCS, index = 4
Name = inlet, index = 5
Name = hollowInlet, index = 6
Name = Farfield, index = 7
Number of surface: nodes - 9462, elements - 18920
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.082233
Creating surface mesh ...
Surface mesh seconds: 0.024667
Recovering boundaries...
Warning: 6 segments are not recovered.
Boundary recovery seconds: 0.23738
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.020335
Suppressing Steiner points ...
Steiner suppression seconds: 6.7e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.031399
Refining mesh...
12616 insertions, added 5206 points, 8134 tetrahedra in queue.
Refinement seconds: 1.00884
Smoothing vertices...
Mesh smoothing seconds: 0.67282
Improving mesh...
Mesh improvement seconds: 0.023638
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.009228
Total running seconds: 2.11603
Statistics:
Input points: 9462
Input facets: 18920
Input segments: 28380
Input holes: 6
Input regions: 0
Mesh points: 14813
Mesh tetrahedra: 61044
Mesh faces: 131551
Mesh faces on exterior boundary: 18926
Mesh faces on input facets: 18926
Mesh edges on input segments: 28383
Steiner points on input segments: 3
Steiner points inside domain: 5348
Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - fuselage
Boundary condition name - fuselage_base
Boundary condition name - hollowInlet
Boundary condition name - horizontalCS
Boundary condition name - inlet
Boundary condition name - verticalCS
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
- bcProps.surfaceProp[3].surfaceType = 1
- bcProps.surfaceProp[4].surfaceType = 1
- bcProps.surfaceProp[5].surfaceType = 1
- bcProps.surfaceProp[6].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 3.5.
Angle of attack (AoA): 3 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_1 (0, 0, 0).
- BC_3 (0, 0, 0).
- BC_4 (0, 0, 0).
- BC_2 (0, 0, 0).
- BC_5 (0, 0, 0).
- BC_6 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_3, BC_6, BC_4, BC_5, BC_2.
Input mesh file name: ../myMesh/tetgen_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| PARAVIEW| 250|
| SURFACE_PARAVIEW| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_x43a_Test.dat.
Surface file name: surface_flow_x43a_Test.
Volume file name: flow_x43a_Test.
Restart file name: restart_flow_x43a_Test.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
| | BC_3|
| | BC_6|
| | BC_4|
| | BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Far-field| BC_7|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
14813 grid points.
61044 volume elements.
7 surface markers.
4460 boundary elements in index 0 (Marker = BC_1).
1686 boundary elements in index 1 (Marker = BC_2).
92 boundary elements in index 2 (Marker = BC_3).
696 boundary elements in index 3 (Marker = BC_4).
436 boundary elements in index 4 (Marker = BC_5).
252 boundary elements in index 5 (Marker = BC_6).
11304 boundary elements in index 6 (Marker = BC_7).
61044 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.67744e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 95.6599. Mean K: 0.658518. Standard deviation K: 2.74782.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.759| 83.6683|
| CV Face Area Aspect Ratio| 1.80563| 60514.2|
| CV Sub-Volume Ratio| 1| 8.7549e+08|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 14813| 1/1.00| 10|
| 1| 2926| 1/5.06| 8.73578|
| 2| 763| 1/3.83| 8.37162|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13761.9 m^2.
Area projection in the x-plane = 776.902 m^2, y-plane = 2106.77 m^2, z-plane = 5468.8 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_3 is a single plane.
Boundary marker BC_6 is NOT a single plane.
Boundary marker BC_4 is NOT a single plane.
Boundary marker BC_5 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 916077| 1| m^2/s^2| 916077|
| Velocity-X| 1189.41| 1| m/s| 1189.41|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 62.3342| 1| m/s| 62.3342|
| Velocity Magnitude| 1191.04| 1| m/s| 1191.04|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 4.3704e-01| 2.731919| 5.652900| 4.718102| 8.731395| -0.522472|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.1694e-01| 3.167847| 6.259056| 5.768590| 9.150983| -0.139661|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.2097e-01| 3.287831| 6.387102| 5.862744| 9.254034| -0.051712|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 4.3635e-01| 3.239493| 6.328939| 5.747105| 9.239192| -0.091054|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.4744e-01| 3.139807| 6.198963| 5.587302| 9.124785| -0.155781|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.13981| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_x43a_Test.dat |
Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|CSV file |surface_flow_x43a_Test.csv |
Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview |flow_x43a_Test.vtu |
Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview surface |surface_flow_x43a_Test.vtu |
Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
+-----------------------------------------------------------------------+
Warning: there are 213 non-physical points in the solution.
Warning: 94 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = -15.349382 Cd = 98.531638
Cmx = -27.598823 Cmy = 10655.287295 Cmz = -206.849785
Cx = 99.199929 Cy = -2.371531 Cz = -10.171598
real 0m13.064s
user 0m14.781s
sys 0m1.400s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'fun3d_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
fun3d_Morph_PyTest.py test;
+ python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
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 = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 83038
Number of elements = 484451
Number of triangles = 15680
Number of quadrilatarals = 0
Number of tetrahedrals = 468771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
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 - 2
Design Variable name - Alpha
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Cd2
Objective name - Const
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
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/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_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 = 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/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_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
real 0m16.618s
user 0m14.968s
sys 0m1.369s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case fun3d_Morph_PyTest.py passed (as expected)
=================================================
Running.... STRUCTURE PyTests
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results mass properties.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Area 3.428666259747
Mass 5383.006027803
Centroid [1.222256036874, 0.1634981473778, -4.234492548615e-11]
CG [1.222256036874, 0.1634981473778, -4.234574416087e-11]
Ixx 22133.97306033
Iyy 23448.30046709
Izz 1389.213122582
Ixy 164.2055275657
Ixz -7.454849830627e-06
Iyz 1.707682983295e-06
I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454849830627e-06, 1.707682983295e-06]
II [[22133.97306033, -164.2055275657, 7.454849830627e-06], [-164.2055275657, 23448.30046709, -1.707682983295e-06], [7.454849830627e-06, -1.707682983295e-06, 1389.213122582]]
real 0m7.568s
user 0m10.369s
sys 0m2.618s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'masstran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_AGARD445_PyTest.py test;
+ python -u masstran_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results mass properties.....
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 36
Number of elements = 25
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 25
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Area 547.7004
Mass 0.01605224431138
Centroid [20.03586282449, 14.01686746988, 0.0]
CG [20.03586282449, 14.01686746988, 0.0]
Ixx 1.140246300554
Iyy 0.919317482675
Izz 2.059563783229
Ixy 0.7352134614013
Ixz 0.0
Iyz 0.0
I [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0]
II [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]]
real 0m1.016s
user 0m0.848s
sys 0m0.284s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
real 0m1.475s
user 0m1.329s
sys 0m0.199s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_CantileverPlate_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 40
Number of elements = 51
Elemental Tria3 = 0
Elemental Quad4 = 27
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedLoad
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
Matrix Non-zero Entries = 1313
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00)
1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.03 0.00)
1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.03 0.00)
2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00)
3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00)
3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00)
4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00)
5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.03 0.00)
6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.03 0.00)
7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00)
8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.07 0.00)
8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.10 0.00)
9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.00 0.00)
10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00)
iter dr dd dp rlx max
11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.10 0.00)
11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.10 0.00)
12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.03 0.00)
13* 0.336E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00)
13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00)
14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.00 0.00)
15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.10 0.00)
16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.10 0.00)
17 0.558E-15 0.304E-14 0.603E-15 1.000 ddx @ ( 1.00 0.00 0.00)
Converging n vectors ...
it = 1 dn = 0.193E+01 rlx = 1.000 ( 12 )
it = 2 dn = 0.435E-15 rlx = 1.000 ( 28 )
Converging e1,e2 vectors ...
it = 1 de = 0.285E+01 rlx = 0.351 ( 24 )
it = 2 de = 0.292E+01 rlx = 0.342 ( 34 )
it = 3 de = 0.226E+01 rlx = 0.442 ( 34 )
it = 4 de = 0.151E+01 rlx = 0.660 ( 34 )
it = 5 de = 0.665E+00 rlx = 1.000 ( 34 )
it = 6 de = 0.609E-01 rlx = 1.000 ( 34 )
it = 7 de = 0.573E-04 rlx = 1.000 ( 34 )
it = 8 de = 0.478E-13 rlx = 1.000 ( 34 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMCantileverPlate.dat
real 0m1.211s
user 0m1.118s
sys 0m0.215s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected)
=================================================
ASTROS_ROOT: /Users/jenkins/util/astros/Astros/Darwin-64bit
=================================================
+ echo 'astros_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = 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 = 1
Name = Rib_Root_Point, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 365
Number of elements = 521
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 188
Elemental Quad4 = 333
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 = 366
Combined Number of elements = 522
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 188
Combined Elemental Quad4 = 333
Getting vortex lattice surface data
VLM surface name - Skin_Top
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
Surface 1: Number of points found for aero-spline = 48
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Getting Aero Reference Parameters.......
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 - 5
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Ribs
No "material" specified for Property tuple Ribs, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Property name - Spar1
No "material" specified for Property tuple Spar1, defaulting to an index of 1
Property name - Spar2
No "material" specified for Property tuple Spar2, 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
42 automatic connections were made for capsConnect Rib_Root (node id 366)
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
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
real 0m15.337s
user 0m21.780s
sys 0m3.108s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_AGARD445_PyTest.py test;
+ python -u astros_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results natural frequencies.....
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 36
Number of elements = 25
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 25
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
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 - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
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....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 2
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Natural freq (Mode 1) = 5.78 (Hz)
Natural freq (Mode 2) = 30.66 (Hz)
real 0m1.248s
user 0m0.943s
sys 0m0.328s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Composite_PyTest.py test;
+ python -u astros_Composite_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 15
Number of elements = 8
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 8
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - cantilever
No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
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 - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
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....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
real 0m1.349s
user 0m1.045s
sys 0m0.413s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Composite_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results for natural frequencies.....
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = wing, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - wing
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = root, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = wing, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = wing, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 429
Number of elements = 817
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 817
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - wing
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - root
No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
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 - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
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....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 5.91949 (Hz)
Natural freq (Mode 2) = 29.79990 (Hz)
Natural freq (Mode 3) = 39.10550 (Hz)
Natural freq (Mode 4) = 77.71580 (Hz)
Natural freq (Mode 5) = 99.79550 (Hz)
Natural freq (Mode 6) = 146.97500 (Hz)
Natural freq (Mode 7) = 176.90300 (Hz)
Natural freq (Mode 8) = 235.53300 (Hz)
Natural freq (Mode 9) = 274.42600 (Hz)
Natural freq (Mode 10) = 311.35900 (Hz)
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
Number of Eigen-Vectors = 10
Number of Grid Points = 429 for each Eigen-Vector
Loading Eigen-Vector = 1
Loading Eigen-Vector = 2
Loading Eigen-Vector = 3
Loading Eigen-Vector = 4
Loading Eigen-Vector = 5
Loading Eigen-Vector = 6
Loading Eigen-Vector = 7
Loading Eigen-Vector = 8
Loading Eigen-Vector = 9
Loading Eigen-Vector = 10
real 1m4.750s
user 1m2.491s
sys 0m1.736s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_CompositeWingFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
real 0m2.416s
user 0m1.596s
sys 0m0.721s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ echo 'astros_MultipleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 16
Number of elements = 9
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 9
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 - 5
Load name - load_0
Load name - load_1
Load name - load_2
Load name - load_3
Load name - load_4
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 5
Analysis name - load_0
Analysis name - load_1
Analysis name - load_2
Analysis name - load_3
Analysis name - load_4
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....
Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
Writing analysis cards
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load ADD cards
Writing constraint cards--all constraints for each subcase
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
real 0m2.117s
user 0m1.412s
sys 0m0.550s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_MultipleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results for natural frequencies.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 293
Number of elements = 217
Number of triangle elements = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes = 293
Total number of elements = 217
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 293
Number of elements = 217
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 217
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
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
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
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 - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
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....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02335 (Hz)
Natural freq (Mode 2) = 0.02335 (Hz)
Natural freq (Mode 3) = 0.11619 (Hz)
Natural freq (Mode 4) = 0.11619 (Hz)
Natural freq (Mode 5) = 0.14468 (Hz)
Natural freq (Mode 6) = 0.14468 (Hz)
Natural freq (Mode 7) = 0.23352 (Hz)
Natural freq (Mode 8) = 0.23352 (Hz)
Natural freq (Mode 9) = 0.30497 (Hz)
Natural freq (Mode 10) = 0.30497 (Hz)
real 0m21.692s
user 0m23.423s
sys 0m3.000s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 6
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 6
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
real 0m1.315s
user 0m1.009s
sys 0m0.406s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u astros_ThreeBarFreq_PyTest.py -outLevel=0
Getting results for natural frequencies.....
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
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 - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
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....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 2
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Natural freq (Mode 1) = 86.13400 (Hz)
Natural freq (Mode 2) = 168.53300 (Hz)
real 0m1.350s
user 0m1.029s
sys 0m0.384s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarLinkDesign_PyTest.py test;
+ python -u astros_ThreeBarLinkDesign_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Getting FEA design variables.......
Number of design variables - 3
Design_Variable name - Bar1A
Design_Variable name - Bar2A
Design_Variable name - Bar3A
Design_Variable_Relation name - Bar1A
Design_Variable_Relation name - Bar2A
Design_Variable_Relation name - Bar3A
Number of design variable relations - 3
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 3
Design_Constraint name - stress1
Design_Constraint name - stress2
Design_Constraint name - stress3
Done getting FEA design constraints
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
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 design constraint cards
Writing load cards
Writing material cards
Writing property cards
Writing design variable cards
Running Astros......
Done running Astros!
real 0m1.515s
user 0m1.137s
sys 0m0.380s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarLinkDesign_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ python -u astros_ThreeBarMultiLoad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 2
Constraint name - conOne
No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
Constraint name - conTwo
No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - loadOne
Load name - loadTwo
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 2
Analysis name - analysisOne
Analysis name - analysisTwo
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 ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
real 0m1.226s
user 0m0.974s
sys 0m0.358s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
real 0m1.225s
user 0m0.962s
sys 0m0.370s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ python -u astros_Trim_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - Body
Property name - Edge
Property name - Root
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - PointSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Getting FEA loads.......
Number of loads - 2
Load name - GravityLoad
No "groupName" specified for Load tuple GravityLoad, going to use load name
Load name - PointLoad
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim
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 load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
real 0m1.697s
user 0m1.275s
sys 0m0.487s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_AGARD445_PyTest.py test;
+ python -u nastran_AGARD445_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 49
Number of elements = 36
Number of triangle elements = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes = 49
Total number of elements = 36
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = constEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Mahogany
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - yatesPlate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Warning: No loads specified for case EigenAnalysis!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing combined constraint cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
Getting results natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
Number of Eigen-Values = 132
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Loading Eigen-Value = 11
Loading Eigen-Value = 12
Loading Eigen-Value = 13
Loading Eigen-Value = 14
Loading Eigen-Value = 15
Loading Eigen-Value = 16
Loading Eigen-Value = 17
Loading Eigen-Value = 18
Loading Eigen-Value = 19
Loading Eigen-Value = 20
Loading Eigen-Value = 21
Loading Eigen-Value = 22
Loading Eigen-Value = 23
Loading Eigen-Value = 24
Loading Eigen-Value = 25
Loading Eigen-Value = 26
Loading Eigen-Value = 27
Loading Eigen-Value = 28
Loading Eigen-Value = 29
Loading Eigen-Value = 30
Loading Eigen-Value = 31
Loading Eigen-Value = 32
Loading Eigen-Value = 33
Loading Eigen-Value = 34
Loading Eigen-Value = 35
Loading Eigen-Value = 36
Loading Eigen-Value = 37
Loading Eigen-Value = 38
Loading Eigen-Value = 39
Loading Eigen-Value = 40
Loading Eigen-Value = 41
Loading Eigen-Value = 42
Loading Eigen-Value = 43
Loading Eigen-Value = 44
Loading Eigen-Value = 45
Loading Eigen-Value = 46
Loading Eigen-Value = 47
Loading Eigen-Value = 48
Loading Eigen-Value = 49
Loading Eigen-Value = 50
Loading Eigen-Value = 51
Loading Eigen-Value = 52
Loading Eigen-Value = 53
Loading Eigen-Value = 54
Loading Eigen-Value = 55
Loading Eigen-Value = 56
Loading Eigen-Value = 57
Loading Eigen-Value = 58
Loading Eigen-Value = 59
Loading Eigen-Value = 60
Loading Eigen-Value = 61
Loading Eigen-Value = 62
Loading Eigen-Value = 63
Loading Eigen-Value = 64
Loading Eigen-Value = 65
Loading Eigen-Value = 66
Loading Eigen-Value = 67
Loading Eigen-Value = 68
Loading Eigen-Value = 69
Loading Eigen-Value = 70
Loading Eigen-Value = 71
Loading Eigen-Value = 72
Loading Eigen-Value = 73
Loading Eigen-Value = 74
Loading Eigen-Value = 75
Loading Eigen-Value = 76
Loading Eigen-Value = 77
Loading Eigen-Value = 78
Loading Eigen-Value = 79
Loading Eigen-Value = 80
Loading Eigen-Value = 81
Loading Eigen-Value = 82
Loading Eigen-Value = 83
Loading Eigen-Value = 84
Loading Eigen-Value = 85
Loading Eigen-Value = 86
Loading Eigen-Value = 87
Loading Eigen-Value = 88
Loading Eigen-Value = 89
Loading Eigen-Value = 90
Loading Eigen-Value = 91
Loading Eigen-Value = 92
Loading Eigen-Value = 93
Loading Eigen-Value = 94
Loading Eigen-Value = 95
Loading Eigen-Value = 96
Loading Eigen-Value = 97
Loading Eigen-Value = 98
Loading Eigen-Value = 99
Loading Eigen-Value = 100
Loading Eigen-Value = 101
Loading Eigen-Value = 102
Loading Eigen-Value = 103
Loading Eigen-Value = 104
Loading Eigen-Value = 105
Loading Eigen-Value = 106
Loading Eigen-Value = 107
Loading Eigen-Value = 108
Loading Eigen-Value = 109
Loading Eigen-Value = 110
Loading Eigen-Value = 111
Loading Eigen-Value = 112
Loading Eigen-Value = 113
Loading Eigen-Value = 114
Loading Eigen-Value = 115
Loading Eigen-Value = 116
Loading Eigen-Value = 117
Loading Eigen-Value = 118
Loading Eigen-Value = 119
Loading Eigen-Value = 120
Loading Eigen-Value = 121
Loading Eigen-Value = 122
Loading Eigen-Value = 123
Loading Eigen-Value = 124
Loading Eigen-Value = 125
Loading Eigen-Value = 126
Loading Eigen-Value = 127
Loading Eigen-Value = 128
Loading Eigen-Value = 129
Loading Eigen-Value = 130
Loading Eigen-Value = 131
Loading Eigen-Value = 132
Natural freq (Mode 0) = 9.44 (Hz)
Natural freq (Mode 1) = 35.99 (Hz)
Natural freq (Mode 2) = 50.58 (Hz)
Natural freq (Mode 3) = 93.48 (Hz)
Natural freq (Mode 4) = 122.58 (Hz)
Natural freq (Mode 5) = 142.96 (Hz)
Natural freq (Mode 6) = 153.81 (Hz)
Natural freq (Mode 7) = 201.18 (Hz)
Natural freq (Mode 8) = 203.69 (Hz)
Natural freq (Mode 9) = 218.54 (Hz)
Natural freq (Mode 10) = 244.49 (Hz)
Natural freq (Mode 11) = 267.52 (Hz)
Natural freq (Mode 12) = 282.33 (Hz)
Natural freq (Mode 13) = 284.46 (Hz)
Natural freq (Mode 14) = 311.84 (Hz)
Natural freq (Mode 15) = 328.87 (Hz)
Natural freq (Mode 16) = 334.68 (Hz)
Natural freq (Mode 17) = 346.25 (Hz)
Natural freq (Mode 18) = 362.24 (Hz)
Natural freq (Mode 19) = 368.68 (Hz)
Natural freq (Mode 20) = 377.76 (Hz)
Natural freq (Mode 21) = 393.48 (Hz)
Natural freq (Mode 22) = 403.01 (Hz)
Natural freq (Mode 23) = 415.98 (Hz)
Natural freq (Mode 24) = 430.66 (Hz)
Natural freq (Mode 25) = 456.25 (Hz)
Natural freq (Mode 26) = 460.70 (Hz)
Natural freq (Mode 27) = 478.12 (Hz)
Natural freq (Mode 28) = 500.39 (Hz)
Natural freq (Mode 29) = 510.45 (Hz)
Natural freq (Mode 30) = 514.48 (Hz)
Natural freq (Mode 31) = 519.72 (Hz)
Natural freq (Mode 32) = 531.28 (Hz)
Natural freq (Mode 33) = 553.76 (Hz)
Natural freq (Mode 34) = 566.65 (Hz)
Natural freq (Mode 35) = 591.27 (Hz)
Natural freq (Mode 36) = 611.71 (Hz)
Natural freq (Mode 37) = 612.08 (Hz)
Natural freq (Mode 38) = 624.35 (Hz)
Natural freq (Mode 39) = 650.56 (Hz)
Natural freq (Mode 40) = 670.08 (Hz)
Natural freq (Mode 41) = 721.11 (Hz)
Natural freq (Mode 42) = 732.49 (Hz)
Natural freq (Mode 43) = 751.28 (Hz)
Natural freq (Mode 44) = 814.54 (Hz)
Natural freq (Mode 45) = 883.96 (Hz)
Natural freq (Mode 46) = 951.75 (Hz)
Natural freq (Mode 47) = 975.90 (Hz)
Natural freq (Mode 48) = 1290.98 (Hz)
Natural freq (Mode 49) = 1356.05 (Hz)
Natural freq (Mode 50) = 1506.01 (Hz)
Natural freq (Mode 51) = 1619.60 (Hz)
Natural freq (Mode 52) = 1631.13 (Hz)
Natural freq (Mode 53) = 1745.44 (Hz)
Natural freq (Mode 54) = 1904.47 (Hz)
Natural freq (Mode 55) = 2010.78 (Hz)
Natural freq (Mode 56) = 2031.59 (Hz)
Natural freq (Mode 57) = 2108.70 (Hz)
Natural freq (Mode 58) = 2215.97 (Hz)
Natural freq (Mode 59) = 2306.66 (Hz)
Natural freq (Mode 60) = 2320.15 (Hz)
Natural freq (Mode 61) = 2390.78 (Hz)
Natural freq (Mode 62) = 2494.64 (Hz)
Natural freq (Mode 63) = 2560.50 (Hz)
Natural freq (Mode 64) = 2584.60 (Hz)
Natural freq (Mode 65) = 2587.28 (Hz)
Natural freq (Mode 66) = 2659.52 (Hz)
Natural freq (Mode 67) = 2737.71 (Hz)
Natural freq (Mode 68) = 2789.18 (Hz)
Natural freq (Mode 69) = 2840.95 (Hz)
Natural freq (Mode 70) = 2888.34 (Hz)
Natural freq (Mode 71) = 2967.46 (Hz)
Natural freq (Mode 72) = 3051.49 (Hz)
Natural freq (Mode 73) = 3112.98 (Hz)
Natural freq (Mode 74) = 3139.85 (Hz)
Natural freq (Mode 75) = 3247.88 (Hz)
Natural freq (Mode 76) = 3303.45 (Hz)
Natural freq (Mode 77) = 3344.57 (Hz)
Natural freq (Mode 78) = 3466.41 (Hz)
Natural freq (Mode 79) = 3489.29 (Hz)
Natural freq (Mode 80) = 3562.75 (Hz)
Natural freq (Mode 81) = 3651.56 (Hz)
Natural freq (Mode 82) = 3712.84 (Hz)
Natural freq (Mode 83) = 3761.27 (Hz)
Natural freq (Mode 84) = 3806.30 (Hz)
Natural freq (Mode 85) = 3902.83 (Hz)
Natural freq (Mode 86) = 3961.00 (Hz)
Natural freq (Mode 87) = 4028.45 (Hz)
Natural freq (Mode 88) = 4110.02 (Hz)
Natural freq (Mode 89) = 4191.05 (Hz)
Natural freq (Mode 90) = 4202.44 (Hz)
Natural freq (Mode 91) = 4299.35 (Hz)
Natural freq (Mode 92) = 4376.59 (Hz)
Natural freq (Mode 93) = 4425.85 (Hz)
Natural freq (Mode 94) = 4501.49 (Hz)
Natural freq (Mode 95) = 4518.77 (Hz)
Natural freq (Mode 96) = 4586.52 (Hz)
Natural freq (Mode 97) = 4621.28 (Hz)
Natural freq (Mode 98) = 4678.52 (Hz)
Natural freq (Mode 99) = 4733.41 (Hz)
Natural freq (Mode 100) = 4788.76 (Hz)
Natural freq (Mode 101) = 4816.52 (Hz)
Natural freq (Mode 102) = 4942.47 (Hz)
Natural freq (Mode 103) = 4997.55 (Hz)
Natural freq (Mode 104) = 5045.56 (Hz)
Natural freq (Mode 105) = 5120.59 (Hz)
Natural freq (Mode 106) = 5155.17 (Hz)
Natural freq (Mode 107) = 5325.08 (Hz)
Natural freq (Mode 108) = 5474.54 (Hz)
Natural freq (Mode 109) = 5512.48 (Hz)
Natural freq (Mode 110) = 5525.67 (Hz)
Natural freq (Mode 111) = 5576.25 (Hz)
Natural freq (Mode 112) = 5647.01 (Hz)
Natural freq (Mode 113) = 5841.96 (Hz)
Natural freq (Mode 114) = 6096.57 (Hz)
Natural freq (Mode 115) = 6188.63 (Hz)
Natural freq (Mode 116) = 6328.76 (Hz)
Natural freq (Mode 117) = 6428.94 (Hz)
Natural freq (Mode 118) = 6468.91 (Hz)
Natural freq (Mode 119) = 6958.88 (Hz)
Natural freq (Mode 120) = 7050.41 (Hz)
Natural freq (Mode 121) = 7389.46 (Hz)
Natural freq (Mode 122) = 7464.28 (Hz)
Natural freq (Mode 123) = 7559.48 (Hz)
Natural freq (Mode 124) = 8076.62 (Hz)
Natural freq (Mode 125) = 8344.67 (Hz)
Natural freq (Mode 126) = 8685.13 (Hz)
Natural freq (Mode 127) = 9093.83 (Hz)
Natural freq (Mode 128) = 9351.46 (Hz)
Natural freq (Mode 129) = 10123.65 (Hz)
Natural freq (Mode 130) = 10828.55 (Hz)
Natural freq (Mode 131) = 11674.11 (Hz)
real 0m1.603s
user 0m0.979s
sys 0m0.621s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_AGARD445_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Aeroelastic_PyTest.py test;
+ python -u nastran_Aeroelastic_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes = 1377
Number of elements = 1514
Number of triangle elements = 0
Number of quadrilateral elements = 1514
Body 2 (of 4)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 17
Number of elements = 10
Number of triangle elements = 0
Number of quadrilateral elements = 10
Body 4 (of 4)
Number of nodes = 17
Number of elements = 10
Number of triangle elements = 0
Number of quadrilateral elements = 10
----------------------------
Total number of nodes = 1412
Total number of elements = 1534
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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 = 1
Name = Rib_Root_Point, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1377
Number of elements = 1514
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 1514
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 17
Number of elements = 10
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 10
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 17
Number of elements = 10
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 10
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 1412
Combined Number of elements = 1535
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 1534
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 = 300
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 - 5
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Ribs
No "material" specified for Property tuple Ribs, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Property name - Spar1
No "material" specified for Property tuple Spar1, defaulting to an index of 1
Property name - Spar2
No "material" specified for Property tuple Spar2, 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
93 automatic connections were made for capsConnect Rib_Root (node id 1378)
Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No loads specified for case Trim1!!!!
Writing mass increment cards
Writing aeros card
Writing aestat cards
Writing analysis cards, 0
Writing constraint ADD cards
Writing constraint cards
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m10.554s
user 0m16.793s
sys 0m2.332s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_Aeroelastic_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_CompositeWingDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_CompositeWingDesign_PyTest.py test;
+ python -u nastran_CompositeWingDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 290
Number of elements = 229
Number of triangle elements = 0
Number of quadrilateral elements = 229
----------------------------
Total number of nodes = 290
Total number of elements = 229
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = wing, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - wing
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = root, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = wing, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = wing, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 290
Number of elements = 229
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 229
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - wing
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 8
Design_Variable name - L1
Design_Variable name - L2
Design_Variable name - L3
Design_Variable name - L4
Design_Variable name - L5
Design_Variable name - L6
Design_Variable name - L7
Design_Variable name - L8
Design_Variable_Relation name - L1R
Design_Variable_Relation name - L2R
Design_Variable_Relation name - L3R
Design_Variable_Relation name - L4R
Design_Variable_Relation name - L5R
Design_Variable_Relation name - L6R
Design_Variable_Relation name - L7R
Design_Variable_Relation name - L8R
Number of design variable relations - 8
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 8
Design_Constraint name - stress1
Design_Constraint name - stress2
Design_Constraint name - stress3
Design_Constraint name - stress4
Design_Constraint name - stress5
Design_Constraint name - stress6
Design_Constraint name - stress7
Design_Constraint name - stress8
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - StaticAnalysis
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing design constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
Writing design variable cards
Writing design variable relation cards
Writing design constraints and responses cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m2.467s
user 0m1.655s
sys 0m0.665s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_CompositeWingDesign_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'nastran_CompositeWingFreq_PyTest.py test;'
nastran_CompositeWingFreq_PyTest.py test;
+ python -u nastran_CompositeWingFreq_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 290
Number of elements = 229
Number of triangle elements = 0
Number of quadrilateral elements = 229
----------------------------
Total number of nodes = 290
Total number of elements = 229
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = wing, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - wing
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = root, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = wing, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = wing, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 290
Number of elements = 229
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 229
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - wing
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - root
No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Warning: No loads specified for case EigenAnalysis!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing combined constraint cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
Getting results for natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
Number of Eigen-Values = 1779
Loading Eigen-Value = 1
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Loading Eigen-Value = 797
Loading Eigen-Value = 798
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Loading Eigen-Value = 1707
Loading Eigen-Value = 1708
Loading Eigen-Value = 1709
Loading Eigen-Value = 1710
Loading Eigen-Value = 1711
Loading Eigen-Value = 1712
Loading Eigen-Value = 1713
Loading Eigen-Value = 1714
Loading Eigen-Value = 1715
Loading Eigen-Value = 1716
Loading Eigen-Value = 1717
Loading Eigen-Value = 1718
Loading Eigen-Value = 1719
Loading Eigen-Value = 1720
Loading Eigen-Value = 1721
Loading Eigen-Value = 1722
Loading Eigen-Value = 1723
Loading Eigen-Value = 1724
Loading Eigen-Value = 1725
Loading Eigen-Value = 1726
Loading Eigen-Value = 1727
Loading Eigen-Value = 1728
Loading Eigen-Value = 1729
Loading Eigen-Value = 1730
Loading Eigen-Value = 1731
Loading Eigen-Value = 1732
Loading Eigen-Value = 1733
Loading Eigen-Value = 1734
Loading Eigen-Value = 1735
Loading Eigen-Value = 1736
Loading Eigen-Value = 1737
Loading Eigen-Value = 1738
Loading Eigen-Value = 1739
Loading Eigen-Value = 1740
Loading Eigen-Value = 1741
Loading Eigen-Value = 1742
Loading Eigen-Value = 1743
Loading Eigen-Value = 1744
Loading Eigen-Value = 1745
Loading Eigen-Value = 1746
Loading Eigen-Value = 1747
Loading Eigen-Value = 1748
Loading Eigen-Value = 1749
Loading Eigen-Value = 1750
Loading Eigen-Value = 1751
Loading Eigen-Value = 1752
Loading Eigen-Value = 1753
Loading Eigen-Value = 1754
Loading Eigen-Value = 1755
Loading Eigen-Value = 1756
Loading Eigen-Value = 1757
Loading Eigen-Value = 1758
Loading Eigen-Value = 1759
Loading Eigen-Value = 1760
Loading Eigen-Value = 1761
Loading Eigen-Value = 1762
Loading Eigen-Value = 1763
Loading Eigen-Value = 1764
Loading Eigen-Value = 1765
Loading Eigen-Value = 1766
Loading Eigen-Value = 1767
Loading Eigen-Value = 1768
Loading Eigen-Value = 1769
Loading Eigen-Value = 1770
Loading Eigen-Value = 1771
Loading Eigen-Value = 1772
Loading Eigen-Value = 1773
Loading Eigen-Value = 1774
Loading Eigen-Value = 1775
Loading Eigen-Value = 1776
Loading Eigen-Value = 1777
Loading Eigen-Value = 1778
Loading Eigen-Value = 1779
Natural freq (Mode 1) = 5.91752 (Hz)
Natural freq (Mode 2) = 29.92398 (Hz)
Natural freq (Mode 3) = 40.01939 (Hz)
Natural freq (Mode 4) = 78.26336 (Hz)
Natural freq (Mode 5) = 102.48770 (Hz)
Natural freq (Mode 6) = 148.28700 (Hz)
Natural freq (Mode 7) = 182.97520 (Hz)
Natural freq (Mode 8) = 238.39370 (Hz)
Natural freq (Mode 9) = 285.36330 (Hz)
Natural freq (Mode 10) = 321.90370 (Hz)
Natural freq (Mode 11) = 338.36210 (Hz)
Natural freq (Mode 12) = 347.87480 (Hz)
Natural freq (Mode 13) = 412.76490 (Hz)
Natural freq (Mode 14) = 446.89790 (Hz)
Natural freq (Mode 15) = 477.26050 (Hz)
Natural freq (Mode 16) = 556.73130 (Hz)
Natural freq (Mode 17) = 582.55570 (Hz)
Natural freq (Mode 18) = 627.20430 (Hz)
Natural freq (Mode 19) = 696.67300 (Hz)
Natural freq (Mode 20) = 750.94670 (Hz)
Natural freq (Mode 21) = 757.10910 (Hz)
Natural freq (Mode 22) = 797.86110 (Hz)
Natural freq (Mode 23) = 847.03330 (Hz)
Natural freq (Mode 24) = 944.72760 (Hz)
Natural freq (Mode 25) = 956.33970 (Hz)
Natural freq (Mode 26) = 978.56320 (Hz)
Natural freq (Mode 27) = 1011.29500 (Hz)
Natural freq (Mode 28) = 1121.40300 (Hz)
Natural freq (Mode 29) = 1155.17800 (Hz)
Natural freq (Mode 30) = 1174.22000 (Hz)
Natural freq (Mode 31) = 1218.32400 (Hz)
Natural freq (Mode 32) = 1289.59300 (Hz)
Natural freq (Mode 33) = 1300.85200 (Hz)
Natural freq (Mode 34) = 1332.20600 (Hz)
Natural freq (Mode 35) = 1359.39700 (Hz)
Natural freq (Mode 36) = 1412.35900 (Hz)
Natural freq (Mode 37) = 1457.87000 (Hz)
Natural freq (Mode 38) = 1504.80200 (Hz)
Natural freq (Mode 39) = 1555.90000 (Hz)
Natural freq (Mode 40) = 1607.07800 (Hz)
Natural freq (Mode 41) = 1655.47400 (Hz)
Natural freq (Mode 42) = 1717.08000 (Hz)
Natural freq (Mode 43) = 1741.97300 (Hz)
Natural freq (Mode 44) = 1801.38700 (Hz)
Natural freq (Mode 45) = 1873.31100 (Hz)
Natural freq (Mode 46) = 1913.09800 (Hz)
Natural freq (Mode 47) = 1980.26900 (Hz)
Natural freq (Mode 48) = 1991.99800 (Hz)
Natural freq (Mode 49) = 2069.91300 (Hz)
Natural freq (Mode 50) = 2113.76400 (Hz)
Natural freq (Mode 51) = 2145.78500 (Hz)
Natural freq (Mode 52) = 2175.50900 (Hz)
Natural freq (Mode 53) = 2224.13400 (Hz)
Natural freq (Mode 54) = 2298.75800 (Hz)
Natural freq (Mode 55) = 2349.76500 (Hz)
Natural freq (Mode 56) = 2413.31600 (Hz)
Natural freq (Mode 57) = 2439.34000 (Hz)
Natural freq (Mode 58) = 2497.21500 (Hz)
Natural freq (Mode 59) = 2499.99000 (Hz)
Natural freq (Mode 60) = 2549.47200 (Hz)
Natural freq (Mode 61) = 2608.88800 (Hz)
Natural freq (Mode 62) = 2632.75600 (Hz)
Natural freq (Mode 63) = 2710.43000 (Hz)
Natural freq (Mode 64) = 2747.45500 (Hz)
Natural freq (Mode 65) = 2787.56600 (Hz)
Natural freq (Mode 66) = 2804.88200 (Hz)
Natural freq (Mode 67) = 2828.01000 (Hz)
Natural freq (Mode 68) = 2891.33900 (Hz)
Natural freq (Mode 69) = 2943.88700 (Hz)
Natural freq (Mode 70) = 2996.34500 (Hz)
Natural freq (Mode 71) = 3038.47900 (Hz)
Natural freq (Mode 72) = 3110.97300 (Hz)
Natural freq (Mode 73) = 3155.74800 (Hz)
Natural freq (Mode 74) = 3171.54500 (Hz)
Natural freq (Mode 75) = 3208.80000 (Hz)
Natural freq (Mode 76) = 3270.76600 (Hz)
Natural freq (Mode 77) = 3337.48000 (Hz)
Natural freq (Mode 78) = 3397.62800 (Hz)
Natural freq (Mode 79) = 3430.15700 (Hz)
Natural freq (Mode 80) = 3486.27900 (Hz)
Natural freq (Mode 81) = 3519.90500 (Hz)
Natural freq (Mode 82) = 3582.41700 (Hz)
Natural freq (Mode 83) = 3644.34000 (Hz)
Natural freq (Mode 84) = 3690.50500 (Hz)
Natural freq (Mode 85) = 3709.94700 (Hz)
Natural freq (Mode 86) = 3751.86800 (Hz)
Natural freq (Mode 87) = 3847.60300 (Hz)
Natural freq (Mode 88) = 3881.69700 (Hz)
Natural freq (Mode 89) = 3929.56900 (Hz)
Natural freq (Mode 90) = 4030.33000 (Hz)
Natural freq (Mode 91) = 4075.24600 (Hz)
Natural freq (Mode 92) = 4112.23100 (Hz)
Natural freq (Mode 93) = 4125.08800 (Hz)
Natural freq (Mode 94) = 4175.94300 (Hz)
Natural freq (Mode 95) = 4249.31900 (Hz)
Natural freq (Mode 96) = 4326.93400 (Hz)
Natural freq (Mode 97) = 4350.07800 (Hz)
Natural freq (Mode 98) = 4422.66200 (Hz)
Natural freq (Mode 99) = 4433.83300 (Hz)
Natural freq (Mode 100) = 4490.80200 (Hz)
Natural freq (Mode 101) = 4533.85600 (Hz)
Natural freq (Mode 102) = 4575.81800 (Hz)
Natural freq (Mode 103) = 4650.17200 (Hz)
Natural freq (Mode 104) = 4653.01800 (Hz)
Natural freq (Mode 105) = 4762.06400 (Hz)
Natural freq (Mode 106) = 4783.26800 (Hz)
Natural freq (Mode 107) = 4833.77500 (Hz)
Natural freq (Mode 108) = 4859.19300 (Hz)
Natural freq (Mode 109) = 4906.46000 (Hz)
Natural freq (Mode 110) = 4983.49100 (Hz)
Natural freq (Mode 111) = 5036.52400 (Hz)
Natural freq (Mode 112) = 5088.89300 (Hz)
Natural freq (Mode 113) = 5131.49800 (Hz)
Natural freq (Mode 114) = 5189.45600 (Hz)
Natural freq (Mode 115) = 5226.69000 (Hz)
Natural freq (Mode 116) = 5312.39900 (Hz)
Natural freq (Mode 117) = 5337.54300 (Hz)
Natural freq (Mode 118) = 5412.15200 (Hz)
Natural freq (Mode 119) = 5468.34800 (Hz)
Natural freq (Mode 120) = 5515.48600 (Hz)
Natural freq (Mode 121) = 5524.08000 (Hz)
Natural freq (Mode 122) = 5619.29500 (Hz)
Natural freq (Mode 123) = 5653.70400 (Hz)
Natural freq (Mode 124) = 5733.63600 (Hz)
Natural freq (Mode 125) = 5773.94900 (Hz)
Natural freq (Mode 126) = 5844.35200 (Hz)
Natural freq (Mode 127) = 5867.65000 (Hz)
Natural freq (Mode 128) = 5906.70100 (Hz)
Natural freq (Mode 129) = 5971.92900 (Hz)
Natural freq (Mode 130) = 6009.02100 (Hz)
Natural freq (Mode 131) = 6072.23100 (Hz)
Natural freq (Mode 132) = 6114.32400 (Hz)
Natural freq (Mode 133) = 6217.45300 (Hz)
Natural freq (Mode 134) = 6258.33500 (Hz)
Natural freq (Mode 135) = 6280.35900 (Hz)
Natural freq (Mode 136) = 6328.06800 (Hz)
Natural freq (Mode 137) = 6380.03600 (Hz)
Natural freq (Mode 138) = 6420.51900 (Hz)
Natural freq (Mode 139) = 6443.62300 (Hz)
Natural freq (Mode 140) = 6482.95600 (Hz)
Natural freq (Mode 141) = 6556.30700 (Hz)
Natural freq (Mode 142) = 6581.93700 (Hz)
Natural freq (Mode 143) = 6681.89000 (Hz)
Natural freq (Mode 144) = 6710.49400 (Hz)
Natural freq (Mode 145) = 6712.56300 (Hz)
Natural freq (Mode 146) = 6757.85200 (Hz)
Natural freq (Mode 147) = 6773.85300 (Hz)
Natural freq (Mode 148) = 6855.24800 (Hz)
Natural freq (Mode 149) = 6906.85000 (Hz)
Natural freq (Mode 150) = 6964.86500 (Hz)
Natural freq (Mode 151) = 7005.47200 (Hz)
Natural freq (Mode 152) = 7093.12700 (Hz)
Natural freq (Mode 153) = 7172.58500 (Hz)
Natural freq (Mode 154) = 7235.36700 (Hz)
Natural freq (Mode 155) = 7284.38800 (Hz)
Natural freq (Mode 156) = 7339.50900 (Hz)
Natural freq (Mode 157) = 7387.76000 (Hz)
Natural freq (Mode 158) = 7432.07800 (Hz)
Natural freq (Mode 159) = 7484.19100 (Hz)
Natural freq (Mode 160) = 7505.65500 (Hz)
Natural freq (Mode 161) = 7575.40800 (Hz)
Natural freq (Mode 162) = 7619.31300 (Hz)
Natural freq (Mode 163) = 7645.70400 (Hz)
Natural freq (Mode 164) = 7763.99600 (Hz)
Natural freq (Mode 165) = 7804.56500 (Hz)
Natural freq (Mode 166) = 7847.62900 (Hz)
Natural freq (Mode 167) = 7884.94000 (Hz)
Natural freq (Mode 168) = 7971.14100 (Hz)
Natural freq (Mode 169) = 7981.26000 (Hz)
Natural freq (Mode 170) = 8018.25500 (Hz)
Natural freq (Mode 171) = 8065.35200 (Hz)
Natural freq (Mode 172) = 8190.58300 (Hz)
Natural freq (Mode 173) = 8219.15300 (Hz)
Natural freq (Mode 174) = 8242.49900 (Hz)
Natural freq (Mode 175) = 8305.01600 (Hz)
Natural freq (Mode 176) = 8338.74300 (Hz)
Natural freq (Mode 177) = 8449.34200 (Hz)
Natural freq (Mode 178) = 8515.47200 (Hz)
Natural freq (Mode 179) = 8589.43700 (Hz)
Natural freq (Mode 180) = 8616.56100 (Hz)
Natural freq (Mode 181) = 8640.13700 (Hz)
Natural freq (Mode 182) = 8712.28800 (Hz)
Natural freq (Mode 183) = 8716.81500 (Hz)
Natural freq (Mode 184) = 8787.58300 (Hz)
Natural freq (Mode 185) = 8846.56900 (Hz)
Natural freq (Mode 186) = 8875.50500 (Hz)
Natural freq (Mode 187) = 8964.94700 (Hz)
Natural freq (Mode 188) = 8992.86500 (Hz)
Natural freq (Mode 189) = 9077.22400 (Hz)
Natural freq (Mode 190) = 9096.26100 (Hz)
Natural freq (Mode 191) = 9145.99500 (Hz)
Natural freq (Mode 192) = 9199.71100 (Hz)
Natural freq (Mode 193) = 9239.19700 (Hz)
Natural freq (Mode 194) = 9335.28900 (Hz)
Natural freq (Mode 195) = 9367.16700 (Hz)
Natural freq (Mode 196) = 9496.20700 (Hz)
Natural freq (Mode 197) = 9506.20900 (Hz)
Natural freq (Mode 198) = 9530.04800 (Hz)
Natural freq (Mode 199) = 9569.59000 (Hz)
Natural freq (Mode 200) = 9612.48400 (Hz)
Natural freq (Mode 201) = 9670.18300 (Hz)
Natural freq (Mode 202) = 9702.23300 (Hz)
Natural freq (Mode 203) = 9772.30000 (Hz)
Natural freq (Mode 204) = 9825.17600 (Hz)
Natural freq (Mode 205) = 9883.47700 (Hz)
Natural freq (Mode 206) = 9901.35100 (Hz)
Natural freq (Mode 207) = 9952.14500 (Hz)
Natural freq (Mode 208) = 10096.61000 (Hz)
Natural freq (Mode 209) = 10117.51000 (Hz)
Natural freq (Mode 210) = 10152.60000 (Hz)
Natural freq (Mode 211) = 10241.89000 (Hz)
Natural freq (Mode 212) = 10283.19000 (Hz)
Natural freq (Mode 213) = 10290.01000 (Hz)
Natural freq (Mode 214) = 10313.76000 (Hz)
Natural freq (Mode 215) = 10380.63000 (Hz)
Natural freq (Mode 216) = 10423.29000 (Hz)
Natural freq (Mode 217) = 10489.16000 (Hz)
Natural freq (Mode 218) = 10534.94000 (Hz)
Natural freq (Mode 219) = 10617.34000 (Hz)
Natural freq (Mode 220) = 10692.66000 (Hz)
Natural freq (Mode 221) = 10724.57000 (Hz)
Natural freq (Mode 222) = 10783.30000 (Hz)
Natural freq (Mode 223) = 10796.14000 (Hz)
Natural freq (Mode 224) = 10837.42000 (Hz)
Natural freq (Mode 225) = 10917.22000 (Hz)
Natural freq (Mode 226) = 10990.39000 (Hz)
Natural freq (Mode 227) = 11032.01000 (Hz)
Natural freq (Mode 228) = 11066.56000 (Hz)
Natural freq (Mode 229) = 11107.64000 (Hz)
Natural freq (Mode 230) = 11181.18000 (Hz)
Natural freq (Mode 231) = 11203.75000 (Hz)
Natural freq (Mode 232) = 11301.06000 (Hz)
Natural freq (Mode 233) = 11368.84000 (Hz)
Natural freq (Mode 234) = 11405.65000 (Hz)
Natural freq (Mode 235) = 11479.89000 (Hz)
Natural freq (Mode 236) = 11556.38000 (Hz)
Natural freq (Mode 237) = 11582.24000 (Hz)
Natural freq (Mode 238) = 11608.71000 (Hz)
Natural freq (Mode 239) = 11663.11000 (Hz)
Natural freq (Mode 240) = 11767.24000 (Hz)
Natural freq (Mode 241) = 11809.88000 (Hz)
Natural freq (Mode 242) = 11869.78000 (Hz)
Natural freq (Mode 243) = 11968.82000 (Hz)
Natural freq (Mode 244) = 11983.42000 (Hz)
Natural freq (Mode 245) = 12042.58000 (Hz)
Natural freq (Mode 246) = 12116.63000 (Hz)
Natural freq (Mode 247) = 12143.37000 (Hz)
Natural freq (Mode 248) = 12143.61000 (Hz)
Natural freq (Mode 249) = 12189.26000 (Hz)
Natural freq (Mode 250) = 12256.66000 (Hz)
Natural freq (Mode 251) = 12310.75000 (Hz)
Natural freq (Mode 252) = 12364.03000 (Hz)
Natural freq (Mode 253) = 12370.65000 (Hz)
Natural freq (Mode 254) = 12548.26000 (Hz)
Natural freq (Mode 255) = 12565.68000 (Hz)
Natural freq (Mode 256) = 12594.88000 (Hz)
Natural freq (Mode 257) = 12712.07000 (Hz)
Natural freq (Mode 258) = 12770.17000 (Hz)
Natural freq (Mode 259) = 12775.62000 (Hz)
Natural freq (Mode 260) = 12825.19000 (Hz)
Natural freq (Mode 261) = 12905.15000 (Hz)
Natural freq (Mode 262) = 12955.70000 (Hz)
Natural freq (Mode 263) = 13036.73000 (Hz)
Natural freq (Mode 264) = 13054.72000 (Hz)
Natural freq (Mode 265) = 13161.42000 (Hz)
Natural freq (Mode 266) = 13192.61000 (Hz)
Natural freq (Mode 267) = 13239.57000 (Hz)
Natural freq (Mode 268) = 13284.37000 (Hz)
Natural freq (Mode 269) = 13384.14000 (Hz)
Natural freq (Mode 270) = 13408.39000 (Hz)
Natural freq (Mode 271) = 13456.16000 (Hz)
Natural freq (Mode 272) = 13472.22000 (Hz)
Natural freq (Mode 273) = 13530.73000 (Hz)
Natural freq (Mode 274) = 13593.85000 (Hz)
Natural freq (Mode 275) = 13760.49000 (Hz)
Natural freq (Mode 276) = 13785.68000 (Hz)
Natural freq (Mode 277) = 13876.39000 (Hz)
Natural freq (Mode 278) = 13897.87000 (Hz)
Natural freq (Mode 279) = 13949.89000 (Hz)
Natural freq (Mode 280) = 13982.83000 (Hz)
Natural freq (Mode 281) = 14036.06000 (Hz)
Natural freq (Mode 282) = 14061.26000 (Hz)
Natural freq (Mode 283) = 14126.31000 (Hz)
Natural freq (Mode 284) = 14289.37000 (Hz)
Natural freq (Mode 285) = 14326.99000 (Hz)
Natural freq (Mode 286) = 14398.55000 (Hz)
Natural freq (Mode 287) = 14484.76000 (Hz)
Natural freq (Mode 288) = 14489.28000 (Hz)
Natural freq (Mode 289) = 14522.37000 (Hz)
Natural freq (Mode 290) = 14565.89000 (Hz)
Natural freq (Mode 291) = 14606.46000 (Hz)
Natural freq (Mode 292) = 14649.44000 (Hz)
Natural freq (Mode 293) = 14786.59000 (Hz)
Natural freq (Mode 294) = 14893.02000 (Hz)
Natural freq (Mode 295) = 14975.89000 (Hz)
Natural freq (Mode 296) = 14990.37000 (Hz)
Natural freq (Mode 297) = 15048.04000 (Hz)
Natural freq (Mode 298) = 15137.92000 (Hz)
Natural freq (Mode 299) = 15180.15000 (Hz)
Natural freq (Mode 300) = 15208.71000 (Hz)
Natural freq (Mode 301) = 15324.33000 (Hz)
Natural freq (Mode 302) = 15358.41000 (Hz)
Natural freq (Mode 303) = 15371.80000 (Hz)
Natural freq (Mode 304) = 15469.29000 (Hz)
Natural freq (Mode 305) = 15502.22000 (Hz)
Natural freq (Mode 306) = 15582.06000 (Hz)
Natural freq (Mode 307) = 15697.16000 (Hz)
Natural freq (Mode 308) = 15716.81000 (Hz)
Natural freq (Mode 309) = 15838.63000 (Hz)
Natural freq (Mode 310) = 15881.20000 (Hz)
Natural freq (Mode 311) = 15983.89000 (Hz)
Natural freq (Mode 312) = 15994.51000 (Hz)
Natural freq (Mode 313) = 16002.53000 (Hz)
Natural freq (Mode 314) = 16137.48000 (Hz)
Natural freq (Mode 315) = 16143.49000 (Hz)
Natural freq (Mode 316) = 16191.25000 (Hz)
Natural freq (Mode 317) = 16444.55000 (Hz)
Natural freq (Mode 318) = 16465.20000 (Hz)
Natural freq (Mode 319) = 16540.14000 (Hz)
Natural freq (Mode 320) = 16545.05000 (Hz)
Natural freq (Mode 321) = 16607.63000 (Hz)
Natural freq (Mode 322) = 16787.41000 (Hz)
Natural freq (Mode 323) = 16809.01000 (Hz)
Natural freq (Mode 324) = 16854.44000 (Hz)
Natural freq (Mode 325) = 16898.50000 (Hz)
Natural freq (Mode 326) = 16931.53000 (Hz)
Natural freq (Mode 327) = 16952.62000 (Hz)
Natural freq (Mode 328) = 17074.71000 (Hz)
Natural freq (Mode 329) = 17099.57000 (Hz)
Natural freq (Mode 330) = 17119.86000 (Hz)
Natural freq (Mode 331) = 17222.80000 (Hz)
Natural freq (Mode 332) = 17266.61000 (Hz)
Natural freq (Mode 333) = 17383.30000 (Hz)
Natural freq (Mode 334) = 17418.65000 (Hz)
Natural freq (Mode 335) = 17488.28000 (Hz)
Natural freq (Mode 336) = 17541.06000 (Hz)
Natural freq (Mode 337) = 17694.88000 (Hz)
Natural freq (Mode 338) = 17700.81000 (Hz)
Natural freq (Mode 339) = 17741.71000 (Hz)
Natural freq (Mode 340) = 17800.10000 (Hz)
Natural freq (Mode 341) = 17816.33000 (Hz)
Natural freq (Mode 342) = 17925.23000 (Hz)
Natural freq (Mode 343) = 17964.70000 (Hz)
Natural freq (Mode 344) = 18050.17000 (Hz)
Natural freq (Mode 345) = 18098.53000 (Hz)
Natural freq (Mode 346) = 18131.22000 (Hz)
Natural freq (Mode 347) = 18183.38000 (Hz)
Natural freq (Mode 348) = 18215.32000 (Hz)
Natural freq (Mode 349) = 18334.29000 (Hz)
Natural freq (Mode 350) = 18362.53000 (Hz)
Natural freq (Mode 351) = 18486.87000 (Hz)
Natural freq (Mode 352) = 18591.83000 (Hz)
Natural freq (Mode 353) = 18709.08000 (Hz)
Natural freq (Mode 354) = 18712.34000 (Hz)
Natural freq (Mode 355) = 18799.42000 (Hz)
Natural freq (Mode 356) = 18829.22000 (Hz)
Natural freq (Mode 357) = 18853.39000 (Hz)
Natural freq (Mode 358) = 18976.00000 (Hz)
Natural freq (Mode 359) = 19059.20000 (Hz)
Natural freq (Mode 360) = 19125.02000 (Hz)
Natural freq (Mode 361) = 19157.08000 (Hz)
Natural freq (Mode 362) = 19255.37000 (Hz)
Natural freq (Mode 363) = 19304.60000 (Hz)
Natural freq (Mode 364) = 19419.35000 (Hz)
Natural freq (Mode 365) = 19455.45000 (Hz)
Natural freq (Mode 366) = 19511.95000 (Hz)
Natural freq (Mode 367) = 19591.56000 (Hz)
Natural freq (Mode 368) = 19646.65000 (Hz)
Natural freq (Mode 369) = 19757.04000 (Hz)
Natural freq (Mode 370) = 19782.00000 (Hz)
Natural freq (Mode 371) = 19921.47000 (Hz)
Natural freq (Mode 372) = 20038.24000 (Hz)
Natural freq (Mode 373) = 20087.59000 (Hz)
Natural freq (Mode 374) = 20247.26000 (Hz)
Natural freq (Mode 375) = 20314.55000 (Hz)
Natural freq (Mode 376) = 20347.61000 (Hz)
Natural freq (Mode 377) = 20409.15000 (Hz)
Natural freq (Mode 378) = 20555.38000 (Hz)
Natural freq (Mode 379) = 20745.27000 (Hz)
Natural freq (Mode 380) = 20826.08000 (Hz)
Natural freq (Mode 381) = 20926.47000 (Hz)
Natural freq (Mode 382) = 20927.93000 (Hz)
Natural freq (Mode 383) = 20961.74000 (Hz)
Natural freq (Mode 384) = 21049.74000 (Hz)
Natural freq (Mode 385) = 21086.09000 (Hz)
Natural freq (Mode 386) = 21226.15000 (Hz)
Natural freq (Mode 387) = 21285.19000 (Hz)
Natural freq (Mode 388) = 21322.08000 (Hz)
Natural freq (Mode 389) = 21443.02000 (Hz)
Natural freq (Mode 390) = 21485.59000 (Hz)
Natural freq (Mode 391) = 21498.71000 (Hz)
Natural freq (Mode 392) = 21600.59000 (Hz)
Natural freq (Mode 393) = 21699.40000 (Hz)
Natural freq (Mode 394) = 21749.01000 (Hz)
Natural freq (Mode 395) = 21760.19000 (Hz)
Natural freq (Mode 396) = 21871.83000 (Hz)
Natural freq (Mode 397) = 21968.82000 (Hz)
Natural freq (Mode 398) = 22004.93000 (Hz)
Natural freq (Mode 399) = 22037.06000 (Hz)
Natural freq (Mode 400) = 22132.05000 (Hz)
Natural freq (Mode 401) = 22272.75000 (Hz)
Natural freq (Mode 402) = 22284.71000 (Hz)
Natural freq (Mode 403) = 22343.19000 (Hz)
Natural freq (Mode 404) = 22492.85000 (Hz)
Natural freq (Mode 405) = 22675.22000 (Hz)
Natural freq (Mode 406) = 22726.67000 (Hz)
Natural freq (Mode 407) = 22795.38000 (Hz)
Natural freq (Mode 408) = 22847.12000 (Hz)
Natural freq (Mode 409) = 23027.21000 (Hz)
Natural freq (Mode 410) = 23066.16000 (Hz)
Natural freq (Mode 411) = 23111.55000 (Hz)
Natural freq (Mode 412) = 23264.07000 (Hz)
Natural freq (Mode 413) = 23277.39000 (Hz)
Natural freq (Mode 414) = 23280.87000 (Hz)
Natural freq (Mode 415) = 23489.27000 (Hz)
Natural freq (Mode 416) = 23508.29000 (Hz)
Natural freq (Mode 417) = 23538.90000 (Hz)
Natural freq (Mode 418) = 23734.87000 (Hz)
Natural freq (Mode 419) = 23748.21000 (Hz)
Natural freq (Mode 420) = 23776.47000 (Hz)
Natural freq (Mode 421) = 23836.88000 (Hz)
Natural freq (Mode 422) = 23851.33000 (Hz)
Natural freq (Mode 423) = 23996.21000 (Hz)
Natural freq (Mode 424) = 24072.71000 (Hz)
Natural freq (Mode 425) = 24231.38000 (Hz)
Natural freq (Mode 426) = 24326.89000 (Hz)
Natural freq (Mode 427) = 24335.46000 (Hz)
Natural freq (Mode 428) = 24378.13000 (Hz)
Natural freq (Mode 429) = 24422.91000 (Hz)
Natural freq (Mode 430) = 24535.55000 (Hz)
Natural freq (Mode 431) = 24612.28000 (Hz)
Natural freq (Mode 432) = 24749.69000 (Hz)
Natural freq (Mode 433) = 24864.25000 (Hz)
Natural freq (Mode 434) = 25020.23000 (Hz)
Natural freq (Mode 435) = 25036.26000 (Hz)
Natural freq (Mode 436) = 25255.07000 (Hz)
Natural freq (Mode 437) = 25348.07000 (Hz)
Natural freq (Mode 438) = 25376.09000 (Hz)
Natural freq (Mode 439) = 25408.28000 (Hz)
Natural freq (Mode 440) = 25484.80000 (Hz)
Natural freq (Mode 441) = 25615.76000 (Hz)
Natural freq (Mode 442) = 25669.87000 (Hz)
Natural freq (Mode 443) = 25819.13000 (Hz)
Natural freq (Mode 444) = 25981.25000 (Hz)
Natural freq (Mode 445) = 25999.63000 (Hz)
Natural freq (Mode 446) = 26070.56000 (Hz)
Natural freq (Mode 447) = 26145.77000 (Hz)
Natural freq (Mode 448) = 26279.59000 (Hz)
Natural freq (Mode 449) = 26351.51000 (Hz)
Natural freq (Mode 450) = 26395.38000 (Hz)
Natural freq (Mode 451) = 26502.02000 (Hz)
Natural freq (Mode 452) = 26532.53000 (Hz)
Natural freq (Mode 453) = 26637.85000 (Hz)
Natural freq (Mode 454) = 26643.48000 (Hz)
Natural freq (Mode 455) = 26745.91000 (Hz)
Natural freq (Mode 456) = 26934.27000 (Hz)
Natural freq (Mode 457) = 27070.38000 (Hz)
Natural freq (Mode 458) = 27164.86000 (Hz)
Natural freq (Mode 459) = 27237.99000 (Hz)
Natural freq (Mode 460) = 27380.39000 (Hz)
Natural freq (Mode 461) = 27500.71000 (Hz)
Natural freq (Mode 462) = 27556.49000 (Hz)
Natural freq (Mode 463) = 27702.19000 (Hz)
Natural freq (Mode 464) = 27702.94000 (Hz)
Natural freq (Mode 465) = 27916.39000 (Hz)
Natural freq (Mode 466) = 28012.95000 (Hz)
Natural freq (Mode 467) = 28161.58000 (Hz)
Natural freq (Mode 468) = 28179.12000 (Hz)
Natural freq (Mode 469) = 28422.62000 (Hz)
Natural freq (Mode 470) = 28474.77000 (Hz)
Natural freq (Mode 471) = 28560.92000 (Hz)
Natural freq (Mode 472) = 28566.15000 (Hz)
Natural freq (Mode 473) = 28710.87000 (Hz)
Natural freq (Mode 474) = 28781.45000 (Hz)
Natural freq (Mode 475) = 28999.03000 (Hz)
Natural freq (Mode 476) = 29078.86000 (Hz)
Natural freq (Mode 477) = 29154.48000 (Hz)
Natural freq (Mode 478) = 29296.92000 (Hz)
Natural freq (Mode 479) = 29356.81000 (Hz)
Natural freq (Mode 480) = 29380.71000 (Hz)
Natural freq (Mode 481) = 29478.38000 (Hz)
Natural freq (Mode 482) = 29553.13000 (Hz)
Natural freq (Mode 483) = 29622.04000 (Hz)
Natural freq (Mode 484) = 29712.53000 (Hz)
Natural freq (Mode 485) = 30011.06000 (Hz)
Natural freq (Mode 486) = 30035.66000 (Hz)
Natural freq (Mode 487) = 30102.46000 (Hz)
Natural freq (Mode 488) = 30209.47000 (Hz)
Natural freq (Mode 489) = 30280.31000 (Hz)
Natural freq (Mode 490) = 30323.96000 (Hz)
Natural freq (Mode 491) = 30365.31000 (Hz)
Natural freq (Mode 492) = 30520.68000 (Hz)
Natural freq (Mode 493) = 30541.57000 (Hz)
Natural freq (Mode 494) = 30606.26000 (Hz)
Natural freq (Mode 495) = 30742.72000 (Hz)
Natural freq (Mode 496) = 30869.45000 (Hz)
Natural freq (Mode 497) = 30969.95000 (Hz)
Natural freq (Mode 498) = 31100.58000 (Hz)
Natural freq (Mode 499) = 31169.65000 (Hz)
Natural freq (Mode 500) = 31244.07000 (Hz)
Natural freq (Mode 501) = 31425.86000 (Hz)
Natural freq (Mode 502) = 31537.51000 (Hz)
Natural freq (Mode 503) = 31639.96000 (Hz)
Natural freq (Mode 504) = 31754.34000 (Hz)
Natural freq (Mode 505) = 31760.84000 (Hz)
Natural freq (Mode 506) = 31883.20000 (Hz)
Natural freq (Mode 507) = 32002.92000 (Hz)
Natural freq (Mode 508) = 32220.74000 (Hz)
Natural freq (Mode 509) = 32290.88000 (Hz)
Natural freq (Mode 510) = 32391.40000 (Hz)
Natural freq (Mode 511) = 32608.03000 (Hz)
Natural freq (Mode 512) = 32647.91000 (Hz)
Natural freq (Mode 513) = 32720.89000 (Hz)
Natural freq (Mode 514) = 32949.41000 (Hz)
Natural freq (Mode 515) = 32988.75000 (Hz)
Natural freq (Mode 516) = 33115.60000 (Hz)
Natural freq (Mode 517) = 33200.03000 (Hz)
Natural freq (Mode 518) = 33318.92000 (Hz)
Natural freq (Mode 519) = 33330.25000 (Hz)
Natural freq (Mode 520) = 33333.78000 (Hz)
Natural freq (Mode 521) = 33486.56000 (Hz)
Natural freq (Mode 522) = 33531.17000 (Hz)
Natural freq (Mode 523) = 33683.28000 (Hz)
Natural freq (Mode 524) = 33797.57000 (Hz)
Natural freq (Mode 525) = 33906.94000 (Hz)
Natural freq (Mode 526) = 33914.80000 (Hz)
Natural freq (Mode 527) = 33989.41000 (Hz)
Natural freq (Mode 528) = 34210.63000 (Hz)
Natural freq (Mode 529) = 34378.73000 (Hz)
Natural freq (Mode 530) = 34494.40000 (Hz)
Natural freq (Mode 531) = 34582.28000 (Hz)
Natural freq (Mode 532) = 34836.82000 (Hz)
Natural freq (Mode 533) = 34902.17000 (Hz)
Natural freq (Mode 534) = 34987.61000 (Hz)
Natural freq (Mode 535) = 35067.79000 (Hz)
Natural freq (Mode 536) = 35153.96000 (Hz)
Natural freq (Mode 537) = 35173.18000 (Hz)
Natural freq (Mode 538) = 35315.79000 (Hz)
Natural freq (Mode 539) = 35452.04000 (Hz)
Natural freq (Mode 540) = 35564.39000 (Hz)
Natural freq (Mode 541) = 35577.60000 (Hz)
Natural freq (Mode 542) = 35671.63000 (Hz)
Natural freq (Mode 543) = 35764.36000 (Hz)
Natural freq (Mode 544) = 35817.39000 (Hz)
Natural freq (Mode 545) = 35987.39000 (Hz)
Natural freq (Mode 546) = 35988.65000 (Hz)
Natural freq (Mode 547) = 36149.87000 (Hz)
Natural freq (Mode 548) = 36216.11000 (Hz)
Natural freq (Mode 549) = 36374.59000 (Hz)
Natural freq (Mode 550) = 36456.40000 (Hz)
Natural freq (Mode 551) = 36643.81000 (Hz)
Natural freq (Mode 552) = 36841.90000 (Hz)
Natural freq (Mode 553) = 36898.49000 (Hz)
Natural freq (Mode 554) = 36940.48000 (Hz)
Natural freq (Mode 555) = 37109.42000 (Hz)
Natural freq (Mode 556) = 37109.45000 (Hz)
Natural freq (Mode 557) = 37157.88000 (Hz)
Natural freq (Mode 558) = 37177.07000 (Hz)
Natural freq (Mode 559) = 37287.62000 (Hz)
Natural freq (Mode 560) = 37387.53000 (Hz)
Natural freq (Mode 561) = 37522.76000 (Hz)
Natural freq (Mode 562) = 37628.77000 (Hz)
Natural freq (Mode 563) = 37734.15000 (Hz)
Natural freq (Mode 564) = 37824.32000 (Hz)
Natural freq (Mode 565) = 37936.66000 (Hz)
Natural freq (Mode 566) = 38054.42000 (Hz)
Natural freq (Mode 567) = 38287.95000 (Hz)
Natural freq (Mode 568) = 38432.25000 (Hz)
Natural freq (Mode 569) = 38489.84000 (Hz)
Natural freq (Mode 570) = 38652.49000 (Hz)
Natural freq (Mode 571) = 38702.59000 (Hz)
Natural freq (Mode 572) = 38877.29000 (Hz)
Natural freq (Mode 573) = 39004.32000 (Hz)
Natural freq (Mode 574) = 39191.21000 (Hz)
Natural freq (Mode 575) = 39286.07000 (Hz)
Natural freq (Mode 576) = 39329.37000 (Hz)
Natural freq (Mode 577) = 39574.73000 (Hz)
Natural freq (Mode 578) = 39720.89000 (Hz)
Natural freq (Mode 579) = 40162.23000 (Hz)
Natural freq (Mode 580) = 40253.22000 (Hz)
Natural freq (Mode 581) = 40293.79000 (Hz)
Natural freq (Mode 582) = 40337.32000 (Hz)
Natural freq (Mode 583) = 40474.10000 (Hz)
Natural freq (Mode 584) = 40602.31000 (Hz)
Natural freq (Mode 585) = 40635.95000 (Hz)
Natural freq (Mode 586) = 40660.85000 (Hz)
Natural freq (Mode 587) = 40743.75000 (Hz)
Natural freq (Mode 588) = 40756.84000 (Hz)
Natural freq (Mode 589) = 40949.57000 (Hz)
Natural freq (Mode 590) = 40995.24000 (Hz)
Natural freq (Mode 591) = 41223.55000 (Hz)
Natural freq (Mode 592) = 41359.39000 (Hz)
Natural freq (Mode 593) = 41528.88000 (Hz)
Natural freq (Mode 594) = 41791.72000 (Hz)
Natural freq (Mode 595) = 41887.48000 (Hz)
Natural freq (Mode 596) = 42118.45000 (Hz)
Natural freq (Mode 597) = 42198.64000 (Hz)
Natural freq (Mode 598) = 42348.55000 (Hz)
Natural freq (Mode 599) = 42370.13000 (Hz)
Natural freq (Mode 600) = 42416.97000 (Hz)
Natural freq (Mode 601) = 42462.20000 (Hz)
Natural freq (Mode 602) = 42642.21000 (Hz)
Natural freq (Mode 603) = 42726.17000 (Hz)
Natural freq (Mode 604) = 42854.97000 (Hz)
Natural freq (Mode 605) = 42962.25000 (Hz)
Natural freq (Mode 606) = 43123.13000 (Hz)
Natural freq (Mode 607) = 43203.68000 (Hz)
Natural freq (Mode 608) = 43400.77000 (Hz)
Natural freq (Mode 609) = 43508.95000 (Hz)
Natural freq (Mode 610) = 43597.38000 (Hz)
Natural freq (Mode 611) = 43700.77000 (Hz)
Natural freq (Mode 612) = 43704.76000 (Hz)
Natural freq (Mode 613) = 43877.68000 (Hz)
Natural freq (Mode 614) = 44012.25000 (Hz)
Natural freq (Mode 615) = 44106.74000 (Hz)
Natural freq (Mode 616) = 44292.90000 (Hz)
Natural freq (Mode 617) = 44314.06000 (Hz)
Natural freq (Mode 618) = 44374.05000 (Hz)
Natural freq (Mode 619) = 44397.46000 (Hz)
Natural freq (Mode 620) = 44586.68000 (Hz)
Natural freq (Mode 621) = 44696.46000 (Hz)
Natural freq (Mode 622) = 44741.60000 (Hz)
Natural freq (Mode 623) = 45054.47000 (Hz)
Natural freq (Mode 624) = 45140.14000 (Hz)
Natural freq (Mode 625) = 45249.72000 (Hz)
Natural freq (Mode 626) = 45385.59000 (Hz)
Natural freq (Mode 627) = 45567.35000 (Hz)
Natural freq (Mode 628) = 45605.37000 (Hz)
Natural freq (Mode 629) = 45735.81000 (Hz)
Natural freq (Mode 630) = 45752.43000 (Hz)
Natural freq (Mode 631) = 46051.15000 (Hz)
Natural freq (Mode 632) = 46420.19000 (Hz)
Natural freq (Mode 633) = 46488.60000 (Hz)
Natural freq (Mode 634) = 46552.35000 (Hz)
Natural freq (Mode 635) = 46577.11000 (Hz)
Natural freq (Mode 636) = 46578.90000 (Hz)
Natural freq (Mode 637) = 46694.76000 (Hz)
Natural freq (Mode 638) = 46912.64000 (Hz)
Natural freq (Mode 639) = 46981.14000 (Hz)
Natural freq (Mode 640) = 47193.58000 (Hz)
Natural freq (Mode 641) = 47238.25000 (Hz)
Natural freq (Mode 642) = 47338.20000 (Hz)
Natural freq (Mode 643) = 47429.59000 (Hz)
Natural freq (Mode 644) = 47576.44000 (Hz)
Natural freq (Mode 645) = 47611.71000 (Hz)
Natural freq (Mode 646) = 47691.93000 (Hz)
Natural freq (Mode 647) = 47807.08000 (Hz)
Natural freq (Mode 648) = 47890.22000 (Hz)
Natural freq (Mode 649) = 47917.94000 (Hz)
Natural freq (Mode 650) = 48003.06000 (Hz)
Natural freq (Mode 651) = 48405.16000 (Hz)
Natural freq (Mode 652) = 48501.56000 (Hz)
Natural freq (Mode 653) = 48589.31000 (Hz)
Natural freq (Mode 654) = 48598.45000 (Hz)
Natural freq (Mode 655) = 48779.29000 (Hz)
Natural freq (Mode 656) = 48883.09000 (Hz)
Natural freq (Mode 657) = 48930.20000 (Hz)
Natural freq (Mode 658) = 49088.71000 (Hz)
Natural freq (Mode 659) = 49207.57000 (Hz)
Natural freq (Mode 660) = 49256.51000 (Hz)
Natural freq (Mode 661) = 49376.35000 (Hz)
Natural freq (Mode 662) = 49480.93000 (Hz)
Natural freq (Mode 663) = 49565.85000 (Hz)
Natural freq (Mode 664) = 49718.37000 (Hz)
Natural freq (Mode 665) = 49722.37000 (Hz)
Natural freq (Mode 666) = 49790.09000 (Hz)
Natural freq (Mode 667) = 49897.80000 (Hz)
Natural freq (Mode 668) = 50054.08000 (Hz)
Natural freq (Mode 669) = 50090.88000 (Hz)
Natural freq (Mode 670) = 50160.08000 (Hz)
Natural freq (Mode 671) = 50228.52000 (Hz)
Natural freq (Mode 672) = 50465.21000 (Hz)
Natural freq (Mode 673) = 50484.11000 (Hz)
Natural freq (Mode 674) = 50692.21000 (Hz)
Natural freq (Mode 675) = 50853.68000 (Hz)
Natural freq (Mode 676) = 50857.21000 (Hz)
Natural freq (Mode 677) = 50936.92000 (Hz)
Natural freq (Mode 678) = 51135.05000 (Hz)
Natural freq (Mode 679) = 51171.95000 (Hz)
Natural freq (Mode 680) = 51382.60000 (Hz)
Natural freq (Mode 681) = 51500.84000 (Hz)
Natural freq (Mode 682) = 51551.45000 (Hz)
Natural freq (Mode 683) = 51604.40000 (Hz)
Natural freq (Mode 684) = 51794.87000 (Hz)
Natural freq (Mode 685) = 51921.50000 (Hz)
Natural freq (Mode 686) = 52077.61000 (Hz)
Natural freq (Mode 687) = 52106.14000 (Hz)
Natural freq (Mode 688) = 52156.48000 (Hz)
Natural freq (Mode 689) = 52196.38000 (Hz)
Natural freq (Mode 690) = 52375.95000 (Hz)
Natural freq (Mode 691) = 52511.88000 (Hz)
Natural freq (Mode 692) = 52690.02000 (Hz)
Natural freq (Mode 693) = 52760.29000 (Hz)
Natural freq (Mode 694) = 52983.51000 (Hz)
Natural freq (Mode 695) = 53151.14000 (Hz)
Natural freq (Mode 696) = 53168.78000 (Hz)
Natural freq (Mode 697) = 53351.66000 (Hz)
Natural freq (Mode 698) = 53457.94000 (Hz)
Natural freq (Mode 699) = 53501.50000 (Hz)
Natural freq (Mode 700) = 53568.66000 (Hz)
Natural freq (Mode 701) = 53771.08000 (Hz)
Natural freq (Mode 702) = 53815.28000 (Hz)
Natural freq (Mode 703) = 53819.51000 (Hz)
Natural freq (Mode 704) = 54018.69000 (Hz)
Natural freq (Mode 705) = 54206.11000 (Hz)
Natural freq (Mode 706) = 54242.44000 (Hz)
Natural freq (Mode 707) = 54451.73000 (Hz)
Natural freq (Mode 708) = 54504.73000 (Hz)
Natural freq (Mode 709) = 54515.07000 (Hz)
Natural freq (Mode 710) = 54603.34000 (Hz)
Natural freq (Mode 711) = 54798.02000 (Hz)
Natural freq (Mode 712) = 54826.34000 (Hz)
Natural freq (Mode 713) = 54976.60000 (Hz)
Natural freq (Mode 714) = 55099.90000 (Hz)
Natural freq (Mode 715) = 55233.76000 (Hz)
Natural freq (Mode 716) = 55312.55000 (Hz)
Natural freq (Mode 717) = 55359.35000 (Hz)
Natural freq (Mode 718) = 55622.14000 (Hz)
Natural freq (Mode 719) = 55794.26000 (Hz)
Natural freq (Mode 720) = 55892.18000 (Hz)
Natural freq (Mode 721) = 56015.41000 (Hz)
Natural freq (Mode 722) = 56088.41000 (Hz)
Natural freq (Mode 723) = 56115.56000 (Hz)
Natural freq (Mode 724) = 56334.32000 (Hz)
Natural freq (Mode 725) = 56351.92000 (Hz)
Natural freq (Mode 726) = 56609.43000 (Hz)
Natural freq (Mode 727) = 56690.62000 (Hz)
Natural freq (Mode 728) = 56781.62000 (Hz)
Natural freq (Mode 729) = 56865.87000 (Hz)
Natural freq (Mode 730) = 56948.31000 (Hz)
Natural freq (Mode 731) = 57119.90000 (Hz)
Natural freq (Mode 732) = 57228.48000 (Hz)
Natural freq (Mode 733) = 57330.72000 (Hz)
Natural freq (Mode 734) = 57473.44000 (Hz)
Natural freq (Mode 735) = 57547.01000 (Hz)
Natural freq (Mode 736) = 57627.58000 (Hz)
Natural freq (Mode 737) = 57732.92000 (Hz)
Natural freq (Mode 738) = 57822.45000 (Hz)
Natural freq (Mode 739) = 57992.67000 (Hz)
Natural freq (Mode 740) = 58178.70000 (Hz)
Natural freq (Mode 741) = 58235.37000 (Hz)
Natural freq (Mode 742) = 58342.95000 (Hz)
Natural freq (Mode 743) = 58393.04000 (Hz)
Natural freq (Mode 744) = 58548.01000 (Hz)
Natural freq (Mode 745) = 58743.37000 (Hz)
Natural freq (Mode 746) = 58747.77000 (Hz)
Natural freq (Mode 747) = 58763.92000 (Hz)
Natural freq (Mode 748) = 58967.43000 (Hz)
Natural freq (Mode 749) = 59096.52000 (Hz)
Natural freq (Mode 750) = 59102.65000 (Hz)
Natural freq (Mode 751) = 59219.30000 (Hz)
Natural freq (Mode 752) = 59386.15000 (Hz)
Natural freq (Mode 753) = 59562.50000 (Hz)
Natural freq (Mode 754) = 59631.56000 (Hz)
Natural freq (Mode 755) = 59639.75000 (Hz)
Natural freq (Mode 756) = 59712.64000 (Hz)
Natural freq (Mode 757) = 59838.64000 (Hz)
Natural freq (Mode 758) = 59903.59000 (Hz)
Natural freq (Mode 759) = 60006.47000 (Hz)
Natural freq (Mode 760) = 60127.36000 (Hz)
Natural freq (Mode 761) = 60224.49000 (Hz)
Natural freq (Mode 762) = 60294.48000 (Hz)
Natural freq (Mode 763) = 60324.69000 (Hz)
Natural freq (Mode 764) = 60396.43000 (Hz)
Natural freq (Mode 765) = 60515.33000 (Hz)
Natural freq (Mode 766) = 60559.32000 (Hz)
Natural freq (Mode 767) = 60678.05000 (Hz)
Natural freq (Mode 768) = 60828.19000 (Hz)
Natural freq (Mode 769) = 60907.92000 (Hz)
Natural freq (Mode 770) = 61254.36000 (Hz)
Natural freq (Mode 771) = 61307.17000 (Hz)
Natural freq (Mode 772) = 61381.37000 (Hz)
Natural freq (Mode 773) = 61481.29000 (Hz)
Natural freq (Mode 774) = 61562.68000 (Hz)
Natural freq (Mode 775) = 61716.24000 (Hz)
Natural freq (Mode 776) = 61781.28000 (Hz)
Natural freq (Mode 777) = 61795.57000 (Hz)
Natural freq (Mode 778) = 61994.89000 (Hz)
Natural freq (Mode 779) = 62094.15000 (Hz)
Natural freq (Mode 780) = 62113.02000 (Hz)
Natural freq (Mode 781) = 62222.04000 (Hz)
Natural freq (Mode 782) = 62288.52000 (Hz)
Natural freq (Mode 783) = 62385.94000 (Hz)
Natural freq (Mode 784) = 62396.24000 (Hz)
Natural freq (Mode 785) = 62527.74000 (Hz)
Natural freq (Mode 786) = 62579.81000 (Hz)
Natural freq (Mode 787) = 62721.25000 (Hz)
Natural freq (Mode 788) = 62738.94000 (Hz)
Natural freq (Mode 789) = 62865.63000 (Hz)
Natural freq (Mode 790) = 62948.16000 (Hz)
Natural freq (Mode 791) = 63042.76000 (Hz)
Natural freq (Mode 792) = 63143.53000 (Hz)
Natural freq (Mode 793) = 63170.49000 (Hz)
Natural freq (Mode 794) = 63233.18000 (Hz)
Natural freq (Mode 795) = 63391.41000 (Hz)
Natural freq (Mode 796) = 63540.32000 (Hz)
Natural freq (Mode 797) = 63602.34000 (Hz)
Natural freq (Mode 798) = 63750.55000 (Hz)
Natural freq (Mode 799) = 63885.63000 (Hz)
Natural freq (Mode 800) = 63965.49000 (Hz)
Natural freq (Mode 801) = 64042.26000 (Hz)
Natural freq (Mode 802) = 64146.40000 (Hz)
Natural freq (Mode 803) = 64163.32000 (Hz)
Natural freq (Mode 804) = 64321.53000 (Hz)
Natural freq (Mode 805) = 64416.47000 (Hz)
Natural freq (Mode 806) = 64596.16000 (Hz)
Natural freq (Mode 807) = 64668.98000 (Hz)
Natural freq (Mode 808) = 64816.43000 (Hz)
Natural freq (Mode 809) = 64962.29000 (Hz)
Natural freq (Mode 810) = 65109.30000 (Hz)
Natural freq (Mode 811) = 65160.50000 (Hz)
Natural freq (Mode 812) = 65187.46000 (Hz)
Natural freq (Mode 813) = 65332.37000 (Hz)
Natural freq (Mode 814) = 65388.61000 (Hz)
Natural freq (Mode 815) = 65410.63000 (Hz)
Natural freq (Mode 816) = 65475.19000 (Hz)
Natural freq (Mode 817) = 65597.51000 (Hz)
Natural freq (Mode 818) = 65661.34000 (Hz)
Natural freq (Mode 819) = 65720.16000 (Hz)
Natural freq (Mode 820) = 65867.98000 (Hz)
Natural freq (Mode 821) = 66059.62000 (Hz)
Natural freq (Mode 822) = 66131.58000 (Hz)
Natural freq (Mode 823) = 66322.35000 (Hz)
Natural freq (Mode 824) = 66464.03000 (Hz)
Natural freq (Mode 825) = 66530.87000 (Hz)
Natural freq (Mode 826) = 66564.12000 (Hz)
Natural freq (Mode 827) = 66605.34000 (Hz)
Natural freq (Mode 828) = 66789.47000 (Hz)
Natural freq (Mode 829) = 66945.90000 (Hz)
Natural freq (Mode 830) = 66998.07000 (Hz)
Natural freq (Mode 831) = 67080.26000 (Hz)
Natural freq (Mode 832) = 67189.01000 (Hz)
Natural freq (Mode 833) = 67243.66000 (Hz)
Natural freq (Mode 834) = 67296.74000 (Hz)
Natural freq (Mode 835) = 67376.41000 (Hz)
Natural freq (Mode 836) = 67513.82000 (Hz)
Natural freq (Mode 837) = 67567.81000 (Hz)
Natural freq (Mode 838) = 67666.32000 (Hz)
Natural freq (Mode 839) = 67841.24000 (Hz)
Natural freq (Mode 840) = 67908.45000 (Hz)
Natural freq (Mode 841) = 68016.58000 (Hz)
Natural freq (Mode 842) = 68079.98000 (Hz)
Natural freq (Mode 843) = 68176.81000 (Hz)
Natural freq (Mode 844) = 68460.19000 (Hz)
Natural freq (Mode 845) = 68554.47000 (Hz)
Natural freq (Mode 846) = 68590.22000 (Hz)
Natural freq (Mode 847) = 68651.88000 (Hz)
Natural freq (Mode 848) = 68687.21000 (Hz)
Natural freq (Mode 849) = 68786.12000 (Hz)
Natural freq (Mode 850) = 68856.07000 (Hz)
Natural freq (Mode 851) = 68911.45000 (Hz)
Natural freq (Mode 852) = 68921.30000 (Hz)
Natural freq (Mode 853) = 69021.59000 (Hz)
Natural freq (Mode 854) = 69065.40000 (Hz)
Natural freq (Mode 855) = 69205.85000 (Hz)
Natural freq (Mode 856) = 69252.89000 (Hz)
Natural freq (Mode 857) = 69340.47000 (Hz)
Natural freq (Mode 858) = 69375.84000 (Hz)
Natural freq (Mode 859) = 69440.12000 (Hz)
Natural freq (Mode 860) = 69512.06000 (Hz)
Natural freq (Mode 861) = 69654.96000 (Hz)
Natural freq (Mode 862) = 69777.94000 (Hz)
Natural freq (Mode 863) = 69802.79000 (Hz)
Natural freq (Mode 864) = 69841.16000 (Hz)
Natural freq (Mode 865) = 69862.84000 (Hz)
Natural freq (Mode 866) = 70097.50000 (Hz)
Natural freq (Mode 867) = 70162.36000 (Hz)
Natural freq (Mode 868) = 70263.24000 (Hz)
Natural freq (Mode 869) = 70382.94000 (Hz)
Natural freq (Mode 870) = 70458.26000 (Hz)
Natural freq (Mode 871) = 70518.42000 (Hz)
Natural freq (Mode 872) = 70586.77000 (Hz)
Natural freq (Mode 873) = 70696.01000 (Hz)
Natural freq (Mode 874) = 70815.79000 (Hz)
Natural freq (Mode 875) = 70909.97000 (Hz)
Natural freq (Mode 876) = 70983.21000 (Hz)
Natural freq (Mode 877) = 71056.86000 (Hz)
Natural freq (Mode 878) = 71154.90000 (Hz)
Natural freq (Mode 879) = 71186.77000 (Hz)
Natural freq (Mode 880) = 71297.27000 (Hz)
Natural freq (Mode 881) = 71311.62000 (Hz)
Natural freq (Mode 882) = 71367.08000 (Hz)
Natural freq (Mode 883) = 71546.12000 (Hz)
Natural freq (Mode 884) = 71616.69000 (Hz)
Natural freq (Mode 885) = 71716.84000 (Hz)
Natural freq (Mode 886) = 71918.26000 (Hz)
Natural freq (Mode 887) = 72018.71000 (Hz)
Natural freq (Mode 888) = 72140.89000 (Hz)
Natural freq (Mode 889) = 72189.70000 (Hz)
Natural freq (Mode 890) = 72303.92000 (Hz)
Natural freq (Mode 891) = 72392.19000 (Hz)
Natural freq (Mode 892) = 72479.59000 (Hz)
Natural freq (Mode 893) = 72685.64000 (Hz)
Natural freq (Mode 894) = 72758.08000 (Hz)
Natural freq (Mode 895) = 72772.19000 (Hz)
Natural freq (Mode 896) = 72899.19000 (Hz)
Natural freq (Mode 897) = 73060.15000 (Hz)
Natural freq (Mode 898) = 73133.38000 (Hz)
Natural freq (Mode 899) = 73302.51000 (Hz)
Natural freq (Mode 900) = 73340.19000 (Hz)
Natural freq (Mode 901) = 73393.19000 (Hz)
Natural freq (Mode 902) = 73522.47000 (Hz)
Natural freq (Mode 903) = 73626.04000 (Hz)
Natural freq (Mode 904) = 73721.49000 (Hz)
Natural freq (Mode 905) = 73739.77000 (Hz)
Natural freq (Mode 906) = 73766.51000 (Hz)
Natural freq (Mode 907) = 73944.32000 (Hz)
Natural freq (Mode 908) = 74006.82000 (Hz)
Natural freq (Mode 909) = 74121.25000 (Hz)
Natural freq (Mode 910) = 74153.07000 (Hz)
Natural freq (Mode 911) = 74175.30000 (Hz)
Natural freq (Mode 912) = 74249.00000 (Hz)
Natural freq (Mode 913) = 74364.63000 (Hz)
Natural freq (Mode 914) = 74494.14000 (Hz)
Natural freq (Mode 915) = 74538.38000 (Hz)
Natural freq (Mode 916) = 74634.16000 (Hz)
Natural freq (Mode 917) = 74679.94000 (Hz)
Natural freq (Mode 918) = 74739.85000 (Hz)
Natural freq (Mode 919) = 74803.58000 (Hz)
Natural freq (Mode 920) = 74993.28000 (Hz)
Natural freq (Mode 921) = 75053.98000 (Hz)
Natural freq (Mode 922) = 75093.93000 (Hz)
Natural freq (Mode 923) = 75299.71000 (Hz)
Natural freq (Mode 924) = 75358.80000 (Hz)
Natural freq (Mode 925) = 75425.58000 (Hz)
Natural freq (Mode 926) = 75536.12000 (Hz)
Natural freq (Mode 927) = 75713.14000 (Hz)
Natural freq (Mode 928) = 75834.39000 (Hz)
Natural freq (Mode 929) = 75884.56000 (Hz)
Natural freq (Mode 930) = 76007.14000 (Hz)
Natural freq (Mode 931) = 76120.42000 (Hz)
Natural freq (Mode 932) = 76225.74000 (Hz)
Natural freq (Mode 933) = 76255.57000 (Hz)
Natural freq (Mode 934) = 76430.79000 (Hz)
Natural freq (Mode 935) = 76638.92000 (Hz)
Natural freq (Mode 936) = 76687.01000 (Hz)
Natural freq (Mode 937) = 76810.80000 (Hz)
Natural freq (Mode 938) = 76828.09000 (Hz)
Natural freq (Mode 939) = 76925.01000 (Hz)
Natural freq (Mode 940) = 77008.94000 (Hz)
Natural freq (Mode 941) = 77102.92000 (Hz)
Natural freq (Mode 942) = 77151.28000 (Hz)
Natural freq (Mode 943) = 77289.38000 (Hz)
Natural freq (Mode 944) = 77372.04000 (Hz)
Natural freq (Mode 945) = 77376.51000 (Hz)
Natural freq (Mode 946) = 77440.76000 (Hz)
Natural freq (Mode 947) = 77523.43000 (Hz)
Natural freq (Mode 948) = 77561.89000 (Hz)
Natural freq (Mode 949) = 77587.38000 (Hz)
Natural freq (Mode 950) = 77748.95000 (Hz)
Natural freq (Mode 951) = 77853.38000 (Hz)
Natural freq (Mode 952) = 77858.82000 (Hz)
Natural freq (Mode 953) = 77953.25000 (Hz)
Natural freq (Mode 954) = 78000.41000 (Hz)
Natural freq (Mode 955) = 78099.35000 (Hz)
Natural freq (Mode 956) = 78253.68000 (Hz)
Natural freq (Mode 957) = 78382.22000 (Hz)
Natural freq (Mode 958) = 78418.48000 (Hz)
Natural freq (Mode 959) = 78515.48000 (Hz)
Natural freq (Mode 960) = 78610.92000 (Hz)
Natural freq (Mode 961) = 78645.10000 (Hz)
Natural freq (Mode 962) = 78727.57000 (Hz)
Natural freq (Mode 963) = 78863.91000 (Hz)
Natural freq (Mode 964) = 78937.32000 (Hz)
Natural freq (Mode 965) = 79053.58000 (Hz)
Natural freq (Mode 966) = 79077.26000 (Hz)
Natural freq (Mode 967) = 79215.24000 (Hz)
Natural freq (Mode 968) = 79294.12000 (Hz)
Natural freq (Mode 969) = 79324.82000 (Hz)
Natural freq (Mode 970) = 79362.91000 (Hz)
Natural freq (Mode 971) = 79527.23000 (Hz)
Natural freq (Mode 972) = 79611.69000 (Hz)
Natural freq (Mode 973) = 79647.10000 (Hz)
Natural freq (Mode 974) = 79832.89000 (Hz)
Natural freq (Mode 975) = 79866.64000 (Hz)
Natural freq (Mode 976) = 79970.43000 (Hz)
Natural freq (Mode 977) = 80030.32000 (Hz)
Natural freq (Mode 978) = 80104.74000 (Hz)
Natural freq (Mode 979) = 80123.64000 (Hz)
Natural freq (Mode 980) = 80182.67000 (Hz)
Natural freq (Mode 981) = 80321.53000 (Hz)
Natural freq (Mode 982) = 80385.61000 (Hz)
Natural freq (Mode 983) = 80444.38000 (Hz)
Natural freq (Mode 984) = 80581.53000 (Hz)
Natural freq (Mode 985) = 80665.28000 (Hz)
Natural freq (Mode 986) = 80757.29000 (Hz)
Natural freq (Mode 987) = 80846.96000 (Hz)
Natural freq (Mode 988) = 81004.13000 (Hz)
Natural freq (Mode 989) = 81044.79000 (Hz)
Natural freq (Mode 990) = 81140.53000 (Hz)
Natural freq (Mode 991) = 81244.66000 (Hz)
Natural freq (Mode 992) = 81434.94000 (Hz)
Natural freq (Mode 993) = 81460.92000 (Hz)
Natural freq (Mode 994) = 81502.50000 (Hz)
Natural freq (Mode 995) = 81572.23000 (Hz)
Natural freq (Mode 996) = 81703.12000 (Hz)
Natural freq (Mode 997) = 81809.87000 (Hz)
Natural freq (Mode 998) = 81917.77000 (Hz)
Natural freq (Mode 999) = 81922.97000 (Hz)
Natural freq (Mode 1000) = 82100.35000 (Hz)
Natural freq (Mode 1001) = 82120.03000 (Hz)
Natural freq (Mode 1002) = 82160.63000 (Hz)
Natural freq (Mode 1003) = 82272.67000 (Hz)
Natural freq (Mode 1004) = 82375.92000 (Hz)
Natural freq (Mode 1005) = 82426.08000 (Hz)
Natural freq (Mode 1006) = 82607.53000 (Hz)
Natural freq (Mode 1007) = 82667.54000 (Hz)
Natural freq (Mode 1008) = 82795.73000 (Hz)
Natural freq (Mode 1009) = 82830.25000 (Hz)
Natural freq (Mode 1010) = 82913.56000 (Hz)
Natural freq (Mode 1011) = 83117.39000 (Hz)
Natural freq (Mode 1012) = 83264.48000 (Hz)
Natural freq (Mode 1013) = 83303.87000 (Hz)
Natural freq (Mode 1014) = 83383.77000 (Hz)
Natural freq (Mode 1015) = 83474.57000 (Hz)
Natural freq (Mode 1016) = 83564.55000 (Hz)
Natural freq (Mode 1017) = 83612.36000 (Hz)
Natural freq (Mode 1018) = 83635.59000 (Hz)
Natural freq (Mode 1019) = 83660.44000 (Hz)
Natural freq (Mode 1020) = 83784.58000 (Hz)
Natural freq (Mode 1021) = 83861.33000 (Hz)
Natural freq (Mode 1022) = 83937.67000 (Hz)
Natural freq (Mode 1023) = 84023.90000 (Hz)
Natural freq (Mode 1024) = 84139.57000 (Hz)
Natural freq (Mode 1025) = 84188.86000 (Hz)
Natural freq (Mode 1026) = 84266.69000 (Hz)
Natural freq (Mode 1027) = 84269.75000 (Hz)
Natural freq (Mode 1028) = 84309.34000 (Hz)
Natural freq (Mode 1029) = 84427.03000 (Hz)
Natural freq (Mode 1030) = 84673.20000 (Hz)
Natural freq (Mode 1031) = 84725.60000 (Hz)
Natural freq (Mode 1032) = 84802.77000 (Hz)
Natural freq (Mode 1033) = 84921.77000 (Hz)
Natural freq (Mode 1034) = 84960.34000 (Hz)
Natural freq (Mode 1035) = 85091.32000 (Hz)
Natural freq (Mode 1036) = 85116.43000 (Hz)
Natural freq (Mode 1037) = 85264.96000 (Hz)
Natural freq (Mode 1038) = 85286.54000 (Hz)
Natural freq (Mode 1039) = 85306.32000 (Hz)
Natural freq (Mode 1040) = 85421.91000 (Hz)
Natural freq (Mode 1041) = 85547.09000 (Hz)
Natural freq (Mode 1042) = 85661.92000 (Hz)
Natural freq (Mode 1043) = 85719.86000 (Hz)
Natural freq (Mode 1044) = 85749.15000 (Hz)
Natural freq (Mode 1045) = 85924.99000 (Hz)
Natural freq (Mode 1046) = 86089.57000 (Hz)
Natural freq (Mode 1047) = 86148.53000 (Hz)
Natural freq (Mode 1048) = 86302.17000 (Hz)
Natural freq (Mode 1049) = 86373.30000 (Hz)
Natural freq (Mode 1050) = 86491.27000 (Hz)
Natural freq (Mode 1051) = 86624.46000 (Hz)
Natural freq (Mode 1052) = 86658.50000 (Hz)
Natural freq (Mode 1053) = 86688.69000 (Hz)
Natural freq (Mode 1054) = 86846.44000 (Hz)
Natural freq (Mode 1055) = 86952.64000 (Hz)
Natural freq (Mode 1056) = 87074.96000 (Hz)
Natural freq (Mode 1057) = 87237.35000 (Hz)
Natural freq (Mode 1058) = 87398.33000 (Hz)
Natural freq (Mode 1059) = 87464.73000 (Hz)
Natural freq (Mode 1060) = 87561.27000 (Hz)
Natural freq (Mode 1061) = 87628.88000 (Hz)
Natural freq (Mode 1062) = 87672.54000 (Hz)
Natural freq (Mode 1063) = 87868.90000 (Hz)
Natural freq (Mode 1064) = 87909.61000 (Hz)
Natural freq (Mode 1065) = 87948.39000 (Hz)
Natural freq (Mode 1066) = 88031.61000 (Hz)
Natural freq (Mode 1067) = 88056.46000 (Hz)
Natural freq (Mode 1068) = 88172.09000 (Hz)
Natural freq (Mode 1069) = 88206.87000 (Hz)
Natural freq (Mode 1070) = 88308.04000 (Hz)
Natural freq (Mode 1071) = 88352.02000 (Hz)
Natural freq (Mode 1072) = 88465.10000 (Hz)
Natural freq (Mode 1073) = 88565.23000 (Hz)
Natural freq (Mode 1074) = 88657.34000 (Hz)
Natural freq (Mode 1075) = 88700.26000 (Hz)
Natural freq (Mode 1076) = 88709.47000 (Hz)
Natural freq (Mode 1077) = 88724.85000 (Hz)
Natural freq (Mode 1078) = 88816.78000 (Hz)
Natural freq (Mode 1079) = 88873.34000 (Hz)
Natural freq (Mode 1080) = 89020.17000 (Hz)
Natural freq (Mode 1081) = 89078.82000 (Hz)
Natural freq (Mode 1082) = 89146.32000 (Hz)
Natural freq (Mode 1083) = 89216.51000 (Hz)
Natural freq (Mode 1084) = 89285.04000 (Hz)
Natural freq (Mode 1085) = 89306.96000 (Hz)
Natural freq (Mode 1086) = 89439.18000 (Hz)
Natural freq (Mode 1087) = 89528.18000 (Hz)
Natural freq (Mode 1088) = 89620.32000 (Hz)
Natural freq (Mode 1089) = 89716.06000 (Hz)
Natural freq (Mode 1090) = 89813.61000 (Hz)
Natural freq (Mode 1091) = 89915.21000 (Hz)
Natural freq (Mode 1092) = 89957.09000 (Hz)
Natural freq (Mode 1093) = 90076.36000 (Hz)
Natural freq (Mode 1094) = 90217.64000 (Hz)
Natural freq (Mode 1095) = 90281.78000 (Hz)
Natural freq (Mode 1096) = 90337.50000 (Hz)
Natural freq (Mode 1097) = 90383.03000 (Hz)
Natural freq (Mode 1098) = 90467.45000 (Hz)
Natural freq (Mode 1099) = 90504.77000 (Hz)
Natural freq (Mode 1100) = 90625.35000 (Hz)
Natural freq (Mode 1101) = 90713.12000 (Hz)
Natural freq (Mode 1102) = 90740.85000 (Hz)
Natural freq (Mode 1103) = 90752.30000 (Hz)
Natural freq (Mode 1104) = 90845.66000 (Hz)
Natural freq (Mode 1105) = 90901.66000 (Hz)
Natural freq (Mode 1106) = 91071.76000 (Hz)
Natural freq (Mode 1107) = 91110.43000 (Hz)
Natural freq (Mode 1108) = 91256.23000 (Hz)
Natural freq (Mode 1109) = 91418.58000 (Hz)
Natural freq (Mode 1110) = 91547.07000 (Hz)
Natural freq (Mode 1111) = 91607.19000 (Hz)
Natural freq (Mode 1112) = 91650.98000 (Hz)
Natural freq (Mode 1113) = 91713.15000 (Hz)
Natural freq (Mode 1114) = 91833.30000 (Hz)
Natural freq (Mode 1115) = 91977.28000 (Hz)
Natural freq (Mode 1116) = 92097.01000 (Hz)
Natural freq (Mode 1117) = 92197.90000 (Hz)
Natural freq (Mode 1118) = 92227.72000 (Hz)
Natural freq (Mode 1119) = 92254.49000 (Hz)
Natural freq (Mode 1120) = 92434.76000 (Hz)
Natural freq (Mode 1121) = 92530.93000 (Hz)
Natural freq (Mode 1122) = 92547.32000 (Hz)
Natural freq (Mode 1123) = 92617.38000 (Hz)
Natural freq (Mode 1124) = 92860.10000 (Hz)
Natural freq (Mode 1125) = 92989.60000 (Hz)
Natural freq (Mode 1126) = 93070.57000 (Hz)
Natural freq (Mode 1127) = 93135.01000 (Hz)
Natural freq (Mode 1128) = 93268.29000 (Hz)
Natural freq (Mode 1129) = 93358.34000 (Hz)
Natural freq (Mode 1130) = 93369.00000 (Hz)
Natural freq (Mode 1131) = 93384.06000 (Hz)
Natural freq (Mode 1132) = 93491.51000 (Hz)
Natural freq (Mode 1133) = 93537.09000 (Hz)
Natural freq (Mode 1134) = 93562.33000 (Hz)
Natural freq (Mode 1135) = 93754.73000 (Hz)
Natural freq (Mode 1136) = 93814.21000 (Hz)
Natural freq (Mode 1137) = 93871.80000 (Hz)
Natural freq (Mode 1138) = 93938.57000 (Hz)
Natural freq (Mode 1139) = 94024.20000 (Hz)
Natural freq (Mode 1140) = 94128.21000 (Hz)
Natural freq (Mode 1141) = 94232.26000 (Hz)
Natural freq (Mode 1142) = 94351.51000 (Hz)
Natural freq (Mode 1143) = 94409.17000 (Hz)
Natural freq (Mode 1144) = 94558.20000 (Hz)
Natural freq (Mode 1145) = 94631.15000 (Hz)
Natural freq (Mode 1146) = 94732.62000 (Hz)
Natural freq (Mode 1147) = 94826.06000 (Hz)
Natural freq (Mode 1148) = 94976.99000 (Hz)
Natural freq (Mode 1149) = 95048.56000 (Hz)
Natural freq (Mode 1150) = 95181.86000 (Hz)
Natural freq (Mode 1151) = 95192.30000 (Hz)
Natural freq (Mode 1152) = 95297.16000 (Hz)
Natural freq (Mode 1153) = 95436.33000 (Hz)
Natural freq (Mode 1154) = 95618.01000 (Hz)
Natural freq (Mode 1155) = 95702.23000 (Hz)
Natural freq (Mode 1156) = 95750.83000 (Hz)
Natural freq (Mode 1157) = 95867.23000 (Hz)
Natural freq (Mode 1158) = 95962.79000 (Hz)
Natural freq (Mode 1159) = 96041.91000 (Hz)
Natural freq (Mode 1160) = 96091.17000 (Hz)
Natural freq (Mode 1161) = 96284.30000 (Hz)
Natural freq (Mode 1162) = 96348.77000 (Hz)
Natural freq (Mode 1163) = 96411.30000 (Hz)
Natural freq (Mode 1164) = 96457.12000 (Hz)
Natural freq (Mode 1165) = 96570.81000 (Hz)
Natural freq (Mode 1166) = 96623.90000 (Hz)
Natural freq (Mode 1167) = 96696.38000 (Hz)
Natural freq (Mode 1168) = 96737.32000 (Hz)
Natural freq (Mode 1169) = 96846.65000 (Hz)
Natural freq (Mode 1170) = 97008.36000 (Hz)
Natural freq (Mode 1171) = 97119.42000 (Hz)
Natural freq (Mode 1172) = 97233.69000 (Hz)
Natural freq (Mode 1173) = 97270.07000 (Hz)
Natural freq (Mode 1174) = 97447.92000 (Hz)
Natural freq (Mode 1175) = 97506.07000 (Hz)
Natural freq (Mode 1176) = 97594.28000 (Hz)
Natural freq (Mode 1177) = 97805.04000 (Hz)
Natural freq (Mode 1178) = 97894.72000 (Hz)
Natural freq (Mode 1179) = 97928.87000 (Hz)
Natural freq (Mode 1180) = 97981.40000 (Hz)
Natural freq (Mode 1181) = 98086.96000 (Hz)
Natural freq (Mode 1182) = 98117.62000 (Hz)
Natural freq (Mode 1183) = 98245.71000 (Hz)
Natural freq (Mode 1184) = 98360.74000 (Hz)
Natural freq (Mode 1185) = 98519.72000 (Hz)
Natural freq (Mode 1186) = 98691.42000 (Hz)
Natural freq (Mode 1187) = 98754.68000 (Hz)
Natural freq (Mode 1188) = 98877.99000 (Hz)
Natural freq (Mode 1189) = 98986.09000 (Hz)
Natural freq (Mode 1190) = 99067.69000 (Hz)
Natural freq (Mode 1191) = 99222.21000 (Hz)
Natural freq (Mode 1192) = 99324.10000 (Hz)
Natural freq (Mode 1193) = 99363.49000 (Hz)
Natural freq (Mode 1194) = 99552.85000 (Hz)
Natural freq (Mode 1195) = 99565.86000 (Hz)
Natural freq (Mode 1196) = 99651.71000 (Hz)
Natural freq (Mode 1197) = 99914.16000 (Hz)
Natural freq (Mode 1198) = 99997.05000 (Hz)
Natural freq (Mode 1199) = 100086.10000 (Hz)
Natural freq (Mode 1200) = 100112.50000 (Hz)
Natural freq (Mode 1201) = 100320.50000 (Hz)
Natural freq (Mode 1202) = 100334.10000 (Hz)
Natural freq (Mode 1203) = 100410.10000 (Hz)
Natural freq (Mode 1204) = 100520.60000 (Hz)
Natural freq (Mode 1205) = 100611.10000 (Hz)
Natural freq (Mode 1206) = 100756.50000 (Hz)
Natural freq (Mode 1207) = 100857.90000 (Hz)
Natural freq (Mode 1208) = 100906.60000 (Hz)
Natural freq (Mode 1209) = 101024.70000 (Hz)
Natural freq (Mode 1210) = 101217.30000 (Hz)
Natural freq (Mode 1211) = 101378.20000 (Hz)
Natural freq (Mode 1212) = 101425.90000 (Hz)
Natural freq (Mode 1213) = 101568.40000 (Hz)
Natural freq (Mode 1214) = 101649.20000 (Hz)
Natural freq (Mode 1215) = 101854.50000 (Hz)
Natural freq (Mode 1216) = 101859.60000 (Hz)
Natural freq (Mode 1217) = 102032.30000 (Hz)
Natural freq (Mode 1218) = 102118.70000 (Hz)
Natural freq (Mode 1219) = 102163.20000 (Hz)
Natural freq (Mode 1220) = 102309.80000 (Hz)
Natural freq (Mode 1221) = 102376.90000 (Hz)
Natural freq (Mode 1222) = 102475.10000 (Hz)
Natural freq (Mode 1223) = 102587.10000 (Hz)
Natural freq (Mode 1224) = 102626.40000 (Hz)
Natural freq (Mode 1225) = 102808.10000 (Hz)
Natural freq (Mode 1226) = 102999.10000 (Hz)
Natural freq (Mode 1227) = 103055.40000 (Hz)
Natural freq (Mode 1228) = 103153.30000 (Hz)
Natural freq (Mode 1229) = 103210.50000 (Hz)
Natural freq (Mode 1230) = 103389.80000 (Hz)
Natural freq (Mode 1231) = 103567.90000 (Hz)
Natural freq (Mode 1232) = 103741.10000 (Hz)
Natural freq (Mode 1233) = 103800.40000 (Hz)
Natural freq (Mode 1234) = 103844.10000 (Hz)
Natural freq (Mode 1235) = 103957.40000 (Hz)
Natural freq (Mode 1236) = 104142.80000 (Hz)
Natural freq (Mode 1237) = 104186.80000 (Hz)
Natural freq (Mode 1238) = 104368.90000 (Hz)
Natural freq (Mode 1239) = 104521.90000 (Hz)
Natural freq (Mode 1240) = 104605.60000 (Hz)
Natural freq (Mode 1241) = 104640.40000 (Hz)
Natural freq (Mode 1242) = 104752.90000 (Hz)
Natural freq (Mode 1243) = 104877.60000 (Hz)
Natural freq (Mode 1244) = 104974.20000 (Hz)
Natural freq (Mode 1245) = 105069.10000 (Hz)
Natural freq (Mode 1246) = 105261.70000 (Hz)
Natural freq (Mode 1247) = 105316.40000 (Hz)
Natural freq (Mode 1248) = 105535.40000 (Hz)
Natural freq (Mode 1249) = 105616.20000 (Hz)
Natural freq (Mode 1250) = 105792.20000 (Hz)
Natural freq (Mode 1251) = 105817.40000 (Hz)
Natural freq (Mode 1252) = 105974.60000 (Hz)
Natural freq (Mode 1253) = 106104.30000 (Hz)
Natural freq (Mode 1254) = 106143.00000 (Hz)
Natural freq (Mode 1255) = 106291.00000 (Hz)
Natural freq (Mode 1256) = 106393.00000 (Hz)
Natural freq (Mode 1257) = 106517.20000 (Hz)
Natural freq (Mode 1258) = 106601.60000 (Hz)
Natural freq (Mode 1259) = 106776.20000 (Hz)
Natural freq (Mode 1260) = 106847.60000 (Hz)
Natural freq (Mode 1261) = 106928.10000 (Hz)
Natural freq (Mode 1262) = 107010.40000 (Hz)
Natural freq (Mode 1263) = 107146.40000 (Hz)
Natural freq (Mode 1264) = 107311.10000 (Hz)
Natural freq (Mode 1265) = 107361.80000 (Hz)
Natural freq (Mode 1266) = 107415.20000 (Hz)
Natural freq (Mode 1267) = 107609.10000 (Hz)
Natural freq (Mode 1268) = 107719.30000 (Hz)
Natural freq (Mode 1269) = 108001.00000 (Hz)
Natural freq (Mode 1270) = 108061.80000 (Hz)
Natural freq (Mode 1271) = 108076.50000 (Hz)
Natural freq (Mode 1272) = 108252.70000 (Hz)
Natural freq (Mode 1273) = 108325.20000 (Hz)
Natural freq (Mode 1274) = 108375.60000 (Hz)
Natural freq (Mode 1275) = 108506.50000 (Hz)
Natural freq (Mode 1276) = 108549.10000 (Hz)
Natural freq (Mode 1277) = 108709.70000 (Hz)
Natural freq (Mode 1278) = 108776.70000 (Hz)
Natural freq (Mode 1279) = 108840.10000 (Hz)
Natural freq (Mode 1280) = 109176.60000 (Hz)
Natural freq (Mode 1281) = 109253.60000 (Hz)
Natural freq (Mode 1282) = 109305.80000 (Hz)
Natural freq (Mode 1283) = 109383.00000 (Hz)
Natural freq (Mode 1284) = 109470.60000 (Hz)
Natural freq (Mode 1285) = 109580.90000 (Hz)
Natural freq (Mode 1286) = 109637.50000 (Hz)
Natural freq (Mode 1287) = 109903.10000 (Hz)
Natural freq (Mode 1288) = 109941.40000 (Hz)
Natural freq (Mode 1289) = 109970.10000 (Hz)
Natural freq (Mode 1290) = 110176.20000 (Hz)
Natural freq (Mode 1291) = 110262.20000 (Hz)
Natural freq (Mode 1292) = 110397.60000 (Hz)
Natural freq (Mode 1293) = 110469.50000 (Hz)
Natural freq (Mode 1294) = 110498.80000 (Hz)
Natural freq (Mode 1295) = 110660.80000 (Hz)
Natural freq (Mode 1296) = 110709.90000 (Hz)
Natural freq (Mode 1297) = 110855.40000 (Hz)
Natural freq (Mode 1298) = 111003.50000 (Hz)
Natural freq (Mode 1299) = 111108.40000 (Hz)
Natural freq (Mode 1300) = 111239.20000 (Hz)
Natural freq (Mode 1301) = 111263.50000 (Hz)
Natural freq (Mode 1302) = 111446.80000 (Hz)
Natural freq (Mode 1303) = 111644.50000 (Hz)
Natural freq (Mode 1304) = 111765.20000 (Hz)
Natural freq (Mode 1305) = 111843.10000 (Hz)
Natural freq (Mode 1306) = 111987.60000 (Hz)
Natural freq (Mode 1307) = 112035.40000 (Hz)
Natural freq (Mode 1308) = 112128.30000 (Hz)
Natural freq (Mode 1309) = 112392.30000 (Hz)
Natural freq (Mode 1310) = 112433.70000 (Hz)
Natural freq (Mode 1311) = 112461.80000 (Hz)
Natural freq (Mode 1312) = 112598.60000 (Hz)
Natural freq (Mode 1313) = 112674.70000 (Hz)
Natural freq (Mode 1314) = 112785.90000 (Hz)
Natural freq (Mode 1315) = 112877.40000 (Hz)
Natural freq (Mode 1316) = 112951.70000 (Hz)
Natural freq (Mode 1317) = 113078.10000 (Hz)
Natural freq (Mode 1318) = 113182.60000 (Hz)
Natural freq (Mode 1319) = 113251.80000 (Hz)
Natural freq (Mode 1320) = 113572.60000 (Hz)
Natural freq (Mode 1321) = 113614.80000 (Hz)
Natural freq (Mode 1322) = 113655.60000 (Hz)
Natural freq (Mode 1323) = 114032.30000 (Hz)
Natural freq (Mode 1324) = 114186.80000 (Hz)
Natural freq (Mode 1325) = 114294.00000 (Hz)
Natural freq (Mode 1326) = 114354.20000 (Hz)
Natural freq (Mode 1327) = 114521.20000 (Hz)
Natural freq (Mode 1328) = 114551.30000 (Hz)
Natural freq (Mode 1329) = 114600.10000 (Hz)
Natural freq (Mode 1330) = 114716.60000 (Hz)
Natural freq (Mode 1331) = 114808.50000 (Hz)
Natural freq (Mode 1332) = 114961.50000 (Hz)
Natural freq (Mode 1333) = 115052.60000 (Hz)
Natural freq (Mode 1334) = 115156.20000 (Hz)
Natural freq (Mode 1335) = 115377.20000 (Hz)
Natural freq (Mode 1336) = 115484.80000 (Hz)
Natural freq (Mode 1337) = 115597.90000 (Hz)
Natural freq (Mode 1338) = 115718.90000 (Hz)
Natural freq (Mode 1339) = 115960.20000 (Hz)
Natural freq (Mode 1340) = 116114.10000 (Hz)
Natural freq (Mode 1341) = 116243.00000 (Hz)
Natural freq (Mode 1342) = 116262.40000 (Hz)
Natural freq (Mode 1343) = 116413.40000 (Hz)
Natural freq (Mode 1344) = 116477.70000 (Hz)
Natural freq (Mode 1345) = 116555.20000 (Hz)
Natural freq (Mode 1346) = 116672.70000 (Hz)
Natural freq (Mode 1347) = 116713.00000 (Hz)
Natural freq (Mode 1348) = 116874.30000 (Hz)
Natural freq (Mode 1349) = 117031.80000 (Hz)
Natural freq (Mode 1350) = 117183.70000 (Hz)
Natural freq (Mode 1351) = 117264.80000 (Hz)
Natural freq (Mode 1352) = 117412.80000 (Hz)
Natural freq (Mode 1353) = 117527.50000 (Hz)
Natural freq (Mode 1354) = 117697.90000 (Hz)
Natural freq (Mode 1355) = 117771.70000 (Hz)
Natural freq (Mode 1356) = 117868.10000 (Hz)
Natural freq (Mode 1357) = 117969.50000 (Hz)
Natural freq (Mode 1358) = 118129.50000 (Hz)
Natural freq (Mode 1359) = 118302.40000 (Hz)
Natural freq (Mode 1360) = 118370.90000 (Hz)
Natural freq (Mode 1361) = 118419.00000 (Hz)
Natural freq (Mode 1362) = 118571.50000 (Hz)
Natural freq (Mode 1363) = 118877.20000 (Hz)
Natural freq (Mode 1364) = 118947.70000 (Hz)
Natural freq (Mode 1365) = 118997.70000 (Hz)
Natural freq (Mode 1366) = 119126.20000 (Hz)
Natural freq (Mode 1367) = 119270.50000 (Hz)
Natural freq (Mode 1368) = 119406.20000 (Hz)
Natural freq (Mode 1369) = 119511.30000 (Hz)
Natural freq (Mode 1370) = 119574.30000 (Hz)
Natural freq (Mode 1371) = 119781.00000 (Hz)
Natural freq (Mode 1372) = 119933.60000 (Hz)
Natural freq (Mode 1373) = 120145.60000 (Hz)
Natural freq (Mode 1374) = 120190.00000 (Hz)
Natural freq (Mode 1375) = 120321.80000 (Hz)
Natural freq (Mode 1376) = 120353.10000 (Hz)
Natural freq (Mode 1377) = 120597.80000 (Hz)
Natural freq (Mode 1378) = 120644.50000 (Hz)
Natural freq (Mode 1379) = 120725.60000 (Hz)
Natural freq (Mode 1380) = 120837.90000 (Hz)
Natural freq (Mode 1381) = 120870.10000 (Hz)
Natural freq (Mode 1382) = 121080.50000 (Hz)
Natural freq (Mode 1383) = 121177.30000 (Hz)
Natural freq (Mode 1384) = 121278.30000 (Hz)
Natural freq (Mode 1385) = 121504.70000 (Hz)
Natural freq (Mode 1386) = 121567.70000 (Hz)
Natural freq (Mode 1387) = 121628.50000 (Hz)
Natural freq (Mode 1388) = 121743.40000 (Hz)
Natural freq (Mode 1389) = 121787.00000 (Hz)
Natural freq (Mode 1390) = 122020.70000 (Hz)
Natural freq (Mode 1391) = 122085.30000 (Hz)
Natural freq (Mode 1392) = 122227.70000 (Hz)
Natural freq (Mode 1393) = 122430.00000 (Hz)
Natural freq (Mode 1394) = 122517.90000 (Hz)
Natural freq (Mode 1395) = 122566.40000 (Hz)
Natural freq (Mode 1396) = 122794.80000 (Hz)
Natural freq (Mode 1397) = 122905.20000 (Hz)
Natural freq (Mode 1398) = 123064.90000 (Hz)
Natural freq (Mode 1399) = 123171.70000 (Hz)
Natural freq (Mode 1400) = 123264.40000 (Hz)
Natural freq (Mode 1401) = 123359.30000 (Hz)
Natural freq (Mode 1402) = 123494.90000 (Hz)
Natural freq (Mode 1403) = 123758.80000 (Hz)
Natural freq (Mode 1404) = 123897.70000 (Hz)
Natural freq (Mode 1405) = 124106.20000 (Hz)
Natural freq (Mode 1406) = 124163.70000 (Hz)
Natural freq (Mode 1407) = 124297.60000 (Hz)
Natural freq (Mode 1408) = 124377.30000 (Hz)
Natural freq (Mode 1409) = 124544.60000 (Hz)
Natural freq (Mode 1410) = 124658.30000 (Hz)
Natural freq (Mode 1411) = 124674.60000 (Hz)
Natural freq (Mode 1412) = 124969.70000 (Hz)
Natural freq (Mode 1413) = 125010.20000 (Hz)
Natural freq (Mode 1414) = 125106.50000 (Hz)
Natural freq (Mode 1415) = 125287.30000 (Hz)
Natural freq (Mode 1416) = 125364.30000 (Hz)
Natural freq (Mode 1417) = 125496.00000 (Hz)
Natural freq (Mode 1418) = 125668.20000 (Hz)
Natural freq (Mode 1419) = 125806.90000 (Hz)
Natural freq (Mode 1420) = 125859.20000 (Hz)
Natural freq (Mode 1421) = 126124.10000 (Hz)
Natural freq (Mode 1422) = 126336.10000 (Hz)
Natural freq (Mode 1423) = 126512.70000 (Hz)
Natural freq (Mode 1424) = 126539.10000 (Hz)
Natural freq (Mode 1425) = 126620.50000 (Hz)
Natural freq (Mode 1426) = 126877.60000 (Hz)
Natural freq (Mode 1427) = 126962.30000 (Hz)
Natural freq (Mode 1428) = 127132.20000 (Hz)
Natural freq (Mode 1429) = 127254.70000 (Hz)
Natural freq (Mode 1430) = 127477.10000 (Hz)
Natural freq (Mode 1431) = 127659.30000 (Hz)
Natural freq (Mode 1432) = 127893.90000 (Hz)
Natural freq (Mode 1433) = 127957.60000 (Hz)
Natural freq (Mode 1434) = 128099.20000 (Hz)
Natural freq (Mode 1435) = 128180.30000 (Hz)
Natural freq (Mode 1436) = 128320.40000 (Hz)
Natural freq (Mode 1437) = 128363.50000 (Hz)
Natural freq (Mode 1438) = 128546.60000 (Hz)
Natural freq (Mode 1439) = 128764.90000 (Hz)
Natural freq (Mode 1440) = 128804.00000 (Hz)
Natural freq (Mode 1441) = 128925.30000 (Hz)
Natural freq (Mode 1442) = 128959.00000 (Hz)
Natural freq (Mode 1443) = 128969.90000 (Hz)
Natural freq (Mode 1444) = 129220.00000 (Hz)
Natural freq (Mode 1445) = 129323.20000 (Hz)
Natural freq (Mode 1446) = 129474.70000 (Hz)
Natural freq (Mode 1447) = 129675.90000 (Hz)
Natural freq (Mode 1448) = 129703.10000 (Hz)
Natural freq (Mode 1449) = 130113.10000 (Hz)
Natural freq (Mode 1450) = 130185.80000 (Hz)
Natural freq (Mode 1451) = 130348.10000 (Hz)
Natural freq (Mode 1452) = 130578.30000 (Hz)
Natural freq (Mode 1453) = 130708.50000 (Hz)
Natural freq (Mode 1454) = 130869.20000 (Hz)
Natural freq (Mode 1455) = 130922.50000 (Hz)
Natural freq (Mode 1456) = 131020.90000 (Hz)
Natural freq (Mode 1457) = 131122.90000 (Hz)
Natural freq (Mode 1458) = 131424.50000 (Hz)
Natural freq (Mode 1459) = 131584.80000 (Hz)
Natural freq (Mode 1460) = 131684.30000 (Hz)
Natural freq (Mode 1461) = 131809.90000 (Hz)
Natural freq (Mode 1462) = 131858.60000 (Hz)
Natural freq (Mode 1463) = 131958.50000 (Hz)
Natural freq (Mode 1464) = 132233.70000 (Hz)
Natural freq (Mode 1465) = 132449.40000 (Hz)
Natural freq (Mode 1466) = 132607.40000 (Hz)
Natural freq (Mode 1467) = 132729.70000 (Hz)
Natural freq (Mode 1468) = 132880.40000 (Hz)
Natural freq (Mode 1469) = 133046.80000 (Hz)
Natural freq (Mode 1470) = 133201.30000 (Hz)
Natural freq (Mode 1471) = 133234.10000 (Hz)
Natural freq (Mode 1472) = 133629.50000 (Hz)
Natural freq (Mode 1473) = 133796.90000 (Hz)
Natural freq (Mode 1474) = 133948.40000 (Hz)
Natural freq (Mode 1475) = 134006.30000 (Hz)
Natural freq (Mode 1476) = 134324.40000 (Hz)
Natural freq (Mode 1477) = 134507.70000 (Hz)
Natural freq (Mode 1478) = 134620.10000 (Hz)
Natural freq (Mode 1479) = 134837.70000 (Hz)
Natural freq (Mode 1480) = 134916.50000 (Hz)
Natural freq (Mode 1481) = 135097.00000 (Hz)
Natural freq (Mode 1482) = 135137.40000 (Hz)
Natural freq (Mode 1483) = 135476.30000 (Hz)
Natural freq (Mode 1484) = 135553.40000 (Hz)
Natural freq (Mode 1485) = 135680.90000 (Hz)
Natural freq (Mode 1486) = 135723.70000 (Hz)
Natural freq (Mode 1487) = 136137.20000 (Hz)
Natural freq (Mode 1488) = 136254.00000 (Hz)
Natural freq (Mode 1489) = 136531.70000 (Hz)
Natural freq (Mode 1490) = 136629.60000 (Hz)
Natural freq (Mode 1491) = 136739.30000 (Hz)
Natural freq (Mode 1492) = 136927.00000 (Hz)
Natural freq (Mode 1493) = 136989.70000 (Hz)
Natural freq (Mode 1494) = 137183.70000 (Hz)
Natural freq (Mode 1495) = 137230.00000 (Hz)
Natural freq (Mode 1496) = 137313.30000 (Hz)
Natural freq (Mode 1497) = 137520.90000 (Hz)
Natural freq (Mode 1498) = 137639.00000 (Hz)
Natural freq (Mode 1499) = 138090.60000 (Hz)
Natural freq (Mode 1500) = 138387.40000 (Hz)
Natural freq (Mode 1501) = 138465.10000 (Hz)
Natural freq (Mode 1502) = 138815.80000 (Hz)
Natural freq (Mode 1503) = 138915.10000 (Hz)
Natural freq (Mode 1504) = 138942.60000 (Hz)
Natural freq (Mode 1505) = 139174.70000 (Hz)
Natural freq (Mode 1506) = 139199.90000 (Hz)
Natural freq (Mode 1507) = 139357.90000 (Hz)
Natural freq (Mode 1508) = 139425.70000 (Hz)
Natural freq (Mode 1509) = 139577.30000 (Hz)
Natural freq (Mode 1510) = 139690.00000 (Hz)
Natural freq (Mode 1511) = 139888.50000 (Hz)
Natural freq (Mode 1512) = 140098.70000 (Hz)
Natural freq (Mode 1513) = 140249.80000 (Hz)
Natural freq (Mode 1514) = 140367.30000 (Hz)
Natural freq (Mode 1515) = 140657.00000 (Hz)
Natural freq (Mode 1516) = 140786.00000 (Hz)
Natural freq (Mode 1517) = 141026.50000 (Hz)
Natural freq (Mode 1518) = 141186.20000 (Hz)
Natural freq (Mode 1519) = 141405.70000 (Hz)
Natural freq (Mode 1520) = 141619.60000 (Hz)
Natural freq (Mode 1521) = 141793.30000 (Hz)
Natural freq (Mode 1522) = 142003.20000 (Hz)
Natural freq (Mode 1523) = 142060.70000 (Hz)
Natural freq (Mode 1524) = 142212.40000 (Hz)
Natural freq (Mode 1525) = 142235.00000 (Hz)
Natural freq (Mode 1526) = 142422.80000 (Hz)
Natural freq (Mode 1527) = 142663.20000 (Hz)
Natural freq (Mode 1528) = 143052.20000 (Hz)
Natural freq (Mode 1529) = 143084.90000 (Hz)
Natural freq (Mode 1530) = 143132.30000 (Hz)
Natural freq (Mode 1531) = 143274.40000 (Hz)
Natural freq (Mode 1532) = 143396.20000 (Hz)
Natural freq (Mode 1533) = 143756.70000 (Hz)
Natural freq (Mode 1534) = 143943.30000 (Hz)
Natural freq (Mode 1535) = 144127.80000 (Hz)
Natural freq (Mode 1536) = 144235.40000 (Hz)
Natural freq (Mode 1537) = 144542.10000 (Hz)
Natural freq (Mode 1538) = 144662.30000 (Hz)
Natural freq (Mode 1539) = 144690.70000 (Hz)
Natural freq (Mode 1540) = 144771.30000 (Hz)
Natural freq (Mode 1541) = 145039.90000 (Hz)
Natural freq (Mode 1542) = 145151.10000 (Hz)
Natural freq (Mode 1543) = 145284.10000 (Hz)
Natural freq (Mode 1544) = 145642.50000 (Hz)
Natural freq (Mode 1545) = 146249.40000 (Hz)
Natural freq (Mode 1546) = 146402.00000 (Hz)
Natural freq (Mode 1547) = 146685.30000 (Hz)
Natural freq (Mode 1548) = 146725.90000 (Hz)
Natural freq (Mode 1549) = 146784.20000 (Hz)
Natural freq (Mode 1550) = 146916.60000 (Hz)
Natural freq (Mode 1551) = 147213.30000 (Hz)
Natural freq (Mode 1552) = 147379.50000 (Hz)
Natural freq (Mode 1553) = 147702.80000 (Hz)
Natural freq (Mode 1554) = 148135.00000 (Hz)
Natural freq (Mode 1555) = 148211.80000 (Hz)
Natural freq (Mode 1556) = 148385.40000 (Hz)
Natural freq (Mode 1557) = 148579.80000 (Hz)
Natural freq (Mode 1558) = 148840.20000 (Hz)
Natural freq (Mode 1559) = 148989.20000 (Hz)
Natural freq (Mode 1560) = 149117.70000 (Hz)
Natural freq (Mode 1561) = 149384.50000 (Hz)
Natural freq (Mode 1562) = 149901.10000 (Hz)
Natural freq (Mode 1563) = 150012.00000 (Hz)
Natural freq (Mode 1564) = 150026.60000 (Hz)
Natural freq (Mode 1565) = 150123.80000 (Hz)
Natural freq (Mode 1566) = 150212.80000 (Hz)
Natural freq (Mode 1567) = 150535.40000 (Hz)
Natural freq (Mode 1568) = 150791.90000 (Hz)
Natural freq (Mode 1569) = 151291.00000 (Hz)
Natural freq (Mode 1570) = 151469.60000 (Hz)
Natural freq (Mode 1571) = 151604.60000 (Hz)
Natural freq (Mode 1572) = 151672.40000 (Hz)
Natural freq (Mode 1573) = 151822.30000 (Hz)
Natural freq (Mode 1574) = 152226.20000 (Hz)
Natural freq (Mode 1575) = 152338.60000 (Hz)
Natural freq (Mode 1576) = 152687.80000 (Hz)
Natural freq (Mode 1577) = 152820.80000 (Hz)
Natural freq (Mode 1578) = 153515.50000 (Hz)
Natural freq (Mode 1579) = 153649.70000 (Hz)
Natural freq (Mode 1580) = 153716.80000 (Hz)
Natural freq (Mode 1581) = 154080.40000 (Hz)
Natural freq (Mode 1582) = 154227.00000 (Hz)
Natural freq (Mode 1583) = 154281.30000 (Hz)
Natural freq (Mode 1584) = 154350.30000 (Hz)
Natural freq (Mode 1585) = 154510.10000 (Hz)
Natural freq (Mode 1586) = 154829.60000 (Hz)
Natural freq (Mode 1587) = 155355.80000 (Hz)
Natural freq (Mode 1588) = 155436.70000 (Hz)
Natural freq (Mode 1589) = 155641.50000 (Hz)
Natural freq (Mode 1590) = 155881.40000 (Hz)
Natural freq (Mode 1591) = 155898.70000 (Hz)
Natural freq (Mode 1592) = 156045.80000 (Hz)
Natural freq (Mode 1593) = 156632.20000 (Hz)
Natural freq (Mode 1594) = 156715.70000 (Hz)
Natural freq (Mode 1595) = 156944.30000 (Hz)
Natural freq (Mode 1596) = 156959.70000 (Hz)
Natural freq (Mode 1597) = 157074.30000 (Hz)
Natural freq (Mode 1598) = 157281.40000 (Hz)
Natural freq (Mode 1599) = 157509.00000 (Hz)
Natural freq (Mode 1600) = 157672.90000 (Hz)
Natural freq (Mode 1601) = 157765.50000 (Hz)
Natural freq (Mode 1602) = 157847.60000 (Hz)
Natural freq (Mode 1603) = 157987.50000 (Hz)
Natural freq (Mode 1604) = 158062.80000 (Hz)
Natural freq (Mode 1605) = 158390.60000 (Hz)
Natural freq (Mode 1606) = 158600.10000 (Hz)
Natural freq (Mode 1607) = 158957.10000 (Hz)
Natural freq (Mode 1608) = 159008.80000 (Hz)
Natural freq (Mode 1609) = 159347.70000 (Hz)
Natural freq (Mode 1610) = 159448.00000 (Hz)
Natural freq (Mode 1611) = 160017.90000 (Hz)
Natural freq (Mode 1612) = 160125.80000 (Hz)
Natural freq (Mode 1613) = 160197.70000 (Hz)
Natural freq (Mode 1614) = 160403.10000 (Hz)
Natural freq (Mode 1615) = 160624.50000 (Hz)
Natural freq (Mode 1616) = 160755.70000 (Hz)
Natural freq (Mode 1617) = 160803.50000 (Hz)
Natural freq (Mode 1618) = 160976.60000 (Hz)
Natural freq (Mode 1619) = 161448.10000 (Hz)
Natural freq (Mode 1620) = 161586.90000 (Hz)
Natural freq (Mode 1621) = 161815.20000 (Hz)
Natural freq (Mode 1622) = 161986.90000 (Hz)
Natural freq (Mode 1623) = 162466.80000 (Hz)
Natural freq (Mode 1624) = 162566.50000 (Hz)
Natural freq (Mode 1625) = 162608.40000 (Hz)
Natural freq (Mode 1626) = 162717.60000 (Hz)
Natural freq (Mode 1627) = 162844.00000 (Hz)
Natural freq (Mode 1628) = 163278.60000 (Hz)
Natural freq (Mode 1629) = 163309.40000 (Hz)
Natural freq (Mode 1630) = 163964.70000 (Hz)
Natural freq (Mode 1631) = 164005.10000 (Hz)
Natural freq (Mode 1632) = 164261.60000 (Hz)
Natural freq (Mode 1633) = 164326.10000 (Hz)
Natural freq (Mode 1634) = 164590.90000 (Hz)
Natural freq (Mode 1635) = 164656.90000 (Hz)
Natural freq (Mode 1636) = 165096.90000 (Hz)
Natural freq (Mode 1637) = 165297.50000 (Hz)
Natural freq (Mode 1638) = 165804.30000 (Hz)
Natural freq (Mode 1639) = 166068.20000 (Hz)
Natural freq (Mode 1640) = 166457.30000 (Hz)
Natural freq (Mode 1641) = 166514.40000 (Hz)
Natural freq (Mode 1642) = 166618.00000 (Hz)
Natural freq (Mode 1643) = 167181.10000 (Hz)
Natural freq (Mode 1644) = 167769.30000 (Hz)
Natural freq (Mode 1645) = 167803.40000 (Hz)
Natural freq (Mode 1646) = 167887.70000 (Hz)
Natural freq (Mode 1647) = 167937.00000 (Hz)
Natural freq (Mode 1648) = 168171.80000 (Hz)
Natural freq (Mode 1649) = 168637.70000 (Hz)
Natural freq (Mode 1650) = 168827.00000 (Hz)
Natural freq (Mode 1651) = 168918.90000 (Hz)
Natural freq (Mode 1652) = 169013.80000 (Hz)
Natural freq (Mode 1653) = 169143.70000 (Hz)
Natural freq (Mode 1654) = 169595.50000 (Hz)
Natural freq (Mode 1655) = 169874.10000 (Hz)
Natural freq (Mode 1656) = 169886.40000 (Hz)
Natural freq (Mode 1657) = 169891.20000 (Hz)
Natural freq (Mode 1658) = 169934.80000 (Hz)
Natural freq (Mode 1659) = 170188.10000 (Hz)
Natural freq (Mode 1660) = 170651.40000 (Hz)
Natural freq (Mode 1661) = 170659.80000 (Hz)
Natural freq (Mode 1662) = 171236.50000 (Hz)
Natural freq (Mode 1663) = 171387.80000 (Hz)
Natural freq (Mode 1664) = 171667.50000 (Hz)
Natural freq (Mode 1665) = 171785.20000 (Hz)
Natural freq (Mode 1666) = 172104.00000 (Hz)
Natural freq (Mode 1667) = 172379.30000 (Hz)
Natural freq (Mode 1668) = 172531.20000 (Hz)
Natural freq (Mode 1669) = 173061.80000 (Hz)
Natural freq (Mode 1670) = 173218.80000 (Hz)
Natural freq (Mode 1671) = 173992.60000 (Hz)
Natural freq (Mode 1672) = 174199.60000 (Hz)
Natural freq (Mode 1673) = 174311.20000 (Hz)
Natural freq (Mode 1674) = 174609.30000 (Hz)
Natural freq (Mode 1675) = 174851.40000 (Hz)
Natural freq (Mode 1676) = 175088.40000 (Hz)
Natural freq (Mode 1677) = 175104.80000 (Hz)
Natural freq (Mode 1678) = 175240.60000 (Hz)
Natural freq (Mode 1679) = 175725.80000 (Hz)
Natural freq (Mode 1680) = 175958.00000 (Hz)
Natural freq (Mode 1681) = 176785.50000 (Hz)
Natural freq (Mode 1682) = 176887.90000 (Hz)
Natural freq (Mode 1683) = 176960.70000 (Hz)
Natural freq (Mode 1684) = 177004.30000 (Hz)
Natural freq (Mode 1685) = 177410.10000 (Hz)
Natural freq (Mode 1686) = 177613.00000 (Hz)
Natural freq (Mode 1687) = 177999.40000 (Hz)
Natural freq (Mode 1688) = 178203.10000 (Hz)
Natural freq (Mode 1689) = 178443.20000 (Hz)
Natural freq (Mode 1690) = 179265.20000 (Hz)
Natural freq (Mode 1691) = 179577.40000 (Hz)
Natural freq (Mode 1692) = 179735.20000 (Hz)
Natural freq (Mode 1693) = 179903.20000 (Hz)
Natural freq (Mode 1694) = 180130.10000 (Hz)
Natural freq (Mode 1695) = 180359.50000 (Hz)
Natural freq (Mode 1696) = 180434.90000 (Hz)
Natural freq (Mode 1697) = 181385.00000 (Hz)
Natural freq (Mode 1698) = 181992.60000 (Hz)
Natural freq (Mode 1699) = 182050.10000 (Hz)
Natural freq (Mode 1700) = 182062.40000 (Hz)
Natural freq (Mode 1701) = 183019.60000 (Hz)
Natural freq (Mode 1702) = 183208.80000 (Hz)
Natural freq (Mode 1703) = 183609.70000 (Hz)
Natural freq (Mode 1704) = 184158.80000 (Hz)
Natural freq (Mode 1705) = 184251.30000 (Hz)
Natural freq (Mode 1706) = 184789.50000 (Hz)
Natural freq (Mode 1707) = 184832.80000 (Hz)
Natural freq (Mode 1708) = 185132.10000 (Hz)
Natural freq (Mode 1709) = 185327.30000 (Hz)
Natural freq (Mode 1710) = 185472.20000 (Hz)
Natural freq (Mode 1711) = 185901.70000 (Hz)
Natural freq (Mode 1712) = 186622.70000 (Hz)
Natural freq (Mode 1713) = 187198.40000 (Hz)
Natural freq (Mode 1714) = 187443.40000 (Hz)
Natural freq (Mode 1715) = 187507.80000 (Hz)
Natural freq (Mode 1716) = 187872.30000 (Hz)
Natural freq (Mode 1717) = 188187.00000 (Hz)
Natural freq (Mode 1718) = 188741.90000 (Hz)
Natural freq (Mode 1719) = 188959.60000 (Hz)
Natural freq (Mode 1720) = 189275.20000 (Hz)
Natural freq (Mode 1721) = 190410.90000 (Hz)
Natural freq (Mode 1722) = 190828.60000 (Hz)
Natural freq (Mode 1723) = 191294.90000 (Hz)
Natural freq (Mode 1724) = 191352.10000 (Hz)
Natural freq (Mode 1725) = 191490.70000 (Hz)
Natural freq (Mode 1726) = 191801.40000 (Hz)
Natural freq (Mode 1727) = 192067.80000 (Hz)
Natural freq (Mode 1728) = 192128.50000 (Hz)
Natural freq (Mode 1729) = 192910.30000 (Hz)
Natural freq (Mode 1730) = 193493.10000 (Hz)
Natural freq (Mode 1731) = 193667.50000 (Hz)
Natural freq (Mode 1732) = 193707.10000 (Hz)
Natural freq (Mode 1733) = 194562.50000 (Hz)
Natural freq (Mode 1734) = 194671.90000 (Hz)
Natural freq (Mode 1735) = 194895.90000 (Hz)
Natural freq (Mode 1736) = 195986.20000 (Hz)
Natural freq (Mode 1737) = 196046.40000 (Hz)
Natural freq (Mode 1738) = 196164.80000 (Hz)
Natural freq (Mode 1739) = 196916.80000 (Hz)
Natural freq (Mode 1740) = 196945.90000 (Hz)
Natural freq (Mode 1741) = 196963.30000 (Hz)
Natural freq (Mode 1742) = 198742.00000 (Hz)
Natural freq (Mode 1743) = 198832.90000 (Hz)
Natural freq (Mode 1744) = 199305.40000 (Hz)
Natural freq (Mode 1745) = 200294.70000 (Hz)
Natural freq (Mode 1746) = 200419.80000 (Hz)
Natural freq (Mode 1747) = 201244.20000 (Hz)
Natural freq (Mode 1748) = 201284.70000 (Hz)
Natural freq (Mode 1749) = 201362.20000 (Hz)
Natural freq (Mode 1750) = 201875.70000 (Hz)
Natural freq (Mode 1751) = 202090.90000 (Hz)
Natural freq (Mode 1752) = 202691.80000 (Hz)
Natural freq (Mode 1753) = 203016.30000 (Hz)
Natural freq (Mode 1754) = 204512.00000 (Hz)
Natural freq (Mode 1755) = 205046.80000 (Hz)
Natural freq (Mode 1756) = 205539.70000 (Hz)
Natural freq (Mode 1757) = 206255.10000 (Hz)
Natural freq (Mode 1758) = 209931.40000 (Hz)
Natural freq (Mode 1759) = 210310.70000 (Hz)
Natural freq (Mode 1760) = 211454.20000 (Hz)
Natural freq (Mode 1761) = 211898.10000 (Hz)
Natural freq (Mode 1762) = 212483.80000 (Hz)
Natural freq (Mode 1763) = 213805.00000 (Hz)
Natural freq (Mode 1764) = 215284.00000 (Hz)
Natural freq (Mode 1765) = 216529.80000 (Hz)
Natural freq (Mode 1766) = 217898.60000 (Hz)
Natural freq (Mode 1767) = 219200.70000 (Hz)
Natural freq (Mode 1768) = 220852.30000 (Hz)
Natural freq (Mode 1769) = 222877.80000 (Hz)
Natural freq (Mode 1770) = 223804.40000 (Hz)
Natural freq (Mode 1771) = 230522.70000 (Hz)
Natural freq (Mode 1772) = 231395.10000 (Hz)
Natural freq (Mode 1773) = 234055.50000 (Hz)
Natural freq (Mode 1774) = 237433.60000 (Hz)
Natural freq (Mode 1775) = 240144.30000 (Hz)
Natural freq (Mode 1776) = 240535.30000 (Hz)
Natural freq (Mode 1777) = 243767.00000 (Hz)
Natural freq (Mode 1778) = 253575.70000 (Hz)
Natural freq (Mode 1779) = 267124.30000 (Hz)
real 0m2.180s
user 0m1.588s
sys 0m0.564s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_CompositeWingFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Composite_PyTest.py test;
+ python -u nastran_Composite_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 49
Number of elements = 36
Number of triangle elements = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes = 49
Total number of elements = 36
Mapping Csys attributes ................
Number of unique Csys attributes = 1
Name = plate, index = 1
Getting FEA coordinate systems.......
Number of coordinate systems - 1
Coordinate system name - plate
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plateTip, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - cantilever
No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Warning: No loads specified for case EigenAnalysis!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing combined constraint cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.111s
user 0m0.799s
sys 0m0.398s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_Composite_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Flutter_15degree.py test;
+ python -u nastran_Flutter_15degree.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
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 = 133
Number of elements = 108
Number of triangle elements = 0
Number of quadrilateral elements = 108
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 = 134
Total number of elements = 108
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 133
Number of elements = 108
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 108
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 = 134
Combined Number of elements = 109
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 108
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 133
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
7 automatic connections were made for capsConnect Root (node id 134)
Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No loads specified for case Flutter!!!!
Writing mass increment cards
Writing aero card
Writing analysis cards, 0
Writing constraint ADD cards
Writing constraint cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.103s
user 0m0.814s
sys 0m0.380s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_MultiLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_MultiLoadCase_PyTest.py test;
+ python -u nastran_MultiLoadCase_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 49
Number of elements = 36
Number of triangle elements = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes = 49
Total number of elements = 36
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
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 - 5
Load name - load_0
Load name - load_1
Load name - load_2
Load name - load_3
Load name - load_4
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 5
Analysis name - load_0
Analysis name - load_1
Analysis name - load_2
Analysis name - load_3
Analysis name - load_4
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing combined constraint cards
Writing load ADD cards
Writing combined constraint cards
Writing load ADD cards
Writing combined constraint cards
Writing load ADD cards
Writing combined constraint cards
Writing load ADD cards
Writing combined constraint cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.050s
user 0m0.768s
sys 0m0.407s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_MultiLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_OptimizationMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_OptimizationMultiLoad_PyTest.py test;
+ python -u nastran_OptimizationMultiLoad_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 49
Number of elements = 36
Number of triangle elements = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes = 49
Total number of elements = 36
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
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 - 2
Load name - load_0
Load name - load_1
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - materialDV
Design_Variable name - propertyDV
Design_Variable_Relation name - materialDVR
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - propertyDVR
Number of design variable relations - 2
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 2
Design_Constraint name - stress1
Design_Constraint name - stress2
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 2
Analysis name - load_0
Analysis name - load_1
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing combined constraint cards
Writing design constraint ADD cards
Writing load ADD cards
Writing combined constraint cards
Writing design constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Writing design constraints and responses cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running NASTRAN!
real 0m1.032s
user 0m0.767s
sys 0m0.391s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_OptimizationMultiLoad_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_PlateMisc_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_PlateMisc_PyTest.py test;
+ python -u nastran_PlateMisc_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 49
Number of elements = 36
Number of triangle elements = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes = 49
Total number of elements = 36
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 49
Number of elements = 36
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 36
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 - 3
Load name - moment
Load name - pressure
Load name - thermal
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - pltvar
Number of design variable relations - 0
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 1
Design_Constraint name - pltcon
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing design constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design constraints and responses cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.097s
user 0m0.796s
sys 0m0.417s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_PlateMisc_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_PyTest.py test;
+ python -u nastran_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 2091
Number of elements = 1845
Number of triangle elements = 0
Number of quadrilateral elements = 1845
----------------------------
Total number of nodes = 2091
Total number of elements = 1845
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2091
Number of elements = 1845
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 1845
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
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
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Warning: No loads specified for case EigenAnalysis!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing combined constraint cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
Getting results for natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02165 (Hz)
Natural freq (Mode 2) = 0.02165 (Hz)
Natural freq (Mode 3) = 0.10665 (Hz)
Natural freq (Mode 4) = 0.10665 (Hz)
Natural freq (Mode 5) = 0.13547 (Hz)
Natural freq (Mode 6) = 0.13547 (Hz)
Natural freq (Mode 7) = 0.23092 (Hz)
Natural freq (Mode 8) = 0.23092 (Hz)
Natural freq (Mode 9) = 0.27609 (Hz)
Natural freq (Mode 10) = 0.27609 (Hz)
real 0m8.667s
user 0m11.956s
sys 0m3.243s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_SingleLoadCase_PyTest.py test;
+ python -u nastran_SingleLoadCase_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 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
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.338s
user 0m0.844s
sys 0m0.518s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_ThreeBarDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarDesign_PyTest.py test;
+ python -u nastran_ThreeBarDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 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 = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 3
Design_Variable name - Bar1A
Design_Variable name - Bar2A
Design_Variable name - Bar3A
Design_Variable_Relation name - Bar1A
Design_Variable_Relation name - Bar2A
Design_Variable_Relation name - Bar3A
Number of design variable relations - 3
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 3
Design_Constraint name - stress1
Design_Constraint name - stress2
Design_Constraint name - stress3
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing design constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Writing design constraints and responses cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.377s
user 0m0.916s
sys 0m0.485s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarDesign_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'nastran_ThreeBarFreq_PyTest.py test;'
nastran_ThreeBarFreq_PyTest.py test;
+ python -u nastran_ThreeBarFreq_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 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 = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Warning: No loads specified for case EigenAnalysis!!!!
Writing mass increment cards
Writing analysis cards, 0
Writing combined constraint cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.116s
user 0m0.820s
sys 0m0.427s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarFreq_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarLinkDesign_PyTest.py test;
+ python -u nastran_ThreeBarLinkDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 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 = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 3
Design_Variable name - Bar1A
Design_Variable name - Bar2A
Design_Variable name - Bar3A
Design_Variable_Relation name - Bar1A
Design_Variable_Relation name - Bar2A
Design_Variable_Relation name - Bar3A
Number of design variable relations - 3
Done getting FEA design variables
Getting FEA design constraints.......
Number of design constraints - 3
Design_Constraint name - stress1
Design_Constraint name - stress2
Design_Constraint name - stress3
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing design constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Writing design constraints and responses cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.194s
user 0m0.796s
sys 0m0.478s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarLinkDesign_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarMultiLoad_PyTest.py test;
+ python -u nastran_ThreeBarMultiLoad_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 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 = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 2
Constraint name - conOne
No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
Constraint name - conTwo
No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - loadOne
Load name - loadTwo
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 2
Analysis name - caseOne
Analysis name - caseTwo
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.891s
user 0m1.202s
sys 0m0.598s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBar_PyTest.py test;
+ python -u nastran_ThreeBar_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 4
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4
Total number of elements = 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 = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Writing mass increment cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.692s
user 0m1.045s
sys 0m0.609s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'nastran_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Trim_15degree.py test;
+ python -u nastran_Trim_15degree.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
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 = 117
Number of elements = 96
Number of triangle elements = 0
Number of quadrilateral elements = 96
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 = 118
Total number of elements = 96
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 117
Number of elements = 96
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 96
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 = 118
Combined Number of elements = 97
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 96
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 117
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - Body
Property name - Edge
Property name - Root
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - PointSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
9 automatic connections were made for capsConnect Root (node id 118)
Done getting FEA connections
Getting FEA loads.......
Number of loads - 2
Load name - GravityLoad
No "groupName" specified for Load tuple GravityLoad, going to use load name
Load name - PointLoad
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim
Done getting FEA analyses
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing mass increment set
Writing Nastran instruction file....
Warning: No loads specified for case Trim, assuming all loads are applied!!!!
Writing mass increment cards
Writing aeros card
Writing aestat cards
Writing analysis cards, 0
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Done writing aeroelastic cards
Done writing files
Running Nastran......
Done running Nastran!
real 0m1.084s
user 0m0.810s
sys 0m0.399s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case nastran_Trim_15degree.py passed (as expected)
=================================================
Running.... AEROELASTIC PyTests
=================================================
+ echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Pressure_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Pressure_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1293 2452 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3418 6687 0
AFLR4 : Nodes, Trias,Quads= 3008 5867 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1315 2496 0
AFLR4 : Nodes, Trias,Quads= 1297 2460 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1319 2504 0
AFLR4 : Nodes, Trias,Quads= 1294 2454 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 200 344 0
AFLR4 : Nodes, Trias,Quads= 160 264 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 193 330 0
AFLR4 : Nodes, Trias,Quads= 155 254 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 17 21 0
AFLR4 : Nodes, Trias,Quads= 11 9 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9344 18684 928
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 9344 18684
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1335 2536 0
AFLR4 : Nodes, Trias,Quads= 1317 2500 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3787 7420 0
AFLR4 : Nodes, Trias,Quads= 2943 5732 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1341 2548 0
AFLR4 : Nodes, Trias,Quads= 1321 2508 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1342 2550 0
AFLR4 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 233 404 0
AFLR4 : Nodes, Trias,Quads= 210 358 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 224 386 0
AFLR4 : Nodes, Trias,Quads= 196 330 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9478 18952 946
OVERALL : CPU Time = 0.311 seconds
Body 1 (of 1)
Number of nodes = 9478
Number of elements = 18952
Number of triangle elements = 18952
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9478
Total number of elements = 18952
Total number of triangle elements = 18952
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 61788
Number of elements = 355965
Number of triangles = 18952
Number of quadrilatarals = 0
Number of tetrahedrals = 337013
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Pressure_SA.dat.
Surface file name: surface_flow_aeroelasticSimple_Pressure_SA.
Volume file name: flow_aeroelasticSimple_Pressure_SA.
Restart file name: restart_flow_aeroelasticSimple_Pressure_SA.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
61788 grid points.
337013 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
337013 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.4538. Mean K: 0.863308. Standard deviation K: 5.00657.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 54.7348| 86.7581|
| CV Face Area Aspect Ratio| 1.06698| 21.5651|
| CV Sub-Volume Ratio| 1| 6.22786|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 61788| 1/1.00| 10|
| 1| 10504| 1/5.88| 8.3095|
| 2| 1841| 1/5.71| 6.97535|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.2771e+00| -1.361370| 0.918961| 0.580745| 4.107735| -0.945745|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.3739e+00| -1.753698| 0.759192| 0.409261| 3.702741| -0.508573|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.3051e+00| -1.769228| 0.570930| 0.229342| 3.687595| 1.615844|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.76923| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Pressure_SA.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|CSV file |surface_flow_aeroelasticSimple_Pressure_SA.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary |flow_aeroelasticSimple_Pressure_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Pressure_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
Running ...... astros
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 180
Number of elements = 194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 32
Elemental Quad4 = 162
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 - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
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
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 3.101708e+09, tgt = 3.101708e+09, diff = 1.858783e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 3.017715e+09, tgt = 3.017715e+09, diff = 2.021653e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 4.373425e+07, tgt = 4.373425e+07, diff = 2.773415e-02
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
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
real 0m25.422s
user 0m23.624s
sys 0m2.652s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Displacement_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... astros
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 180
Number of elements = 194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 32
Elemental Quad4 = 162
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 - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureInternal
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
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Running PostAnalysis ...... astros
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1293 2452 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3418 6687 0
AFLR4 : Nodes, Trias,Quads= 3008 5867 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1315 2496 0
AFLR4 : Nodes, Trias,Quads= 1297 2460 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1319 2504 0
AFLR4 : Nodes, Trias,Quads= 1294 2454 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 200 344 0
AFLR4 : Nodes, Trias,Quads= 160 264 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 193 330 0
AFLR4 : Nodes, Trias,Quads= 155 254 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 17 21 0
AFLR4 : Nodes, Trias,Quads= 11 9 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9344 18684 928
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 9344 18684
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1335 2536 0
AFLR4 : Nodes, Trias,Quads= 1317 2500 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3787 7420 0
AFLR4 : Nodes, Trias,Quads= 2943 5732 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1341 2548 0
AFLR4 : Nodes, Trias,Quads= 1321 2508 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1342 2550 0
AFLR4 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 233 404 0
AFLR4 : Nodes, Trias,Quads= 210 358 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 224 386 0
AFLR4 : Nodes, Trias,Quads= 196 330 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9478 18952 946
OVERALL : CPU Time = 0.351 seconds
Body 1 (of 1)
Number of nodes = 9478
Number of elements = 18952
Number of triangle elements = 18952
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9478
Total number of elements = 18952
Total number of triangle elements = 18952
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 61788
Number of elements = 355965
Number of triangles = 18952
Number of quadrilatarals = 0
Number of tetrahedrals = 337013
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Displacement_SA_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
61788 grid points.
337013 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
337013 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 26.027356 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Displacement_SA.dat.
Surface file name: surface_flow_aeroelasticSimple_Displacement_SA.
Volume file name: flow_aeroelasticSimple_Displacement_SA.
Restart file name: restart_flow_aeroelasticSimple_Displacement_SA.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
61788 grid points.
337013 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
337013 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63997.8.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.9101. Mean K: 0.903752. Standard deviation K: 4.4801.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 42.7246| 86.7623|
| CV Face Area Aspect Ratio| 1.05988| 23.4731|
| CV Sub-Volume Ratio| 1| 155.18|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 61788| 1/1.00| 10|
| 1| 10504| 1/5.88| 8.3095|
| 2| 1841| 1/5.71| 6.97535|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89892 m.
Wetted area = 11.6151 m^2.
Area projection in the x-plane = 2.90002 m^2, y-plane = 1.28883 m^2, z-plane = 4.27937 m^2.
Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89892 m, z-direction = 0.526515 m.
Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86329e-18 m, z-direction = -0.706552 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.8661e+00| -0.691634| 1.737097| 1.249935| 4.777472| 0.053881|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.4575e+00| -1.143706| 1.454258| 1.101774| 4.327378| 0.043383|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.3178e+00| -1.163565| 1.229507| 0.914066| 4.302377| 0.103716|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.16356| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Displacement_SA.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|CSV file |surface_flow_aeroelasticSimple_Displacement_SA.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary |flow_aeroelasticSimple_Displacement_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Displacement_SA.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
real 1m0.107s
user 0m51.927s
sys 0m8.621s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Displacement_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ echo 'aeroelasticSimple_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Iterative_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
AFLR4 : Global Scale Factor = 2
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 374 678 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 927 1777 0
AFLR4 : Nodes, Trias,Quads= 821 1565 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 374 678 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 378 686 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 63 96 0
AFLR4 : Nodes, Trias,Quads= 55 80 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 64 96 0
AFLR4 : Nodes, Trias,Quads= 57 82 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 7 5 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2592 5180 482
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 2592 5180
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 385 700 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 383 696 0
AFLR4 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1004 1929 0
AFLR4 : Nodes, Trias,Quads= 955 1831 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Nodes, Trias,Quads= 378 686 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 386 702 0
AFLR4 : Nodes, Trias,Quads= 379 688 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 382 694 0
AFLR4 : Nodes, Trias,Quads= 379 688 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 74 115 0
AFLR4 : Nodes, Trias,Quads= 65 97 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 75 116 0
AFLR4 : Nodes, Trias,Quads= 63 92 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2737 5470 490
OVERALL : CPU Time = 0.187 seconds
Body 1 (of 1)
Number of nodes = 2737
Number of elements = 5470
Number of triangle elements = 5470
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2737
Total number of elements = 5470
Total number of triangle elements = 5470
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 11189
Number of elements = 63352
Number of triangles = 5470
Number of quadrilatarals = 0
Number of tetrahedrals = 57882
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 47.1143. Mean K: 0.755831. Standard deviation K: 3.51256.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 50.9576| 84.7141|
| CV Face Area Aspect Ratio| 1.07213| 21.5536|
| CV Sub-Volume Ratio| 1| 10.2891|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11189| 1/1.00| 10|
| 1| 1972| 1/5.67| 8.41001|
| 2| 394| 1/5.01| 7.37481|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.08979 m^2.
Area projection in the x-plane = 0.572014 m^2, y-plane = 0.261888 m^2, z-plane = 3.84035 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380358 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.8602e-18 m, z-direction = -0.0467106 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.7272e-01| -0.788239| 1.511706| 1.187262| 4.680867| -1.151636|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.5110e-01| -1.114115| 1.416686| 1.030318| 4.340813| -0.880779|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.4857e-01| -1.184774| 1.271379| 0.880364| 4.266950| -0.265222|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.18477| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 180
Number of elements = 194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 32
Elemental Quad4 = 162
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 - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
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
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 3.096416e+09, tgt = 3.096415e+09, diff = 1.073042e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 3.009946e+09, tgt = 3.009946e+09, diff = 2.106818e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 4.109924e+07, tgt = 4.109924e+07, diff = 1.236494e-01
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
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
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 1.362918 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 959 TETRAHEDRON volume elements.
There has been a re-orientation of 51 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 64528.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 26.5359. Mean K: 0.52967. Standard deviation K: 1.76188.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 3.57703| 84.8668|
| CV Face Area Aspect Ratio| 1.06228| 397.662|
| CV Sub-Volume Ratio| 1| 3693.18|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11189| 1/1.00| 10|
| 1| 1970| 1/5.68| 8.40717|
| 2| 394| 1/5| 7.37481|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 4.41651 m.
Wetted area = 165.461 m^2.
Area projection in the x-plane = 65.909 m^2, y-plane = 36.9308 m^2, z-plane = 5.43389 m^2.
Max. coordinate in the x-direction = 2.7212 m, y-direction = 4.41651 m, z-direction = 18.1582 m.
Min. coordinate in the x-direction = -0.739572 m, y-direction = -0.0620634 m, z-direction = -19.0371 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.4770e-01| 1.853605| 4.808189| 4.873938| 7.322711| -0.010914|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.4886e-01| 2.158629| 4.741718| 4.915208| 7.657720| -0.029122|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.5869e-01| 2.349932| 4.816196| 4.782367| 7.732429| -0.070902|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 2.34993| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 31 non-physical points in the solution.
Warning: 2 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 2.064700e+09, tgt = 2.064700e+09, diff = 1.259066e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.544262e+09, tgt = 1.544262e+09, diff = 3.041722e+00
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 2.280527e+07, tgt = 2.280527e+07, diff = 8.781843e-03
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
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
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 959 TETRAHEDRON volume elements.
There has been a re-orientation of 51 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 64528.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 7.761708 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 22651 TETRAHEDRON volume elements.
There has been a re-orientation of 1173 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 139326.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 155.346. Mean K: 1.5774. Standard deviation K: 7.35704.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 2.17622| 84.0844|
| CV Face Area Aspect Ratio| 1.46454| 1585.46|
| CV Sub-Volume Ratio| 1| 98320.3|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11189| 1/1.00| 10|
| 1| 1988| 1/5.63| 8.43269|
| 2| 408| 1/4.87| 7.46115|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 1.38681 m.
Wetted area = 523.796 m^2.
Area projection in the x-plane = 230.038 m^2, y-plane = 79.8096 m^2, z-plane = 6.63348 m^2.
Max. coordinate in the x-direction = 8.71276 m, y-direction = 1.38681 m, z-direction = 118.362 m.
Min. coordinate in the x-direction = 0.0330272 m, y-direction = -7.946 m, z-direction = -0.858419 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.7585e-01| 2.952787| 5.916503| 5.925140| 8.421893| -0.254645|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.7786e-01| 3.442936| 6.030135| 6.000298| 8.838401| -0.220818|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.8128e-01| 3.562615| 6.168302| 6.086319| 8.966328| -0.193914|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.56261| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 436 non-physical points in the solution.
Warning: 18 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 2.087986e+09, tgt = 2.087985e+09, diff = 5.493975e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.695766e+09, tgt = 1.695766e+09, diff = 8.276410e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 1.753619e+07, tgt = 1.753619e+07, diff = 1.487993e-04
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 16 (total = 178)
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
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 22651 TETRAHEDRON volume elements.
There has been a re-orientation of 1173 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 139326.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 41.960785 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 33373 TETRAHEDRON volume elements.
There has been a re-orientation of 3503 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 1.26188e+12.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 46.3582. Mean K: 0.351963. Standard deviation K: 1.75997.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.467366| 84.5943|
| CV Face Area Aspect Ratio| 1.58521| 480468|
| CV Sub-Volume Ratio| 1| 1.23326e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11189| 1/1.00| 10|
| 1| 2000| 1/5.59| 8.44963|
| 2| 414| 1/4.83| 7.49754|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.2382 m.
Wetted area = 63827 m^2.
Area projection in the x-plane = 45829.5 m^2, y-plane = 5453.15 m^2, z-plane = 435.098 m^2.
Max. coordinate in the x-direction = 23.2403 m, y-direction = 3.2382 m, z-direction = 1540.19 m.
Min. coordinate in the x-direction = -2.17316 m, y-direction = -114.437 m, z-direction = -0.179221 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.9825e-01| 7.719292| 10.686148| 10.633344| 13.188398| -0.039434|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.1736e-01| 8.221627| 10.706445| 10.637616| 13.707352| -0.042749|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.1598e-01| 8.277206| 10.818296| 10.544196| 13.587094| -0.044207|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 8.27721| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file |surface_flow_aeroelasticSimple_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary |flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 635 non-physical points in the solution.
Warning: 35 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
Cl = 13098.742528
Cd = -296305.688432
real 1m13.209s
user 1m8.632s
sys 0m4.435s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Iterative_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ echo 'aeroelastic_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelastic_Iterative_SU2_and_Astros.py test;
+ python -u aeroelastic_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
AFLR4 : Global Scale Factor = 2
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 374 678 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 927 1777 0
AFLR4 : Nodes, Trias,Quads= 821 1565 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 374 678 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 376 682 0
AFLR4 : Nodes, Trias,Quads= 378 686 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 63 96 0
AFLR4 : Nodes, Trias,Quads= 55 80 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 64 96 0
AFLR4 : Nodes, Trias,Quads= 57 82 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 7 5 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2592 5180 482
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 2592 5180
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 385 700 0
AFLR4 : Nodes, Trias,Quads= 380 690 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 383 696 0
AFLR4 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1004 1929 0
AFLR4 : Nodes, Trias,Quads= 955 1831 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 381 692 0
AFLR4 : Nodes, Trias,Quads= 378 686 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 386 702 0
AFLR4 : Nodes, Trias,Quads= 379 688 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 382 694 0
AFLR4 : Nodes, Trias,Quads= 379 688 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 74 115 0
AFLR4 : Nodes, Trias,Quads= 65 97 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 75 116 0
AFLR4 : Nodes, Trias,Quads= 63 92 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2737 5470 490
OVERALL : CPU Time = 0.150 seconds
Body 1 (of 1)
Number of nodes = 2737
Number of elements = 5470
Number of triangle elements = 5470
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2737
Total number of elements = 5470
Total number of triangle elements = 5470
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 11189
Number of elements = 63352
Number of triangles = 5470
Number of quadrilatarals = 0
Number of tetrahedrals = 57882
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 47.1143. Mean K: 0.755831. Standard deviation K: 3.51256.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 50.9576| 84.7141|
| CV Face Area Aspect Ratio| 1.07213| 21.5536|
| CV Sub-Volume Ratio| 1| 10.2891|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11189| 1/1.00| 10|
| 1| 1972| 1/5.67| 8.41001|
| 2| 394| 1/5.01| 7.37481|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.08979 m^2.
Area projection in the x-plane = 0.572014 m^2, y-plane = 0.261888 m^2, z-plane = 3.84035 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380358 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.8602e-18 m, z-direction = -0.0467106 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.9058e-01| -0.788239| 1.511706| 1.187262| 4.680867| -1.151636|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.9486e-01| -1.114115| 1.416686| 1.030318| 4.340813| -0.880779|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.9775e-01| -1.184774| 1.271379| 0.880364| 4.266950| -0.265222|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.18477| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse 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 = Ribs_and_Spars, index = 1
Name = Skin, index = 2
Name = Rib_Root, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 746
Number of elements = 898
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 120
Elemental Quad4 = 778
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - Rib_Root
Property name - Ribs_and_Spars
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
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
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 3.096416e+09, tgt = 3.096416e+09, diff = 7.733565e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 3.009946e+09, tgt = 3.009946e+09, diff = 6.083825e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 4.109924e+07, tgt = 4.109924e+07, diff = 1.668003e+00
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 30 (total = 690)
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
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 1.371946 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 14880 TETRAHEDRON volume elements.
There has been a re-orientation of 747 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 117384.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 405.677. Mean K: 3.64694. Standard deviation K: 20.0542.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 3.31568| 83.9604|
| CV Face Area Aspect Ratio| 1.03244| 309.65|
| CV Sub-Volume Ratio| 1| 74320.5|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11189| 1/1.00| 10|
| 1| 1986| 1/5.63| 8.42986|
| 2| 397| 1/5| 7.39348|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 12.4281 m.
Wetted area = 1437.77 m^2.
Area projection in the x-plane = 477.415 m^2, y-plane = 489.875 m^2, z-plane = 61.3163 m^2.
Max. coordinate in the x-direction = 3.712 m, y-direction = 12.4281 m, z-direction = 36.4483 m.
Min. coordinate in the x-direction = -13.6258 m, y-direction = -0.914733 m, z-direction = -76.7716 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 4.3848e-01| 2.942393| 5.901937| 6.281442| 8.411499| 0.200160|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.2505e-01| 3.381201| 5.896320| 6.239543| 8.911050| -2.031947|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.2051e-01| 3.486782| 5.971795| 6.207062| 8.952183| -0.068916|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.48678| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 138 non-physical points in the solution.
Warning: 3 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 1.665664e+09, tgt = 1.665662e+09, diff = 1.354985e+03
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.565774e+09, tgt = 1.565774e+09, diff = 2.317646e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 1.026818e+07, tgt = 1.026821e+07, diff = 2.600373e+01
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 30 (total = 690)
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
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 14880 TETRAHEDRON volume elements.
There has been a re-orientation of 747 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 117384.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 6.866808 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 32647 TETRAHEDRON volume elements.
There has been a re-orientation of 1729 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 8.42456e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 17.3445. Mean K: 0.271106. Standard deviation K: 0.872252.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.158267| 81.1825|
| CV Face Area Aspect Ratio| 1.08063| 64701.1|
| CV Sub-Volume Ratio| 1| 1.29145e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11189| 1/1.00| 10|
| 1| 1993| 1/5.61| 8.43976|
| 2| 418| 1/4.77| 7.52161|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 18.787 m.
Wetted area = 2.03132e+06 m^2.
Area projection in the x-plane = 676346 m^2, y-plane = 377082 m^2, z-plane = 21844.1 m^2.
Max. coordinate in the x-direction = 28.6953 m, y-direction = 18.787 m, z-direction = 8014.26 m.
Min. coordinate in the x-direction = -42.7756 m, y-direction = -585.579 m, z-direction = -0.0467106 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.5126e-01| 7.130954| 10.095885| 10.042605| 12.600060| -0.015751|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.5790e-01| 7.417851| 10.026146| 9.963905| 12.841572| -0.016442|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.6364e-01| 7.497783| 10.099626| 10.027466| 12.944525| -0.015842|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 7.49778| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 423 non-physical points in the solution.
Warning: 59 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 1.646540e+09, tgt = 1.646540e+09, diff = 3.843121e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.350299e+09, tgt = 1.350299e+09, diff = 7.153354e+00
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 104
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 1.438119e+07, tgt = 1.438112e+07, diff = 7.043509e+01
Extracting external pressure loads from data transfer....
TransferName = Skin_Top
Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
TransferName = Skin_Bottom
Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
TransferName = Skin_Tip
Number of Elements = 30 (total = 690)
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
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 32647 TETRAHEDRON volume elements.
There has been a re-orientation of 1729 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 8.42456e+10.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 41.218099 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11189 grid points.
57882 volume elements.
3 surface markers.
3444 boundary elements in index 0 (Marker = BC_1).
1831 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
57882 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 33140 TETRAHEDRON volume elements.
There has been a re-orientation of 2846 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 8.586e+13.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 12.5581. Mean K: 0.244836. Standard deviation K: 0.957256.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.154366| 80.0576|
| CV Face Area Aspect Ratio| 1.50305| 2.99554e+08|
| CV Sub-Volume Ratio| 1| 2.02824e+10|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11189| 1/1.00| 10|
| 1| 1994| 1/5.61| 8.44117|
| 2| 416| 1/4.79| 7.5096|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 121.933 m.
Wetted area = 94584.5 m^2.
Area projection in the x-plane = 44339 m^2, y-plane = 12667.1 m^2, z-plane = 998.251 m^2.
Max. coordinate in the x-direction = 14.9317 m, y-direction = 121.933 m, z-direction = 31.3447 m.
Min. coordinate in the x-direction = -41.4907 m, y-direction = -1.80731 m, z-direction = -1545.06 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.9801e-01| 8.948112| 11.914968| 11.851545| 14.417218| -0.122706|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.1112e-01| 9.294124| 11.889659| 11.826417| 14.715823| -0.129444|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.0890e-01| 9.347261| 11.933459| 11.877931| 14.801676| -0.155743|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 9.34726| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelastic_Iterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file |surface_flow_aeroelastic_Iterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary |flow_aeroelastic_Iterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface |surface_flow_aeroelastic_Iterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 677 non-physical points in the solution.
Warning: 58 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
real 1m42.669s
user 1m41.544s
sys 0m7.693s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelastic_Iterative_SU2_and_Astros.py passed (as expected)
=================================================
=================================================
+ echo 'aeroelasticSimple_Temperature_SU2_and_TACS.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Temperature_SU2_and_TACS.py test;
+ python -u aeroelasticSimple_Temperature_SU2_and_TACS.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 9 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 12 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 4 5
EGADS : 2 Yes 0 0 1 0 1 1 3 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 4 6 7 8
EGADS : 4 Yes 0 0 1 0 1 1 3 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 4 6
EGADS : 6 Yes 0 0 1 0 1 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 3 8 9
EGADS : 8 Yes 0 0 1 0 1 3 7 9
EGADS : 9 Yes 0 0 1 0 1 7 8
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8 -10 -11
EGADS : 4 -12 3 8 -13
EGADS : 5 4 12 -14 -5
EGADS : 6 -6 14 13 -9
EGADS : 7 15 10 -17 -16
EGADS : 8 17 11 -15 -18
EGADS : 9 16 18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3 4
EGADS : 4 5
EGADS : 5 6
EGADS : 6 7
EGADS : 7 8
EGADS : 8 9
EGADS : 9 10
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 -11
EGADS : 5 Yes -12 3 8 -13
EGADS : 6 Yes 4 12 -14 -5
EGADS : 7 Yes -6 14 13 -9
EGADS : 8 Yes 15 10 -17 -16
EGADS : 9 Yes 17 11 -15 -18
EGADS : 10 Yes 16 18
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 2 5 1 2 5
EGADS : 6 0 Yes 5 6 1 2 6
EGADS : 7 0 Yes 1 6 1 2 3
EGADS : 8 0 Yes 3 7 1 3 4
EGADS : 9 0 Yes 6 7 1 3 6
EGADS : 10 0 Yes 8 9 1 3 7
EGADS : 11 0 Yes 9 8 1 3 8
EGADS : 12 0 Yes 4 10 1 4 5
EGADS : 13 0 Yes 10 7 1 4 6
EGADS : 14 0 Yes 5 10 1 5 6
EGADS : 15 0 Yes 11 8 1 7 8
EGADS : 16 0 Yes 11 12 1 7 9
EGADS : 17 0 Yes 12 9 1 7 8
EGADS : 18 0 Yes 12 11 1 8 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 0 40 0
EGADS : 3 Yes 0 0 20
EGADS : 4 Yes 0 40 20
EGADS : 5 Yes 20 40 0
EGADS : 6 Yes 20 0 0
EGADS : 7 Yes 20 0 20
EGADS : 8 Yes 1.61374306 0 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 20 40 20
EGADS : 11 Yes 2.53650745 3.87298335 0.334116517
EGADS : 12 Yes 1.57194608 3.87298335 0.249728332
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 40
AFLR4 : Min Bounding Box Length = 40
AFLR4 : Max Ref Bounding Box Length = 40
AFLR4 : Min Ref Bounding Box Length = 40
AFLR4 : Reference Length = 1.61374
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.00403436
AFLR4 : Min Surf Spacing = 0.161374
AFLR4 : Max Surf Spacing = 1.21031
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1293 2452 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3418 6687 0
AFLR4 : Nodes, Trias,Quads= 3008 5867 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1315 2496 0
AFLR4 : Nodes, Trias,Quads= 1297 2460 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Nodes, Trias,Quads= 1298 2462 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1319 2504 0
AFLR4 : Nodes, Trias,Quads= 1294 2454 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 200 344 0
AFLR4 : Nodes, Trias,Quads= 160 264 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 193 330 0
AFLR4 : Nodes, Trias,Quads= 155 254 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 17 21 0
AFLR4 : Nodes, Trias,Quads= 11 9 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9344 18684 928
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 9344 18684
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1335 2536 0
AFLR4 : Nodes, Trias,Quads= 1317 2500 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3787 7420 0
AFLR4 : Nodes, Trias,Quads= 2943 5732 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1341 2548 0
AFLR4 : Nodes, Trias,Quads= 1321 2508 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1337 2540 0
AFLR4 : Nodes, Trias,Quads= 1320 2506 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1342 2550 0
AFLR4 : Nodes, Trias,Quads= 1318 2502 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 233 404 0
AFLR4 : Nodes, Trias,Quads= 210 358 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 224 386 0
AFLR4 : Nodes, Trias,Quads= 196 330 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 9478 18952 946
OVERALL : CPU Time = 0.316 seconds
Body 1 (of 1)
Number of nodes = 9478
Number of elements = 18952
Number of triangle elements = 18952
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9478
Total number of elements = 18952
Total number of triangle elements = 18952
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Farfield, index = 1
Name = SymmPlane, index = 2
Name = Skin, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 61788
Number of elements = 355965
Number of triangles = 18952
Number of quadrilatarals = 0
Number of tetrahedrals = 337013
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Skin
Boundary condition name - SymmPlane
Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.
Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Temperature_SM.dat.
Surface file name: surface_flow_aeroelasticSimple_Temperature_SM.
Volume file name: flow_aeroelasticSimple_Temperature_SM.
Restart file name: restart_flow_aeroelasticSimple_Temperature_SM.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
| Symmetry plane| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
61788 grid points.
337013 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
337013 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.4538. Mean K: 0.863308. Standard deviation K: 5.00657.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 54.7348| 86.7581|
| CV Face Area Aspect Ratio| 1.06698| 21.5651|
| CV Sub-Volume Ratio| 1| 6.22786|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 61788| 1/1.00| 10|
| 1| 10504| 1/5.88| 8.3095|
| 2| 1841| 1/5.71| 6.97535|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.1617e+00| -1.361370| 0.918961| 0.580745| 4.107735| -0.945745|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.1752e+00| -1.753698| 0.759192| 0.409261| 3.702741| -0.508573|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.1425e+00| -1.769228| 0.570930| 0.229342| 3.687595| 1.615844|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.76923| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticSimple_Temperature_SM.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|CSV file |surface_flow_aeroelasticSimple_Temperature_SM.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|Tecplot binary |flow_aeroelasticSimple_Temperature_SM.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|Tecplot binary surface |surface_flow_aeroelasticSimple_Temperature_SM.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Running PostAnalysis ...... su2
Running PreAnalysis ...... tacs
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 12
Number of elements = 12
Number of triangle elements = 4
Number of quadrilateral elements = 8
----------------------------
Total number of nodes = 12
Total number of elements = 12
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 12
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4
Elemental Quad4 = 8
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
Property name - Skin
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - Skin
No "groupName" specified for Load tuple Skin, going to use load name
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 12
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4
Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature'
Rank 0: src = 1.497486e+03, tgt = 1.497486e+03, diff = 4.587847e-06
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 12
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4
Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature'
Rank 0: src = 1.453112e+03, tgt = 1.453112e+03, diff = 4.579270e-06
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA 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, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Skin, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 3
Name = Skin_Top, index = 1
Name = Skin_Bottom, index = 2
Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Skin, index = 1
Name = Rib_Root, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 12
Number of elements = 12
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4
Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
Number of variables = 16
Number of data points = 361
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature'
Rank 0: src = 2.097348e+01, tgt = 2.097348e+01, diff = 3.279155e-12
Extracting external thermal loads from data transfer....
TransferName = Skin_Top
Number of Nodes = 9 (total = 9)
Extracting external thermal loads from data transfer....
TransferName = Skin_Bottom
Number of Nodes = 9 (total = 18)
Extracting external thermal loads from data transfer....
TransferName = Skin_Tip
Number of Nodes = 4 (total = 16)
Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Running PostAnalysis ...... tacs
real 0m25.104s
user 0m23.101s
sys 0m2.411s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Temperature_SU2_and_TACS.py passed (as expected)
=================================================
Running.... CORSAIRLITE PyTests
=================================================
+ echo 'gp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
gp.py test;
+ python -u gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
0.00713 dimensionless
Variables
---------
x : 3.00000 [-] The X variable
y : 81.00008 [-] The Y variable
z : 0.19245 [-] The Z variable
Sensitivities
-------------
No Constants in the Formulation
Solve Report
------------
Solve Method : Geometric Program
Classification : Convex
Solver : cvxopt
real 0m9.897s
user 0m2.095s
sys 0m0.380s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case gp.py passed (as expected)
=================================================
=================================================
+ echo 'qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
qp.py test;
+ python -u qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
-21.56250 dimensionless
Variables
---------
x : 1.62500 [-] The X variable
y : 1.37500 [-] The Y variable
Constants
---------
c : 3 [-] A constant
c2 : 2 [-] A constant
Sensitivities
-------------
c : + 0.46957 A constant
c2 : - 0.22338 A constant
Solve Report
------------
Solve Method : Quadratic Program
Classification : Convex
Solver : cvxopt
real 0m2.221s
user 0m2.179s
sys 0m0.261s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case qp.py passed (as expected)
=================================================
=================================================
+ echo 'sp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
sp.py test;
+ python -u sp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
0.45721 dimensionless
Variables
---------
x : 2.56155 [-] The X variable
y : 6.56155 [-] The Y variable
z : 1.17116 [-] The Z variable
Constants
---------
c : 2 [-] A constant
Sensitivities
-------------
Sensitivities not computed
Solve Report
------------
Solve Method : Signomial Program--Standard
Classification : Iterative
Solver : cvxopt
Number of Iterations : 3
Termination Status : Converged, relative error (3.15e-04) is less than specified tolerance (1.00e-03)
real 0m2.258s
user 0m2.109s
sys 0m0.283s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case sp.py passed (as expected)
=================================================
=================================================
+ echo 'boydBox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
boydBox.py test;
+ python -u boydBox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
0.00520 1 / meter ** 3
Variables
---------
d : 11.26658 meter The Z variable
h : 2.92246 meter The Y variable
w : 5.84486 meter The X variable
Constants
---------
Aflr : 1000 meter ** 2 Area of floor
Awall : 100 meter ** 2 Area of wall
alpha : 0.50000 [-] Aspect Ratio Constraint
beta : 2 [-] Aspect Ratio Constraint
delta : 2 [-] Aspect Ratio Constraint
gamma : 0.50000 [-] Aspect Ratio Constraint
Sensitivities
-------------
Sensitivities not computed
Solve Report
------------
Solve Method : Geometric Program
Classification : Convex
Solver : cvxopt
real 0m1.875s
user 0m1.823s
sys 0m0.259s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case boydBox.py passed (as expected)
=================================================
=================================================
+ echo 'hoburg_gp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_gp.py test;
+ python -u hoburg_gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
5905.58568 newton
Variables
---------
AR : 20.36983 [-] aspect ratio
C_D_0 : 0.01271 [-] Drag Coefficient, segment 0
C_D_1 : 0.01273 [-] Drag Coefficient, segment 1
C_D_2 : 0.00778 [-] Drag Coefficient, segment 2
C_Dfuse_0 : 0.00180 [-] Fuselage Drag Coefficient, segment 0
C_Dfuse_1 : 0.00180 [-] Fuselage Drag Coefficient, segment 1
C_Dfuse_2 : 0.00180 [-] Fuselage Drag Coefficient, segment 2
C_Di_0 : 0.00542 [-] Induced Drag Coefficient, segment 0
C_Di_1 : 0.00542 [-] Induced Drag Coefficient, segment 1
C_Di_2 : 0.00023 [-] Induced Drag Coefficient, segment 2
C_Dp_0 : 0.00549 [-] Wing Profile Drag Coefficient, segment 0
C_Dp_1 : 0.00551 [-] Wing Profile Drag Coefficient, segment 1
C_Dp_2 : 0.00575 [-] Wing Profile Drag Coefficient, segment 2
C_L_0 : 0.57420 [-] Lift Coefficient, segment 0
C_L_1 : 0.57421 [-] Lift Coefficient, segment 1
C_L_2 : 0.11881 [-] Lift Coefficient, segment 2
I_cap_bar : 0.00002 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4
M_r_bar : 36139.20785 newton Root Bending unit per unit chord
P_max : 1185884.98442 watt Maximum Engine Power
R : 4999.98983 kilometer Single Segment range
Re_0 : 4232645.50367 [-] Reynolds Number, segment 0
Re_1 : 4051247.93913 [-] Reynolds Number, segment 1
Re_2 : 9305153.26607 [-] Reynolds Number, segment 2
S : 27.73109 meter ** 2 total wing area
T_0 : 746.21338 newton Thrust, segment 0
T_1 : 684.51827 newton Thrust, segment 1
T_2 : 2208.51611 newton Thrust, segment 2
V_0 : 68.23357 meter / second Velocity, segment 0
V_1 : 65.30930 meter / second Velocity, segment 1
V_2 : 150.00638 meter / second Velocity, segment 2
V_stall : 37.99896 meter / second stall speed
W_0 : 33698.97702 newton Weight, segment 0
W_1 : 30873.13301 newton Weight, segment 1
W_2 : 33698.96566 newton Weight, segment 2
W_MTO : 36788.13387 newton Maximum Takeoff Weight
W_cap : 4091.65066 newton Weight of Wing Spar Cap
W_eng : 2806.10727 newton Engine Weight
W_fuel_out : 3079.86524 newton Weight of fuel, outbound
W_fuel_ret : 2825.71897 newton Weight of fuel, return
W_pay : 4905.15902 newton Payload Weight
W_tilde : 22409.98513 newton Dry Weight, no wing
W_web : 139.91823 newton Weight of Wing Spar Shear Web
W_wing : 8462.91404 newton wing weight
W_zfw : 30872.92436 newton Zero Fuel Weight
eta_0_0 : 0.26999 [-] Overall Efficiency, segment 0
eta_0_1 : 0.26996 [-] Overall Efficiency, segment 1
eta_0_2 : 0.27945 [-] Overall Efficiency, segment 2
eta_i_0 : 0.90752 [-] Inviscid Propeller Efficiency, segment 0
eta_i_1 : 0.90742 [-] Inviscid Propeller Efficiency, segment 1
eta_i_2 : 0.93932 [-] Inviscid Propeller Efficiency, segment 2
eta_prop_0 : 0.77139 [-] Propeller Efficiency, segment 0
eta_prop_1 : 0.77131 [-] Propeller Efficiency, segment 1
eta_prop_2 : 0.79842 [-] Propeller Efficiency, segment 2
nu : 0.78603 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2
p : 1.90003 [-] Dummy Variable (1+2*lam_w)
q : 1.45002 [-] Dummy Variable (1+lam_w)
t_cap_bar : 0.00456 [-] Spar cap thickness per unit chord
t_web_bar : 0.00069 [-] Spar web thickness per unit chord
tau : 0.15000 [-] airfoil thickness to chord ratio
z_bre_0 : 0.08745 [-] Breguet Range Factor, segment 0
z_bre_1 : 0.08758 [-] Breguet Range Factor, segment 1
Constants
---------
A_prop : 0.78500 meter ** 2 Disk area of propeller
CDA0 : 0.05000 meter ** 2 fuselage drag area
C_Lmax : 1.50000 [-] max CL with flaps down
N_lift : 6 [-] Ultimate Load Factor
W_fixed : 14700 newton fixed weight
e : 0.95000 [-] Oswald efficiency factor
eta_eng : 0.35000 [-] Engine Efficiency
eta_v : 0.85000 [-] Propeller Viscous Efficiency
f_wadd : 2 [-] Added Weight Fraction
g : 9.81000 meter / second ** 2 Gravitational constant
h_fuel : 46000000 joule / kilogram Fuel Specific energy density
k_ew : 0.03720 newton / watt ** 0.803 Constant for engine weight
mu : 0.00002 kilogram / meter / second viscosity of air
r_h : 0.75000 [-] Ratio of height at rear spar to maximum wing height
rho : 0.90912 kilogram / meter ** 3 density of air
rho_SL : 1.22500 kilogram / meter ** 3 density of air, sea level
rho_cap : 2700 kilogram / meter ** 3 Density of wing cap material (aluminum)
rho_web : 2700 kilogram / meter ** 3 Density of wing web material (aluminum)
sigma_max : 310 megapascal Allowable tensile stress of aluminum
sigma_max_shear : 167 megapascal Allowable shear stress of aluminum
w_bar : 0.50000 [-] Ratio of spar box width to chord length
Sensitivities
-------------
Sensitivities not computed
Solve Report
------------
Solve Method : Geometric Program
Classification : Convex
Solver : cvxopt
real 0m15.830s
user 0m15.195s
sys 0m0.784s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hoburg_gp.py passed (as expected)
=================================================
=================================================
+ echo 'hoburg_blackbox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_blackbox.py test;
+ python -u hoburg_blackbox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
5905.2294 newton
Variables
---------
AR : 20.3737 [-] aspect ratio
C_D_0 : 0.0127 [-] Drag Coefficient, segment 0
C_D_1 : 0.0127 [-] Drag Coefficient, segment 1
C_D_2 : 0.0078 [-] Drag Coefficient, segment 2
C_Dfuse_0 : 0.0018 [-] Fuselage Drag Coefficient, segment 0
C_Dfuse_1 : 0.0018 [-] Fuselage Drag Coefficient, segment 1
C_Dfuse_2 : 0.0018 [-] Fuselage Drag Coefficient, segment 2
C_Di_0 : 0.0054 [-] Induced Drag Coefficient, segment 0
C_Di_1 : 0.0054 [-] Induced Drag Coefficient, segment 1
C_Di_2 : 0.0002 [-] Induced Drag Coefficient, segment 2
C_Dp_0 : 0.0055 [-] Wing Profile Drag Coefficient, segment 0
C_Dp_1 : 0.0055 [-] Wing Profile Drag Coefficient, segment 1
C_Dp_2 : 0.0057 [-] Wing Profile Drag Coefficient, segment 2
C_L_0 : 0.5743 [-] Lift Coefficient, segment 0
C_L_1 : 0.5743 [-] Lift Coefficient, segment 1
C_L_2 : 0.1189 [-] Lift Coefficient, segment 2
I_cap_bar : 0.0000 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4
M_r_bar : 36141.5015 newton Root Bending unit per unit chord
P_max : 1184357.7688 watt Maximum Engine Power
R : 5000.0000 kilometer Single Segment range
Re_0 : 4231748.4656 [-] Reynolds Number, segment 0
Re_1 : 4050340.4364 [-] Reynolds Number, segment 1
Re_2 : 9301869.2065 [-] Reynolds Number, segment 2
S : 27.7189 meter ** 2 total wing area
T_0 : 746.1648 newton Thrust, segment 0
T_1 : 684.5072 newton Thrust, segment 1
T_2 : 2206.5587 newton Thrust, segment 2
V_0 : 68.2403 meter / second Velocity, segment 0
V_1 : 65.3149 meter / second Velocity, segment 1
V_2 : 150.0000 meter / second Velocity, segment 2
V_stall : 38.0000 meter / second stall speed
W_0 : 33694.3546 newton Weight, segment 0
W_1 : 30868.7209 newton Weight, segment 1
W_2 : 33694.3546 newton Weight, segment 2
W_MTO : 36773.9503 newton Maximum Takeoff Weight
W_cap : 4091.0280 newton Weight of Wing Spar Cap
W_eng : 2802.5264 newton Engine Weight
W_fuel_out : 3079.5957 newton Weight of fuel, outbound
W_fuel_ret : 2825.6337 newton Weight of fuel, return
W_pay : 4905.0000 newton Payload Weight
W_tilde : 22407.5264 newton Dry Weight, no wing
W_web : 139.5692 newton Weight of Wing Spar Shear Web
W_wing : 8461.1945 newton wing weight
W_zfw : 30868.7209 newton Zero Fuel Weight
eta_0_0 : 0.2700 [-] Overall Efficiency, segment 0
eta_0_1 : 0.2700 [-] Overall Efficiency, segment 1
eta_0_2 : 0.2795 [-] Overall Efficiency, segment 2
eta_i_0 : 0.9075 [-] Inviscid Propeller Efficiency, segment 0
eta_i_1 : 0.9074 [-] Inviscid Propeller Efficiency, segment 1
eta_i_2 : 0.9394 [-] Inviscid Propeller Efficiency, segment 2
eta_prop_0 : 0.7714 [-] Propeller Efficiency, segment 0
eta_prop_1 : 0.7713 [-] Propeller Efficiency, segment 1
eta_prop_2 : 0.7985 [-] Propeller Efficiency, segment 2
nu : 0.7860 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2
p : 1.9000 [-] Dummy Variable (1+2*lam_w)
q : 1.4500 [-] Dummy Variable (1+lam_w)
t_cap_bar : 0.0046 [-] Spar cap thickness per unit chord
t_web_bar : 0.0007 [-] Spar web thickness per unit chord
tau : 0.1500 [-] airfoil thickness to chord ratio
z_bre_0 : 0.0875 [-] Breguet Range Factor, segment 0
z_bre_1 : 0.0876 [-] Breguet Range Factor, segment 1
Constants
---------
A_prop : 0.7850 meter ** 2 Disk area of propeller
CDA0 : 0.0500 meter ** 2 fuselage drag area
C_Lmax : 1.5000 [-] max CL with flaps down
N_lift : 6 [-] Ultimate Load Factor
W_fixed : 14700 newton fixed weight
e : 0.9500 [-] Oswald efficiency factor
eta_eng : 0.3500 [-] Engine Efficiency
eta_v : 0.8500 [-] Propeller Viscous Efficiency
f_wadd : 2 [-] Added Weight Fraction
g : 9.8100 meter / second ** 2 Gravitational constant
h_fuel : 46000000 joule / kilogram Fuel Specific energy density
k_ew : 0.0372 newton / watt ** 0.803 Constant for engine weight
mu : 0.0000 kilogram / meter / second viscosity of air
r_h : 0.7500 [-] Ratio of height at rear spar to maximum wing height
rho : 0.9091 kilogram / meter ** 3 density of air
rho_SL : 1.2250 kilogram / meter ** 3 density of air, sea level
rho_cap : 2700 kilogram / meter ** 3 Density of wing cap material (aluminum)
rho_web : 2700 kilogram / meter ** 3 Density of wing web material (aluminum)
sigma_max : 310 megapascal Ultimate tensile stress of aluminum
sigma_max_shear : 167 megapascal Ultimate shear stress of aluminum
w_bar : 0.5000 [-] Ratio of spar box width to chord length
Sensitivities
-------------
Sensitivities not currently implemented for optimization type Logspace Sequential Quadratic Program
Solve Report
------------
Solve Method : Logspace Sequential Quadratic Program
Classification : Iterative
Solver : cvxopt
Number of Iterations : 7
Termination Status : Converged, gradient of Lagrangian (9.638917e-07) within tolerance (1.000000e-06)
Messages
--------
1. Wolfe Condition 1 failed at iteration 5 (Step 5). Watchdog counter is 1
2. Wolfe Condition 1 failed at iteration 6 (Step 6). Watchdog counter is 2
real 1m3.235s
user 1m2.017s
sys 0m0.951s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hoburg_blackbox.py passed (as expected)
=================================================
=================================================
+ echo 'pyCAPS/sizeWing.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/sizeWing.py test;
+ python -u pyCAPS/sizeWing.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2
Objective
---------
0.075 dimensionless
Variables
---------
AR : 10.000 [-] Wing aspect ratio
CD : 0.075 [-] Drag Coefficient
CL : 0.999 [-] Lift Coefficient
S : 2.642 meter ** 2 Wing area
V : 2.722 meter / second Airspeed
W : 11.979 newton Aircraft weight
Wwing : 1.598 newton Wing weight
Constants
---------
ARmax : 10 [-] Max AR
CD0 : 0.040 [-] Profile drag
CLmax : 1 [-] Max CL
E0 : 10 joule Maximum elastic potential energy in rubber band
Wfixed : 0.100 newton Weight of fixed components
Wrock : 2 newton Weight of each rock
e : 0.900 [-] Oswawld efficiency factor
g : 9.810 meter / second ** 2 Gravitational constant
nrock : 2 [-] Number of rocks to carry
rho : 1.225 kilogram / meter ** 3 Density of air
rho_wing : 1 kilogram / meter ** 3 Weight density of wing
tau : 0.120 [-] Airfoil thickness as t/c
Sensitivities
-------------
Sensitivities not computed
Solve Report
------------
Solve Method : Geometric Program
Classification : Convex
Solver : cvxopt
Optimized L/D: 13.267784561972134
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
real 0m2.965s
user 0m2.782s
sys 0m0.371s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case pyCAPS/sizeWing.py passed (as expected)
=================================================
avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/avl
=================================================
+ echo 'pyCAPS/optTaperAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optTaperAvl.py test;
+ python -u pyCAPS/optTaperAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Objective
---------
1.00805 dimensionless
Variables
---------
e : 0.99202 [-] Oswald efficiency factor
lam : 0.39881 [-] Wing taper ratio
Sensitivities
-------------
Sensitivities not available for optimizations of type Sequential Log Convex Program
Solve Report
------------
Solve Method : Sequential Log Convex Program
Classification : Iterative
Solver : cvxopt
Number of Iterations : 6
Termination Status : Converged, gradient of Lagrangian (5.888798e-08) within tolerance (1.000000e-06)
Messages
--------
1. Wolfe Condition 1 failed at iteration 5 (Step 5). Watchdog counter is 1
real 0m10.814s
user 0m6.997s
sys 0m3.445s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case pyCAPS/optTaperAvl.py passed (as expected)
=================================================
=================================================
+ echo 'pyCAPS/optWingAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optWingAvl.py test;
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u pyCAPS/optWingAvl.py -outLevel=0
nrock 2
Starting iteration 0 at 0.4478 seconds
AR : 9.0 dimensionless
CD : 0.1 dimensionless
CL : 1.0 dimensionless
S : 1.0 meter ** 2
V : 1.0 meter / second
W : 10.0 newton
Wwing : 0.1 newton
e : 1.0 dimensionless
lam : 0.3 dimensionless
AVL run case - lam, AR: 0.3 9.0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
y: 0.9905504143712881 dimensionless
dydx: [<Quantity(0.06083473495514524, 'dimensionless')>, <Quantity(-0.0014769756676580315, 'dimensionless')>]
Calling cvxopt.solvers.cp at 2.5927 seconds
Got sol from cvxopt at 2.6195 seconds
status optimal
x [ 1.05e-01]
[-3.26e-01]
[-1.49e-11]
[-4.10e-01]
[ 1.28e+00]
[-6.40e-01]
[ 7.00e-01]
[-1.08e-02]
[ 5.73e-03]
[-3.20e-16]
[ 3.50e-16]
[ 1.56e-16]
[ 5.20e-16]
[ 2.70e-16]
[ 4.16e-27]
[ 3.37e-16]
[ 2.07e-23]
y [-6.40e-01]
[ 7.00e-01]
[ 3.11e-01]
znl [ 6.74e-01]
[ 4.14e-08]
zl [ 1.04e+00]
[ 5.41e-01]
[ 8.31e-12]
snl [ 8.55e-11]
[ 2.03e-01]
sl [ 1.49e-11]
[ 4.30e-10]
[ 8.74e-01]
gap 8.743959706206368e-09
relative gap 7.194197617463699e-09
primal objective -1.2154183372695613
dual objective -1.2154183416835473
primal slack 1.3843122277350236e-11
dual slack 8.310943825859287e-12
primal infeasibility 1.1390346865902829e-09
dual infeasibility 2.382340215936626e-11
AVL run case - lam, AR: 0.3017253411785192 9.999999995701312
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
y: 0.9892210301573763 dimensionless
dydx: [<Quantity(0.06359341837018362, 'dimensionless')>, <Quantity(-0.0014812479868592243, 'dimensionless')>]
logspace stuff at 4.7388 seconds
Starting iteration 1 at 4.7811 seconds
AR : 9.999999995701312 dimensionless
CD : 0.07217671497330203 dimensionless
CL : 0.9999999999851361 dimensionless
S : 0.6639217992634345 meter ** 2
V : 3.600068783658014 meter / second
W : 5.270412635736404 newton
Wwing : 0.20138431695627712 newton
e : 0.9892553874048055 dimensionless
lam : 0.3017253411785192 dimensionless
Calling cvxopt.solvers.cp at 4.7999 seconds
Got sol from cvxopt at 4.8342 seconds
status optimal
x [ 3.90e-10]
[-5.94e-05]
[-1.96e-07]
[ 1.14e-08]
[ 7.38e-08]
[-3.68e-08]
[ 1.70e-08]
[ 1.33e-04]
[ 8.64e-03]
[ 6.35e-21]
[-6.95e-21]
[ 2.23e-16]
[ 5.42e-17]
[ 2.20e-16]
[ 1.27e-26]
[ 5.00e-16]
[ 6.63e-26]
y [ 1.27e-05]
[-1.39e-05]
[ 4.46e-01]
znl [ 1.00e+00]
[ 1.33e-10]
zl [ 1.08e-01]
[ 4.39e-01]
[ 2.53e-11]
snl [ 2.06e-11]
[ 2.03e-01]
sl [ 1.96e-07]
[ 4.02e-11]
[ 8.74e-01]
gap 2.1363031594082996e-08
relative gap 8.126967446318895e-09
primal objective -2.628659673511965
dual objective -2.6286596843378565
primal slack 2.057784648141205e-11
dual slack 2.5305040678747188e-11
primal infeasibility 3.0858031730676883e-09
dual infeasibility 3.1339132207348104e-09
AVL run case - lam, AR: 0.3043446483574454 9.99999999959832
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
y: 0.9893844569300864 dimensionless
dydx: [<Quantity(0.0613587900901158, 'dimensionless')>, <Quantity(-0.0014697917148703832, 'dimensionless')>]
logspace stuff at 6.5114 seconds
Starting iteration 2 at 6.5689 seconds
AR : 9.99999999959832 dimensionless
CD : 0.07217242517886534 dimensionless
CL : 0.9999998041107226 dimensionless
S : 0.6639218068635588 meter ** 2
V : 3.6000690493939635 meter / second
W : 5.270412441791246 newton
Wwing : 0.20138432037500312 newton
e : 0.989386895901959 dimensionless
lam : 0.3043446483574454 dimensionless
Calling cvxopt.solvers.cp at 6.5857 seconds
Got sol from cvxopt at 6.6143 seconds
status optimal
x [ 7.75e-13]
[-3.52e-04]
[ 4.29e-09]
[-2.11e-10]
[-1.42e-09]
[ 1.25e-09]
[-3.17e-10]
[ 7.91e-04]
[ 4.20e-02]
[ 7.26e-21]
[-7.89e-21]
[ 2.23e-16]
[ 5.45e-17]
[ 2.20e-16]
[ 1.24e-26]
[ 5.00e-16]
[ 6.65e-26]
y [ 1.45e-05]
[-1.58e-05]
[ 4.45e-01]
znl [ 1.00e+00]
[ 1.33e-10]
zl [ 1.09e-01]
[ 4.39e-01]
[ 2.49e-11]
snl [ 2.02e-11]
[ 2.03e-01]
sl [ 1.92e-07]
[ 3.94e-11]
[ 8.74e-01]
gap 2.0979541929842845e-08
relative gap 7.980432611695012e-09
primal objective -2.628872763000109
dual objective -2.628872773631958
primal slack 2.02261955200119e-11
dual slack 2.487027023449014e-11
primal infeasibility 3.030673451220543e-09
dual infeasibility 3.0769324710021364e-09
AVL run case - lam, AR: 0.3174093513141959 9.999999999606068
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
y: 0.9901147289475967 dimensionless
dydx: [<Quantity(0.05073085616900119, 'dimensionless')>, <Quantity(-0.0014191909878552567, 'dimensionless')>]
logspace stuff at 8.4138 seconds
Starting iteration 3 at 8.4792 seconds
AR : 9.999999999606068 dimensionless
CD : 0.0721469915733377 dimensionless
CL : 0.9999998084033913 dimensionless
S : 0.6639218067235316 meter ** 2
V : 3.6000690442960233 meter / second
W : 5.270412448377285 newton
Wwing : 0.20138432031121437 newton
e : 0.9901696737886684 dimensionless
lam : 0.3174093513141959 dimensionless
Calling cvxopt.solvers.cp at 8.4963 seconds
Got sol from cvxopt at 8.5348 seconds
status optimal
x [ 2.14e-12]
[-1.28e-03]
[ 1.17e-08]
[-5.10e-10]
[-3.51e-09]
[ 4.16e-09]
[-7.67e-10]
[ 2.88e-03]
[ 1.81e-01]
[-4.10e-21]
[ 4.49e-21]
[ 2.23e-16]
[ 5.51e-17]
[ 2.20e-16]
[ 1.18e-26]
[ 5.00e-16]
[ 6.61e-26]
y [-8.19e-06]
[ 8.98e-06]
[ 4.45e-01]
znl [ 1.00e+00]
[ 1.32e-10]
zl [ 1.10e-01]
[ 4.40e-01]
[ 2.37e-11]
snl [ 1.92e-11]
[ 2.03e-01]
sl [ 1.80e-07]
[ 3.73e-11]
[ 8.74e-01]
gap 1.9913348950487102e-08
relative gap 7.572537674639902e-09
primal objective -2.6296797462198227
dual objective -2.629679756312197
primal slack 1.9233234441874093e-11
dual slack 2.3654666052959533e-11
primal infeasibility 2.8765759486725376e-09
dual infeasibility 2.9202708054711625e-09
AVL run case - lam, AR: 0.3802990571782025 9.999999999627487
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
y: 0.9919295458295875 dimensionless
dydx: [<Quantity(0.009583432732673813, 'dimensionless')>, <Quantity(-0.0013533445524671617, 'dimensionless')>]
logspace stuff at 10.2780 seconds
Starting iteration 4 at 10.3333 seconds
AR : 9.999999999627487 dimensionless
CD : 0.07205440311148241 dimensionless
CL : 0.9999998201037487 dimensionless
S : 0.6639218063847038 meter ** 2
V : 3.600069031643119 meter / second
W : 5.270412470306208 newton
Wwing : 0.20138432015683602 newton
e : 0.9930297814905515 dimensionless
lam : 0.3802990571782025 dimensionless
Calling cvxopt.solvers.cp at 10.3482 seconds
Got sol from cvxopt at 10.3837 seconds
status optimal
x [-1.57e-12]
[ 4.08e-04]
[-8.59e-09]
[ 5.53e-10]
[ 3.53e-09]
[-9.72e-10]
[ 8.30e-10]
[-9.18e-04]
[ 5.19e-02]
[-2.12e-20]
[ 2.32e-20]
[ 2.24e-16]
[ 5.46e-17]
[ 2.20e-16]
[ 1.23e-26]
[ 5.00e-16]
[ 6.59e-26]
y [-4.25e-05]
[ 4.64e-05]
[ 4.47e-01]
znl [ 1.00e+00]
[ 1.32e-10]
zl [ 1.09e-01]
[ 4.39e-01]
[ 2.45e-11]
snl [ 1.99e-11]
[ 2.03e-01]
sl [ 1.88e-07]
[ 3.88e-11]
[ 8.74e-01]
gap 2.0688403479273492e-08
relative gap 7.866667127599179e-09
primal objective -2.629881644119772
dual objective -2.629881654604474
primal slack 1.9944303018455954e-11
dual slack 2.4539201182166233e-11
primal infeasibility 2.9853821718634855e-09
dual infeasibility 3.0364291201811334e-09
AVL run case - lam, AR: 0.40055731597956656 9.999999999611775
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
y: 0.9920150584836676 dimensionless
dydx: [<Quantity(-0.0008541793324268188, 'dimensionless')>, <Quantity(-0.0013850816280086553, 'dimensionless')>]
logspace stuff at 12.0285 seconds
Starting iteration 5 at 12.0848 seconds
AR : 9.999999999611775 dimensionless
CD : 0.07208383829260291 dimensionless
CL : 0.9999998115160276 dimensionless
S : 0.6639218067517705 meter ** 2
V : 3.600069044356998 meter / second
W : 5.270412465184867 newton
Wwing : 0.20138432032400524 newton
e : 0.9921187131764531 dimensionless
lam : 0.40055731597956656 dimensionless
Calling cvxopt.solvers.cp at 12.0982 seconds
Got sol from cvxopt at 12.1332 seconds
status optimal
x [ 8.00e-13]
[ 4.58e-05]
[ 4.24e-09]
[-2.43e-10]
[-1.58e-09]
[ 8.36e-10]
[-3.65e-10]
[-1.03e-04]
[-4.33e-03]
[-2.09e-21]
[ 2.29e-21]
[ 2.23e-16]
[ 5.49e-17]
[ 2.19e-16]
[ 1.20e-26]
[ 5.00e-16]
[ 6.74e-26]
y [-4.18e-06]
[ 4.57e-06]
[ 4.45e-01]
znl [ 1.00e+00]
[ 1.35e-10]
zl [ 1.10e-01]
[ 4.39e-01]
[ 2.41e-11]
snl [ 1.96e-11]
[ 2.03e-01]
sl [ 1.84e-07]
[ 3.80e-11]
[ 8.74e-01]
gap 2.0319558430018127e-08
relative gap 7.72642316948719e-09
primal objective -2.629879050666436
dual objective -2.6298790609642557
primal slack 1.9617027174043307e-11
dual slack 2.4096853737193532e-11
primal infeasibility 2.9323641616395997e-09
dual infeasibility 2.9672633006208335e-09
AVL run case - lam, AR: 0.39882645454821797 9.999999999619773
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
y: 0.9920158805953564 dimensionless
dydx: [<Quantity(-6.436458188652239e-06, 'dimensionless')>, <Quantity(-0.0013814190269922921, 'dimensionless')>]
logspace stuff at 13.8044 seconds
Starting iteration 6 at 13.8913 seconds
AR : 9.999999999619773 dimensionless
CD : 0.07208714305299325 dimensionless
CL : 0.9999998157581855 dimensionless
S : 0.6639218065905538 meter ** 2
V : 3.6000690386621352 meter / second
W : 5.270412469588729 newton
Wwing : 0.20138432025057307 newton
e : 0.9920165401543815 dimensionless
lam : 0.39882645454821797 dimensionless
Calling cvxopt.solvers.cp at 13.9046 seconds
Got sol from cvxopt at 13.9412 seconds
status optimal
x [ 2.35e-13]
[ 2.97e-07]
[ 1.09e-09]
[-5.55e-11]
[-3.69e-10]
[ 2.96e-10]
[-8.34e-11]
[-6.65e-07]
[-3.26e-05]
[ 1.22e-24]
[-1.28e-24]
[ 2.23e-16]
[ 5.49e-17]
[ 2.19e-16]
[ 1.20e-26]
[ 5.00e-16]
[ 6.76e-26]
y [ 2.45e-09]
[-2.57e-09]
[ 4.45e-01]
znl [ 1.00e+00]
[ 1.35e-10]
zl [ 1.10e-01]
[ 4.39e-01]
[ 2.40e-11]
snl [ 1.95e-11]
[ 2.03e-01]
sl [ 1.83e-07]
[ 3.78e-11]
[ 8.74e-01]
gap 2.0211071384418575e-08
relative gap 7.685171307020508e-09
primal objective -2.6298790979396243
dual objective -2.6298791081822794
primal slack 1.9527381358931494e-11
dual slack 2.3958347059954e-11
primal infeasibility 2.91563113889845e-09
dual infeasibility 2.9337880900448994e-09
AVL run case - lam, AR: 0.3988134371869373 9.999999999622123
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wing, index = 1
Getting vortex lattice surface data
VLM surface name - wing
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 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
y: 0.9920158812322937 dimensionless
dydx: [<Quantity(-5.70957042755893e-07, 'dimensionless')>, <Quantity(-0.0013813957758401774, 'dimensionless')>]
logspace stuff at 15.5530 seconds
Objective
---------
0.072 dimensionless
Variables
---------
AR : 10.000 [-] Wing aspect ratio
CD : 0.072 [-] Drag Coefficient
CL : 1.000 [-] Lift Coefficient
S : 0.664 meter ** 2 Wing area
V : 3.600 meter / second Airspeed
W : 5.270 newton Aircraft weight
Wwing : 0.201 newton Wing weight
e : 0.992 [-] Oswald efficiency factor
lam : 0.399 [-] Wing taper ratio
Sensitivities
-------------
Sensitivities not available for optimizations of type Sequential Log Convex Program
Solve Report
------------
Solve Method : Sequential Log Convex Program
Classification : Iterative
Solver : cvxopt
Number of Iterations : 7
Termination Status : Converged, gradient of Lagrangian (1.043845e-07) within tolerance (1.000000e-06)
Messages
--------
1. Wolfe Condition 1 failed at iteration 3 (Step 3). Watchdog counter is 1
13.872092548132564
real 0m18.301s
user 0m11.217s
sys 0m5.810s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case pyCAPS/optWingAvl.py passed (as expected)
=================================================
=================================================
+ echo 'pyCAPS/GPSize.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/GPSize.py test;
+ python -u pyCAPS/GPSize.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
6339.9402476213 newton
Variables
---------
AR : 18.0583068591 [-] aspect ratio
C_D_0 : 0.0127966186 [-] Drag Coefficient, segment 0
C_D_1 : 0.0128135534 [-] Drag Coefficient, segment 1
C_D_2 : 0.0077622395 [-] Drag Coefficient, segment 2
C_Dfuse_0 : 0.0017626506 [-] Fuselage Drag Coefficient, segment 0
C_Dfuse_1 : 0.0017626506 [-] Fuselage Drag Coefficient, segment 1
C_Dfuse_2 : 0.0017626510 [-] Fuselage Drag Coefficient, segment 2
C_Di_0 : 0.0056016002 [-] Induced Drag Coefficient, segment 0
C_Di_1 : 0.0056028716 [-] Induced Drag Coefficient, segment 1
C_Di_2 : 0.0002594009 [-] Induced Drag Coefficient, segment 2
C_Dp_0 : 0.0054327043 [-] Wing Profile Drag Coefficient, segment 0
C_Dp_1 : 0.0054483614 [-] Wing Profile Drag Coefficient, segment 1
C_Dp_2 : 0.0057382717 [-] Wing Profile Drag Coefficient, segment 2
C_L_0 : 0.5494535783 [-] Lift Coefficient, segment 0
C_L_1 : 0.5495159270 [-] Lift Coefficient, segment 1
C_L_2 : 0.1182390122 [-] Lift Coefficient, segment 2
I_cap_bar : 0.0000193397 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4
M_r_bar : 32106.9717613474 newton Root Bending unit per unit chord
P_max : 1211155.7559680410 watt Maximum Engine Power
R : 4999.9816129528 kilometer Single Segment range
Re_0 : 4636790.3991634697 [-] Reynolds Number, segment 0
Re_1 : 4427330.4209076529 [-] Reynolds Number, segment 1
Re_2 : 9995446.9239517339 [-] Reynolds Number, segment 2
S : 28.3664420021 meter ** 2 total wing area
T_0 : 799.0178645705 newton Thrust, segment 0
T_1 : 729.4239244544 newton Thrust, segment 1
T_2 : 2252.7493855701 newton Thrust, segment 2
V_0 : 69.5874592840 meter / second Velocity, segment 0
V_1 : 66.4439512429 meter / second Velocity, segment 1
V_2 : 150.0084591036 meter / second Velocity, segment 2
V_stall : 37.9986643205 meter / second stall speed
W_0 : 34307.5807516552 newton Weight, segment 0
W_1 : 31281.5531631161 newton Weight, segment 1
W_2 : 34307.5610637156 newton Weight, segment 2
W_MTO : 37630.4011124297 newton Maximum Takeoff Weight
W_cap : 4278.1047592241 newton Weight of Wing Spar Cap
W_eng : 2854.2361754189 newton Engine Weight
W_fuel_out : 3314.0247993997 newton Weight of fuel, outbound
W_fuel_ret : 3025.9122892774 newton Weight of fuel, return
W_pay : 4905.2326701420 newton Payload Weight
W_tilde : 22457.8594632444 newton Dry Weight, no wing
W_web : 133.6940460361 newton Weight of Wing Spar Shear Web
W_wing : 8823.3040844200 newton wing weight
W_zfw : 31281.2018350684 newton Zero Fuel Weight
eta_0_0 : 0.2693167459 [-] Overall Efficiency, segment 0
eta_0_1 : 0.2692858916 [-] Overall Efficiency, segment 1
eta_0_2 : 0.2791280518 [-] Overall Efficiency, segment 2
eta_i_0 : 0.9052651192 [-] Inviscid Propeller Efficiency, segment 0
eta_i_1 : 0.9051614203 [-] Inviscid Propeller Efficiency, segment 1
eta_i_2 : 0.9382448822 [-] Inviscid Propeller Efficiency, segment 2
eta_prop_0 : 0.7694756986 [-] Propeller Efficiency, segment 0
eta_prop_1 : 0.7693875506 [-] Propeller Efficiency, segment 1
eta_prop_2 : 0.7975082496 [-] Propeller Efficiency, segment 2
nu : 0.7860410805 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2
p : 1.9000448519 [-] Dummy Variable (1+2*lam_w)
q : 1.4500404597 [-] Dummy Variable (1+lam_w)
t_cap_bar : 0.0043345438 [-] Spar cap thickness per unit chord
t_web_bar : 0.0006000270 [-] Spar web thickness per unit chord
tau : 0.1499996279 [-] airfoil thickness to chord ratio
z_bre_0 : 0.0922115805 [-] Breguet Range Factor, segment 0
z_bre_1 : 0.0923337617 [-] Breguet Range Factor, segment 1
Constants
---------
A_prop : 0.7850000000 meter ** 2 Disk area of propeller
CDA0 : 0.0500000000 meter ** 2 fuselage drag area
C_Lmax : 1.5000000000 [-] max CL with flaps down
N_lift : 6 [-] Ultimate Load Factor
W_fixed : 14700 newton fixed weight
e : 0.9500000000 [-] Oswald efficiency factor
eta_eng : 0.3500000000 [-] Engine Efficiency
eta_v : 0.8500000000 [-] Propeller Viscous Efficiency
f_wadd : 2 [-] Added Weight Fraction
g : 9.8100000000 meter / second ** 2 Gravitational constant
h_fuel : 46000000 joule / kilogram Fuel Specific energy density
k_ew : 0.0372000000 newton / watt ** 0.803 Constant for engine weight
mu : 0.0000171000 kilogram / meter / second viscosity of air
r_h : 0.7500000000 [-] Ratio of height at rear spar to maximum wing height
rho : 0.9091220000 kilogram / meter ** 3 density of air
rho_SL : 1.2250000000 kilogram / meter ** 3 density of air, sea level
rho_cap : 2700 kilogram / meter ** 3 Density of wing cap material (aluminum)
rho_web : 2700 kilogram / meter ** 3 Density of wing web material (aluminum)
sigma_max : 250 megapascal Allowable tensile stress of aluminum
sigma_max_shear : 167 megapascal Allowable shear stress of aluminum
w_bar : 0.5000000000 [-] Ratio of spar box width to chord length
Sensitivities
-------------
Sensitivities not computed
Solve Report
------------
Solve Method : Geometric Program
Classification : Convex
Solver : cvxopt
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
real 0m15.958s
user 0m15.166s
sys 0m0.991s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case pyCAPS/GPSize.py passed (as expected)
=================================================
mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/mses
=================================================
+ echo 'pyCAPS/MSES.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/MSES.py test;
+ python -u pyCAPS/MSES.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Objective
---------
6436.3912141344 newton
Variables
---------
AR : 17.9064478129 [-] aspect ratio
Alpha_p20_MSES_0 : 22.7211519990 degree Angle of Attack + 20deg from MSES, segment 0
Alpha_p20_MSES_1 : 22.6953218092 degree Angle of Attack + 20deg from MSES, segment 1
Alpha_p20_MSES_2 : 18.8665108253 degree Angle of Attack + 20deg from MSES, segment 2
C_D_0 : 0.0128868885 [-] Drag Coefficient, segment 0
C_D_1 : 0.0128291749 [-] Drag Coefficient, segment 1
C_D_2 : 0.0074753921 [-] Drag Coefficient, segment 2
C_Dfuse_0 : 0.0017722656 [-] Fuselage Drag Coefficient, segment 0
C_Dfuse_1 : 0.0017722656 [-] Fuselage Drag Coefficient, segment 1
C_Dfuse_2 : 0.0017722656 [-] Fuselage Drag Coefficient, segment 2
C_Di_0 : 0.0054778078 [-] Induced Drag Coefficient, segment 0
C_Di_1 : 0.0054168632 [-] Induced Drag Coefficient, segment 1
C_Di_2 : 0.0002607206 [-] Induced Drag Coefficient, segment 2
C_Dp_0 : 0.0056368154 [-] Wing Profile Drag Coefficient, segment 0
C_Dp_1 : 0.0056400462 [-] Wing Profile Drag Coefficient, segment 1
C_Dp_2 : 0.0054424037 [-] Wing Profile Drag Coefficient, segment 2
C_L_0 : 0.5410592839 [-] Lift Coefficient, segment 0
C_L_1 : 0.5380410261 [-] Lift Coefficient, segment 1
C_L_2 : 0.1180399880 [-] Lift Coefficient, segment 2
C_L_MSES_0 : 0.5410592839 [-] Lift Coefficient from MSES, segment 0
C_L_MSES_1 : 0.5380410261 [-] Lift Coefficient from MSES, segment 1
C_L_MSES_2 : 0.1180399880 [-] Lift Coefficient from MSES, segment 2
I_cap_bar : 0.0000190294 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4
M_r_bar : 31688.9338344574 newton Root Bending unit per unit chord
P_max : 1156269.6009418026 watt Maximum Engine Power
R : 5000.0000009406 kilometer Single Segment range
Re_0 : 4675471.1359547451 [-] Reynolds Number, segment 0
Re_1 : 4472446.0471084677 [-] Reynolds Number, segment 1
Re_2 : 10009980.4347200561 [-] Reynolds Number, segment 2
S : 28.2124755016 meter ** 2 total wing area
T_0 : 811.2380859869 newton Thrust, segment 0
T_1 : 738.9898037834 newton Thrust, segment 1
T_2 : 2156.9995885670 newton Thrust, segment 2
V_0 : 70.0621477319 meter / second Velocity, segment 0
V_1 : 67.0198075368 meter / second Velocity, segment 1
V_2 : 150.0000123234 meter / second Velocity, segment 2
V_stall : 37.9999995456 meter / second stall speed
W_0 : 34060.0367985338 newton Weight, segment 0
W_1 : 30992.3930809630 newton Weight, segment 1
W_2 : 34060.0367985338 newton Weight, segment 2
W_MTO : 37428.7850409815 newton Maximum Takeoff Weight
W_cap : 4187.4657136299 newton Weight of Wing Spar Cap
W_eng : 2749.0298144962 newton Engine Weight
W_fuel_out : 3368.7476046609 newton Weight of fuel, outbound
W_fuel_ret : 3067.6436094735 newton Weight of fuel, return
W_pay : 4905.0000770013 newton Payload Weight
W_tilde : 22354.0298493220 newton Dry Weight, no wing
W_web : 131.7165615697 newton Weight of Wing Spar Shear Web
W_wing : 8638.3641164558 newton wing weight
W_zfw : 30992.3930605310 newton Zero Fuel Weight
eta_0_0 : 0.2692787194 [-] Overall Efficiency, segment 0
eta_0_1 : 0.2693832845 [-] Overall Efficiency, segment 1
eta_0_2 : 0.2798223310 [-] Overall Efficiency, segment 2
eta_i_0 : 0.9051385526 [-] Inviscid Propeller Efficiency, segment 0
eta_i_1 : 0.9054900321 [-] Inviscid Propeller Efficiency, segment 1
eta_i_2 : 0.9405792639 [-] Inviscid Propeller Efficiency, segment 2
eta_prop_0 : 0.7693677697 [-] Propeller Efficiency, segment 0
eta_prop_1 : 0.7696665273 [-] Propeller Efficiency, segment 1
eta_prop_2 : 0.7994923743 [-] Propeller Efficiency, segment 2
nu : 0.7859964130 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2
p : 1.9000000028 [-] Dummy Variable (1+2*lam_w)
q : 1.4500000050 [-] Dummy Variable (1+lam_w)
t_cap_bar : 0.0042599266 [-] Spar cap thickness per unit chord
t_web_bar : 0.0005954185 [-] Spar web thickness per unit chord
tau : 0.1499999997 [-] airfoil thickness to chord ratio
z_bre_0 : 0.0943153467 [-] Breguet Range Factor, segment 0
z_bre_1 : 0.0943830203 [-] Breguet Range Factor, segment 1
Sensitivities
-------------
Sensitivities not available for optimizations of type Sequential Log Convex Program
Solve Report
------------
Solve Method : Sequential Log Convex Program
Classification : Iterative
Solver : cvxopt
Number of Iterations : 16
Termination Status : Converged, relative change in the objective function (8.64e-06) is witin specified tolerance (1.00e-05)
Messages
--------
1. Attempted step of size 1.00e+00 at iteration 2 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
2. Attempted step of size 9.00e-01 at iteration 2 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
3. Wolfe Condition 1 failed at iteration 4 (Step 4). Watchdog counter is 1
4. Wolfe Condition 1 failed at iteration 7 (Step 7). Watchdog counter is 1
5. Wolfe Condition 1 failed at iteration 10 (Step 10). Watchdog counter is 1
6. Wolfe Condition 1 failed at iteration 11 (Step 11). Watchdog counter is 2
7. Wolfe Condition 1 failed at iteration 12 (Step 12). Watchdog counter is 3
real 4m0.279s
user 3m45.862s
sys 0m11.188s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case pyCAPS/MSES.py passed (as expected)
=================================================
=================================================
+ echo 'pyCAPS/Camber.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/Camber.py test;
+ python -u pyCAPS/Camber.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
maxloc = 1.002482 >= 1
ERROR:: (egads_rangerr) in Branch Brch_000043 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/corsairlite/multifidelity/hoburg/Camber/capsCSMFiles/naca.csm:62]]
maxloc = 1.002482 >= 1
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Objective
---------
5444.9476280478 newton
Variables
---------
AR : 18.4901973512 [-] aspect ratio
Alpha_p20_MSES_0 : 17.9528371532 degree Angle of Attack + 20deg from MSES, segment 0
Alpha_p20_MSES_1 : 18.0474152851 degree Angle of Attack + 20deg from MSES, segment 1
Alpha_p20_MSES_2 : 14.3726836491 degree Angle of Attack + 20deg from MSES, segment 2
C_D_0 : 0.0109818327 [-] Drag Coefficient, segment 0
C_D_1 : 0.0112190590 [-] Drag Coefficient, segment 1
C_D_2 : 0.0067072042 [-] Drag Coefficient, segment 2
C_Dfuse_0 : 0.0018227711 [-] Fuselage Drag Coefficient, segment 0
C_Dfuse_1 : 0.0018227711 [-] Fuselage Drag Coefficient, segment 1
C_Dfuse_2 : 0.0018227711 [-] Fuselage Drag Coefficient, segment 2
C_Di_0 : 0.0050991382 [-] Induced Drag Coefficient, segment 0
C_Di_1 : 0.0053109555 [-] Induced Drag Coefficient, segment 1
C_Di_2 : 0.0002596858 [-] Induced Drag Coefficient, segment 2
C_Dp_0 : 0.0040599234 [-] Wing Profile Drag Coefficient, segment 0
C_Dp_1 : 0.0040853325 [-] Wing Profile Drag Coefficient, segment 1
C_Dp_2 : 0.0046247461 [-] Wing Profile Drag Coefficient, segment 2
C_L_0 : 0.5301555732 [-] Lift Coefficient, segment 0
C_L_1 : 0.5408804300 [-] Lift Coefficient, segment 1
C_L_2 : 0.1196310531 [-] Lift Coefficient, segment 2
C_L_MSES_0 : 0.5301555732 [-] Lift Coefficient from MSES, segment 0
C_L_MSES_1 : 0.5408804300 [-] Lift Coefficient from MSES, segment 1
C_L_MSES_2 : 0.1196310531 [-] Lift Coefficient from MSES, segment 2
I_cap_bar : 0.0000205274 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4
M_r_bar : 32282.9387918620 newton Root Bending unit per unit chord
P_max : 1001419.9954321110 watt Maximum Engine Power
R : 5000.0000016548 kilometer Single Segment range
Re_0 : 4626593.0529566435 [-] Reynolds Number, segment 0
Re_1 : 4400555.1302864701 [-] Reynolds Number, segment 1
Re_2 : 9717957.1433745287 [-] Reynolds Number, segment 2
S : 27.4391704426 meter ** 2 total wing area
T_0 : 696.2621974610 newton Thrust, segment 0
T_1 : 642.8205037338 newton Thrust, segment 1
T_2 : 1881.6565831794 newton Thrust, segment 2
V_0 : 71.3878188257 meter / second Velocity, segment 0
V_1 : 67.8976808420 meter / second Velocity, segment 1
V_2 : 150.0000079267 meter / second Velocity, segment 2
V_stall : 37.9999897863 meter / second stall speed
W_0 : 33573.5550654004 newton Weight, segment 0
W_1 : 30957.3717720614 newton Weight, segment 1
W_2 : 33573.5550654004 newton Weight, segment 2
W_MTO : 36402.8422115107 newton Maximum Takeoff Weight
W_cap : 4321.3600258130 newton Weight of Wing Spar Cap
W_eng : 2449.1885460739 newton Engine Weight
W_fuel_out : 2828.7644163103 newton Weight of fuel, outbound
W_fuel_ret : 2616.1832117374 newton Weight of fuel, return
W_pay : 4905.0000311107 newton Payload Weight
W_tilde : 22054.1885403676 newton Dry Weight, no wing
W_web : 130.2317539101 newton Weight of Wing Spar Shear Web
W_wing : 8903.1832157470 newton wing weight
W_zfw : 30957.3717490756 newton Zero Fuel Weight
camberLocation : 0.7425836997 [-] location of maximum airfoil camber scaled by chord
eta_0_0 : 0.2733861489 [-] Overall Efficiency, segment 0
eta_0_1 : 0.2729458786 [-] Overall Efficiency, segment 1
eta_0_2 : 0.2818547308 [-] Overall Efficiency, segment 2
eta_i_0 : 0.9189450383 [-] Inviscid Propeller Efficiency, segment 0
eta_i_1 : 0.9174651383 [-] Inviscid Propeller Efficiency, segment 1
eta_i_2 : 0.9474108599 [-] Inviscid Propeller Efficiency, segment 2
eta_prop_0 : 0.7811032825 [-] Propeller Efficiency, segment 0
eta_prop_1 : 0.7798453676 [-] Propeller Efficiency, segment 1
eta_prop_2 : 0.8052992309 [-] Propeller Efficiency, segment 2
maxCamber : 0.0424943188 [-] maximum airfoil camber scaled by chord
nu : 0.7859963990 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2
p : 1.9000000016 [-] Dummy Variable (1+2*lam_w)
q : 1.4500000030 [-] Dummy Variable (1+lam_w)
t_cap_bar : 0.0046546586 [-] Spar cap thickness per unit chord
t_web_bar : 0.0006253929 [-] Spar web thickness per unit chord
tau : 0.1495437269 [-] airfoil thickness to chord ratio
z_bre_0 : 0.0809143871 [-] Breguet Range Factor, segment 0
z_bre_1 : 0.0811481449 [-] Breguet Range Factor, segment 1
Sensitivities
-------------
Sensitivities not available for optimizations of type Sequential Log Convex Program
Solve Report
------------
Solve Method : Sequential Log Convex Program
Classification : Iterative
Solver : cvxopt
Number of Iterations : 44
Termination Status : Converged, relative change in the objective function (3.04e-07) is witin specified tolerance (1.00e-05)
Messages
--------
1. Attempted step of size 1.00e+00 at iteration 4 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
2. Wolfe Condition 1 failed at iteration 5 (Step 5). Watchdog counter is 1
3. Wolfe Condition 1 failed at iteration 7 (Step 7). Watchdog counter is 1
4. Wolfe Condition 1 failed at iteration 8 (Step 8). Watchdog counter is 2
5. Attempted step of size 1.00e+00 at iteration 9 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
6. Attempted step of size 1.00e+00 at iteration 10 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
7. Wolfe Condition 1 failed at iteration 11 (Step 11). Watchdog counter is 1
8. Wolfe Condition 1 failed at iteration 13 (Step 13). Watchdog counter is 1
9. Wolfe Condition 1 failed at iteration 16 (Step 16). Watchdog counter is 1
10. Wolfe Condition 1 failed at iteration 18 (Step 18). Watchdog counter is 1
11. Attempted step of size 2.37e-01 at iteration 25 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
12. Attempted step of size 7.12e-02 at iteration 25 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
13. Wolfe Condition 1 failed at iteration 25 (Step 25). Watchdog counter is 1
14. Wolfe Condition 1 failed at iteration 32 (Step 32). Watchdog counter is 1
15. Wolfe Condition 1 failed at iteration 34 (Step 34). Watchdog counter is 1
16. Wolfe Condition 1 failed at iteration 35 (Step 35). Watchdog counter is 2
17. Wolfe Condition 1 failed at iteration 36 (Step 36). Watchdog counter is 3
18. Wolfe Condition 1 failed at iteration 42 (Step 42). Watchdog counter is 1
real 11m19.505s
user 10m18.427s
sys 0m32.366s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case pyCAPS/Camber.py passed (as expected)
=================================================
=================================================
+ echo 'pyCAPS/CMConstraint.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/CMConstraint.py test;
+ python -u pyCAPS/CMConstraint.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Getting CFD design variables.......
Number of design variables - 3
Design Variable name - camber
Design Variable name - maxloc
Design Variable name - thickness
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
Objective
---------
6394.7504675664 newton
Variables
---------
AR : 17.8913753447 [-] aspect ratio
Alpha_p20_MSES_0 : 22.3270790919 degree Angle of Attack + 20deg from MSES, segment 0
Alpha_p20_MSES_1 : 22.3914756112 degree Angle of Attack + 20deg from MSES, segment 1
Alpha_p20_MSES_2 : 18.5106875432 degree Angle of Attack + 20deg from MSES, segment 2
C_D_0 : 0.0127821144 [-] Drag Coefficient, segment 0
C_D_1 : 0.0129251719 [-] Drag Coefficient, segment 1
C_D_2 : 0.0075836100 [-] Drag Coefficient, segment 2
C_Dfuse_0 : 0.0017725945 [-] Fuselage Drag Coefficient, segment 0
C_Dfuse_1 : 0.0017725945 [-] Fuselage Drag Coefficient, segment 1
C_Dfuse_2 : 0.0017725945 [-] Fuselage Drag Coefficient, segment 2
C_Di_0 : 0.0054658617 [-] Induced Drag Coefficient, segment 0
C_Di_1 : 0.0055913053 [-] Induced Drag Coefficient, segment 1
C_Di_2 : 0.0002612825 [-] Induced Drag Coefficient, segment 2
C_Dp_0 : 0.0055436584 [-] Wing Profile Drag Coefficient, segment 0
C_Dp_1 : 0.0055612722 [-] Wing Profile Drag Coefficient, segment 1
C_Dp_2 : 0.0055497273 [-] Wing Profile Drag Coefficient, segment 2
C_L_0 : 0.5400363899 [-] Lift Coefficient, segment 0
C_L_1 : 0.5462287478 [-] Lift Coefficient, segment 1
C_L_2 : 0.1181168079 [-] Lift Coefficient, segment 2
C_L_MSES_0 : 0.5400363899 [-] Lift Coefficient from MSES, segment 0
C_L_MSES_1 : 0.5462287478 [-] Lift Coefficient from MSES, segment 1
C_L_MSES_2 : 0.1181168079 [-] Lift Coefficient from MSES, segment 2
I_cap_bar : 0.0000190292 [-] Area moment of inertia of cap on 2D cross section, normalized by chord^4
M_r_bar : 31709.4081507628 newton Root Bending unit per unit chord
P_max : 1173731.2996940832 watt Maximum Engine Power
R : 5000.0000185573 kilometer Single Segment range
Re_0 : 4684429.6694883015 [-] Reynolds Number, segment 0
Re_1 : 4444409.0185610838 [-] Reynolds Number, segment 1
Re_2 : 10013302.6010992285 [-] Reynolds Number, segment 2
S : 28.2072955874 meter ** 2 total wing area
T_0 : 806.6032366274 newton Thrust, segment 0
T_1 : 734.2363339161 newton Thrust, segment 1
T_2 : 2187.8204431749 newton Thrust, segment 2
V_0 : 70.1727920571 meter / second Velocity, segment 0
V_1 : 66.5771317503 meter / second Velocity, segment 1
V_2 : 150.0000250137 meter / second Velocity, segment 2
V_stall : 37.9999989707 meter / second stall speed
W_0 : 34075.9562944454 newton Weight, segment 0
W_1 : 31027.1592613867 newton Weight, segment 1
W_2 : 34075.9562944454 newton Weight, segment 2
W_MTO : 37421.9118468609 newton Maximum Takeoff Weight
W_cap : 4188.0636047371 newton Weight of Wing Spar Cap
W_eng : 2782.3174517949 newton Engine Weight
W_fuel_out : 3345.9535538813 newton Weight of fuel, outbound
W_fuel_ret : 3048.7969136851 newton Weight of fuel, return
W_pay : 4905.0003715348 newton Payload Weight
W_tilde : 22387.3178053338 newton Dry Weight, no wing
W_web : 131.8568932923 newton Weight of Wing Spar Shear Web
W_wing : 8639.8409715248 newton wing weight
W_zfw : 31027.1589167478 newton Zero Fuel Weight
camberLocation : 0.3845642839 [-] location of maximum airfoil camber scaled by chord
eta_0_0 : 0.2694753058 [-] Overall Efficiency, segment 0
eta_0_1 : 0.2692157528 [-] Overall Efficiency, segment 1
eta_0_2 : 0.2795983708 [-] Overall Efficiency, segment 2
eta_i_0 : 0.9057993471 [-] Inviscid Propeller Efficiency, segment 0
eta_i_1 : 0.9049269001 [-] Inviscid Propeller Efficiency, segment 1
eta_i_2 : 0.9398264564 [-] Inviscid Propeller Efficiency, segment 2
eta_prop_0 : 0.7699294450 [-] Propeller Efficiency, segment 0
eta_prop_1 : 0.7691878651 [-] Propeller Efficiency, segment 1
eta_prop_2 : 0.7988524879 [-] Propeller Efficiency, segment 2
maxCamber : 0.0236403205 [-] maximum airfoil camber scaled by chord
negCMp1_0 : 1.0578681152 [-] Negative CM about 0.25c + 1, segment 0
negCMp1_1 : 1.0576218708 [-] Negative CM about 0.25c + 1, segment 1
negCMp1_2 : 1.0596323386 [-] Negative CM about 0.25c + 1, segment 2
nu : 0.7859964982 [-] Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2
p : 1.9000000145 [-] Dummy Variable (1+2*lam_w)
q : 1.4500000244 [-] Dummy Variable (1+lam_w)
t_cap_bar : 0.0042598978 [-] Spar cap thickness per unit chord
t_web_bar : 0.0005959117 [-] Spar web thickness per unit chord
tau : 0.1499998633 [-] airfoil thickness to chord ratio
z_bre_0 : 0.0936645407 [-] Breguet Range Factor, segment 0
z_bre_1 : 0.0937293082 [-] Breguet Range Factor, segment 1
Sensitivities
-------------
Sensitivities not available for optimizations of type Sequential Log Convex Program
Solve Report
------------
Solve Method : Sequential Log Convex Program
Classification : Iterative
Solver : cvxopt
Number of Iterations : 23
Termination Status : Converged, relative change in the objective function (1.10e-06) is witin specified tolerance (1.00e-05)
Messages
--------
1. Wolfe Condition 1 failed at iteration 2 (Step 2). Watchdog counter is 1
2. Wolfe Condition 1 failed at iteration 3 (Step 3). Watchdog counter is 2
3. Wolfe Condition 1 failed at iteration 4 (Step 4). Watchdog counter is 3
4. Attempted step of size 1.00e+00 at iteration 5 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
5. Wolfe Condition 1 failed at iteration 8 (Step 8). Watchdog counter is 1
6. Wolfe Condition 1 failed at iteration 9 (Step 9). Watchdog counter is 2
7. Attempted step of size 1.00e+00 at iteration 10 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
8. Attempted step of size 3.00e-01 at iteration 10 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
9. Attempted step of size 1.00e+00 at iteration 11 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
10. Attempted step of size 1.00e+00 at iteration 12 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
11. Wolfe Condition 1 failed at iteration 14 (Step 14). Watchdog counter is 1
12. Wolfe Condition 1 failed at iteration 15 (Step 15). Watchdog counter is 2
13. Wolfe Condition 1 failed at iteration 16 (Step 16). Watchdog counter is 3
14. Wolfe Condition 1 failed at iteration 18 (Step 18). Watchdog counter is 1
15. Attempted step of size 3.81e-01 at iteration 19 is too large and is causing a constraint to return as imaginary. Decreasing according to the tau schedule.
16. Wolfe Condition 1 failed at iteration 21 (Step 21). Watchdog counter is 1
17. Wolfe Condition 1 failed at iteration 22 (Step 22). Watchdog counter is 2
real 7m11.350s
user 6m35.120s
sys 0m19.326s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case pyCAPS/CMConstraint.py passed (as expected)
=================================================
Traceback (most recent call last):
File "<string>", line 1, in <module>
ModuleNotFoundError: No module named 'torch'
*************************************************
*************************************************
=================================================
Did not run examples for:
awave
autoLink
Pointwise
Cart3D
Fun3D
abaqus
Nastran
Mystran
Plato
Mystran
=================================================
All tests pass!
=================================================
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023
+ bash -e execute_Training.sh
=================================================
Using python : /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python
=================================================
=================================================
+ echo 'transport.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
transport.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 transport.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/transport.vfy", so verification is being skipped
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
MESSAGE:: Building wingHinges
MESSAGE:: Building nacelleOml
MESSAGE:: Building htailOml
MESSAGE:: Building htailWaffle
MESSAGE:: Building htailHinges
MESSAGE:: Building vtailOml
MESSAGE:: Building vtailWaffle
MESSAGE:: Building vtailHinges
MESSAGE:: Building fuseOml
MESSAGE:: Building fuseWaffle
MESSAGE:: Building fuseIml
MESSAGE:: Building payload
==> serveESP completed successfully with 5 warnings and no verification data
real 0m21.109s
user 0m26.298s
sys 0m3.263s
+ status=0
+ set +x
=================================================
data/ESP/transport passed (as expected)
=================================================
execute_Training.sh: line 157: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/test/template_avl: No such file or directory
=================================================
template_avl.py test;
+ python template_avl.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Setting Build Variables and Geometry Values...
==> Creating AVL aim...
{'wingHinge1': {'deflectionAngle': -10.0}, 'wingHinge2': {'deflectionAngle': 10.0}, 'wingHinge3': {'deflectionAngle': 15.0}, 'wingHinge4': {'deflectionAngle': 15.0}, 'wingHinge5': {'deflectionAngle': 10.0}, 'wingHinge6': {'deflectionAngle': 10.0}, 'htailHinge1': {'deflectionAngle': 5.0}, 'htailHinge2': {'deflectionAngle': 5.0}}
==> Running AVL...
MESSAGE:: Building wingOml
MESSAGE:: Building wingHinges
MESSAGE:: Building htailOml
MESSAGE:: Building htailHinges
MESSAGE:: Building vtailOml
MESSAGE:: Building vtailHinges
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing, index = 1
Name = Htail, index = 2
Name = Vtail, index = 3
Getting vortex lattice control surface data
VLM control surface name - htailHinge1
VLM control surface name - htailHinge2
VLM control surface name - wingHinge1
VLM control surface name - wingHinge2
VLM control surface name - wingHinge3
VLM control surface name - wingHinge4
VLM control surface name - wingHinge5
VLM control surface name - wingHinge6
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Htail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl4 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl4 not found in controls tuple! Only defaults will be used.
Writing surface - Htail (ID = 0)
Section 1 of 7 (ID = 0)
Section 2 of 7 (ID = 3)
Control surface 1 of 1
Section 3 of 7 (ID = 4)
Control surface 1 of 1
Section 4 of 7 (ID = 1)
Section 5 of 7 (ID = 5)
Control surface 1 of 1
Section 6 of 7 (ID = 6)
Control surface 1 of 1
Section 7 of 7 (ID = 2)
Writing surface - Wing (ID = 1)
Section 1 of 17 (ID = 0)
Section 2 of 17 (ID = 5)
Control surface 1 of 1
Section 3 of 17 (ID = 6)
Control surface 1 of 1
Section 4 of 17 (ID = 7)
Control surface 1 of 1
Section 5 of 17 (ID = 8)
Control surface 1 of 1
Section 6 of 17 (ID = 4)
Section 7 of 17 (ID = 9)
Control surface 1 of 1
Section 8 of 17 (ID = 10)
Control surface 1 of 1
Section 9 of 17 (ID = 1)
Section 10 of 17 (ID = 11)
Control surface 1 of 1
Section 11 of 17 (ID = 12)
Control surface 1 of 1
Section 12 of 17 (ID = 3)
Section 13 of 17 (ID = 13)
Control surface 1 of 1
Section 14 of 17 (ID = 14)
Control surface 1 of 1
Section 15 of 17 (ID = 15)
Control surface 1 of 1
Section 16 of 17 (ID = 16)
Control surface 1 of 1
Section 17 of 17 (ID = 2)
================ run_avl.py complete ==================
Force/moment coefficients:
CXtot : 0.1440096424064962
CYtot : -2.354427059781186e-09
CZtot : -1.170781415636729
Cltot : -7.74027428929831e-12
Cmtot : -1.825894044461429
Cntot : -1.081704204546593e-10
CLtot : 1.178001627172014
CDtot : 0.06148224692119385
e : 0.7858933406059764
real 0m31.632s
user 0m28.949s
sys 0m9.346s
+ status=0
+ set +x
=================================================
data/session01/template_avl.py passed (as expected)
=================================================
=================================================
+ echo 'f118-A.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
f118-A.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-A.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/f118-A.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.111s
user 0m0.081s
sys 0m0.028s
+ status=0
+ set +x
=================================================
data/session02/f118-A passed (as expected)
=================================================
=================================================
1_f118_Geom.py test;
+ python 1_f118_Geom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-A.csm"...
==> Bulding and viewing geometry...
real 0m1.323s
user 0m0.848s
sys 0m0.299s
+ status=0
+ set +x
=================================================
data/session02/1_f118_Geom.py passed (as expected)
=================================================
=================================================
2_f118_DESPMTR.py test;
+ python 2_f118_DESPMTR.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-A.csm"...
--> old htail:area = 1210.0
--> new htail:area = 2420.0
==> Bulding and viewing Wide Body geometry...
==> Bulding and viewing Canard geometry...
==> All design parameters
--> wing:area = 1210.0
--> wing:aspect = 9.0
--> wing:thick = 0.1
--> wing:xroot = 54.0
--> wing:zroot = -5.0
--> htail:area = 4240.0
--> htail:aspect = 4.15
--> htail:thick = 0.08
--> htail:xroot = 145.0
--> htail:zroot = 5.0
--> vtail = [[1220.0, 1.8, 0.08, 150.0, -8.0, 9.0], [1220.0, 1.8, 0.08, 150.0, 8.0, 9.0]]
--> fuse:length = 180.0
--> fuse:width = 20.0
--> fuse:height = 20.0
real 0m1.151s
user 0m0.914s
sys 0m0.328s
+ status=0
+ set +x
=================================================
data/session02/2_f118_DESPMTR.py passed (as expected)
=================================================
=================================================
3_f118_Save.py test;
+ python 3_f118_Save.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-A.csm"...
--> old htail:area = 1210.0
--> new htail:area = 2420.0
==> Bulding and saving Wide Body geometry...
==> Bulding and saving Canard geometry...
==> All design parameters
--> wing:area = 1210.0
--> wing:aspect = 9.0
--> wing:thick = 0.1
--> wing:xroot = 54.0
--> wing:zroot = -5.0
--> htail:area = 4240.0
--> htail:aspect = 4.15
--> htail:thick = 0.08
--> htail:xroot = 145.0
--> htail:zroot = 5.0
--> vtail = [[1220.0, 1.8, 0.08, 150.0, -8.0, 9.0], [1220.0, 1.8, 0.08, 150.0, 8.0, 9.0]]
--> fuse:length = 180.0
--> fuse:width = 20.0
--> fuse:height = 20.0
real 0m1.038s
user 0m0.878s
sys 0m0.288s
+ status=0
+ set +x
=================================================
data/session02/3_f118_Save.py passed (as expected)
=================================================
=================================================
4_f118_Shortcut.py test;
+ python 4_f118_Shortcut.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-A.csm"...
--> old htail:area = 1210.0
--> new htail:area = 2420.0
==> Bulding and viewing Wide Body geometry...
==> Bulding and viewing Canard geometry...
==> Grouped parameters
--> fuse
fuse:length = 180.0
fuse:width = 20.0
fuse:height = 20.0
--> wing
wing:area = 1210.0
wing:aspect = 9.0
wing:thick = 0.1
wing:xroot = 54.0
wing:zroot = -5.0
--> htail
htail:area = 4240.0
htail:aspect = 4.15
htail:thick = 0.08
htail:xroot = 145.0
htail:zroot = 5.0
real 0m1.185s
user 0m0.938s
sys 0m0.330s
+ status=0
+ set +x
=================================================
data/session02/4_f118_Shortcut.py passed (as expected)
=================================================
=================================================
5_f118_writeParameters.py test;
+ python 5_f118_writeParameters.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-A.csm"...
==> Saving parameters to "f118_4.params"...
==> Loading 2nd geometry from file "f118-A.csm"...
==> Reading parameters from "f118_4.params"...
--> Opening DESPMTR file "f118_4.params"
updating CFGPMTR nrow [ 1, 1] = 1.000000
updating DESPMTR wing:area [ 1, 1] = 4240.000000
updating DESPMTR wing:aspect [ 1, 1] = 9.000000
updating DESPMTR wing:thick [ 1, 1] = 0.100000
updating DESPMTR wing:xroot [ 1, 1] = 54.000000
updating DESPMTR wing:zroot [ 1, 1] = -5.000000
updating DESPMTR htail:area [ 1, 1] = 2420.000000
updating DESPMTR htail:aspect [ 1, 1] = 4.150000
updating DESPMTR htail:thick [ 1, 1] = 0.080000
updating DESPMTR htail:xroot [ 1, 1] = 145.000000
updating DESPMTR htail:zroot [ 1, 1] = 5.000000
updating DESPMTR vtail [ 1, 1] = 1220.000000
updating DESPMTR vtail [ 1, 2] = 1.800000
updating DESPMTR vtail [ 1, 3] = 0.080000
updating DESPMTR vtail [ 1, 4] = 150.000000
updating DESPMTR vtail [ 1, 5] = 0.000000
updating DESPMTR vtail [ 1, 6] = 9.000000
updating DESPMTR fuse:length [ 1, 1] = 180.000000
updating DESPMTR fuse:width [ 1, 1] = 60.000000
updating DESPMTR fuse:height [ 1, 1] = 20.000000
==> Building and viewing the geometry...
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
real 0m1.229s
user 0m0.903s
sys 0m0.403s
+ status=0
+ set +x
=================================================
data/session02/5_f118_writeParameters.py passed (as expected)
=================================================
=================================================
6_f118_bodies.py test;
+ python 6_f118_bodies.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-A.csm"...
==> pyEGADS egos...
Wing <pyEGADS.egads_common.ego object at 0x115db5d90>
Htail <pyEGADS.egads_common.ego object at 0x118d13610>
Vtail1 <pyEGADS.egads_common.ego object at 0x118d13690>
Fuselage <pyEGADS.egads_common.ego object at 0x118d13190>
real 0m1.060s
user 0m0.866s
sys 0m0.287s
+ status=0
+ set +x
=================================================
data/session02/6_f118_bodies.py passed (as expected)
=================================================
=================================================
+ echo '7_f118_OUTPMTR.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
7_f118_OUTPMTR.py test;
+ python 7_f118_OUTPMTR.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-A.csm"...
--> wing:wet = 9422.222222222223
--> wing:volume = 9202.959910328365
--> htail:prop[0] = 2660.2506024096383
--> htail:prop[1] = 1652.8901595442062
--> vtail:prop = [1371.822222222222, None]
--> fuse:wet = None
--> fuse:volume = None
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session02/7_f118_OUTPMTR.py", line 34, in <module>
print ("--> wing:span =", f118.outpmtr.wing.span )
^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/pyCAPS/problem.py", line 1954, in __getattr__
raise AttributeError("No Out Value: {!r}".format(name))
AttributeError: No Out Value: 'span'
real 0m1.172s
user 0m0.859s
sys 0m0.274s
+ status=1
+ set +x
=================================================
data/session02/7_f118_OUTPMTR.py failed (as expected)
=================================================
=================================================
8_f118_Phasing.py test;
+ python 8_f118_Phasing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-A.csm"...
--> old htail:area = 1210.0
--> new htail:area = 2420.0
==> Bulding and viewing Wide Body geometry...
==> Bulding and viewing geometry from WideBody phase...
==> Bulding and viewing Canard geometry...
real 0m1.370s
user 0m0.904s
sys 0m0.483s
+ status=0
+ set +x
=================================================
data/session02/8_f118_Phasing.py passed (as expected)
=================================================
=================================================
f118_Custom.py test;
+ python f118_Custom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../../data/session02/f118-A.csm"...
==> Bulding and viewing geometry...
real 0m1.080s
user 0m0.887s
sys 0m0.298s
+ status=0
+ set +x
=================================================
solutions/session02/f118_Custom.py passed (as expected)
=================================================
=================================================
+ echo 'f118-B.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
f118-B.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-B.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/f118-B.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.130s
user 0m0.079s
sys 0m0.022s
+ status=0
+ set +x
=================================================
data/session03/f118-B passed (as expected)
=================================================
=================================================
+ echo 'f118-C.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
f118-C.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-C.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/f118-C.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.078s
user 0m0.077s
sys 0m0.021s
+ status=0
+ set +x
=================================================
data/session03/f118-C passed (as expected)
=================================================
=================================================
+ echo 'naca.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
naca.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 naca.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/naca.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.092s
user 0m0.073s
sys 0m0.021s
+ status=0
+ set +x
=================================================
data/session03/naca passed (as expected)
=================================================
=================================================
01_xfoil_input.py test;
+ python 01_xfoil_input.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
==> Creating xfoilAIM
==> Modified Mach = 0.5
==> Default Alpha = None
==> Modified Alpha = 2.5
==> Modified Alpha = [0.0, 3.0, 5.0, 7.0, 8.0]
==> Unset Alpha = None
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
real 0m1.058s
user 0m0.895s
sys 0m0.260s
+ status=0
+ set +x
=================================================
data/session03/01_xfoil_input.py passed (as expected)
=================================================
=================================================
02_xfoil_Analysis.py test;
+ python 02_xfoil_Analysis.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
==> Creating xfoilAIM
==> Setting analysis values
==> Running preAnalysis
==> Running xFoil......
==> Running postAnalysis
==> Retrieve analysis results
--> Alpha = [0.0, 3.0, 5.0, 7.0, 8.0]
--> Cl = [-3.53757485379788e-07, 0.377437462009177, 0.642259371967897, 0.955175660661444, 1.00909750957735]
--> Cd = [0.00617285380994743, 0.00729426778019865, 0.0100194565543492, 0.014871080086931, 0.0185150448281248]
real 0m2.708s
user 0m2.235s
sys 0m0.299s
+ status=0
+ set +x
=================================================
data/session03/02_xfoil_Analysis.py passed (as expected)
=================================================
=================================================
03_xfoil_AutoExec.py test;
+ python 03_xfoil_AutoExec.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
==> Creating xfoilAIM
==> Setting analysis values
==> Retrieve analysis results
--> Alpha = [0.0, 3.0, 5.0, 7.0, 8.0]
--> Cl = [-3.53757485379788e-07, 0.377437462009177, 0.642259371967897, 0.955175660661444, 1.00909750957735]
--> Cd = [0.00617285380994743, 0.00729426778019865, 0.0100194565543492, 0.014871080086931, 0.0185150448281248]
real 0m2.297s
user 0m2.075s
sys 0m0.263s
+ status=0
+ set +x
=================================================
data/session03/03_xfoil_AutoExec.py passed (as expected)
=================================================
=================================================
04_xfoil_MultiAnalysis.py test;
+ python 04_xfoil_MultiAnalysis.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
==> Creating xfoilAIM
==> Setting analysis values
==> Retrieve analysis results
--> Alpha = [0.0, 3.0, 5.0, 7.0, 8.0]
--> Cl = [-3.53757485379788e-07, 0.377437462009177, 0.642259371967897, 0.955175660661444, 1.00909750957735]
--> Cd = [0.00617285380994743, 0.00729426778019865, 0.0100194565543492, 0.014871080086931, 0.0185150448281248]
==> Retrieve analysis results
--> Alpha = [2.87619487667565e-06, 0.789686474042309, 1.18477801663685, 2.37671255179611, 3.18364393502677]
--> Cl = [8.20895546206445e-17, 0.1, 0.150000000000232, 0.300000000000163, 0.4]
--> Cd = [0.00617285381077468, 0.0062302134848261, 0.00630554753827264, 0.00680929883615267, 0.00747424244865481]
real 0m3.014s
user 0m2.703s
sys 0m0.337s
+ status=0
+ set +x
=================================================
data/session03/04_xfoil_MultiAnalysis.py passed (as expected)
=================================================
=================================================
05_xfoil_Camber_Plot.py test;
+ python 05_xfoil_Camber_Plot.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
==> Creating xfoilAIM
==> Setting analysis values
==> Retrieve analysis results. camber = 0.0
==> Retrieve analysis results. camber = 0.01
==> Retrieve analysis results. camber = 0.04
==> Retrieve analysis results. camber = 0.07
==> Plotting analysis results (close plot window to finish Python script
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session03/05_xfoil_Camber_Plot.py:65: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown
plt.show()
real 0m10.795s
user 0m9.041s
sys 0m0.600s
+ status=0
+ set +x
=================================================
data/session03/05_xfoil_Camber_Plot.py passed (as expected)
=================================================
=================================================
05_xfoil_Camber.py test;
+ python 05_xfoil_Camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
==> Creating xfoilAIM
==> Setting analysis values
==> Retrieve analysis results. camber = 0.0
==> Retrieve analysis results. camber = 0.01
==> Retrieve analysis results. camber = 0.04
==> Retrieve analysis results. camber = 0.07
--> Cambers = [0.0, 0.01, 0.04, 0.07]
--> Alpha = [[0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0]]
--> Cl = [[-3.53757485379788e-07, 0.126697477361245, 0.377437462181301], [0.140339949737298, 0.266469023977218, 0.514670926888676], [0.554542727545582, 0.680708956698583, 0.940291957324466], [0.919771481558351, 1.03861131519064]]
--> Cd = [[0.00617285380994743, 0.00627268560115741, 0.00729426778763049], [0.00625861871528587, 0.00622635244564028, 0.00706717658622408], [0.00787687247022662, 0.00739456756394001, 0.00782133651724137], [0.00972065010483813, 0.0101041953398965]]
real 0m5.200s
user 0m4.565s
sys 0m0.504s
+ status=0
+ set +x
=================================================
data/session03/05_xfoil_Camber.py passed (as expected)
=================================================
=================================================
06_xfoil_CleanDirty.py test;
+ python 06_xfoil_CleanDirty.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
==> Creating xfoilAIM
1. No Errors --------------------------------------------------------------------------------
==> Setting alpha sequence
==> Running preAnalysis
==> Running xFoil......
==> Running postAnalysis
--> Cl = [-3.53757485379788e-07, 0.377437462009177, 0.642259371967897, 0.955175660661444, 1.00909750957735]
2. DIRTY AnalysisVal Error --------------------------------------------------------------------------------
==> Setting new alpha sequence
==> Attempting to get Cl
==> CAPSError = CAPS_DIRTY:
================================================================================
================================================================================
==> Running preAnalysis
==> Running xFoil......
==> Running postAnalysis
==> Attempting to get Cl
--> Cl = 0.252764696628542
3. DIRTY GeometryVal Error --------------------------------------------------------------------------------
==> Modifying camber
==> Attempting to get Cl
==> CAPSError = CAPS_DIRTY:
================================================================================
================================================================================
==> Running preAnalysis
==> Running xFoil......
==> Running postAnalysis
==> Attempting to get Cl
--> Cl = [1.03861130997165, 1.15325582947854]
4. DIRTY pre- but no postAnalysis Error --------------------------------------------------------------------------------
==> Modifying Mach
==> Running preAnalysis but not running postAnalysis
==> Attempting to get Cl
==> CAPSError = CAPS_DIRTY:
================================================================================
================================================================================
==> Running xFoil......
==> Running postAnalysis
==> Attempting to get Cl
--> Cl = [0.967203918354729, 1.07899610948986]
5. CLEAN Error --------------------------------------------------------------------------------
==> Running preAnalysis
==> CAPSError = CAPS_CLEAN:
================================================================================
================================================================================
real 0m4.984s
user 0m4.517s
sys 0m0.490s
+ status=0
+ set +x
=================================================
data/session03/06_xfoil_CleanDirty.py passed (as expected)
=================================================
=================================================
07_masstran_f118_AIM.py test;
+ python 07_masstran_f118_AIM.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-B.csm"...
==> Geometry used by masstranAll instance with no capsIntent
==> Geometry used by Wing instance with capsIntent='wing'
==> Geometry used by Tail instance with capsIntent='tail'
==> Geometry used by WingFuse instance with capsIntent=['wing','fuse']
real 0m2.470s
user 0m1.025s
sys 0m1.162s
+ status=0
+ set +x
=================================================
data/session03/07_masstran_f118_AIM.py passed (as expected)
=================================================
=================================================
08_masstran_f118_Wing.py test;
+ python 08_masstran_f118_Wing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-C.csm"...
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = wing:faces, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
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 - 1
Property name - wing:faces
Done getting FEA properties
Updating mesh element types based on properties input
--> Mass = 14792888.88889
--> CG = [64.85254706407, 4.613994176513e-14, -3.914745293593]
real 0m1.544s
user 0m1.014s
sys 0m0.537s
+ status=0
+ set +x
=================================================
data/session03/08_masstran_f118_Wing.py passed (as expected)
=================================================
=================================================
09_masstran_f118.py test;
+ python 09_masstran_f118.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-C.csm"...
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 6
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 6
Property name - fuse:nose
Property name - fuse:side
Property name - fuse:tail
Property name - htail:faces
Property name - vtail:faces
Property name - wing:faces
Done getting FEA properties
Updating mesh element types based on properties input
-->Mass = 52825838.86801
-->CG = [91.69615213878, 9.02135549621e-15, 0.7254947287442]
real 0m2.086s
user 0m1.235s
sys 0m0.755s
+ status=0
+ set +x
=================================================
data/session03/09_masstran_f118.py passed (as expected)
=================================================
=================================================
10_masstran_f118_journal.py test;
+ python 10_masstran_f118_journal.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
################################################################################
==> First execution
==> Loading geometry from file "f118-C.csm"...
================================================================================
==> Computing mass 1
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = wing:faces, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 488
Number of elements = 972
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 972
Elemental Quad4 = 0
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 - 1
Property name - wing:faces
Done getting FEA properties
Updating mesh element types based on properties input
--> 14792888.88889
Something went wrong!
################################################################################
==> Second execution
==> Loading geometry from file "f118-C.csm"...
================================================================================
==> Computing mass 1
--> 14792888.88889
CAPS Info: Hit last success -- going live!
================================================================================
==> Computing mass 2
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = wing:faces, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 488
Number of elements = 972
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 972
Elemental Quad4 = 0
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 - 1
Property name - wing:faces
Done getting FEA properties
Updating mesh element types based on properties input
--> 1479288.888889
Something went wrong!
################################################################################
==> Third execution
==> Loading geometry from file "f118-C.csm"...
================================================================================
==> Computing mass 1
--> 14792888.88889
================================================================================
==> Computing mass 2
--> 1479288.888889
CAPS Info: Hit last success -- going live!
================================================================================
==> Computing mass 3
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = wing:faces, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 488
Number of elements = 972
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 972
Elemental Quad4 = 0
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 - 1
Property name - wing:faces
Done getting FEA properties
Updating mesh element types based on properties input
--> 147928.8888889
################################################################################
==> Fourth execution
==> Loading geometry from file "f118-C.csm"...
================================================================================
==> Computing mass 1
--> 14792888.88889
================================================================================
==> Computing mass 2
--> 1479288.888889
================================================================================
==> Computing mass 3
--> 147928.8888889
real 0m1.929s
user 0m1.180s
sys 0m0.708s
+ status=0
+ set +x
=================================================
data/session03/10_masstran_f118_journal.py passed (as expected)
=================================================
=================================================
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
+ echo 'f118-C.csm test;'
f118-C.csm test;
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-C.csm
WARNING:: cannot open "./verify_7.8.1/f118-C.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.122s
user 0m0.085s
sys 0m0.039s
+ status=0
+ set +x
=================================================
solutions/session03/f118-C passed (as expected)
=================================================
=================================================
xfoil_thickness.py test;
+ python xfoil_thickness.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../../data/session03/naca.csm"...
==> Create xfoilAIM
==> Setting analysis values
==> Retrieve analysis results
==> Retrieve analysis results
==> Retrieve analysis results
==> Retrieve analysis results
--> Thickness = [0.08, 0.1, 0.12, 0.16]
--> Alpha = [[0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0, 3.0]]
--> Cl = [[4.33419511114853e-07, 0.118003705247099, 0.407823091300777], [3.88197201209935e-07, 0.123993123613511, 0.371340021266889], [-3.53757485379788e-07, 0.126697477361245, 0.377437462181301], [-2.73508054507172e-07, 0.127624902798225, 0.38086778943914]]
--> Cd = [[0.00449613835213644, 0.00482192214519885, 0.00769709940290386], [0.00540044826496712, 0.00554773736538764, 0.00718424709042918], [0.00617285380994743, 0.00627268560115741, 0.00729426778763049], [0.00752780925540312, 0.00759373202201033, 0.00822814692467068]]
real 0m3.430s
user 0m2.858s
sys 0m0.477s
+ status=0
+ set +x
=================================================
solutions/session03/xfoil_thickness.py passed (as expected)
=================================================
=================================================
f118_masstran.py test;
+ python f118_masstran.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../../data/session03/f118-B.csm"...
==> Geometry with capsIntent=['wing','fuse', 'htail']
real 0m1.322s
user 0m0.913s
sys 0m0.476s
+ status=0
+ set +x
=================================================
solutions/session03/f118_masstran.py passed (as expected)
=================================================
=================================================
masstran_topbot.py test;
+ python masstran_topbot.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-C.csm"...
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 8
Property name - fuse:bottom
Property name - fuse:nose
Property name - fuse:side
Property name - fuse:tail
Property name - fuse:top
Property name - htail:faces
Property name - vtail:faces
Property name - wing:faces
Done getting FEA properties
Updating mesh element types based on properties input
-->Mass = 52073438.86801
-->CG = [91.72065954403, 0.04009689171826, 0.1932821772294]
real 0m1.574s
user 0m0.960s
sys 0m0.622s
+ status=0
+ set +x
=================================================
solutions/session03/masstran_topbot.py passed (as expected)
=================================================
=================================================
masstran_CG.py test;
+ python masstran_CG.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "f118-C.csm"...
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 8
Property name - fuse:bottom
Property name - fuse:nose
Property name - fuse:side
Property name - fuse:tail
Property name - fuse:top
Property name - htail:faces
Property name - vtail:faces
Property name - wing:faces
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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined 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 = 8
Name = wing:faces, index = 1
Name = htail:faces, index = 2
Name = vtail:faces, index = 3
Name = fuse:nose, index = 4
Name = fuse:tail, index = 5
Name = fuse:side, index = 6
Name = fuse:bottom, index = 7
Name = fuse:top, index = 8
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 900
Number of elements = 1796
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 1796
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 170
Number of elements = 336
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 336
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 90
Number of elements = 176
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 176
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 1698
Number of elements = 3392
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3392
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 2858
Combined Number of elements = 5700
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 5700
Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
-->Oringal CG = 91.72065954403
-->CG sweep = [84.05056882825, 85.58458697141, 87.11860511456, 88.65262325772, 90.18664140087, 91.72065954403, 93.25467768718, 94.78869583034, 96.32271397349, 97.85673211665, 99.3907502598]
real 0m2.513s
user 0m1.451s
sys 0m1.144s
+ status=0
+ set +x
=================================================
solutions/session03/masstran_CG.py passed (as expected)
=================================================
=================================================
+ echo 'f118-D.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
f118-D.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-D.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/f118-D.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.095s
user 0m0.075s
sys 0m0.022s
+ status=0
+ set +x
=================================================
data/session04/f118-D passed (as expected)
=================================================
=================================================
+ echo 'naca.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
naca.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 naca.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/naca.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.106s
user 0m0.072s
sys 0m0.022s
+ status=0
+ set +x
=================================================
data/session04/naca passed (as expected)
=================================================
=================================================
1_mses_Deriv.py test;
+ python 1_mses_Deriv.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
==> Area and Area derivatives...
--> Area 0.08221896898506213
--> dArea/dthick 0.6847211877073475
==> Drag and Drag derivatives...
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - camber
Design Variable name - thick
Done getting CFD design variables
--> CD = 0.005288406846931541
--> dCD/dAlpha = -2.942742400634222e-07
--> dCD/dMach = 0.0012453361427576114
--> dCD/dcamber = -3.160438517971385e-05
--> dCD/dthick = 0.01572064644523116
==> All Drag derivatives...
--> CD derivs = {'Alpha': -2.942742400634222e-07, 'Mach': 0.0012453361427576114, 'Re': -3.6387781085334707e-11, 'camber': -3.160438517971385e-05, 'thick': 0.01572064644523116}
real 0m4.754s
user 0m3.864s
sys 0m0.449s
+ status=0
+ set +x
=================================================
data/session04/1_mses_Deriv.py passed (as expected)
=================================================
=================================================
2_mses_DerivPlot_CD_Alpha.py test;
+ python 2_mses_DerivPlot_CD_Alpha.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
--> Alpha -3.0
--> Alpha -2.5714285714285716
--> Alpha -2.142857142857143
--> Alpha -1.7142857142857144
--> Alpha -1.2857142857142858
--> Alpha -0.8571428571428572
--> Alpha -0.4285714285714288
--> Alpha 0.0
--> Alpha 0.4285714285714284
--> Alpha 0.8571428571428568
--> Alpha 1.2857142857142856
--> Alpha 1.7142857142857144
--> Alpha 2.1428571428571423
--> Alpha 2.571428571428571
--> Alpha 3.0
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/2_mses_DerivPlot_CD_Alpha.py:77: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown
plt.show()
real 0m47.916s
user 0m44.644s
sys 0m2.240s
+ status=0
+ set +x
=================================================
data/session04/2_mses_DerivPlot_CD_Alpha.py passed (as expected)
=================================================
=================================================
3_mses_OpenMDAO_CD_Alpha.py test;
+ python 3_mses_OpenMDAO_CD_Alpha.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[macys-VM:47182] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/3808821248/sm_segment.macys-VM.502.e3060000.0 could be created.
==> Starting Optimization...
--> Alpha [3.]
--> CD [0.00803595]
--> Alpha [3.]
--> CD [0.00803595]
--> Alpha [3.]
--> CD_alpha [[0.00014124]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 1 M = 10
At X0 0 variables are exactly at the bounds
At iterate 0 f= 8.03595D-03 |proj g|= 1.41235D-04
--> Alpha [2.99985876]
--> CD [0.00803593]
--> Alpha [2.99985876]
--> CD_alpha [[0.00014123]]
At iterate 1 f= 8.03593D-03 |proj g|= 1.41231D-04
--> Alpha [-1.95868784]
--> CD [0.00791991]
--> Alpha [-1.95868784]
--> CD_alpha [[-8.82295429e-05]]
At iterate 2 f= 7.91991D-03 |proj g|= 8.82295D-05
--> Alpha [-0.05208413]
--> CD [0.00783466]
--> Alpha [-0.05208413]
--> CD_alpha [[-2.58049269e-06]]
At iterate 3 f= 7.83466D-03 |proj g|= 2.58049D-06
--> Alpha [0.00535932]
--> CD [0.0078346]
--> Alpha [0.00535932]
--> CD_alpha [[1.70395921e-08]]
At iterate 4 f= 7.83460D-03 |proj g|= 1.70396D-08
--> Alpha [0.00498249]
--> CD [0.0078346]
--> Alpha [0.00498249]
--> CD_alpha [[-2.03053106e-09]]
At iterate 5 f= 7.83460D-03 |proj g|= 2.03053D-09
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
1 5 6 5 0 0 2.031D-09 7.835D-03
F = 7.8346002301430146E-003
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
--> Optimized value: [0.00498249]
real 0m33.433s
user 0m20.255s
sys 0m1.817s
+ status=0
+ set +x
=================================================
data/session04/3_mses_OpenMDAO_CD_Alpha.py passed (as expected)
=================================================
=================================================
4_mses_DerivPlot_CD_camber.py test;
+ python 4_mses_DerivPlot_CD_camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
--> camber -0.1
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - camber
Done getting CFD design variables
--> camber -0.08571428571428572
--> camber -0.07142857142857142
--> camber -0.05714285714285715
--> camber -0.04285714285714286
--> camber -0.028571428571428567
--> camber -0.01428571428571429
--> camber 0.0
--> camber 0.01428571428571429
--> camber 0.02857142857142858
--> camber 0.04285714285714287
--> camber 0.05714285714285716
--> camber 0.07142857142857142
--> camber 0.08571428571428572
--> camber 0.1
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/4_mses_DerivPlot_CD_camber.py:80: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown
plt.show()
real 0m55.100s
user 0m48.747s
sys 0m3.051s
+ status=0
+ set +x
=================================================
data/session04/4_mses_DerivPlot_CD_camber.py passed (as expected)
=================================================
=================================================
5_mses_OpenMDAO_CD_camber.py test;
+ python 5_mses_OpenMDAO_CD_camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[macys-VM:47344] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/2722234368/sm_segment.macys-VM.502.a2420000.0 could be created.
==> Starting Optimization...
--> camber [0.1]
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - camber
Done getting CFD design variables
--> CD [0.01370217]
--> camber [0.1]
--> CD [0.01370217]
--> camber [0.1]
--> CD_camber [[0.17593484]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 1 M = 10
At X0 1 variables are exactly at the bounds
At iterate 0 f= 1.37022D-02 |proj g|= 1.75935D-01
--> camber [-0.07593484]
--> CD [0.01053685]
--> camber [-0.07593484]
--> CD_camber [[-0.07712955]]
At iterate 1 f= 1.05368D-02 |proj g|= 7.71296D-02
--> camber [-0.02231302]
--> CD [0.00803517]
--> camber [-0.02231302]
--> CD_camber [[-0.01711041]]
At iterate 2 f= 8.03517D-03 |proj g|= 1.71104D-02
--> camber [-0.00702637]
--> CD [0.00785371]
--> camber [-0.00702637]
--> CD_camber [[-0.00523687]]
At iterate 3 f= 7.85371D-03 |proj g|= 5.23687D-03
--> camber [-0.00028414]
--> CD [0.00783469]
--> camber [-0.00028414]
--> CD_camber [[-0.00015021]]
At iterate 4 f= 7.83469D-03 |proj g|= 1.50214D-04
--> camber [-8.50372178e-05]
--> CD [0.00783469]
--> camber [-8.50372178e-05]
--> CD_camber [[-1.22615302e-06]]
At iterate 5 f= 7.83469D-03 |proj g|= 1.22615D-06
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
1 5 6 5 0 0 1.226D-06 7.835D-03
F = 7.8346852164040588E-003
CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL
Optimization Complete
-----------------------------------
--> Optimized value: [-8.50372178e-05]
real 0m25.781s
user 0m21.265s
sys 0m1.822s
+ status=0
+ set +x
=================================================
data/session04/5_mses_OpenMDAO_CD_camber.py passed (as expected)
=================================================
=================================================
6_mses_DerivPlot_CL2_camber.py test;
+ python 6_mses_DerivPlot_CL2_camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "naca.csm"...
--> camber -0.1
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - camber
Done getting CFD design variables
--> camber -0.08571428571428572
--> camber -0.07142857142857142
--> camber -0.05714285714285715
--> camber -0.04285714285714286
--> camber -0.028571428571428567
--> camber -0.01428571428571429
--> camber 0.0
--> camber 0.01428571428571429
--> camber 0.02857142857142858
--> camber 0.04285714285714287
--> camber 0.05714285714285716
--> camber 0.07142857142857142
--> camber 0.08571428571428572
--> camber 0.1
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/6_mses_DerivPlot_CL2_camber.py:82: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown
plt.show()
real 0m50.548s
user 0m47.177s
sys 0m2.446s
+ status=0
+ set +x
=================================================
data/session04/6_mses_DerivPlot_CL2_camber.py passed (as expected)
=================================================
=================================================
7_mses_OpenMDAO_CL2_camber.py test;
+ python 7_mses_OpenMDAO_CL2_camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[macys-VM:47516] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/3907649536/sm_segment.macys-VM.502.e8ea0000.0 could be created.
==> Starting Optimization...
--> camber [0.1]
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - camber
Done getting CFD design variables
--> CL2 [1.23491816]
--> camber [0.1]
--> CL2 [1.23491816]
--> camber [0.1]
--> CL2_camber [[14.37226759]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 1 M = 10
At X0 1 variables are exactly at the bounds
At iterate 0 f= 1.23492D+00 |proj g|= 2.00000D-01
--> camber [-0.1]
--> CL2 [1.23490173]
--> camber [-0.1]
--> CL2_camber [[-14.37230183]]
--> camber [9.92558193e-05]
--> CL2 [1.68716435e-06]
--> camber [9.92558193e-05]
--> CL2_camber [[0.03422627]]
At iterate 1 f= 1.68716D-06 |proj g|= 3.42263D-02
--> camber [-0.00013922]
--> CL2 [3.35684832e-06]
--> camber [-0.00013922]
--> CL2_camber [[-0.04827804]]
--> camber [2.46989211e-07]
--> CL2 [1.06678519e-12]
--> camber [2.46989211e-07]
--> CL2_camber [[-2.72158112e-05]]
At iterate 2 f= 1.06679D-12 |proj g|= 2.72158D-05
--> camber [3.2565583e-07]
--> CL2 [1.06525442e-14]
--> camber [3.2565583e-07]
--> CL2_camber [[2.71962989e-06]]
At iterate 3 f= 1.06525D-14 |proj g|= 2.71963D-06
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
1 3 6 3 0 0 2.720D-06 1.065D-14
F = 1.0652544204695267E-014
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
--> Optimized value: [3.2565583e-07]
real 0m24.559s
user 0m20.945s
sys 0m1.929s
+ status=0
+ set +x
=================================================
data/session04/7_mses_OpenMDAO_CL2_camber.py passed (as expected)
=================================================
=================================================
8_mses_OpenMDAO_CDCL.py test;
+ python 8_mses_OpenMDAO_CDCL.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[macys-VM:47573] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/4132700160/sm_segment.macys-VM.502.f6540000.0 could be created.
==> Starting Optimization...
--> Alpha [0.]
--> camber [0.1]
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - camber
Done getting CFD design variables
--> CD [0.01370217]
--> CL [1.11126872]
--> Alpha [0.]
--> camber [0.1]
--> CD [0.01370217]
--> CL [1.11126872]
--> Alpha [0.]
--> camber [0.1]
--> CD_Alpha [[0.00105841]]
--> CL_Alpha [[0.09897644]]
--> CD_camber [[0.17593484]]
--> CL_camber [[6.46660315]]
--> Alpha [0.00077914]
--> camber [0.04412123]
--> CD [0.00864297]
--> CL [0.57037493]
--> Alpha [0.00077914]
--> camber [0.04412123]
--> CD_Alpha [[0.00023874]]
--> CL_Alpha [[0.12984116]]
--> CD_camber [[0.03642554]]
--> CL_camber [[12.53395276]]
--> Alpha [0.00103084]
--> camber [0.0584497]
--> CD [0.00930221]
--> CL [0.74439506]
--> Alpha [0.00103084]
--> camber [0.0584497]
--> CD_Alpha [[0.00033987]]
--> CL_Alpha [[0.12673085]]
--> CD_camber [[0.05177185]]
--> CL_camber [[11.83400798]]
--> Alpha [0.00125705]
--> camber [0.05892091]
--> CD [0.00932812]
--> CL [0.74994585]
Optimization terminated successfully (Exit mode 0)
Current function value: 0.009328118059401761
Iterations: 3
Function evaluations: 4
Gradient evaluations: 3
Optimization Complete
-----------------------------------
--> Optimized value: [0.05892091]
real 0m18.887s
user 0m15.463s
sys 0m1.441s
+ status=0
+ set +x
=================================================
data/session04/8_mses_OpenMDAO_CDCL.py passed (as expected)
=================================================
=================================================
9_masstran_OpenMDAO_thick.py test;
+ python 9_masstran_OpenMDAO_thick.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[macys-VM:47618] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/2159083520/sm_segment.macys-VM.502.80b10000.0 could be created.
==> Starting Optimization...
/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages/openmdao/core/driver.py:619: DriverWarning:The following design variable initial conditions are out of their specified bounds:
masstranSystem.x2
val: [0.]
lower: 0.01
upper: 10.0
Set the initial value of the design variable to a valid value or set the driver option['invalid_desvar_behavior'] to 'ignore'.
--> x1 [0.1]
--> x2 [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 = 4
Name = wing, index = 1
Name = htail, index = 2
Name = vtail, index = 3
Name = fuse, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 8672
Combined Number of elements = 8664
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 8664
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 4
Property name - fuse
Property name - htail
Property name - vtail
Property name - wing
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [2.75695334]
--> x1 [0.1]
--> x2 [0.01]
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/9_masstran_OpenMDAO_thick.py:52: DeprecationWarning: Conversion of an array with ndim > 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.)
"x1": {"initialValue":float(inputs['x1'])},
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/9_masstran_OpenMDAO_thick.py:53: DeprecationWarning: Conversion of an array with ndim > 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.)
"x2": {"initialValue":float(inputs['x2'])},
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [2.70119648]
--> x1 [0.1]
--> x2 [0.01]
--> dCGx_x1 [[-68.82272937]]
--> dCGx_x2 [[-5.53091882]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 2 M = 10
At X0 1 variables are exactly at the bounds
At iterate 0 f= 2.70120D+00 |proj g|= 9.90000D+00
--> x1 [10.]
--> x2 [5.54091882]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [10.16370853]
--> x1 [10.]
--> x2 [5.54091882]
--> dCGx_x1 [[0.04843981]]
--> dCGx_x2 [[0.03754845]]
--> x1 [3.33378327]
--> x2 [1.81664573]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [8.85443326]
--> x1 [3.33378327]
--> x2 [1.81664573]
--> dCGx_x1 [[0.48418692]]
--> dCGx_x2 [[0.1268106]]
--> x1 [1.12760341]
--> x2 [0.5841001]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [5.7972651]
--> x1 [1.12760341]
--> x2 [0.5841001]
--> dCGx_x1 [[3.182136]]
--> dCGx_x2 [[0.42790152]]
--> x1 [0.42334159]
--> x2 [0.19064405]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [1.60230885]
--> x1 [0.42334159]
--> x2 [0.19064405]
--> dCGx_x1 [[8.88674345]]
--> dCGx_x2 [[0.86253194]]
At iterate 1 f= 1.60231D+00 |proj g|= 4.13342D-01
--> x1 [0.38612876]
--> x2 [0.16914154]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [1.24954556]
--> x1 [0.38612876]
--> x2 [0.16914154]
--> dCGx_x1 [[9.04121089]]
--> dCGx_x2 [[0.8599867]]
--> x1 [0.23727742]
--> x2 [0.08313149]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [0.04927766]
--> x1 [0.23727742]
--> x2 [0.08313149]
--> dCGx_x1 [[3.58807069]]
--> dCGx_x2 [[0.31359947]]
At iterate 2 f= 4.92777D-02 |proj g|= 2.27277D-01
--> x1 [0.11213433]
--> x2 [0.01347811]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [1.95060563]
--> x1 [0.11213433]
--> x2 [0.01347811]
--> dCGx_x1 [[-52.76118222]]
--> dCGx_x2 [[-4.27221829]]
--> x1 [0.21361795]
--> x2 [0.06996287]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [5.61440048e-05]
--> x1 [0.21361795]
--> x2 [0.06996287]
--> dCGx_x1 [[0.13868009]]
--> dCGx_x2 [[0.01195172]]
At iterate 3 f= 5.61440D-05 |proj g|= 1.38680D-01
--> x1 [0.21266725]
--> x2 [0.06943529]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [3.06804662e-06]
--> x1 [0.21266725]
--> x2 [0.06943529]
--> dCGx_x1 [[-0.03260179]]
--> dCGx_x2 [[-0.00280809]]
At iterate 4 f= 3.06805D-06 |proj g|= 3.26018D-02
--> x1 [0.2128482]
--> x2 [0.0695357]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [1.43517333e-10]
--> x1 [0.2128482]
--> x2 [0.0695357]
--> dCGx_x1 [[0.00022274]]
--> dCGx_x2 [[1.91872562e-05]]
At iterate 5 f= 1.43517D-10 |proj g|= 2.22739D-04
--> x1 [0.21284697]
--> x2 [0.06953502]
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - x1
Design_Variable name - x2
Design_Variable_Relation name - fuseRel
Design_Variable_Relation name - wingRel
Number of design variable relations - 2
Done getting FEA design variables
--> dCGx [3.63550505e-16]
--> x1 [0.21284697]
--> x2 [0.06953502]
--> dCGx_x1 [[3.54510824e-07]]
--> dCGx_x2 [[3.05383747e-08]]
At iterate 6 f= 3.63551D-16 |proj g|= 3.54511D-07
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
2 6 12 7 0 0 3.545D-07 3.636D-16
F = 3.6355050512987024E-016
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
==> Optimized value:
--> x1 [0.21284697]
--> x2 [0.06953502]
real 0m5.831s
user 0m3.262s
sys 0m1.686s
+ status=0
+ set +x
=================================================
data/session04/9_masstran_OpenMDAO_thick.py passed (as expected)
=================================================
=================================================
masstran_OpenMDAO_geom.py test;
+ python masstran_OpenMDAO_geom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[macys-VM:47664] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/129499136/sm_segment.macys-VM.502.7b80000.0 could be created.
==> Initial values:
htail:lh 5.0
wing:xroot 4.0
==> Starting Optimization...
--> htail:lh [5.]
--> wing:xroot [4.]
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wing, index = 1
Name = htail, index = 2
Name = vtail, index = 3
Name = fuse, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 8672
Combined Number of elements = 8664
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 8664
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 4
Property name - fuse
Property name - htail
Property name - vtail
Property name - wing
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - htail:lh
Design_Variable name - wing:xroot
Number of design variable relations - 0
Done getting FEA design variables
--> dCGx [2.10539929]
--> htail:lh [5.]
--> wing:xroot [4.]
--> dCGx [2.10539929]
--> htail:lh [5.]
--> wing:xroot [4.]
--> dCGx_htail:lh [[-0.40374365]]
--> dCGx_wing:xroot [[-1.15229479]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 2 M = 10
At X0 0 variables are exactly at the bounds
At iterate 0 f= 2.10540D+00 |proj g|= 1.15229D+00
--> htail:lh [5.40374365]
--> wing:xroot [5.15229479]
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wing, index = 1
Name = htail, index = 2
Name = vtail, index = 3
Name = fuse, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 8672
Combined Number of elements = 8664
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - htail:lh
Design_Variable name - wing:xroot
Number of design variable relations - 0
Done getting FEA design variables
--> dCGx [0.86918465]
--> htail:lh [5.40374365]
--> wing:xroot [5.15229479]
--> dCGx_htail:lh [[-0.30002756]]
--> dCGx_wing:xroot [[-0.74124931]]
At iterate 1 f= 8.69185D-01 |proj g|= 7.41249D-01
--> htail:lh [6.474753]
--> wing:xroot [7.25471671]
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wing, index = 1
Name = htail, index = 2
Name = vtail, index = 3
Name = fuse, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 8672
Combined Number of elements = 8664
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - htail:lh
Design_Variable name - wing:xroot
Number of design variable relations - 0
Done getting FEA design variables
--> dCGx [0.00905292]
--> htail:lh [6.474753]
--> wing:xroot [7.25471671]
--> dCGx_htail:lh [[0.03711399]]
--> dCGx_wing:xroot [[0.07531706]]
At iterate 2 f= 9.05292D-03 |proj g|= 7.53171D-02
--> htail:lh [6.35917671]
--> wing:xroot [7.05983716]
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wing, index = 1
Name = htail, index = 2
Name = vtail, index = 3
Name = fuse, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 8672
Combined Number of elements = 8664
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - htail:lh
Design_Variable name - wing:xroot
Number of design variable relations - 0
Done getting FEA design variables
--> dCGx [1.94377289e-05]
--> htail:lh [6.35917671]
--> wing:xroot [7.05983716]
--> dCGx_htail:lh [[-0.00169617]]
--> dCGx_wing:xroot [[-0.00349307]]
At iterate 3 f= 1.94377D-05 |proj g|= 3.49307D-03
--> htail:lh [6.3642348]
--> wing:xroot [7.06847132]
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wing, index = 1
Name = htail, index = 2
Name = vtail, index = 3
Name = fuse, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 8672
Combined Number of elements = 8664
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - htail:lh
Design_Variable name - wing:xroot
Number of design variable relations - 0
Done getting FEA design variables
--> dCGx [2.31615861e-10]
--> htail:lh [6.3642348]
--> wing:xroot [7.06847132]
--> dCGx_htail:lh [[-5.85873617e-06]]
--> dCGx_wing:xroot [[-1.20573655e-05]]
At iterate 4 f= 2.31616D-10 |proj g|= 1.20574D-05
--> htail:lh [6.36425233]
--> wing:xroot [7.06850123]
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wing, index = 1
Name = htail, index = 2
Name = vtail, index = 3
Name = fuse, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 8672
Combined Number of elements = 8664
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - htail:lh
Design_Variable name - wing:xroot
Number of design variable relations - 0
Done getting FEA design variables
--> dCGx [6.3756283e-18]
--> htail:lh [6.36425233]
--> wing:xroot [7.06850123]
--> dCGx_htail:lh [[9.72035735e-10]]
--> dCGx_wing:xroot [[2.00045928e-09]]
At iterate 5 f= 6.37563D-18 |proj g|= 2.00046D-09
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
2 5 6 5 0 0 2.000D-09 6.376D-18
F = 6.3756282976940919E-018
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
==> Optimized values:
--> htail:lh 6.364252334270465
--> wing:xroot 7.06850122864588
real 0m4.442s
user 0m3.350s
sys 0m1.168s
+ status=0
+ set +x
=================================================
solutions/session04/masstran_OpenMDAO_geom.py passed (as expected)
=================================================
=================================================
+ echo 'avlPlaneVanilla.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
avlPlaneVanilla.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 avlPlaneVanilla.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/avlPlaneVanilla.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.410s
user 0m0.326s
sys 0m0.032s
+ status=0
+ set +x
=================================================
data/session06/avlPlaneVanilla passed (as expected)
=================================================
=================================================
1_avl_PlaneVanilla.py test;
+ python 1_avl_PlaneVanilla.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "avlPlaneVanilla.csm"...
==> Viewing Plane Vanilla bodies...
==> Create avlAIM
==> Viewing AVL Plane Vanilla bodies...
==> Setting analysis values
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing, index = 1
Name = Htail, index = 2
Name = Vtail, index = 3
Getting vortex lattice surface data
VLM surface name - Htail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vtail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
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.
Warning: Control AileronRight not found in controls tuple! Only defaults will be used.
Warning: Control AileronLeft not found in controls tuple! Only defaults will be used.
Warning: Control AileronRight not found in controls tuple! Only defaults will be used.
Warning: Control AileronLeft not found in controls tuple! Only defaults will be used.
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 1)
Control surface 1 of 1
Section 2 of 3 (ID = 0)
Control surface 1 of 1
Section 3 of 3 (ID = 2)
Control surface 1 of 1
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Control surface 1 of 1
Section 2 of 2 (ID = 0)
Control surface 1 of 1
Writing surface - Wing (ID = 2)
Section 1 of 3 (ID = 1)
Control surface 1 of 1
Section 2 of 3 (ID = 0)
Control surface 1 of 2
Control surface 2 of 2
Section 3 of 3 (ID = 2)
Control surface 1 of 1
--> CLtot = 0.5813612009207021
--> CDtot = 0.006414738598480186
--> CDind = 0.006414738598480186
--> e = 0.9155417145048191
real 0m2.313s
user 0m1.330s
sys 0m0.908s
+ status=0
+ set +x
=================================================
data/session06/1_avl_PlaneVanilla.py passed (as expected)
=================================================
=================================================
2_avl_PlaneVanillaControl.py test;
+ python 2_avl_PlaneVanillaControl.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "avlPlaneVanilla.csm"...
==> Creating avlAIM
==> Setting analysis values
==> Some stability derivatives (old)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing, index = 1
Name = Htail, index = 2
Name = Vtail, index = 3
Getting vortex lattice control surface data
VLM control surface name - AileronLeft
VLM control surface name - AileronRight
VLM control surface name - Elevator
VLM control surface name - Rudder
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Htail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vtail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 1)
Control surface 1 of 1
Section 2 of 3 (ID = 0)
Control surface 1 of 1
Section 3 of 3 (ID = 2)
Control surface 1 of 1
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Control surface 1 of 1
Section 2 of 2 (ID = 0)
Control surface 1 of 1
Writing surface - Wing (ID = 2)
Section 1 of 3 (ID = 1)
Control surface 1 of 1
Section 2 of 3 (ID = 0)
Control surface 1 of 2
Control surface 2 of 2
Section 3 of 3 (ID = 2)
Control surface 1 of 1
--> CLa = 6.186807004016531
--> CLb = 0.06076552936219984
--> CLp' = 0.07726884267630249
--> CLq' = 11.77186898082121
--> CLr' = 0.9883703770411724
--> dCL/dAileronRight = 0.02247452142342
--> dCL/dAileronLeft = 0.0225246749619
--> dCL/dElevator = 0.005432144424888
--> dCL/dRudder = -2.654019499439e-06
==> Some stability derivatives (new)
--> dCL/dAlpha = 6.186807004016531
--> dCL/dBeta = 0.06076552936219984
--> dCL/dp' = 0.07726884267630249
--> dCL/dq' = 11.77186898082121
--> dCL/dr' = 0.9883703770411724
--> dCL/dAileronRight = 0.02247452142342404
--> dCL/dAileronLeft = 0.02252467496190029
--> dCL/dElevator = 0.005432144424888405
--> dCL/dRudder = -2.654019499439076e-06
real 0m2.133s
user 0m1.295s
sys 0m0.911s
+ status=0
+ set +x
=================================================
data/session06/2_avl_PlaneVanillaControl.py passed (as expected)
=================================================
=================================================
3_avl_TransportGeom.py test;
+ python 3_avl_TransportGeom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Viewing transport bodies...
MESSAGE:: Building wingOml
MESSAGE:: Building wingHinges
MESSAGE:: Building htailOml
MESSAGE:: Building htailHinges
MESSAGE:: Building vtailOml
MESSAGE:: Building vtailHinges
==> Create AVL aim...
==> Viewing avl bodies...
real 0m19.885s
user 0m21.657s
sys 0m8.218s
+ status=0
+ set +x
=================================================
data/session06/3_avl_TransportGeom.py passed (as expected)
=================================================
=================================================
4_avl_TransportControl.py test;
+ python 4_avl_TransportControl.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Setting Build Variables and Geometry Values...
==> Creating AVL aim...
MESSAGE:: Building wingOml
MESSAGE:: Building wingHinges
MESSAGE:: Building htailOml
MESSAGE:: Building htailHinges
MESSAGE:: Building vtailOml
MESSAGE:: Building vtailHinges
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing, index = 1
Name = Htail, index = 2
Name = Vtail, index = 3
Getting vortex lattice control surface data
VLM control surface name - HtailControl_1
VLM control surface name - VtailControl_1
VLM control surface name - WingControl_1
VLM control surface name - WingControl_2
VLM control surface name - WingControl_3
VLM control surface name - WingControl_4
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Htail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vtail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control VtailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control VtailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl4 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl4 not found in controls tuple! Only defaults will be used.
Writing surface - Htail (ID = 0)
Section 1 of 7 (ID = 0)
Section 2 of 7 (ID = 3)
Control surface 1 of 1
Section 3 of 7 (ID = 4)
Control surface 1 of 1
Section 4 of 7 (ID = 1)
Section 5 of 7 (ID = 5)
Control surface 1 of 1
Section 6 of 7 (ID = 6)
Control surface 1 of 1
Section 7 of 7 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 4 (ID = 1)
Section 2 of 4 (ID = 3)
Control surface 1 of 1
Section 3 of 4 (ID = 2)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 17 (ID = 0)
Section 2 of 17 (ID = 5)
Control surface 1 of 1
Section 3 of 17 (ID = 6)
Control surface 1 of 1
Section 4 of 17 (ID = 7)
Control surface 1 of 1
Section 5 of 17 (ID = 8)
Control surface 1 of 1
Section 6 of 17 (ID = 4)
Section 7 of 17 (ID = 9)
Control surface 1 of 1
Section 8 of 17 (ID = 10)
Control surface 1 of 1
Section 9 of 17 (ID = 1)
Section 10 of 17 (ID = 11)
Control surface 1 of 1
Section 11 of 17 (ID = 12)
Control surface 1 of 1
Section 12 of 17 (ID = 3)
Section 13 of 17 (ID = 13)
Control surface 1 of 1
Section 14 of 17 (ID = 14)
Control surface 1 of 1
Section 15 of 17 (ID = 15)
Control surface 1 of 1
Section 16 of 17 (ID = 16)
Control surface 1 of 1
Section 17 of 17 (ID = 2)
==> Some stability derivatives
--> CLa = 5.329631112234144
--> CLb = 1.651864185398326e-09
--> CLp' = -4.001376233674891e-10
--> CLq' = 28.72846790224948
--> CLr' = -2.767805233677674e-09
--> Xcg = 55.4263
--> Xnp = 91.29113415652209
--> StaticMargin = 1.6523694366308268
--> htailControl1 {'CLtot': 0.008154370285814, 'CYtot': 9.075194510381e-11, "Cl'tot": 4.489035946149e-12, 'Cmtot': -0.03748884222584, "Cn'tot": -5.410997993488e-11, 'CDff': 0.001133243689262, 'e': -0.003225847672438}
--> VtailControl1 {'CLtot': -3.031950282476e-11, 'CYtot': 0.001746902748416, "Cl'tot": 0.0001578887965311, 'Cmtot': 1.479167618946e-10, "Cn'tot": -0.0009155267170673, 'CDff': 3.05051259299e-13, 'e': -4.238167293539e-12}
--> WingControl1 {'CLtot': 0.002454272406152, 'CYtot': 0.0001047561437285, "Cl'tot": 0.0008699288714632, 'Cmtot': -0.006084028398663, "Cn'tot": 0.0001105826995691, 'CDff': 4.762256182255e-05, 'e': 0.002671723839937}
--> WingControl2 {'CLtot': 0.008875217411974, 'CYtot': 6.234219060462e-12, "Cl'tot": 8.928483522817e-14, 'Cmtot': -0.01681584091322, "Cn'tot": -3.519260150842e-12, 'CDff': 0.000369541483347, 'e': 0.007231131090133}
--> WingControl3 {'CLtot': 0.005956182097902, 'CYtot': -1.9932307583e-11, "Cl'tot": -5.706407696973e-13, 'Cmtot': -0.005500424200486, "Cn'tot": 1.166099661329e-11, 'CDff': 0.0007054644635254, 'e': -0.0007874262943396}
--> WingControl4 {'CLtot': 0.002454272405997, 'CYtot': -0.0001047561404806, "Cl'tot": -0.0008699288714121, 'Cmtot': -0.00608402839677, "Cn'tot": -0.0001105827014567, 'CDff': 4.762256175753e-05, 'e': 0.002671723841347}
real 0m22.875s
user 0m22.396s
sys 0m7.930s
+ status=0
+ set +x
=================================================
data/session06/4_avl_TransportControl.py passed (as expected)
=================================================
=================================================
5_avl_TransportEigen.py test;
+ python 5_avl_TransportEigen.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Setting Build Variables and Geometry Values...
==> Create AVL aim...
==> Running Analysis
MESSAGE:: Building wingOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing, index = 1
Name = Htail, index = 2
Name = Vtail, index = 3
Getting vortex lattice surface data
VLM surface name - Htail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vtail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
==> Outputs
--> Xcg = 89.3122 meter
--> Xnp = 92.43912770212773 meter
--> StaticMargin = 0.47265167768451544
--> EigenValues {'case 1': [[-3.1240286, 0.0], [0.01975706, 0.97330897], [0.01975706, -0.97330897], [-0.013027091, 0.0], [-0.32616585, 0.92439209], [-0.32616585, -0.92439209], [-0.013243773, 0.13183873], [-0.013243773, -0.13183873]]}
--> Real Eigen Values = [-3.1240286, 0.01975706, 0.01975706, -0.013027091, -0.32616585, -0.32616585, -0.013243773, -0.013243773]
real 0m8.274s
user 0m5.994s
sys 0m3.225s
+ status=0
+ set +x
=================================================
data/session06/5_avl_TransportEigen.py passed (as expected)
=================================================
=================================================
6_avl_masstran_Geom.py test;
+ python 6_avl_masstran_Geom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Vewing AVL geometry
MESSAGE:: Building wingOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
MESSAGE:: Building fuseOml
==> Vewing Masstran geometry
real 0m7.165s
user 0m5.303s
sys 0m3.715s
+ status=0
+ set +x
=================================================
data/session06/6_avl_masstran_Geom.py passed (as expected)
=================================================
=================================================
7_avl_masstran_Eigen.py test;
+ python 7_avl_masstran_Eigen.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Setting Build Variables and Geometry Values...
==> Creating masstran aim...
==> Creating AVL aim...
==> Running Analysis
MESSAGE:: Building wingOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
MESSAGE:: Building fuseOml
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wingSkin, index = 1
Name = fuseSkin, index = 2
Name = htailSkin, index = 3
Name = vtailSkin, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 5622
Number of elements = 11240
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 11240
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 5460
Number of elements = 10916
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 10916
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 4599
Number of elements = 9194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 9194
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2722
Number of elements = 5440
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5440
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 18403
Combined Number of elements = 36790
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 36790
Combined Elemental Quad4 = 0
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 - 4
Property name - fuseSkin
Property name - htailSkin
Property name - vtailSkin
Property name - wingSkin
Done getting FEA properties
Updating mesh element types based on properties input
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing, index = 1
Name = Htail, index = 2
Name = Vtail, index = 3
Getting vortex lattice surface data
VLM surface name - Htail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vtail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
==> Outputs
--> Xcg = 89.6946 meter
--> Xnp = 92.4242670979591 meter
--> StaticMargin = 0.41260363406953277
--> EigenValues {'case 1': [[-0.70465113, 0.0], [0.13846754, 0.5514659], [0.13846754, -0.5514659], [-0.1614276, 0.51358138], [-0.1614276, -0.51358138], [-0.0068180511, 0.0], [-0.016473647, 0.12085977], [-0.016473647, -0.12085977]]}
--> Real Eigen Values = [-0.70465113, 0.13846754, 0.13846754, -0.1614276, -0.1614276, -0.0068180511, -0.016473647, -0.016473647]
real 0m10.984s
user 0m9.319s
sys 0m4.071s
+ status=0
+ set +x
=================================================
data/session06/7_avl_masstran_Eigen.py passed (as expected)
=================================================
=================================================
8_avl_friction_Link.py test;
+ python 8_avl_friction_Link.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
MESSAGE:: Building wingOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
Lifting Surface: Body = 1, units ft
XLE: 118.390617 -97.671924 3.992604
XTE: 123.551941 -97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 2, units ft
XLE: 50.000000 0.000000 -8.000000
XTE: 97.200785 -0.000000 -7.176107
Chord: 47.207975
Arc: 97.395848
T/C: 0.145499
Type: Wing
Lifting Surface: Body = 3, units ft
XLE: 118.390617 97.671924 3.992604
XTE: 123.551941 97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 4, units ft
XLE: 75.304787 36.138982 -3.562691
XTE: 97.933561 36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 5, units ft
XLE: 75.304787 -36.138982 -3.562691
XTE: 97.933561 -36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 6, units ft
XLE: 165.023151 -35.780198 13.605316
XTE: 173.282263 -35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
XLE: 135.000000 0.000000 6.000000
XTE: 160.026192 -0.000000 6.000000
Chord: 25.026192
Arc: 50.556450
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
XLE: 165.023151 35.780198 13.605316
XTE: 173.282263 35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
XLE: 136.456162 0.000000 9.001500
XTE: 159.447890 -0.000000 9.001500
Chord: 22.991728
Arc: 46.446544
T/C: 0.080010
Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
XLE: 162.940713 0.000000 35.486051
XTE: 169.379597 -0.000000 35.486051
Chord: 6.438884
Arc: 13.007456
T/C: 0.080010
Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing, index = 1
Name = Htail, index = 2
Name = Vtail, index = 3
Getting vortex lattice surface data
VLM surface name - Htail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vtail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
XLE: 118.390617 -97.671924 3.992604
XTE: 123.551941 -97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 2, units ft
XLE: 50.000000 0.000000 -8.000000
XTE: 97.200785 -0.000000 -7.176107
Chord: 47.207975
Arc: 97.395848
T/C: 0.145499
Type: Wing
Lifting Surface: Body = 3, units ft
XLE: 118.390617 97.671924 3.992604
XTE: 123.551941 97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 4, units ft
XLE: 75.304787 36.138982 -3.562691
XTE: 97.933561 36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 5, units ft
XLE: 75.304787 -36.138982 -3.562691
XTE: 97.933561 -36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 6, units ft
XLE: 165.023151 -35.780198 13.605316
XTE: 173.282263 -35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
XLE: 135.000000 0.000000 6.000000
XTE: 160.026192 -0.000000 6.000000
Chord: 25.026192
Arc: 50.556450
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
XLE: 165.023151 35.780198 13.605316
XTE: 173.282263 35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
XLE: 136.456162 0.000000 9.001500
XTE: 159.447890 -0.000000 9.001500
Chord: 22.991728
Arc: 46.446544
T/C: 0.080010
Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
XLE: 162.940713 0.000000 35.486051
XTE: 169.379597 -0.000000 35.486051
Chord: 6.438884
Arc: 13.007456
T/C: 0.080010
Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
XLE: 118.390617 -97.671924 3.992604
XTE: 123.551941 -97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 2, units ft
XLE: 50.000000 0.000000 -8.000000
XTE: 97.200785 -0.000000 -7.176107
Chord: 47.207975
Arc: 97.395848
T/C: 0.145499
Type: Wing
Lifting Surface: Body = 3, units ft
XLE: 118.390617 97.671924 3.992604
XTE: 123.551941 97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 4, units ft
XLE: 75.304787 36.138982 -3.562691
XTE: 97.933561 36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 5, units ft
XLE: 75.304787 -36.138982 -3.562691
XTE: 97.933561 -36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 6, units ft
XLE: 165.023151 -35.780198 13.605316
XTE: 173.282263 -35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
XLE: 135.000000 0.000000 6.000000
XTE: 160.026192 -0.000000 6.000000
Chord: 25.026192
Arc: 50.556450
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
XLE: 165.023151 35.780198 13.605316
XTE: 173.282263 35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
XLE: 136.456162 0.000000 9.001500
XTE: 159.447890 -0.000000 9.001500
Chord: 22.991728
Arc: 46.446544
T/C: 0.080010
Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
XLE: 162.940713 0.000000 35.486051
XTE: 169.379597 -0.000000 35.486051
Chord: 6.438884
Arc: 13.007456
T/C: 0.080010
Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
XLE: 118.390617 -97.671924 3.992604
XTE: 123.551941 -97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 2, units ft
XLE: 50.000000 0.000000 -8.000000
XTE: 97.200785 -0.000000 -7.176107
Chord: 47.207975
Arc: 97.395848
T/C: 0.145499
Type: Wing
Lifting Surface: Body = 3, units ft
XLE: 118.390617 97.671924 3.992604
XTE: 123.551941 97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 4, units ft
XLE: 75.304787 36.138982 -3.562691
XTE: 97.933561 36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 5, units ft
XLE: 75.304787 -36.138982 -3.562691
XTE: 97.933561 -36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 6, units ft
XLE: 165.023151 -35.780198 13.605316
XTE: 173.282263 -35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
XLE: 135.000000 0.000000 6.000000
XTE: 160.026192 -0.000000 6.000000
Chord: 25.026192
Arc: 50.556450
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
XLE: 165.023151 35.780198 13.605316
XTE: 173.282263 35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
XLE: 136.456162 0.000000 9.001500
XTE: 159.447890 -0.000000 9.001500
Chord: 22.991728
Arc: 46.446544
T/C: 0.080010
Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
XLE: 162.940713 0.000000 35.486051
XTE: 169.379597 -0.000000 35.486051
Chord: 6.438884
Arc: 13.007456
T/C: 0.080010
Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
XLE: 118.390617 -97.671924 3.992604
XTE: 123.551941 -97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 2, units ft
XLE: 50.000000 0.000000 -8.000000
XTE: 97.200785 -0.000000 -7.176107
Chord: 47.207975
Arc: 97.395848
T/C: 0.145499
Type: Wing
Lifting Surface: Body = 3, units ft
XLE: 118.390617 97.671924 3.992604
XTE: 123.551941 97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 4, units ft
XLE: 75.304787 36.138982 -3.562691
XTE: 97.933561 36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 5, units ft
XLE: 75.304787 -36.138982 -3.562691
XTE: 97.933561 -36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 6, units ft
XLE: 165.023151 -35.780198 13.605316
XTE: 173.282263 -35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
XLE: 135.000000 0.000000 6.000000
XTE: 160.026192 -0.000000 6.000000
Chord: 25.026192
Arc: 50.556450
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
XLE: 165.023151 35.780198 13.605316
XTE: 173.282263 35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
XLE: 136.456162 0.000000 9.001500
XTE: 159.447890 -0.000000 9.001500
Chord: 22.991728
Arc: 46.446544
T/C: 0.080010
Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
XLE: 162.940713 0.000000 35.486051
XTE: 169.379597 -0.000000 35.486051
Chord: 6.438884
Arc: 13.007456
T/C: 0.080010
Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
XLE: 118.390617 -97.671924 3.992604
XTE: 123.551941 -97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 2, units ft
XLE: 50.000000 0.000000 -8.000000
XTE: 97.200785 -0.000000 -7.176107
Chord: 47.207975
Arc: 97.395848
T/C: 0.145499
Type: Wing
Lifting Surface: Body = 3, units ft
XLE: 118.390617 97.671924 3.992604
XTE: 123.551941 97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 4, units ft
XLE: 75.304787 36.138982 -3.562691
XTE: 97.933561 36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 5, units ft
XLE: 75.304787 -36.138982 -3.562691
XTE: 97.933561 -36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 6, units ft
XLE: 165.023151 -35.780198 13.605316
XTE: 173.282263 -35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
XLE: 135.000000 0.000000 6.000000
XTE: 160.026192 -0.000000 6.000000
Chord: 25.026192
Arc: 50.556450
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
XLE: 165.023151 35.780198 13.605316
XTE: 173.282263 35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
XLE: 136.456162 0.000000 9.001500
XTE: 159.447890 -0.000000 9.001500
Chord: 22.991728
Arc: 46.446544
T/C: 0.080010
Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
XLE: 162.940713 0.000000 35.486051
XTE: 169.379597 -0.000000 35.486051
Chord: 6.438884
Arc: 13.007456
T/C: 0.080010
Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
XLE: 118.390617 -97.671924 3.992604
XTE: 123.551941 -97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 2, units ft
XLE: 50.000000 0.000000 -8.000000
XTE: 97.200785 -0.000000 -7.176107
Chord: 47.207975
Arc: 97.395848
T/C: 0.145499
Type: Wing
Lifting Surface: Body = 3, units ft
XLE: 118.390617 97.671924 3.992604
XTE: 123.551941 97.671924 4.717949
Chord: 5.212043
Arc: 10.531921
T/C: 0.153243
Type: Wing
Lifting Surface: Body = 4, units ft
XLE: 75.304787 36.138982 -3.562691
XTE: 97.933561 36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 5, units ft
XLE: 75.304787 -36.138982 -3.562691
XTE: 97.933561 -36.138982 -2.376767
Chord: 22.659828
Arc: 46.801094
T/C: 0.167991
Type: Wing
Lifting Surface: Body = 6, units ft
XLE: 165.023151 -35.780198 13.605316
XTE: 173.282263 -35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
XLE: 135.000000 0.000000 6.000000
XTE: 160.026192 -0.000000 6.000000
Chord: 25.026192
Arc: 50.556450
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
XLE: 165.023151 35.780198 13.605316
XTE: 173.282263 35.780198 13.605316
Chord: 8.259112
Arc: 16.684575
T/C: 0.080010
Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
XLE: 136.456162 0.000000 9.001500
XTE: 159.447890 -0.000000 9.001500
Chord: 22.991728
Arc: 46.446544
T/C: 0.080010
Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
XLE: 162.940713 0.000000 35.486051
XTE: 169.379597 -0.000000 35.486051
Chord: 6.438884
Arc: 13.007456
T/C: 0.080010
Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
--> Mach = [0.1, 0.2, 0.30000000000000004, 0.4, 0.5, 0.6, 0.7000000000000001]
--> CDp = [0.01592, 0.01416, 0.01323, 0.01259, 0.01209, 0.01167, 0.0113]
--> CD = [0.02455060230115759, 0.02466896359668807, 0.02487666267824443, 0.02519203560974491, 0.02564765944813627, 0.02630249014988715, 0.02727263674182199]
real 0m14.663s
user 0m10.948s
sys 0m5.046s
+ status=0
+ set +x
=================================================
data/session06/8_avl_friction_Link.py passed (as expected)
=================================================
=================================================
avl_masstran_MainGear.py test;
+ python avl_masstran_MainGear.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../../data/ESP/transport.csm"...
==> Setting Build Variables and Geometry Values...
==> Create masstran aim...
==> Computing mass properties...
MESSAGE:: Building wingOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
MESSAGE:: Building fuseOml
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wingSkin, index = 1
Name = fuseSkin, index = 2
Name = htailSkin, index = 3
Name = vtailSkin, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 5622
Number of elements = 11240
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 11240
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 5460
Number of elements = 10916
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 10916
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 4599
Number of elements = 9194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 9194
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2722
Number of elements = 5440
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5440
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 18403
Combined Number of elements = 36790
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 36790
Combined Elemental Quad4 = 0
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 - 4
Property name - fuseSkin
Property name - htailSkin
Property name - vtailSkin
Property name - wingSkin
Done getting FEA properties
Updating mesh element types based on properties input
==> Computed mass properties...
--> aircraft_skin = {'mass': <Quantity 37678.41936443 kg>, 'CG': <Quantity [28.71060165257, 0.0004847831045987, 0.3509074373672] meter>, 'massInertia': <Quantity [3048890.7105, 5626736.457971, 8319844.174801, 317.928029578, 521075.1859613, 50.57897871269] m2.kg>}
==> Creating AVL aim...
==> Outputs
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing, index = 1
Name = Htail, index = 2
Name = Vtail, index = 3
Getting vortex lattice surface data
VLM surface name - Htail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vtail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
--> Xcg = 89.1649 meter
--> Xnp = 92.42451154634462 meter
--> StaticMargin = 0.49270754323205207
--> EigenValues {'case 1': [[-0.70485396, 0.0], [0.13848718, 0.55142164], [0.13848718, -0.55142164], [-0.16432037, 0.56448129], [-0.16432037, -0.56448129], [-0.0068132786, 0.0], [-0.013683554, 0.11022262], [-0.013683554, -0.11022262]]}
--> Real Eigen Values = [-0.70485396, 0.13848718, 0.13848718, -0.16432037, -0.16432037, -0.0068132786, -0.013683554, -0.013683554]
real 0m10.079s
user 0m8.577s
sys 0m3.803s
+ status=0
+ set +x
=================================================
solutions/session06/avl_masstran_MainGear.py passed (as expected)
=================================================
=================================================
avl_masstran_MultiMat.py test;
+ python avl_masstran_MultiMat.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../../data/ESP/transport.csm"...
==> Setting Build Variables and Geometry Values...
==> Create masstran aim...
==> Computing mass properties...
MESSAGE:: Building wingOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
MESSAGE:: Building fuseOml
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wingSkin, index = 1
Name = fuseSkin, index = 2
Name = htailSkin, index = 3
Name = vtailSkin, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 5622
Number of elements = 11240
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 11240
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 5460
Number of elements = 10916
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 10916
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 4599
Number of elements = 9194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 9194
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2722
Number of elements = 5440
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5440
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 18403
Combined Number of elements = 36790
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 36790
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 3
Material name - fuseium
No "materialType" specified for Material tuple fuseium, defaulting to "Isotropic"
Material name - tailium
No "materialType" specified for Material tuple tailium, defaulting to "Isotropic"
Material name - wingium
No "materialType" specified for Material tuple wingium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 4
Property name - fuseSkin
Property name - htailSkin
Property name - vtailSkin
Property name - wingSkin
Done getting FEA properties
Updating mesh element types based on properties input
==> Computed mass properties...
--> aircraft_skin = {'mass': <Quantity 52814.21122638 kg>, 'CG': <Quantity [25.21427105317, 9.440962787871e-05, 0.00714271363998] meter>, 'massInertia': <Quantity [3041321.23867, 6969066.307862, 9624742.735327, 86.35057145667, 262896.8555367, 25.61592046998] m2.kg>}
==> Creating AVL aim...
==> Outputs
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing, index = 1
Name = Htail, index = 2
Name = Vtail, index = 3
Getting vortex lattice surface data
VLM surface name - Htail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Vtail
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
Section 1 of 5 (ID = 0)
Section 2 of 5 (ID = 4)
Section 3 of 5 (ID = 1)
Section 4 of 5 (ID = 3)
Section 5 of 5 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
--> Xcg = 80.225 meter
--> Xnp = 92.49086830506504 meter
--> StaticMargin = 1.8540509359079185
--> EigenValues {'case 1': [[-0.67265796, 0.0], [0.12206579, 0.57566948], [0.12206579, -0.57566948], [-0.15648068, 1.0547055], [-0.15648068, -1.0547055], [-0.0068086676, 0.0], [-0.0003299172, 0.049308002], [-0.0003299172, -0.049308002]]}
--> Real Eigen Values = [-0.67265796, 0.12206579, 0.12206579, -0.15648068, -0.15648068, -0.0068086676, -0.0003299172, -0.0003299172]
real 0m10.419s
user 0m8.614s
sys 0m4.168s
+ status=0
+ set +x
=================================================
solutions/session06/avl_masstran_MultiMat.py passed (as expected)
=================================================
=================================================
masstran_MultiAIM.py test;
+ python masstran_MultiAIM.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../../data/ESP/transport.csm"...
==> Setting Build Variables and Geometry Values...
==> Loading masstran aims...
==> Computing mass properties...
MESSAGE:: Building wingOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
MESSAGE:: Building fuseOml
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = fuseSkin, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 7445
Number of elements = 14886
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 14886
Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - fuseium
No "materialType" specified for Material tuple fuseium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - fuseSkin
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 = 1
Name = wingSkin, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 5622
Number of elements = 11240
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 11240
Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - wingium
No "materialType" specified for Material tuple wingium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - wingSkin
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 = htailSkin, index = 1
Name = vtailSkin, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 3488
Number of elements = 6972
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 6972
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 3480
Number of elements = 6956
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 6956
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6968
Combined Number of elements = 13928
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 13928
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - tailium
No "materialType" specified for Material tuple tailium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - htailSkin
Property name - vtailSkin
Done getting FEA properties
Updating mesh element types based on properties input
==> Computed mass properties...
--> fuse_skin = {'mass': <Quantity 7849.475274166 kg>, 'CG': <Quantity [23.60861887848, -5.594392309454e-05, 0.1631067332576] meter>, 'massInertia': <Quantity [64256.8299145, 1266909.722239, 1265121.586758, -7.997972200572, 26539.85606389, -0.8824247963594] m2.kg>}
--> wing_skin = {'mass': <Quantity 23992.67003648 kg>, 'CG': <Quantity [26.65600801849, 3.49876069442e-05, -0.6718794767923] meter>, 'massInertia': <Quantity [4029452.651317, 529853.8379244, 4523798.230161, -19.40420203263, 69301.12468094, 23.37530324139] m2.kg>}
--> tail_skin = {'mass': <Quantity 748.6464447904 kg>, 'CG': <Quantity [47.57149390357, -1.456429493375e-06, 3.576129105462] meter>, 'massInertia': <Quantity [19383.57137666, 6924.661310063, 21171.65394983, 0.007355715707437, 1134.161304338, 0.004686577707884] m2.kg>}
real 0m7.330s
user 0m4.912s
sys 0m3.139s
+ status=0
+ set +x
=================================================
solutions/session06/masstran_MultiAIM.py passed (as expected)
=================================================
=================================================
masstran_MultiMat.py test;
+ python masstran_MultiMat.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../../data/ESP/transport.csm"...
==> Setting Build Variables and Geometry Values...
==> Loading masstran aim...
==> Computing mass properties...
MESSAGE:: Building wingOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
MESSAGE:: Building fuseOml
Mapping Csys attributes ................
Number of unique Csys attributes = 0
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 = 4
Name = wingSkin, index = 1
Name = fuseSkin, index = 2
Name = htailSkin, index = 3
Name = vtailSkin, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 5622
Number of elements = 11240
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 11240
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 5460
Number of elements = 10916
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 10916
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 4599
Number of elements = 9194
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 9194
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 3
Number of nodal coordinates = 2722
Number of elements = 5440
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5440
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 18403
Combined Number of elements = 36790
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 36790
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 3
Material name - fuseium
No "materialType" specified for Material tuple fuseium, defaulting to "Isotropic"
Material name - tailium
No "materialType" specified for Material tuple tailium, defaulting to "Isotropic"
Material name - wingium
No "materialType" specified for Material tuple wingium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 4
Property name - fuseSkin
Property name - htailSkin
Property name - vtailSkin
Property name - wingSkin
Done getting FEA properties
Updating mesh element types based on properties input
==> Computed mass properties...
--> aircraft_skin = {'mass': <Quantity 71849.22261512026 lb>, 'CG': <Quantity [86.62567835984251, 0.00030731545728628605, -1.2243299067857611] ft>, 'massInertia': <Quantity [97984636.59227683, 52633549.11467294, 147324437.64378545, 650.5842383171774, 3464172.5406802204, 692.2833235513742] lb*ft^2>}
real 0m5.608s
user 0m4.695s
sys 0m1.651s
+ status=0
+ set +x
=================================================
solutions/session06/masstran_MultiMat.py passed (as expected)
=================================================
=================================================
01_aflr4_InviscidWing.py test;
+ python 01_aflr4_InviscidWing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 6
EGADS : 2 Yes 0 0 1 0 1 1 4 5
EGADS : 3 Yes 0 0 1 0 1 1 4 8
EGADS : 4 Yes 0 0 1 0 1 2 3 5
EGADS : 5 Yes 0 0 1 0 1 2 4
EGADS : 6 Yes 0 0 1 0 1 1 7 8
EGADS : 7 Yes 0 0 1 0 1 6 9 10
EGADS : 8 Yes 0 0 1 0 1 3 6 9
EGADS : 9 Yes 0 0 1 0 1 7 8 10
EGADS : 10 Yes 0 0 1 0 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 428.342
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 8732 16959 0
AFLR4 : Nodes, Trias,Quads= 5233 9961 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 18090 35394 0
AFLR4 : Nodes, Trias,Quads= 5568 10350 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 10182 19859 0
AFLR4 : Nodes, Trias,Quads= 4951 9397 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 16338 31891 0
AFLR4 : Nodes, Trias,Quads= 5435 10085 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 45 51 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 8705 16905 0
AFLR4 : Nodes, Trias,Quads= 5312 10119 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 17908 35030 0
AFLR4 : Nodes, Trias,Quads= 5567 10348 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 8823 17141 0
AFLR4 : Nodes, Trias,Quads= 4980 9455 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 16876 32967 0
AFLR4 : Nodes, Trias,Quads= 5357 9929 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 46 53 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 112 186 0
AFLR4 : Nodes, Trias,Quads= 109 180 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 112 186 0
AFLR4 : Nodes, Trias,Quads= 109 180 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 113 188 0
AFLR4 : Nodes, Trias,Quads= 108 178 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 113 188 0
AFLR4 : Nodes, Trias,Quads= 109 180 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 113 188 0
AFLR4 : Nodes, Trias,Quads= 108 178 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 113 188 0
AFLR4 : Nodes, Trias,Quads= 109 180 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 40416 80824 5436
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 40416 80824
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 8498 16494 0
AFLR4 : Nodes, Trias,Quads= 6521 12540 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 14192 27608 0
AFLR4 : Nodes, Trias,Quads= 10030 19284 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 8900 17298 0
AFLR4 : Nodes, Trias,Quads= 6653 12804 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 13499 26224 0
AFLR4 : Nodes, Trias,Quads= 9809 18844 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 59 77 0
AFLR4 : Nodes, Trias,Quads= 49 57 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 8503 16504 0
AFLR4 : Nodes, Trias,Quads= 6543 12584 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 13624 26478 0
AFLR4 : Nodes, Trias,Quads= 9962 19154 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 8761 17020 0
AFLR4 : Nodes, Trias,Quads= 6664 12826 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 13534 26300 0
AFLR4 : Nodes, Trias,Quads= 9962 19156 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 60 79 0
AFLR4 : Nodes, Trias,Quads= 49 57 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 113 188 0
AFLR4 : Nodes, Trias,Quads= 109 180 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 111 184 0
AFLR4 : Nodes, Trias,Quads= 109 180 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 113 188 0
AFLR4 : Nodes, Trias,Quads= 107 176 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 113 188 0
AFLR4 : Nodes, Trias,Quads= 109 180 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 112 186 0
AFLR4 : Nodes, Trias,Quads= 108 178 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 112 186 0
AFLR4 : Nodes, Trias,Quads= 109 180 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 64194 128380 5374
OVERALL : CPU Time = 2.754 seconds
Body 1 (of 2)
Number of nodes = 63655
Number of elements = 127306
Number of triangle elements = 127306
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 539
Number of elements = 1074
Number of triangle elements = 1074
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 64194
Total number of elements = 128380
Total number of triangle elements = 128380
Total number of quadrilateral elements = 0
real 0m7.868s
user 0m5.552s
sys 0m2.082s
+ status=0
+ set +x
=================================================
data/session07/01_aflr4_InviscidWing.py passed (as expected)
=================================================
=================================================
02_aflr4_Farfield.py test;
+ python 02_aflr4_Farfield.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 6
EGADS : 2 Yes 0 0 1 0 1 1 4 5
EGADS : 3 Yes 0 0 1 0 1 1 4 8
EGADS : 4 Yes 0 0 1 0 1 2 3 5
EGADS : 5 Yes 0 0 1 0 1 2 4
EGADS : 6 Yes 0 0 1 0 1 1 7 8
EGADS : 7 Yes 0 0 1 0 1 6 9 10
EGADS : 8 Yes 0 0 1 0 1 3 6 9
EGADS : 9 Yes 0 0 1 0 1 7 8 10
EGADS : 10 Yes 0 0 1 0 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.302
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 8732 16959 0
AFLR4 : Nodes, Trias,Quads= 5233 9961 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 18090 35394 0
AFLR4 : Nodes, Trias,Quads= 5568 10350 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 10182 19859 0
AFLR4 : Nodes, Trias,Quads= 4951 9397 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 16338 31891 0
AFLR4 : Nodes, Trias,Quads= 5435 10085 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 45 51 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 8705 16905 0
AFLR4 : Nodes, Trias,Quads= 5312 10119 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 17908 35030 0
AFLR4 : Nodes, Trias,Quads= 5567 10348 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 8823 17141 0
AFLR4 : Nodes, Trias,Quads= 4980 9455 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 16876 32967 0
AFLR4 : Nodes, Trias,Quads= 5357 9929 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 46 53 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 40196 80384 5388
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 40196 80384
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 8498 16494 0
AFLR4 : Nodes, Trias,Quads= 6521 12540 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 14192 27608 0
AFLR4 : Nodes, Trias,Quads= 10030 19284 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 8900 17298 0
AFLR4 : Nodes, Trias,Quads= 6653 12804 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 13499 26224 0
AFLR4 : Nodes, Trias,Quads= 9809 18844 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 59 77 0
AFLR4 : Nodes, Trias,Quads= 49 57 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 8503 16504 0
AFLR4 : Nodes, Trias,Quads= 6543 12584 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 13624 26478 0
AFLR4 : Nodes, Trias,Quads= 9962 19154 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 8761 17020 0
AFLR4 : Nodes, Trias,Quads= 6664 12826 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 13534 26300 0
AFLR4 : Nodes, Trias,Quads= 9962 19156 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 60 79 0
AFLR4 : Nodes, Trias,Quads= 49 57 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 63975 127942 5326
OVERALL : CPU Time = 2.695 seconds
Body 1 (of 2)
Number of nodes = 63655
Number of elements = 127306
Number of triangle elements = 127306
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 320
Number of elements = 636
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 63975
Total number of elements = 127942
Total number of triangle elements = 127942
Total number of quadrilateral elements = 0
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 6
EGADS : 2 Yes 0 0 1 0 1 1 4 5
EGADS : 3 Yes 0 0 1 0 1 1 4 8
EGADS : 4 Yes 0 0 1 0 1 2 3 5
EGADS : 5 Yes 0 0 1 0 1 2 4
EGADS : 6 Yes 0 0 1 0 1 1 7 8
EGADS : 7 Yes 0 0 1 0 1 6 9 10
EGADS : 8 Yes 0 0 1 0 1 3 6 9
EGADS : 9 Yes 0 0 1 0 1 7 8 10
EGADS : 10 Yes 0 0 1 0 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 168.806
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 8732 16959 0
AFLR4 : Nodes, Trias,Quads= 5233 9961 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 18090 35394 0
AFLR4 : Nodes, Trias,Quads= 5568 10350 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 10182 19859 0
AFLR4 : Nodes, Trias,Quads= 4951 9397 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 16338 31891 0
AFLR4 : Nodes, Trias,Quads= 5435 10085 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 45 51 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 8705 16905 0
AFLR4 : Nodes, Trias,Quads= 5312 10119 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 17908 35030 0
AFLR4 : Nodes, Trias,Quads= 5567 10348 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 8823 17141 0
AFLR4 : Nodes, Trias,Quads= 4980 9455 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 16876 32967 0
AFLR4 : Nodes, Trias,Quads= 5357 9929 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 46 53 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 655 1216 0
AFLR4 : Nodes, Trias,Quads= 646 1198 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 655 1216 0
AFLR4 : Nodes, Trias,Quads= 644 1194 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 657 1220 0
AFLR4 : Nodes, Trias,Quads= 642 1190 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 653 1212 0
AFLR4 : Nodes, Trias,Quads= 644 1194 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 656 1218 0
AFLR4 : Nodes, Trias,Quads= 642 1190 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 654 1214 0
AFLR4 : Nodes, Trias,Quads= 645 1196 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 43459 86910 5772
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 43459 86910
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 8498 16494 0
AFLR4 : Nodes, Trias,Quads= 6521 12540 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 14192 27608 0
AFLR4 : Nodes, Trias,Quads= 10030 19284 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 8900 17298 0
AFLR4 : Nodes, Trias,Quads= 6653 12804 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 13499 26224 0
AFLR4 : Nodes, Trias,Quads= 9809 18844 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 59 77 0
AFLR4 : Nodes, Trias,Quads= 49 57 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 8503 16504 0
AFLR4 : Nodes, Trias,Quads= 6543 12584 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 13624 26478 0
AFLR4 : Nodes, Trias,Quads= 9962 19154 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 8761 17020 0
AFLR4 : Nodes, Trias,Quads= 6664 12826 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 13534 26300 0
AFLR4 : Nodes, Trias,Quads= 9962 19156 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 60 79 0
AFLR4 : Nodes, Trias,Quads= 49 57 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 671 1248 0
AFLR4 : Nodes, Trias,Quads= 642 1190 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 674 1254 0
AFLR4 : Nodes, Trias,Quads= 646 1198 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 670 1246 0
AFLR4 : Nodes, Trias,Quads= 645 1196 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 669 1244 0
AFLR4 : Nodes, Trias,Quads= 648 1202 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 672 1250 0
AFLR4 : Nodes, Trias,Quads= 643 1192 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 670 1246 0
AFLR4 : Nodes, Trias,Quads= 647 1200 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 67246 134484 5710
OVERALL : CPU Time = 2.775 seconds
Body 1 (of 2)
Number of nodes = 63655
Number of elements = 127306
Number of triangle elements = 127306
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 3591
Number of elements = 7178
Number of triangle elements = 7178
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 67246
Total number of elements = 134484
Total number of triangle elements = 134484
Total number of quadrilateral elements = 0
real 0m12.212s
user 0m9.562s
sys 0m2.220s
+ status=0
+ set +x
=================================================
data/session07/02_aflr4_Farfield.py passed (as expected)
=================================================
=================================================
03_aflr4_MeshLength.py test;
+ python 03_aflr4_MeshLength.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 6
EGADS : 2 Yes 0 0 1 0 1 1 4 5
EGADS : 3 Yes 0 0 1 0 1 1 4 8
EGADS : 4 Yes 0 0 1 0 1 2 3 5
EGADS : 5 Yes 0 0 1 0 1 2 4
EGADS : 6 Yes 0 0 1 0 1 1 7 8
EGADS : 7 Yes 0 0 1 0 1 6 9 10
EGADS : 8 Yes 0 0 1 0 1 3 6 9
EGADS : 9 Yes 0 0 1 0 1 7 8 10
EGADS : 10 Yes 0 0 1 0 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.379
AFLR4 : Abs Min Surf Spacing = 0.0217051
AFLR4 : Min Surf Spacing = 0.217051
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 3815 7343 0
AFLR4 : Nodes, Trias,Quads= 2646 5005 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 7205 13986 0
AFLR4 : Nodes, Trias,Quads= 2682 4940 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3862 7438 0
AFLR4 : Nodes, Trias,Quads= 2506 4726 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 6786 13148 0
AFLR4 : Nodes, Trias,Quads= 2612 4800 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 39 50 0
AFLR4 : Nodes, Trias,Quads= 26 24 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 3812 7337 0
AFLR4 : Nodes, Trias,Quads= 2636 4985 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 7155 13886 0
AFLR4 : Nodes, Trias,Quads= 2677 4930 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 3757 7228 0
AFLR4 : Nodes, Trias,Quads= 2510 4734 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 6920 13416 0
AFLR4 : Nodes, Trias,Quads= 2582 4740 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 39 50 0
AFLR4 : Nodes, Trias,Quads= 26 24 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 19776 39544 3046
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 19776 39544
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 3762 7238 0
AFLR4 : Nodes, Trias,Quads= 3236 6186 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 6225 12029 0
AFLR4 : Nodes, Trias,Quads= 4493 8565 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3744 7203 0
AFLR4 : Nodes, Trias,Quads= 3175 6065 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 5992 11563 0
AFLR4 : Nodes, Trias,Quads= 4332 8243 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 43 56 0
AFLR4 : Nodes, Trias,Quads= 29 28 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 3772 7258 0
AFLR4 : Nodes, Trias,Quads= 3224 6162 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 6189 11958 0
AFLR4 : Nodes, Trias,Quads= 4499 8578 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 3662 7039 0
AFLR4 : Nodes, Trias,Quads= 3196 6107 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 6229 12038 0
AFLR4 : Nodes, Trias,Quads= 4380 8340 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 43 56 0
AFLR4 : Nodes, Trias,Quads= 29 28 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 29473 58938 3032
OVERALL : CPU Time = 1.122 seconds
Body 1 (of 2)
Number of nodes = 29153
Number of elements = 58302
Number of triangle elements = 58302
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 320
Number of elements = 636
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 29473
Total number of elements = 58938
Total number of triangle elements = 58938
Total number of quadrilateral elements = 0
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 6
EGADS : 2 Yes 0 0 1 0 1 1 4 5
EGADS : 3 Yes 0 0 1 0 1 1 4 8
EGADS : 4 Yes 0 0 1 0 1 2 3 5
EGADS : 5 Yes 0 0 1 0 1 2 4
EGADS : 6 Yes 0 0 1 0 1 1 7 8
EGADS : 7 Yes 0 0 1 0 1 6 9 10
EGADS : 8 Yes 0 0 1 0 1 3 6 9
EGADS : 9 Yes 0 0 1 0 1 7 8 10
EGADS : 10 Yes 0 0 1 0 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 1591.14
AFLR4 : Abs Min Surf Spacing = 0.0217051
AFLR4 : Min Surf Spacing = 0.217051
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 3
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 890 1664 0
AFLR4 : Nodes, Trias,Quads= 575 1034 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1164 2167 0
AFLR4 : Nodes, Trias,Quads= 586 1011 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 884 1654 0
AFLR4 : Nodes, Trias,Quads= 539 964 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1120 2080 0
AFLR4 : Nodes, Trias,Quads= 569 978 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 17 20 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 887 1658 0
AFLR4 : Nodes, Trias,Quads= 575 1034 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 1168 2175 0
AFLR4 : Nodes, Trias,Quads= 589 1017 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 880 1646 0
AFLR4 : Nodes, Trias,Quads= 535 956 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1113 2066 0
AFLR4 : Nodes, Trias,Quads= 566 972 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 17 20 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 4015 8022 1158
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 4015 8022
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 936 1754 0
AFLR4 : Nodes, Trias,Quads= 785 1452 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1193 2225 0
AFLR4 : Nodes, Trias,Quads= 985 1809 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 937 1757 0
AFLR4 : Nodes, Trias,Quads= 756 1395 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1171 2182 0
AFLR4 : Nodes, Trias,Quads= 949 1738 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 23 30 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 884 1650 0
AFLR4 : Nodes, Trias,Quads= 775 1432 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 1186 2212 0
AFLR4 : Nodes, Trias,Quads= 970 1780 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 884 1651 0
AFLR4 : Nodes, Trias,Quads= 765 1413 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1164 2169 0
AFLR4 : Nodes, Trias,Quads= 949 1739 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 24 32 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 6413 12818 1170
OVERALL : CPU Time = 0.281 seconds
Body 1 (of 2)
Number of nodes = 6393
Number of elements = 12782
Number of triangle elements = 12782
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 6413
Total number of elements = 12818
Total number of triangle elements = 12818
Total number of quadrilateral elements = 0
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 6
EGADS : 2 Yes 0 0 1 0 1 1 4 5
EGADS : 3 Yes 0 0 1 0 1 1 4 8
EGADS : 4 Yes 0 0 1 0 1 2 3 5
EGADS : 5 Yes 0 0 1 0 1 2 4
EGADS : 6 Yes 0 0 1 0 1 1 7 8
EGADS : 7 Yes 0 0 1 0 1 6 9 10
EGADS : 8 Yes 0 0 1 0 1 3 6 9
EGADS : 9 Yes 0 0 1 0 1 7 8 10
EGADS : 10 Yes 0 0 1 0 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 4773.42
AFLR4 : Abs Min Surf Spacing = 0.0217051
AFLR4 : Min Surf Spacing = 0.217051
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 9
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 193 334 0
AFLR4 : Nodes, Trias,Quads= 166 280 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 259 452 0
AFLR4 : Nodes, Trias,Quads= 152 238 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 188 325 0
AFLR4 : Nodes, Trias,Quads= 150 249 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 245 424 0
AFLR4 : Nodes, Trias,Quads= 151 236 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 195 338 0
AFLR4 : Nodes, Trias,Quads= 166 280 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 258 450 0
AFLR4 : Nodes, Trias,Quads= 150 234 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 188 325 0
AFLR4 : Nodes, Trias,Quads= 151 251 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 244 422 0
AFLR4 : Nodes, Trias,Quads= 150 234 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1013 2018 486
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1013 2018
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 208 362 0
AFLR4 : Nodes, Trias,Quads= 203 352 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 242 420 0
AFLR4 : Nodes, Trias,Quads= 185 306 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 203 353 0
AFLR4 : Nodes, Trias,Quads= 190 327 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 243 422 0
AFLR4 : Nodes, Trias,Quads= 182 300 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 209 364 0
AFLR4 : Nodes, Trias,Quads= 200 346 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 246 427 0
AFLR4 : Nodes, Trias,Quads= 185 305 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 207 361 0
AFLR4 : Nodes, Trias,Quads= 195 337 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 248 431 0
AFLR4 : Nodes, Trias,Quads= 188 311 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1316 2624 512
OVERALL : CPU Time = 0.159 seconds
Body 1 (of 2)
Number of nodes = 1296
Number of elements = 2588
Number of triangle elements = 2588
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1316
Total number of elements = 2624
Total number of triangle elements = 2624
Total number of quadrilateral elements = 0
real 0m5.860s
user 0m3.681s
sys 0m1.877s
+ status=0
+ set +x
=================================================
data/session07/03_aflr4_MeshLength.py passed (as expected)
=================================================
=================================================
04_aflr4_EdgeWeight.py test;
+ python 04_aflr4_EdgeWeight.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - leftWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 6
EGADS : 2 Yes 0 0 1 1 1 1 4 5
EGADS : 3 Yes 0 0 1 1 1 1 4 8
EGADS : 4 Yes 0 0 1 1 1 2 3 5
EGADS : 5 Yes 0 0 1 1 1 2 4
EGADS : 6 Yes 0 0 1 0 1 1 7 8
EGADS : 7 Yes 0 0 1 0 1 6 9 10
EGADS : 8 Yes 0 0 1 0 1 3 6 9
EGADS : 9 Yes 0 0 1 0 1 7 8 10
EGADS : 10 Yes 0 0 1 0 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 2651.51
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 5
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1107 2082 0
AFLR4 : Nodes, Trias,Quads= 685 1238 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1473 2759 0
AFLR4 : Nodes, Trias,Quads= 721 1255 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1116 2100 0
AFLR4 : Nodes, Trias,Quads= 671 1210 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1458 2729 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1108 2084 0
AFLR4 : Nodes, Trias,Quads= 683 1234 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 1488 2789 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1112 2092 0
AFLR4 : Nodes, Trias,Quads= 653 1174 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1456 2725 0
AFLR4 : Nodes, Trias,Quads= 708 1229 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 4933 9858 1312
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 4933 9858
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 12796 24695 0
AFLR4 : Nodes, Trias,Quads= 7764 14631 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 29245 57075 0
AFLR4 : Nodes, Trias,Quads= 12448 23481 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 12136 23411 0
AFLR4 : Nodes, Trias,Quads= 7447 14033 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 29424 57435 0
AFLR4 : Nodes, Trias,Quads= 12399 23385 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 196 293 0
AFLR4 : Nodes, Trias,Quads= 188 277 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 2367 4490 0
AFLR4 : Nodes, Trias,Quads= 1726 3208 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 1453 2723 0
AFLR4 : Nodes, Trias,Quads= 1179 2175 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1738 3267 0
AFLR4 : Nodes, Trias,Quads= 1397 2585 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1477 2770 0
AFLR4 : Nodes, Trias,Quads= 1147 2110 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 26 35 0
AFLR4 : Nodes, Trias,Quads= 15 13 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 42971 85934 5550
OVERALL : CPU Time = 1.484 seconds
Body 1 (of 2)
Number of nodes = 42951
Number of elements = 85898
Number of triangle elements = 85898
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 42971
Total number of elements = 85934
Total number of triangle elements = 85934
Total number of quadrilateral elements = 0
real 0m10.870s
user 0m9.111s
sys 0m1.763s
+ status=0
+ set +x
=================================================
data/session07/04_aflr4_EdgeWeight.py passed (as expected)
=================================================
=================================================
05_aflr4_ScaleFactor.py test;
+ python 05_aflr4_ScaleFactor.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 0.5 2 3 6
EGADS : 2 Yes 0 0 1 0 0.5 1 4 5
EGADS : 3 Yes 0 0 1 0 0.5 1 4 8
EGADS : 4 Yes 0 0 1 0 0.5 2 3 5
EGADS : 5 Yes 0 0 1 0 0.5 2 4
EGADS : 6 Yes 0 0 1 0 2 1 7 8
EGADS : 7 Yes 0 0 1 0 2 6 9 10
EGADS : 8 Yes 0 0 1 0 2 3 6 9
EGADS : 9 Yes 0 0 1 0 2 7 8 10
EGADS : 10 Yes 0 0 1 0 2 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 2651.51
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 5
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 2701 5174 0
AFLR4 : Nodes, Trias,Quads= 1493 2758 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 3760 7181 0
AFLR4 : Nodes, Trias,Quads= 1595 2851 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 2824 5420 0
AFLR4 : Nodes, Trias,Quads= 1415 2602 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 3766 7193 0
AFLR4 : Nodes, Trias,Quads= 1566 2793 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 583 1067 0
AFLR4 : Nodes, Trias,Quads= 453 807 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 616 1125 0
AFLR4 : Nodes, Trias,Quads= 323 539 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 595 1091 0
AFLR4 : Nodes, Trias,Quads= 439 779 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 585 1063 0
AFLR4 : Nodes, Trias,Quads= 314 521 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 11 12 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 6848 13688 1584
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 6848 13688
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 2679 5130 0
AFLR4 : Nodes, Trias,Quads= 2106 3984 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 3433 6537 0
AFLR4 : Nodes, Trias,Quads= 2915 5501 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 2738 5248 0
AFLR4 : Nodes, Trias,Quads= 2089 3950 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 3483 6637 0
AFLR4 : Nodes, Trias,Quads= 2902 5475 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 659 1212 0
AFLR4 : Nodes, Trias,Quads= 565 1024 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 636 1162 0
AFLR4 : Nodes, Trias,Quads= 481 852 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 640 1175 0
AFLR4 : Nodes, Trias,Quads= 542 979 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 608 1107 0
AFLR4 : Nodes, Trias,Quads= 462 815 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 11 12 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 11325 22642 1606
OVERALL : CPU Time = 0.444 seconds
Body 1 (of 2)
Number of nodes = 11305
Number of elements = 22606
Number of triangle elements = 22606
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 11325
Total number of elements = 22642
Total number of triangle elements = 22642
Total number of quadrilateral elements = 0
real 0m4.233s
user 0m2.131s
sys 0m1.960s
+ status=0
+ set +x
=================================================
data/session07/05_aflr4_ScaleFactor.py passed (as expected)
=================================================
=================================================
06_aflr4_Proximity.py test;
+ python 06_aflr4_Proximity.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building nacelleOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Nacelle, index = 1
Name = Wing, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Nacelle, index = 1
Name = leftWing, index = 2
Name = riteWing, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - Nacelle
Mesh sizing name - leftWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 4 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 4 Faces
EGADS : Body 0 has 8 Edges
EGADS : Body 0 has 4 Loops
EGADS : Body 0 has 4 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 4 Faces
EGADS : Body 1 has 8 Edges
EGADS : Body 1 has 4 Loops
EGADS : Body 1 has 4 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 10 Faces
EGADS : Body 2 has 18 Edges
EGADS : Body 2 has 10 Loops
EGADS : Body 2 has 10 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 6 Faces
EGADS : Body 3 has 12 Edges
EGADS : Body 3 has 6 Loops
EGADS : Body 3 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 0.5 2 3
EGADS : 2 Yes 0 0 1 0 0.5 1 4
EGADS : 3 Yes 0 0 1 0 0.5 1 4
EGADS : 4 Yes 0 0 1 0 0.5 2 3
EGADS : 5 Yes 1 0 1 0 0.5 6 7
EGADS : 6 Yes 1 0 1 0 0.5 5 8
EGADS : 7 Yes 1 0 1 0 0.5 5 8
EGADS : 8 Yes 1 0 1 0 0.5 6 7
EGADS : 9 Yes 2 0 1 0 50 10 11 14
EGADS : 10 Yes 2 0 1 0 50 9 12 13
EGADS : 11 Yes 2 0 1 0 50 9 12 16
EGADS : 12 Yes 2 0 1 0 50 10 11 13
EGADS : 13 Yes 2 0 1 0 50 10 12
EGADS : 14 Yes 2 0 1 0 1 9 15 16
EGADS : 15 Yes 2 0 1 0 1 14 17 18
EGADS : 16 Yes 2 0 1 0 1 11 14 17
EGADS : 17 Yes 2 0 1 0 1 15 16 18
EGADS : 18 Yes 2 0 1 0 1 15 17
EGADS : 19 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 20 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 21 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 22 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 23 Yes 3 0 1 NA NA 19 20 21 22
EGADS : 24 Yes 3 0 1 NA NA 19 20 21 22
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 3 2 -4
EGADS : 2 -2 5 1 -6
EGADS : 3 7 4 -8 -3
EGADS : 4 8 6 -7 -5
EGADS : 5 9 12 -10 -11
EGADS : 6 10 14 -9 -13
EGADS : 7 -15 11 16 -12
EGADS : 8 -16 13 15 -14
EGADS : 9 -17 18 19 -20
EGADS : 10 -21 20 22 -23
EGADS : 11 -19 24 17 -25
EGADS : 12 -22 25 21 -26
EGADS : 13 23 26
EGADS : 14 27 29 -28 -18
EGADS : 15 30 32 -31 -29
EGADS : 16 28 33 -27 -24
EGADS : 17 31 34 -30 -33
EGADS : 18 -32 -34
EGADS : 19 35 36 -37 -38
EGADS : 20 -39 42 41 -40
EGADS : 21 43 39 -44 -35
EGADS : 22 -45 37 46 -41
EGADS : 23 38 45 -42 -43
EGADS : 24 -36 44 40 -46
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : 19 19
EGADS : 20 20
EGADS : 21 21
EGADS : 22 22
EGADS : 23 23
EGADS : 24 24
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 3 2 -4
EGADS : 2 Yes -2 5 1 -6
EGADS : 3 Yes 7 4 -8 -3
EGADS : 4 Yes 8 6 -7 -5
EGADS : 5 Yes 9 12 -10 -11
EGADS : 6 Yes 10 14 -9 -13
EGADS : 7 Yes -15 11 16 -12
EGADS : 8 Yes -16 13 15 -14
EGADS : 9 Yes -17 18 19 -20
EGADS : 10 Yes -21 20 22 -23
EGADS : 11 Yes -19 24 17 -25
EGADS : 12 Yes -22 25 21 -26
EGADS : 13 Yes 23 26
EGADS : 14 Yes 27 29 -28 -18
EGADS : 15 Yes 30 32 -31 -29
EGADS : 16 Yes 28 33 -27 -24
EGADS : 17 Yes 31 34 -30 -33
EGADS : 18 Yes -32 -34
EGADS : 19 Yes 35 36 -37 -38
EGADS : 20 Yes -39 42 41 -40
EGADS : 21 Yes 43 39 -44 -35
EGADS : 22 Yes -45 37 46 -41
EGADS : 23 Yes 38 45 -42 -43
EGADS : 24 Yes -36 44 40 -46
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 3 4 1 1 2
EGADS : 3 0 Yes 1 3 1 1 3
EGADS : 4 0 Yes 2 4 1 1 3
EGADS : 5 0 Yes 3 1 1 2 4
EGADS : 6 0 Yes 4 2 1 2 4
EGADS : 7 0 Yes 1 2 1 3 4
EGADS : 8 0 Yes 3 4 1 3 4
EGADS : 9 1 Yes 5 6 1 5 6
EGADS : 10 1 Yes 7 8 1 5 6
EGADS : 11 1 Yes 5 7 1 5 7
EGADS : 12 1 Yes 6 8 1 5 7
EGADS : 13 1 Yes 7 5 1 6 8
EGADS : 14 1 Yes 8 6 1 6 8
EGADS : 15 1 Yes 5 6 1 7 8
EGADS : 16 1 Yes 7 8 1 7 8
EGADS : 17 2 Yes 9 10 1 9 11
EGADS : 18 2 Yes 9 11 1 9 14
EGADS : 19 2 Yes 11 12 1 9 11
EGADS : 20 2 Yes 10 12 1 9 10
EGADS : 21 2 Yes 10 13 1 10 12
EGADS : 22 2 Yes 12 14 1 10 12
EGADS : 23 2 Yes 13 14 1 10 13
EGADS : 24 2 Yes 11 9 1 11 16
EGADS : 25 2 Yes 12 10 1 11 12
EGADS : 26 2 Yes 14 13 1 12 13
EGADS : 27 2 Yes 9 15 1 14 16
EGADS : 28 2 Yes 11 16 1 14 16
EGADS : 29 2 Yes 15 16 1 14 15
EGADS : 30 2 Yes 15 17 1 15 17
EGADS : 31 2 Yes 16 18 1 15 17
EGADS : 32 2 Yes 17 18 1 15 18
EGADS : 33 2 Yes 16 15 1 16 17
EGADS : 34 2 Yes 18 17 1 17 18
EGADS : 35 3 Yes 20 19 NA 19 21
EGADS : 36 3 Yes 19 21 NA 19 24
EGADS : 37 3 Yes 22 21 NA 19 22
EGADS : 38 3 Yes 20 22 NA 19 23
EGADS : 39 3 Yes 24 23 NA 20 21
EGADS : 40 3 Yes 23 25 NA 20 24
EGADS : 41 3 Yes 26 25 NA 20 22
EGADS : 42 3 Yes 24 26 NA 20 23
EGADS : 43 3 Yes 20 24 NA 21 23
EGADS : 44 3 Yes 19 23 NA 21 24
EGADS : 45 3 Yes 22 26 NA 22 23
EGADS : 46 3 Yes 21 25 NA 22 24
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 90.5173952 0 0
EGADS : 2 Yes 90.5173952 0 0
EGADS : 3 Yes 60.5173952 0 0
EGADS : 4 Yes 60.5173952 0 0
EGADS : 5 Yes 90.5173952 29.3018771 0
EGADS : 6 Yes 90.5173952 29.3018771 0
EGADS : 7 Yes 60.5173952 29.3018771 0
EGADS : 8 Yes 60.5173952 29.3018771 0
EGADS : 9 Yes 97.2007855 0 0
EGADS : 10 Yes 97.9335611 0 0
EGADS : 11 Yes 50 0 0
EGADS : 12 Yes 75.3047874 0 0
EGADS : 13 Yes 123.552357 0 4.7180639
EGADS : 14 Yes 118.391317 0 3.99272703
EGADS : 15 Yes 97.9335611 36.1389817 0
EGADS : 16 Yes 75.3047874 36.1389817 0
EGADS : 17 Yes 123.552357 97.6729236 4.7180639
EGADS : 18 Yes 118.391317 97.6729236 3.99272703
EGADS : 19 Yes 0 0 1947.05079
EGADS : 20 Yes 0 0 0
EGADS : 21 Yes 0 1953.45847 1947.05079
EGADS : 22 Yes 0 1953.45847 0
EGADS : 23 Yes 2040.21562 0 1947.05079
EGADS : 24 Yes 2040.21562 0 0
EGADS : 25 Yes 2040.21562 1953.45847 1947.05079
EGADS : 26 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 22.2515
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.302
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 FARFIELD
AFLR4 : 20 CAD geometry 0 FARFIELD
AFLR4 : 21 CAD geometry 0 FARFIELD
AFLR4 : 22 CAD geometry 0 FARFIELD
AFLR4 : 23 CAD geometry 0 FARFIELD
AFLR4 : 24 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4 : Component 2 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 13740 26927 0
AFLR4 : Nodes, Trias,Quads= 13723 26893 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 18558 36477 0
AFLR4 : Nodes, Trias,Quads= 16589 32539 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 13776 26999 0
AFLR4 : Nodes, Trias,Quads= 13736 26919 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 18524 36409 0
AFLR4 : Nodes, Trias,Quads= 16538 32437 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 13776 26999 0
AFLR4 : Nodes, Trias,Quads= 13736 26919 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 18524 36409 0
AFLR4 : Nodes, Trias,Quads= 16538 32437 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 13740 26927 0
AFLR4 : Nodes, Trias,Quads= 13723 26893 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 18558 36477 0
AFLR4 : Nodes, Trias,Quads= 16589 32539 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 502 907 0
AFLR4 : Nodes, Trias,Quads= 423 749 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 85 133 0
AFLR4 : Nodes, Trias,Quads= 56 75 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 502 907 0
AFLR4 : Nodes, Trias,Quads= 399 701 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 84 131 0
AFLR4 : Nodes, Trias,Quads= 55 73 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 8705 16905 0
AFLR4 : Nodes, Trias,Quads= 5312 10119 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 17908 35030 0
AFLR4 : Nodes, Trias,Quads= 5567 10348 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 8823 17141 0
AFLR4 : Nodes, Trias,Quads= 4980 9455 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 16876 32967 0
AFLR4 : Nodes, Trias,Quads= 5357 9929 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 46 53 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 139862 279716 7794
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 139862 279716
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 13776 26996 0
AFLR4 : Nodes, Trias,Quads= 13887 27218 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 18675 36709 0
AFLR4 : Nodes, Trias,Quads= 16689 32737 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 13883 27210 0
AFLR4 : Nodes, Trias,Quads= 13963 27370 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 18667 36693 0
AFLR4 : Nodes, Trias,Quads= 16618 32595 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 13883 27210 0
AFLR4 : Nodes, Trias,Quads= 13963 27370 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 18667 36693 0
AFLR4 : Nodes, Trias,Quads= 16618 32595 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 13776 26996 0
AFLR4 : Nodes, Trias,Quads= 13887 27218 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 18675 36709 0
AFLR4 : Nodes, Trias,Quads= 16689 32737 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 525 950 0
AFLR4 : Nodes, Trias,Quads= 470 840 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 91 144 0
AFLR4 : Nodes, Trias,Quads= 59 80 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 538 976 0
AFLR4 : Nodes, Trias,Quads= 443 786 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 90 142 0
AFLR4 : Nodes, Trias,Quads= 58 78 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 8695 16888 0
AFLR4 : Nodes, Trias,Quads= 6539 12576 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 13624 26478 0
AFLR4 : Nodes, Trias,Quads= 9962 19154 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 8700 16899 0
AFLR4 : Nodes, Trias,Quads= 6656 12811 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 13534 26300 0
AFLR4 : Nodes, Trias,Quads= 9962 19156 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 60 79 0
AFLR4 : Nodes, Trias,Quads= 49 57 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 153012 306016 7784
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 153400 306792
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 13935 27308 0
AFLR4 : Nodes, Trias,Quads= 13791 27020 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 18710 36774 0
AFLR4 : Nodes, Trias,Quads= 16564 32482 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 13945 27328 0
AFLR4 : Nodes, Trias,Quads= 13842 27122 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 18677 36708 0
AFLR4 : Nodes, Trias,Quads= 16540 32434 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 13945 27328 0
AFLR4 : Nodes, Trias,Quads= 13842 27122 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 18677 36708 0
AFLR4 : Nodes, Trias,Quads= 16540 32434 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 13935 27308 0
AFLR4 : Nodes, Trias,Quads= 13791 27020 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 18710 36774 0
AFLR4 : Nodes, Trias,Quads= 16564 32482 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 699 1265 0
AFLR4 : Nodes, Trias,Quads= 814 1495 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 103 166 0
AFLR4 : Nodes, Trias,Quads= 63 86 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 1128 2110 0
AFLR4 : Nodes, Trias,Quads= 1749 3352 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 146 239 0
AFLR4 : Nodes, Trias,Quads= 186 319 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 8764 17019 0
AFLR4 : Nodes, Trias,Quads= 7128 13747 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 15673 30550 0
AFLR4 : Nodes, Trias,Quads= 11025 21254 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 9004 17499 0
AFLR4 : Nodes, Trias,Quads= 7783 15057 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 15491 30186 0
AFLR4 : Nodes, Trias,Quads= 11025 21254 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 61 80 0
AFLR4 : Nodes, Trias,Quads= 50 58 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 157692 315376 7994
OVERALL : CPU Time = 12.245 seconds
Body 1 (of 4)
Number of nodes = 59529
Number of elements = 119058
Number of triangle elements = 119058
Number of quadrilateral elements = 0
Body 2 (of 4)
Number of nodes = 59529
Number of elements = 119058
Number of triangle elements = 119058
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 38314
Number of elements = 76624
Number of triangle elements = 76624
Number of quadrilateral elements = 0
Body 4 (of 4)
Number of nodes = 320
Number of elements = 636
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 157692
Total number of elements = 315376
Total number of triangle elements = 315376
Total number of quadrilateral elements = 0
real 0m22.018s
user 0m19.025s
sys 0m2.569s
+ status=0
+ set +x
=================================================
data/session07/06_aflr4_Proximity.py passed (as expected)
=================================================
=================================================
07_aflr4_ProximityComponents.py test;
+ python 07_aflr4_ProximityComponents.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building pylonOml
MESSAGE:: Building nacelleOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing, index = 1
Name = Pylon, index = 2
Name = Nacelle, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Pylon, index = 3
Name = Nacelle, index = 4
Name = Farfield, index = 5
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - Nacelle
Mesh sizing name - Pylon
Mesh sizing name - leftWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 22 Faces
EGADS : Body 0 has 48 Edges
EGADS : Body 0 has 24 Loops
EGADS : Body 0 has 26 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 50 2 3 4
EGADS : 2 Yes 0 0 1 0 50 1 5 6 7 8
EGADS : 3 Yes 0 0 1 0 1 1 5 9
EGADS : 4 Yes 0 0 1 0 50 1 6 10
EGADS : 5 Yes 0 0 1 0 1 2 3 11 12 13
EGADS : 6 Yes 0 0 1 0 50 2 4 10
EGADS : 7 Yes 0 0 1 0 10 2 8 14
EGADS : 8 Yes 0 0 1 0 10 2 7 15
EGADS : 9 Yes 0 0 1 0 1 3 11 16
EGADS : 10 Yes 0 0 1 0 50 4 6
EGADS : 11 Yes 0 0 1 0 1 5 9 16
EGADS : 12 Yes 0 0 1 0 10 5 13 17
EGADS : 13 Yes 0 0 1 0 10 5 12 18
EGADS : 14 Yes 0 0 1 0 0.5 7 15 19
EGADS : 15 Yes 0 0 1 0 0.5 8 14 20
EGADS : 16 Yes 0 0 1 0 1 9 11
EGADS : 17 Yes 0 0 1 0 0.5 12 18 21
EGADS : 18 Yes 0 0 1 0 0.5 13 17 22
EGADS : 19 Yes 0 0 1 0 0.5 14 20
EGADS : 20 Yes 0 0 1 0 0.5 15 19
EGADS : 21 Yes 0 0 1 0 0.5 17 22
EGADS : 22 Yes 0 0 1 0 0.5 18 21
EGADS : 23 Yes 1 0 1 NA NA 25 26 27 28
EGADS : 24 Yes 1 0 1 NA NA 25 26 27 28
EGADS : 25 Yes 1 0 1 NA NA 23 24 27 28
EGADS : 26 Yes 1 0 1 NA NA 23 24 27 28
EGADS : 27 Yes 1 0 1 NA NA 23 24 25 26
EGADS : 28 Yes 1 0 1 NA NA 23 24 25 26
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -3 5 1 -6 7 8
EGADS : 3 9 11 -10 -2
EGADS : 4 -12 4 13 -14
EGADS : 5 10 15 -9 -5 16 17
EGADS : 6 -13 6 12 -18
EGADS : 7 19 20 -7 -21
EGADS : 8 21 -8 -20 -22
EGADS : 9 23 25 -24 -11
EGADS : 10 14 18
EGADS : 11 24 26 -23 -15
EGADS : 12 -27 29 -16 -28
EGADS : 13 -29 30 28 -17
EGADS : 14 31 -19 32 33 -34 -35
EGADS : 15 -31 37 34 -36 -32 22
EGADS : 16 -25 -26
EGADS : 17 38 27 39 40 -41 -42
EGADS : 18 -38 44 41 -43 -39 -30
EGADS : 19 -33 45 35 -46
EGADS : 20 36 46 -37 -45
EGADS : 21 -40 47 42 -48
EGADS : 22 43 48 -44 -47
EGADS : 23 49 50 -51 -52
EGADS : 24 -53 56 55 -54
EGADS : 25 57 53 -58 -49
EGADS : 26 -59 51 60 -55
EGADS : 27 52 59 -56 -57
EGADS : 28 -50 58 54 -60
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2 3
EGADS : 3 4
EGADS : 4 5
EGADS : 5 6 7
EGADS : 6 8
EGADS : 7 9
EGADS : 8 10
EGADS : 9 11
EGADS : 10 12
EGADS : 11 13
EGADS : 12 14
EGADS : 13 15
EGADS : 14 16
EGADS : 15 17
EGADS : 16 18
EGADS : 17 19
EGADS : 18 20
EGADS : 19 21
EGADS : 20 22
EGADS : 21 23
EGADS : 22 24
EGADS : 23 25
EGADS : 24 26
EGADS : 25 27
EGADS : 26 28
EGADS : 27 29
EGADS : 28 30
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -3 5 1 -6
EGADS : 3 Yes 7 8
EGADS : 4 Yes 9 11 -10 -2
EGADS : 5 Yes -12 4 13 -14
EGADS : 6 Yes 10 15 -9 -5
EGADS : 7 Yes 16 17
EGADS : 8 Yes -13 6 12 -18
EGADS : 9 Yes 19 20 -7 -21
EGADS : 10 Yes 21 -8 -20 -22
EGADS : 11 Yes 23 25 -24 -11
EGADS : 12 Yes 14 18
EGADS : 13 Yes 24 26 -23 -15
EGADS : 14 Yes -27 29 -16 -28
EGADS : 15 Yes -29 30 28 -17
EGADS : 16 Yes 31 -19 32 33 -34 -35
EGADS : 17 Yes -31 37 34 -36 -32 22
EGADS : 18 Yes -25 -26
EGADS : 19 Yes 38 27 39 40 -41 -42
EGADS : 20 Yes -38 44 41 -43 -39 -30
EGADS : 21 Yes -33 45 35 -46
EGADS : 22 Yes 36 46 -37 -45
EGADS : 23 Yes -40 47 42 -48
EGADS : 24 Yes 43 48 -44 -47
EGADS : 25 Yes 49 50 -51 -52
EGADS : 26 Yes -53 56 55 -54
EGADS : 27 Yes 57 53 -58 -49
EGADS : 28 Yes -59 51 60 -55
EGADS : 29 Yes 52 59 -56 -57
EGADS : 30 Yes -50 58 54 -60
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 1 3 1 1 3
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 4
EGADS : 5 0 Yes 3 1 1 2 5
EGADS : 6 0 Yes 4 2 1 2 6
EGADS : 7 0 Yes 5 6 1 2 7
EGADS : 8 0 Yes 6 5 1 2 8
EGADS : 9 0 Yes 1 7 1 3 5
EGADS : 10 0 Yes 3 8 1 3 5
EGADS : 11 0 Yes 7 8 1 3 9
EGADS : 12 0 Yes 2 9 1 4 6
EGADS : 13 0 Yes 4 10 1 4 6
EGADS : 14 0 Yes 9 10 1 4 10
EGADS : 15 0 Yes 8 7 1 5 11
EGADS : 16 0 Yes 11 12 1 5 12
EGADS : 17 0 Yes 12 11 1 5 13
EGADS : 18 0 Yes 10 9 1 6 10
EGADS : 19 0 Yes 13 14 1 7 14
EGADS : 20 0 Yes 14 6 1 7 8
EGADS : 21 0 Yes 13 5 1 7 8
EGADS : 22 0 Yes 13 14 1 8 15
EGADS : 23 0 Yes 7 15 1 9 11
EGADS : 24 0 Yes 8 16 1 9 11
EGADS : 25 0 Yes 15 16 1 9 16
EGADS : 26 0 Yes 16 15 1 11 16
EGADS : 27 0 Yes 17 18 1 12 17
EGADS : 28 0 Yes 18 11 1 12 13
EGADS : 29 0 Yes 17 12 1 12 13
EGADS : 30 0 Yes 17 18 1 13 18
EGADS : 31 0 Yes 19 14 1 14 15
EGADS : 32 0 Yes 13 20 1 14 15
EGADS : 33 0 Yes 20 21 1 14 19
EGADS : 34 0 Yes 22 21 1 14 15
EGADS : 35 0 Yes 19 22 1 14 19
EGADS : 36 0 Yes 20 21 1 15 20
EGADS : 37 0 Yes 19 22 1 15 20
EGADS : 38 0 Yes 23 17 1 17 18
EGADS : 39 0 Yes 18 24 1 17 18
EGADS : 40 0 Yes 24 25 1 17 21
EGADS : 41 0 Yes 26 25 1 17 18
EGADS : 42 0 Yes 23 26 1 17 21
EGADS : 43 0 Yes 24 25 1 18 22
EGADS : 44 0 Yes 23 26 1 18 22
EGADS : 45 0 Yes 20 19 1 19 20
EGADS : 46 0 Yes 21 22 1 19 20
EGADS : 47 0 Yes 24 23 1 21 22
EGADS : 48 0 Yes 25 26 1 21 22
EGADS : 49 1 Yes 28 27 NA 23 25
EGADS : 50 1 Yes 27 29 NA 23 28
EGADS : 51 1 Yes 30 29 NA 23 26
EGADS : 52 1 Yes 28 30 NA 23 27
EGADS : 53 1 Yes 32 31 NA 24 25
EGADS : 54 1 Yes 31 33 NA 24 28
EGADS : 55 1 Yes 34 33 NA 24 26
EGADS : 56 1 Yes 32 34 NA 24 27
EGADS : 57 1 Yes 28 32 NA 25 27
EGADS : 58 1 Yes 27 31 NA 25 28
EGADS : 59 1 Yes 30 34 NA 26 27
EGADS : 60 1 Yes 29 33 NA 26 28
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 72.4759225 0 0
EGADS : 6 Yes 83.5054156 0 0
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 0 4.7180639
EGADS : 10 Yes 118.391317 0 3.99272703
EGADS : 11 Yes 72.4759225 29.3018771 0
EGADS : 12 Yes 83.5054156 29.3018771 0
EGADS : 13 Yes 70.524066 0 0
EGADS : 14 Yes 79.4370049 0 0
EGADS : 15 Yes 123.552357 97.6729236 4.7180639
EGADS : 16 Yes 118.391317 97.6729236 3.99272703
EGADS : 17 Yes 79.4370049 29.3018771 0
EGADS : 18 Yes 70.524066 29.3018771 0
EGADS : 19 Yes 90.5173952 0 0
EGADS : 20 Yes 60.5173952 0 0
EGADS : 21 Yes 60.5173952 0 0
EGADS : 22 Yes 90.5173952 0 0
EGADS : 23 Yes 90.5173952 29.3018771 0
EGADS : 24 Yes 60.5173952 29.3018771 0
EGADS : 25 Yes 60.5173952 29.3018771 0
EGADS : 26 Yes 90.5173952 29.3018771 0
EGADS : 27 Yes 0 0 1947.05079
EGADS : 28 Yes 0 0 0
EGADS : 29 Yes 0 1953.45847 1947.05079
EGADS : 30 Yes 0 1953.45847 0
EGADS : 31 Yes 2040.21562 0 1947.05079
EGADS : 32 Yes 2040.21562 0 0
EGADS : 33 Yes 2040.21562 1953.45847 1947.05079
EGADS : 34 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 22.2515
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.302
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : 23 CAD geometry 0 FARFIELD
AFLR4 : 24 CAD geometry 0 FARFIELD
AFLR4 : 25 CAD geometry 0 FARFIELD
AFLR4 : 26 CAD geometry 0 FARFIELD
AFLR4 : 27 CAD geometry 0 FARFIELD
AFLR4 : 28 CAD geometry 0 FARFIELD
AFLR4 : Case has 3 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 9 10 11 16
AFLR4 : Component 2 includes Definitions 14 15 17 18 19 20 21 22
AFLR4 : Component 3 includes Definitions 7 8 12 13
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR4 : Define CAD surface definition 25
AFLR4 : Define CAD surface definition 26
AFLR4 : Define CAD surface definition 27
AFLR4 : Define CAD surface definition 28
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 502 907 0
AFLR4 : Nodes, Trias,Quads= 423 749 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 769 1416 0
AFLR4 : Nodes, Trias,Quads= 579 1036 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 8705 16905 0
AFLR4 : Nodes, Trias,Quads= 5312 10119 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 85 133 0
AFLR4 : Nodes, Trias,Quads= 56 75 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 9412 18267 0
AFLR4 : Nodes, Trias,Quads= 5160 9763 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 84 131 0
AFLR4 : Nodes, Trias,Quads= 55 73 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 382 673 0
AFLR4 : Nodes, Trias,Quads= 221 351 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 377 662 0
AFLR4 : Nodes, Trias,Quads= 227 362 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 17908 35030 0
AFLR4 : Nodes, Trias,Quads= 5567 10348 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 16876 32967 0
AFLR4 : Nodes, Trias,Quads= 5357 9929 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 536 964 0
AFLR4 : Nodes, Trias,Quads= 324 540 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 530 952 0
AFLR4 : Nodes, Trias,Quads= 325 542 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 14942 29305 0
AFLR4 : Nodes, Trias,Quads= 14513 28447 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 14940 29301 0
AFLR4 : Nodes, Trias,Quads= 14427 28275 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 46 53 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 14942 29305 0
AFLR4 : Nodes, Trias,Quads= 14513 28447 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 14928 29277 0
AFLR4 : Nodes, Trias,Quads= 14400 28221 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 18558 36477 0
AFLR4 : Nodes, Trias,Quads= 16589 32539 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 18524 36409 0
AFLR4 : Nodes, Trias,Quads= 16538 32437 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 18558 36477 0
AFLR4 : Nodes, Trias,Quads= 16589 32539 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 18524 36409 0
AFLR4 : Nodes, Trias,Quads= 16538 32437 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 143960 287920 8370
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 143960 287920
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 552 1002 0
AFLR4 : Nodes, Trias,Quads= 474 846 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 803 1479 0
AFLR4 : Nodes, Trias,Quads= 727 1327 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 8664 16826 0
AFLR4 : Nodes, Trias,Quads= 6539 12576 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 94 149 0
AFLR4 : Nodes, Trias,Quads= 60 81 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 9289 18022 0
AFLR4 : Nodes, Trias,Quads= 6959 13362 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 92 145 0
AFLR4 : Nodes, Trias,Quads= 59 79 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 375 660 0
AFLR4 : Nodes, Trias,Quads= 275 460 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 386 681 0
AFLR4 : Nodes, Trias,Quads= 270 449 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 13624 26478 0
AFLR4 : Nodes, Trias,Quads= 9962 19154 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 13541 26314 0
AFLR4 : Nodes, Trias,Quads= 9962 19156 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 573 1036 0
AFLR4 : Nodes, Trias,Quads= 363 616 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 580 1049 0
AFLR4 : Nodes, Trias,Quads= 370 629 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 15123 29666 0
AFLR4 : Nodes, Trias,Quads= 14638 28696 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 15402 30224 0
AFLR4 : Nodes, Trias,Quads= 14606 28632 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 60 79 0
AFLR4 : Nodes, Trias,Quads= 49 57 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 15284 29986 0
AFLR4 : Nodes, Trias,Quads= 14698 28814 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 15598 30614 0
AFLR4 : Nodes, Trias,Quads= 14616 28650 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 18664 36687 0
AFLR4 : Nodes, Trias,Quads= 16684 32727 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 18711 36781 0
AFLR4 : Nodes, Trias,Quads= 16625 32609 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 18664 36687 0
AFLR4 : Nodes, Trias,Quads= 16684 32727 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 18712 36783 0
AFLR4 : Nodes, Trias,Quads= 16612 32583 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 157434 314868 8368
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 159274 318548
AFLR4 : Nodes, Trias = 159694 319388
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1086 2020 0
AFLR4 : Nodes, Trias,Quads= 962 1772 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 2773 5270 0
AFLR4 : Nodes, Trias,Quads= 2797 5318 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 8783 17057 0
AFLR4 : Nodes, Trias,Quads= 7137 13765 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 184 310 0
AFLR4 : Nodes, Trias,Quads= 138 218 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 16222 31763 0
AFLR4 : Nodes, Trias,Quads= 9485 18289 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 232 397 0
AFLR4 : Nodes, Trias,Quads= 221 375 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 1413 2643 0
AFLR4 : Nodes, Trias,Quads= 911 1639 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1587 2978 0
AFLR4 : Nodes, Trias,Quads= 1002 1808 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 15687 30578 0
AFLR4 : Nodes, Trias,Quads= 11055 21314 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 15518 30240 0
AFLR4 : Nodes, Trias,Quads= 11034 21272 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 2345 4452 0
AFLR4 : Nodes, Trias,Quads= 1526 2814 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 2241 4252 0
AFLR4 : Nodes, Trias,Quads= 1462 2694 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 17583 34542 0
AFLR4 : Nodes, Trias,Quads= 14783 28942 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 17575 34524 0
AFLR4 : Nodes, Trias,Quads= 14759 28892 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 61 80 0
AFLR4 : Nodes, Trias,Quads= 50 58 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 19924 39212 0
AFLR4 : Nodes, Trias,Quads= 14954 29272 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 18844 37054 0
AFLR4 : Nodes, Trias,Quads= 14853 29072 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 18691 36736 0
AFLR4 : Nodes, Trias,Quads= 16527 32408 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 18718 36790 0
AFLR4 : Nodes, Trias,Quads= 16525 32404 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 18691 36736 0
AFLR4 : Nodes, Trias,Quads= 16527 32408 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 18709 36772 0
AFLR4 : Nodes, Trias,Quads= 16535 32424 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 168898 337796 9462
OVERALL : CPU Time = 14.698 seconds
Body 1 (of 2)
Number of nodes = 168578
Number of elements = 337160
Number of triangle elements = 337160
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 320
Number of elements = 636
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 168898
Total number of elements = 337796
Total number of triangle elements = 337796
Total number of quadrilateral elements = 0
real 0m30.437s
user 0m30.473s
sys 0m3.430s
+ status=0
+ set +x
=================================================
data/session07/07_aflr4_ProximityComponents.py passed (as expected)
=================================================
=================================================
08_aflr4_InviscidTransport.py test;
+ python 08_aflr4_InviscidTransport.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building wingHinges
MESSAGE:: Building nacelleOml
MESSAGE:: Building htailOml
MESSAGE:: Building htailHinges
MESSAGE:: Building vtailOml
MESSAGE:: Building vtailHinges
MESSAGE:: Building fuseOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Nacelle, index = 1
Name = Vtail, index = 2
Name = Htail, index = 3
Name = Fuselage, index = 4
Name = Wing, index = 5
Name = Farfield, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 7
Name = Nacelle, index = 1
Name = Vtail, index = 2
Name = Htail, index = 3
Name = Fuselage, index = 4
Name = riteWing, index = 5
Name = leftWing, index = 6
Name = Farfield, index = 7
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - Htail
Mesh sizing name - Nacelle
Mesh sizing name - Vtail
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 4 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 4 Faces
EGADS : Body 0 has 8 Edges
EGADS : Body 0 has 4 Loops
EGADS : Body 0 has 4 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 4 Faces
EGADS : Body 1 has 8 Edges
EGADS : Body 1 has 4 Loops
EGADS : Body 1 has 4 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 100 Faces
EGADS : Body 2 has 245 Edges
EGADS : Body 2 has 102 Loops
EGADS : Body 2 has 145 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 6 Faces
EGADS : Body 3 has 12 Edges
EGADS : Body 3 has 6 Loops
EGADS : Body 3 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 5 2 3
EGADS : 2 Yes 0 0 1 0 5 1 4
EGADS : 3 Yes 0 0 1 0 5 1 4
EGADS : 4 Yes 0 0 1 0 5 2 3
EGADS : 5 Yes 1 0 1 0 5 6 7
EGADS : 6 Yes 1 0 1 0 5 5 8
EGADS : 7 Yes 1 0 1 0 5 5 8
EGADS : 8 Yes 1 0 1 0 5 6 7
EGADS : 9 Yes 2 0 1 0 4 10 14 32 107
EGADS : 10 Yes 2 0 1 0 4 9 11 39 108
EGADS : 11 Yes 2 0 1 0 4 10 12 39 108
EGADS : 12 Yes 2 0 1 0 4 11 13 39 108
EGADS : 13 Yes 2 0 1 0 4 12 14 32 107
EGADS : 14 Yes 2 0 1 0 4 9 13 32 107
EGADS : 15 Yes 2 0 1 0 4 16 17 18 19
EGADS : 16 Yes 2 0 1 0 4 15 17 20 21 22
EGADS : 23 24
EGADS : 17 Yes 2 0 1 0 4 15 16 18 22
EGADS : 18 Yes 2 0 1 0 4 15 17 22 25
EGADS : 19 Yes 2 0 1 0 4 15 20 25 26
EGADS : 20 Yes 2 0 1 0 4 16 19 21 23 24
EGADS : 26 27
EGADS : 21 Yes 2 0 1 0 4 16 20
EGADS : 22 Yes 2 0 1 0 4 16 17 18 27
EGADS : 23 Yes 2 0 1 0 1 16 20 24 28 29
EGADS : 30
EGADS : 24 Yes 2 0 1 0 1 16 20 23 29 31
EGADS : 32 33
EGADS : 25 Yes 2 0 1 0 4 18 19 26 27
EGADS : 26 Yes 2 0 1 0 4 19 20 25 27
EGADS : 27 Yes 2 0 1 0 4 20 22 25 26
EGADS : 28 Yes 2 0 1 0 1 23 29 31 34 35
EGADS : 36
EGADS : 29 Yes 2 0 1 0 1 23 24 28 31
EGADS : 30 Yes 2 0 1 0 1 23 33 36 37 38
EGADS : 31 Yes 2 0 1 0 1 24 28 29 34 35
EGADS : 39 40
EGADS : 32 Yes 2 0 1 0 4 9 13 14 24 39 41
EGADS : 33 Yes 2 0 1 0 1 24 30 40
EGADS : 34 Yes 2 0 1 0 4 28 31 35 42 43
EGADS : 44 45
EGADS : 35 Yes 2 0 1 0 4 28 31 34 42 46
EGADS : 47 48
EGADS : 36 Yes 2 0 1 0 1 28 30 40 49 50
EGADS : 37 Yes 2 0 1 0 4 30 38 51 52 53
EGADS : 54
EGADS : 38 Yes 2 0 1 0 4 30 37 55 56 57
EGADS : 58
EGADS : 39 Yes 2 0 1 0 4 10 11 12 31 32
EGADS : 41
EGADS : 40 Yes 2 0 1 0 1 31 33 36
EGADS : 41 Yes 2 0 1 0 4 32 39
EGADS : 42 Yes 2 0 1 0 4 34 35
EGADS : 43 Yes 2 0 1 0 4 34 44 48 59
EGADS : 44 Yes 2 0 1 0 4 34 43 45 59
EGADS : 45 Yes 2 0 1 0 4 34 44 46 59
EGADS : 46 Yes 2 0 1 0 4 35 45 47 60
EGADS : 47 Yes 2 0 1 0 4 35 46 48 60
EGADS : 48 Yes 2 0 1 0 4 35 43 47 60
EGADS : 49 Yes 2 0 1 0 4 36 50 61 62 63
EGADS : 64
EGADS : 50 Yes 2 0 1 0 4 36 49 65 66 67
EGADS : 68
EGADS : 51 Yes 2 0 1 0 4 37 52 58 69
EGADS : 52 Yes 2 0 1 0 4 37 51 53 69
EGADS : 53 Yes 2 0 1 0 4 37 52 56 69
EGADS : 54 Yes 2 0 1 0 4 37 55 70 71 72
EGADS : 73 74 75 76
EGADS : 55 Yes 2 0 1 0 4 38 54 76 77 78
EGADS : 79 80 81 82
EGADS : 56 Yes 2 0 1 0 4 38 53 57 83
EGADS : 57 Yes 2 0 1 0 4 38 56 58 83
EGADS : 58 Yes 2 0 1 0 4 38 51 57 83
EGADS : 59 Yes 2 0 1 0 4 43 44 45 60
EGADS : 60 Yes 2 0 1 0 4 46 47 48 59
EGADS : 61 Yes 2 0 1 0 4 49 68 84 85 86
EGADS : 87 88 89 90
EGADS : 62 Yes 2 0 1 0 4 49 63 67 91
EGADS : 63 Yes 2 0 1 0 4 49 62 64 91
EGADS : 64 Yes 2 0 1 0 4 49 63 65 91
EGADS : 65 Yes 2 0 1 0 4 50 64 66 92
EGADS : 66 Yes 2 0 1 0 4 50 65 67 92
EGADS : 67 Yes 2 0 1 0 4 50 62 66 92
EGADS : 68 Yes 2 0 1 0 4 50 61 84 93 94
EGADS : 95 96 97 98
EGADS : 69 Yes 2 0 1 0 4 51 52 53 83
EGADS : 70 Yes 2 0 1 0 4 54 71 82 99
EGADS : 71 Yes 2 0 1 0 4 54 70 72 99
EGADS : 72 Yes 2 0 1 0 4 54 71 80 99
EGADS : 73 Yes 2 0 1 0 4 54 74 79 100
EGADS : 74 Yes 2 0 1 0 4 54 73 75 100
EGADS : 75 Yes 2 0 1 0 4 54 74 77 100
EGADS : 76 Yes 2 0 1 0 4 54 55
EGADS : 77 Yes 2 0 1 0 4 55 75 78 101
EGADS : 78 Yes 2 0 1 0 4 55 77 79 101
EGADS : 79 Yes 2 0 1 0 4 55 73 78 101
EGADS : 80 Yes 2 0 1 0 4 55 72 81 102
EGADS : 81 Yes 2 0 1 0 4 55 80 82 102
EGADS : 82 Yes 2 0 1 0 4 55 70 81 102
EGADS : 83 Yes 2 0 1 0 4 56 57 58 69
EGADS : 84 Yes 2 0 1 0 4 61 68
EGADS : 85 Yes 2 0 1 0 4 61 86 98 103
EGADS : 86 Yes 2 0 1 0 4 61 85 87 103
EGADS : 87 Yes 2 0 1 0 4 61 86 96 103
EGADS : 88 Yes 2 0 1 0 4 61 89 95 104
EGADS : 89 Yes 2 0 1 0 4 61 88 90 104
EGADS : 90 Yes 2 0 1 0 4 61 89 93 104
EGADS : 91 Yes 2 0 1 0 4 62 63 64 92
EGADS : 92 Yes 2 0 1 0 4 65 66 67 91
EGADS : 93 Yes 2 0 1 0 4 68 90 94 105
EGADS : 94 Yes 2 0 1 0 4 68 93 95 105
EGADS : 95 Yes 2 0 1 0 4 68 88 94 105
EGADS : 96 Yes 2 0 1 0 4 68 87 97 106
EGADS : 97 Yes 2 0 1 0 4 68 96 98 106
EGADS : 98 Yes 2 0 1 0 4 68 85 97 106
EGADS : 99 Yes 2 0 1 0 4 70 71 72 102
EGADS : 100 Yes 2 0 1 0 4 73 74 75 101
EGADS : 101 Yes 2 0 1 0 4 77 78 79 100
EGADS : 102 Yes 2 0 1 0 4 80 81 82 99
EGADS : 103 Yes 2 0 1 0 4 85 86 87 106
EGADS : 104 Yes 2 0 1 0 4 88 89 90 105
EGADS : 105 Yes 2 0 1 0 4 93 94 95 104
EGADS : 106 Yes 2 0 1 0 4 96 97 98 103
EGADS : 107 Yes 2 0 1 0 4 9 13 14 108
EGADS : 108 Yes 2 0 1 0 4 10 11 12 107
EGADS : 109 Yes 3 0 1 NA NA 111 112 113 114
EGADS : 110 Yes 3 0 1 NA NA 111 112 113 114
EGADS : 111 Yes 3 0 1 NA NA 109 110 113 114
EGADS : 112 Yes 3 0 1 NA NA 109 110 113 114
EGADS : 113 Yes 3 0 1 NA NA 109 110 111 112
EGADS : 114 Yes 3 0 1 NA NA 109 110 111 112
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 3 2 -4
EGADS : 2 -2 5 1 -6
EGADS : 3 7 4 -8 -3
EGADS : 4 8 6 -7 -5
EGADS : 5 9 12 -10 -11
EGADS : 6 10 14 -9 -13
EGADS : 7 -15 11 16 -12
EGADS : 8 -16 13 15 -14
EGADS : 9 -17 20 19 -18
EGADS : 10 -21 18 23 -22
EGADS : 11 -24 22 26 -25
EGADS : 12 27 25 -28 -29
EGADS : 13 30 29 -31 -32
EGADS : 14 33 32 -34 -20
EGADS : 15 35 36 -37 -38
EGADS : 16 39 40 -41 42 -43 -35 -44 45 46
EGADS : 17 43 47 -48 -36
EGADS : 18 -49 37 48 -50
EGADS : 19 51 38 -52 -53
EGADS : 20 44 -51 54 55 41 56 -39 57 58
EGADS : 21 -56 -40
EGADS : 22 -42 59 50 -47
EGADS : 23 -60 64 63 -45 -58 62 -61
EGADS : 24 -63 69 68 67 66 -65 -62 -57 -46
EGADS : 25 49 -70 -71 52
EGADS : 26 -54 53 71 -72
EGADS : 27 -55 72 70 -59
EGADS : 28 -73 78 60 -77 -76 75 74
EGADS : 29 61 65 79 77
EGADS : 30 -80 82 81 -64 -83 -84
EGADS : 31 -68 88 73 87 86 76 -79 -66 85
EGADS : 32 -89 -67 92 -91 -90 -30 -33 17
EGADS : 33 -81 93 94 -69
EGADS : 34 -95 -87 -74 101 100 99 -98 97 -96
EGADS : 35 -101 -75 -86 95 -105 -97 -104 -103 102
EGADS : 36 -106 107 80 -78 108 109
EGADS : 37 110 -111 112 113 114 115 -116 83
EGADS : 38 116 117 -114 118 -119 -120 -110 84
EGADS : 39 -92 -85 89 21 24 -27 90 -121
EGADS : 40 -94 122 106 -88
EGADS : 41 91 121
EGADS : 42 105 96
EGADS : 43 98 123 -124 -125
EGADS : 44 -99 127 126 -123
EGADS : 45 -100 129 128 -127
EGADS : 46 -102 131 130 -129
EGADS : 47 103 132 -133 -131
EGADS : 48 104 125 -134 -132
EGADS : 49 -135 -108 141 140 139 -138 137 -136
EGADS : 50 -141 -109 135 -145 -137 -144 -143 142
EGADS : 51 111 146 -147 -148
EGADS : 52 -112 148 150 -149
EGADS : 53 -113 149 152 -151
EGADS : 54 153 -154 155 156 157 -158 159 160 161 162 -163 -115
EGADS : 55 163 164 -161 165 -166 -167 -157 168 -169 -170 -153 -117
EGADS : 56 -118 151 172 -171
EGADS : 57 119 171 -173 -174
EGADS : 58 120 174 -175 -146
EGADS : 59 176 124 -126 -128
EGADS : 60 -176 -130 133 134
EGADS : 61 -177 136 187 186 185 -184 183 182 181 -180 179 -178
EGADS : 62 138 188 -189 -190
EGADS : 63 -139 192 191 -188
EGADS : 64 -140 194 193 -192
EGADS : 65 -142 196 195 -194
EGADS : 66 143 197 -198 -196
EGADS : 67 144 190 -199 -197
EGADS : 68 -187 145 177 -206 -179 -205 -204 203 -183 -202 -201 200
EGADS : 69 207 -152 -150 147
EGADS : 70 154 208 -209 -210
EGADS : 71 -155 210 212 -211
EGADS : 72 -156 211 214 -213
EGADS : 73 158 215 -216 -217
EGADS : 74 -159 217 219 -218
EGADS : 75 -160 218 221 -220
EGADS : 76 -162 -164
EGADS : 77 -165 220 223 -222
EGADS : 78 166 222 -224 -225
EGADS : 79 167 225 -226 -215
EGADS : 80 -168 213 228 -227
EGADS : 81 169 227 -229 -230
EGADS : 82 170 230 -231 -208
EGADS : 83 175 173 -172 -207
EGADS : 84 206 178
EGADS : 85 180 232 -233 -234
EGADS : 86 -181 236 235 -232
EGADS : 87 -182 238 237 -236
EGADS : 88 184 239 -240 -241
EGADS : 89 -185 243 242 -239
EGADS : 90 -186 245 244 -243
EGADS : 91 -193 246 189 -191
EGADS : 92 -246 -195 198 199
EGADS : 93 -200 248 247 -245
EGADS : 94 201 249 -250 -248
EGADS : 95 202 241 -251 -249
EGADS : 96 -203 253 252 -238
EGADS : 97 204 254 -255 -253
EGADS : 98 205 234 -256 -254
EGADS : 99 257 -214 -212 209
EGADS : 100 -221 -219 216 258
EGADS : 101 -258 226 224 -223
EGADS : 102 231 229 -228 -257
EGADS : 103 -237 259 233 -235
EGADS : 104 -244 260 240 -242
EGADS : 105 -260 -247 250 251
EGADS : 106 -259 -252 255 256
EGADS : 107 -261 -19 34 31
EGADS : 108 -23 261 28 -26
EGADS : 109 262 263 -264 -265
EGADS : 110 -266 269 268 -267
EGADS : 111 270 266 -271 -262
EGADS : 112 -272 264 273 -268
EGADS : 113 265 272 -269 -270
EGADS : 114 -263 271 267 -273
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : 19 19
EGADS : 20 20
EGADS : 21 21
EGADS : 22 22
EGADS : 23 23
EGADS : 24 24
EGADS : 25 25
EGADS : 26 26
EGADS : 27 27
EGADS : 28 28
EGADS : 29 29
EGADS : 30 30 31
EGADS : 31 32
EGADS : 32 33
EGADS : 33 34
EGADS : 34 35
EGADS : 35 36
EGADS : 36 37 38
EGADS : 37 39
EGADS : 38 40
EGADS : 39 41
EGADS : 40 42
EGADS : 41 43
EGADS : 42 44
EGADS : 43 45
EGADS : 44 46
EGADS : 45 47
EGADS : 46 48
EGADS : 47 49
EGADS : 48 50
EGADS : 49 51
EGADS : 50 52
EGADS : 51 53
EGADS : 52 54
EGADS : 53 55
EGADS : 54 56
EGADS : 55 57
EGADS : 56 58
EGADS : 57 59
EGADS : 58 60
EGADS : 59 61
EGADS : 60 62
EGADS : 61 63
EGADS : 62 64
EGADS : 63 65
EGADS : 64 66
EGADS : 65 67
EGADS : 66 68
EGADS : 67 69
EGADS : 68 70
EGADS : 69 71
EGADS : 70 72
EGADS : 71 73
EGADS : 72 74
EGADS : 73 75
EGADS : 74 76
EGADS : 75 77
EGADS : 76 78
EGADS : 77 79
EGADS : 78 80
EGADS : 79 81
EGADS : 80 82
EGADS : 81 83
EGADS : 82 84
EGADS : 83 85
EGADS : 84 86
EGADS : 85 87
EGADS : 86 88
EGADS : 87 89
EGADS : 88 90
EGADS : 89 91
EGADS : 90 92
EGADS : 91 93
EGADS : 92 94
EGADS : 93 95
EGADS : 94 96
EGADS : 95 97
EGADS : 96 98
EGADS : 97 99
EGADS : 98 100
EGADS : 99 101
EGADS : 100 102
EGADS : 101 103
EGADS : 102 104
EGADS : 103 105
EGADS : 104 106
EGADS : 105 107
EGADS : 106 108
EGADS : 107 109
EGADS : 108 110
EGADS : 109 111
EGADS : 110 112
EGADS : 111 113
EGADS : 112 114
EGADS : 113 115
EGADS : 114 116
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 3 2 -4
EGADS : 2 Yes -2 5 1 -6
EGADS : 3 Yes 7 4 -8 -3
EGADS : 4 Yes 8 6 -7 -5
EGADS : 5 Yes 9 12 -10 -11
EGADS : 6 Yes 10 14 -9 -13
EGADS : 7 Yes -15 11 16 -12
EGADS : 8 Yes -16 13 15 -14
EGADS : 9 Yes -17 20 19 -18
EGADS : 10 Yes -21 18 23 -22
EGADS : 11 Yes -24 22 26 -25
EGADS : 12 Yes 27 25 -28 -29
EGADS : 13 Yes 30 29 -31 -32
EGADS : 14 Yes 33 32 -34 -20
EGADS : 15 Yes 35 36 -37 -38
EGADS : 16 Yes 39 40 -41 42 -43 -35 -44 45 46
EGADS : 17 Yes 43 47 -48 -36
EGADS : 18 Yes -49 37 48 -50
EGADS : 19 Yes 51 38 -52 -53
EGADS : 20 Yes 44 -51 54 55 41 56 -39 57 58
EGADS : 21 Yes -56 -40
EGADS : 22 Yes -42 59 50 -47
EGADS : 23 Yes -60 64 63 -45 -58 62 -61
EGADS : 24 Yes -63 69 68 67 66 -65 -62 -57 -46
EGADS : 25 Yes 49 -70 -71 52
EGADS : 26 Yes -54 53 71 -72
EGADS : 27 Yes -55 72 70 -59
EGADS : 28 Yes -73 78 60 -77 -76 75 74
EGADS : 29 Yes 61 65 79 77
EGADS : 30 Yes -80 82 81 -64
EGADS : 31 Yes -83 -84
EGADS : 32 Yes -68 88 73 87 86 76 -79 -66 85
EGADS : 33 Yes -89 -67 92 -91 -90 -30 -33 17
EGADS : 34 Yes -81 93 94 -69
EGADS : 35 Yes -95 -87 -74 101 100 99 -98 97 -96
EGADS : 36 Yes -101 -75 -86 95 -105 -97 -104 -103 102
EGADS : 37 Yes -106 107 80 -78
EGADS : 38 Yes 108 109
EGADS : 39 Yes 110 -111 112 113 114 115 -116 83
EGADS : 40 Yes 116 117 -114 118 -119 -120 -110 84
EGADS : 41 Yes -92 -85 89 21 24 -27 90 -121
EGADS : 42 Yes -94 122 106 -88
EGADS : 43 Yes 91 121
EGADS : 44 Yes 105 96
EGADS : 45 Yes 98 123 -124 -125
EGADS : 46 Yes -99 127 126 -123
EGADS : 47 Yes -100 129 128 -127
EGADS : 48 Yes -102 131 130 -129
EGADS : 49 Yes 103 132 -133 -131
EGADS : 50 Yes 104 125 -134 -132
EGADS : 51 Yes -135 -108 141 140 139 -138 137 -136
EGADS : 52 Yes -141 -109 135 -145 -137 -144 -143 142
EGADS : 53 Yes 111 146 -147 -148
EGADS : 54 Yes -112 148 150 -149
EGADS : 55 Yes -113 149 152 -151
EGADS : 56 Yes 153 -154 155 156 157 -158 159 160 161 162 -163 -115
EGADS : 57 Yes 163 164 -161 165 -166 -167 -157 168 -169 -170 -153
EGADS : -117
EGADS : 58 Yes -118 151 172 -171
EGADS : 59 Yes 119 171 -173 -174
EGADS : 60 Yes 120 174 -175 -146
EGADS : 61 Yes 176 124 -126 -128
EGADS : 62 Yes -176 -130 133 134
EGADS : 63 Yes -177 136 187 186 185 -184 183 182 181 -180 179 -178
EGADS : 64 Yes 138 188 -189 -190
EGADS : 65 Yes -139 192 191 -188
EGADS : 66 Yes -140 194 193 -192
EGADS : 67 Yes -142 196 195 -194
EGADS : 68 Yes 143 197 -198 -196
EGADS : 69 Yes 144 190 -199 -197
EGADS : 70 Yes -187 145 177 -206 -179 -205 -204 203 -183 -202 -201
EGADS : 200
EGADS : 71 Yes 207 -152 -150 147
EGADS : 72 Yes 154 208 -209 -210
EGADS : 73 Yes -155 210 212 -211
EGADS : 74 Yes -156 211 214 -213
EGADS : 75 Yes 158 215 -216 -217
EGADS : 76 Yes -159 217 219 -218
EGADS : 77 Yes -160 218 221 -220
EGADS : 78 Yes -162 -164
EGADS : 79 Yes -165 220 223 -222
EGADS : 80 Yes 166 222 -224 -225
EGADS : 81 Yes 167 225 -226 -215
EGADS : 82 Yes -168 213 228 -227
EGADS : 83 Yes 169 227 -229 -230
EGADS : 84 Yes 170 230 -231 -208
EGADS : 85 Yes 175 173 -172 -207
EGADS : 86 Yes 206 178
EGADS : 87 Yes 180 232 -233 -234
EGADS : 88 Yes -181 236 235 -232
EGADS : 89 Yes -182 238 237 -236
EGADS : 90 Yes 184 239 -240 -241
EGADS : 91 Yes -185 243 242 -239
EGADS : 92 Yes -186 245 244 -243
EGADS : 93 Yes -193 246 189 -191
EGADS : 94 Yes -246 -195 198 199
EGADS : 95 Yes -200 248 247 -245
EGADS : 96 Yes 201 249 -250 -248
EGADS : 97 Yes 202 241 -251 -249
EGADS : 98 Yes -203 253 252 -238
EGADS : 99 Yes 204 254 -255 -253
EGADS : 100 Yes 205 234 -256 -254
EGADS : 101 Yes 257 -214 -212 209
EGADS : 102 Yes -221 -219 216 258
EGADS : 103 Yes -258 226 224 -223
EGADS : 104 Yes 231 229 -228 -257
EGADS : 105 Yes -237 259 233 -235
EGADS : 106 Yes -244 260 240 -242
EGADS : 107 Yes -260 -247 250 251
EGADS : 108 Yes -259 -252 255 256
EGADS : 109 Yes -261 -19 34 31
EGADS : 110 Yes -23 261 28 -26
EGADS : 111 Yes 262 263 -264 -265
EGADS : 112 Yes -266 269 268 -267
EGADS : 113 Yes 270 266 -271 -262
EGADS : 114 Yes -272 264 273 -268
EGADS : 115 Yes 265 272 -269 -270
EGADS : 116 Yes -263 271 267 -273
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 3 4 1 1 2
EGADS : 3 0 Yes 1 3 1 1 3
EGADS : 4 0 Yes 2 4 1 1 3
EGADS : 5 0 Yes 3 1 1 2 4
EGADS : 6 0 Yes 4 2 1 2 4
EGADS : 7 0 Yes 1 2 1 3 4
EGADS : 8 0 Yes 3 4 1 3 4
EGADS : 9 1 Yes 5 6 1 5 6
EGADS : 10 1 Yes 7 8 1 5 6
EGADS : 11 1 Yes 5 7 1 5 7
EGADS : 12 1 Yes 6 8 1 5 7
EGADS : 13 1 Yes 7 5 1 6 8
EGADS : 14 1 Yes 8 6 1 6 8
EGADS : 15 1 Yes 5 6 1 7 8
EGADS : 16 1 Yes 7 8 1 7 8
EGADS : 17 2 Yes 9 10 1 9 32
EGADS : 18 2 Yes 10 11 1 9 10
EGADS : 19 2 Yes 12 11 1 9 107
EGADS : 20 2 Yes 9 12 1 9 14
EGADS : 21 2 Yes 10 13 1 10 39
EGADS : 22 2 Yes 13 14 1 10 11
EGADS : 23 2 Yes 11 14 1 10 108
EGADS : 24 2 Yes 13 15 1 11 39
EGADS : 25 2 Yes 15 16 1 11 12
EGADS : 26 2 Yes 14 16 1 11 108
EGADS : 27 2 Yes 17 15 1 12 39
EGADS : 28 2 Yes 18 16 1 12 108
EGADS : 29 2 Yes 17 18 1 12 13
EGADS : 30 2 Yes 19 17 1 13 32
EGADS : 31 2 Yes 20 18 1 13 107
EGADS : 32 2 Yes 19 20 1 13 14
EGADS : 33 2 Yes 9 19 1 14 32
EGADS : 34 2 Yes 12 20 1 14 107
EGADS : 35 2 Yes 21 22 1 15 16
EGADS : 36 2 Yes 22 23 1 15 17
EGADS : 37 2 Yes 24 23 1 15 18
EGADS : 38 2 Yes 21 24 1 15 19
EGADS : 39 2 Yes 25 26 1 16 20
EGADS : 40 2 Yes 26 27 1 16 21
EGADS : 41 2 Yes 28 27 1 16 20
EGADS : 42 2 Yes 28 29 1 16 22
EGADS : 43 2 Yes 22 29 1 16 17
EGADS : 44 2 Yes 30 21 1 16 20
EGADS : 45 2 Yes 30 31 1 16 23
EGADS : 46 2 Yes 31 25 1 16 24
EGADS : 47 2 Yes 29 32 1 17 22
EGADS : 48 2 Yes 23 32 1 17 18
EGADS : 49 2 Yes 24 33 1 18 25
EGADS : 50 2 Yes 33 32 1 18 22
EGADS : 51 2 Yes 34 21 1 19 20
EGADS : 52 2 Yes 35 24 1 19 25
EGADS : 53 2 Yes 34 35 1 19 26
EGADS : 54 2 Yes 34 36 1 20 26
EGADS : 55 2 Yes 36 28 1 20 27
EGADS : 56 2 Yes 27 26 1 20 21
EGADS : 57 2 Yes 25 37 1 20 24
EGADS : 58 2 Yes 37 30 1 20 23
EGADS : 59 2 Yes 28 33 1 22 27
EGADS : 60 2 Yes 38 39 1 23 28
EGADS : 61 2 Yes 39 40 1 23 29
EGADS : 62 2 Yes 37 40 1 23 24
EGADS : 63 2 Yes 41 31 1 23 24
EGADS : 64 2 Yes 38 41 1 23 30
EGADS : 65 2 Yes 40 42 1 24 29
EGADS : 66 2 Yes 43 42 1 24 31
EGADS : 67 2 Yes 44 43 1 24 32
EGADS : 68 2 Yes 45 44 1 24 31
EGADS : 69 2 Yes 41 45 1 24 33
EGADS : 70 2 Yes 46 33 1 25 27
EGADS : 71 2 Yes 35 46 1 25 26
EGADS : 72 2 Yes 36 46 1 26 27
EGADS : 73 2 Yes 47 48 1 28 31
EGADS : 74 2 Yes 49 48 1 28 34
EGADS : 75 2 Yes 50 49 1 28 35
EGADS : 76 2 Yes 50 51 1 28 31
EGADS : 77 2 Yes 51 39 1 28 29
EGADS : 78 2 Yes 47 38 1 28 36
EGADS : 79 2 Yes 42 51 1 29 31
EGADS : 80 2 Yes 52 38 1 30 36
EGADS : 81 2 Yes 52 41 1 30 33
EGADS : 82 2 DEGEN 52 52 - 30
EGADS : 83 2 Yes 53 54 1 30 37
EGADS : 84 2 Yes 54 53 1 30 38
EGADS : 85 2 Yes 43 44 1 31 39
EGADS : 86 2 Yes 55 50 1 31 35
EGADS : 87 2 Yes 48 55 1 31 34
EGADS : 88 2 Yes 45 47 1 31 40
EGADS : 89 2 Yes 43 10 1 32 39
EGADS : 90 2 Yes 17 56 1 32 39
EGADS : 91 2 Yes 56 57 1 32 41
EGADS : 92 2 Yes 44 57 1 32 39
EGADS : 93 2 DEGEN 52 52 - 33
EGADS : 94 2 Yes 52 45 1 33 40
EGADS : 95 2 Yes 55 58 1 34 35
EGADS : 96 2 Yes 58 59 1 34 42
EGADS : 97 2 Yes 60 59 1 34 35
EGADS : 98 2 Yes 60 61 1 34 43
EGADS : 99 2 Yes 62 61 1 34 44
EGADS : 100 2 Yes 63 62 1 34 45
EGADS : 101 2 Yes 49 63 1 34 35
EGADS : 102 2 Yes 64 63 1 35 46
EGADS : 103 2 Yes 64 65 1 35 47
EGADS : 104 2 Yes 65 60 1 35 48
EGADS : 105 2 Yes 59 58 1 35 42
EGADS : 106 2 Yes 52 47 1 36 40
EGADS : 107 2 DEGEN 52 52 - 36
EGADS : 108 2 Yes 66 67 1 36 49
EGADS : 109 2 Yes 67 66 1 36 50
EGADS : 110 2 Yes 54 68 1 37 38
EGADS : 111 2 Yes 69 68 1 37 51
EGADS : 112 2 Yes 69 70 1 37 52
EGADS : 113 2 Yes 70 71 1 37 53
EGADS : 114 2 Yes 71 72 1 37 38
EGADS : 115 2 Yes 72 73 1 37 54
EGADS : 116 2 Yes 53 73 1 37 38
EGADS : 117 2 Yes 73 72 1 38 55
EGADS : 118 2 Yes 71 74 1 38 56
EGADS : 119 2 Yes 75 74 1 38 57
EGADS : 120 2 Yes 68 75 1 38 58
EGADS : 121 2 Yes 57 56 1 39 41
EGADS : 122 2 DEGEN 52 52 - 40
EGADS : 123 2 Yes 61 76 1 43 44
EGADS : 124 2 Yes 77 76 1 43 59
EGADS : 125 2 Yes 60 77 1 43 48
EGADS : 126 2 Yes 78 76 1 44 59
EGADS : 127 2 Yes 62 78 1 44 45
EGADS : 128 2 Yes 79 78 1 45 59
EGADS : 129 2 Yes 63 79 1 45 46
EGADS : 130 2 Yes 80 79 1 46 60
EGADS : 131 2 Yes 64 80 1 46 47
EGADS : 132 2 Yes 65 81 1 47 48
EGADS : 133 2 Yes 80 81 1 47 60
EGADS : 134 2 Yes 81 77 1 48 60
EGADS : 135 2 Yes 67 82 1 49 50
EGADS : 136 2 Yes 82 83 1 49 61
EGADS : 137 2 Yes 84 83 1 49 50
EGADS : 138 2 Yes 84 85 1 49 62
EGADS : 139 2 Yes 86 85 1 49 63
EGADS : 140 2 Yes 87 86 1 49 64
EGADS : 141 2 Yes 66 87 1 49 50
EGADS : 142 2 Yes 88 87 1 50 65
EGADS : 143 2 Yes 88 89 1 50 66
EGADS : 144 2 Yes 89 84 1 50 67
EGADS : 145 2 Yes 83 82 1 50 68
EGADS : 146 2 Yes 68 90 1 51 58
EGADS : 147 2 Yes 91 90 1 51 69
EGADS : 148 2 Yes 69 91 1 51 52
EGADS : 149 2 Yes 70 92 1 52 53
EGADS : 150 2 Yes 91 92 1 52 69
EGADS : 151 2 Yes 71 93 1 53 56
EGADS : 152 2 Yes 92 93 1 53 69
EGADS : 153 2 Yes 72 94 1 54 55
EGADS : 154 2 Yes 95 94 1 54 70
EGADS : 155 2 Yes 95 96 1 54 71
EGADS : 156 2 Yes 96 97 1 54 72
EGADS : 157 2 Yes 97 98 1 54 55
EGADS : 158 2 Yes 99 98 1 54 73
EGADS : 159 2 Yes 99 100 1 54 74
EGADS : 160 2 Yes 100 101 1 54 75
EGADS : 161 2 Yes 101 102 1 54 55
EGADS : 162 2 Yes 102 103 1 54 76
EGADS : 163 2 Yes 73 103 1 54 55
EGADS : 164 2 Yes 103 102 1 55 76
EGADS : 165 2 Yes 101 104 1 55 77
EGADS : 166 2 Yes 105 104 1 55 78
EGADS : 167 2 Yes 98 105 1 55 79
EGADS : 168 2 Yes 97 106 1 55 80
EGADS : 169 2 Yes 107 106 1 55 81
EGADS : 170 2 Yes 94 107 1 55 82
EGADS : 171 2 Yes 74 108 1 56 57
EGADS : 172 2 Yes 93 108 1 56 83
EGADS : 173 2 Yes 109 108 1 57 83
EGADS : 174 2 Yes 75 109 1 57 58
EGADS : 175 2 Yes 90 109 1 58 83
EGADS : 176 2 Yes 79 77 1 59 60
EGADS : 177 2 Yes 82 110 1 61 68
EGADS : 178 2 Yes 110 111 1 61 84
EGADS : 179 2 Yes 112 111 1 61 68
EGADS : 180 2 Yes 112 113 1 61 85
EGADS : 181 2 Yes 114 113 1 61 86
EGADS : 182 2 Yes 115 114 1 61 87
EGADS : 183 2 Yes 116 115 1 61 68
EGADS : 184 2 Yes 116 117 1 61 88
EGADS : 185 2 Yes 118 117 1 61 89
EGADS : 186 2 Yes 119 118 1 61 90
EGADS : 187 2 Yes 83 119 1 61 68
EGADS : 188 2 Yes 85 120 1 62 63
EGADS : 189 2 Yes 121 120 1 62 91
EGADS : 190 2 Yes 84 121 1 62 67
EGADS : 191 2 Yes 122 120 1 63 91
EGADS : 192 2 Yes 86 122 1 63 64
EGADS : 193 2 Yes 123 122 1 64 91
EGADS : 194 2 Yes 87 123 1 64 65
EGADS : 195 2 Yes 124 123 1 65 92
EGADS : 196 2 Yes 88 124 1 65 66
EGADS : 197 2 Yes 89 125 1 66 67
EGADS : 198 2 Yes 124 125 1 66 92
EGADS : 199 2 Yes 125 121 1 67 92
EGADS : 200 2 Yes 126 119 1 68 93
EGADS : 201 2 Yes 126 127 1 68 94
EGADS : 202 2 Yes 127 116 1 68 95
EGADS : 203 2 Yes 128 115 1 68 96
EGADS : 204 2 Yes 128 129 1 68 97
EGADS : 205 2 Yes 129 112 1 68 98
EGADS : 206 2 Yes 111 110 1 68 84
EGADS : 207 2 Yes 90 93 1 69 83
EGADS : 208 2 Yes 94 130 1 70 82
EGADS : 209 2 Yes 131 130 1 70 99
EGADS : 210 2 Yes 95 131 1 70 71
EGADS : 211 2 Yes 96 132 1 71 72
EGADS : 212 2 Yes 131 132 1 71 99
EGADS : 213 2 Yes 97 133 1 72 80
EGADS : 214 2 Yes 132 133 1 72 99
EGADS : 215 2 Yes 98 134 1 73 79
EGADS : 216 2 Yes 135 134 1 73 100
EGADS : 217 2 Yes 99 135 1 73 74
EGADS : 218 2 Yes 100 136 1 74 75
EGADS : 219 2 Yes 135 136 1 74 100
EGADS : 220 2 Yes 101 137 1 75 77
EGADS : 221 2 Yes 136 137 1 75 100
EGADS : 222 2 Yes 104 138 1 77 78
EGADS : 223 2 Yes 137 138 1 77 101
EGADS : 224 2 Yes 139 138 1 78 101
EGADS : 225 2 Yes 105 139 1 78 79
EGADS : 226 2 Yes 134 139 1 79 101
EGADS : 227 2 Yes 106 140 1 80 81
EGADS : 228 2 Yes 133 140 1 80 102
EGADS : 229 2 Yes 141 140 1 81 102
EGADS : 230 2 Yes 107 141 1 81 82
EGADS : 231 2 Yes 130 141 1 82 102
EGADS : 232 2 Yes 113 142 1 85 86
EGADS : 233 2 Yes 143 142 1 85 103
EGADS : 234 2 Yes 112 143 1 85 98
EGADS : 235 2 Yes 144 142 1 86 103
EGADS : 236 2 Yes 114 144 1 86 87
EGADS : 237 2 Yes 145 144 1 87 103
EGADS : 238 2 Yes 115 145 1 87 96
EGADS : 239 2 Yes 117 146 1 88 89
EGADS : 240 2 Yes 147 146 1 88 104
EGADS : 241 2 Yes 116 147 1 88 95
EGADS : 242 2 Yes 148 146 1 89 104
EGADS : 243 2 Yes 118 148 1 89 90
EGADS : 244 2 Yes 149 148 1 90 104
EGADS : 245 2 Yes 119 149 1 90 93
EGADS : 246 2 Yes 123 121 1 91 92
EGADS : 247 2 Yes 150 149 1 93 105
EGADS : 248 2 Yes 126 150 1 93 94
EGADS : 249 2 Yes 127 151 1 94 95
EGADS : 250 2 Yes 150 151 1 94 105
EGADS : 251 2 Yes 151 147 1 95 105
EGADS : 252 2 Yes 152 145 1 96 106
EGADS : 253 2 Yes 128 152 1 96 97
EGADS : 254 2 Yes 129 153 1 97 98
EGADS : 255 2 Yes 152 153 1 97 106
EGADS : 256 2 Yes 153 143 1 98 106
EGADS : 257 2 Yes 130 133 1 99 102
EGADS : 258 2 Yes 134 137 1 100 101
EGADS : 259 2 Yes 145 143 1 103 106
EGADS : 260 2 Yes 149 147 1 104 105
EGADS : 261 2 Yes 11 18 1 107 108
EGADS : 262 3 Yes 155 154 NA 109 111
EGADS : 263 3 Yes 154 156 NA 109 114
EGADS : 264 3 Yes 157 156 NA 109 112
EGADS : 265 3 Yes 155 157 NA 109 113
EGADS : 266 3 Yes 159 158 NA 110 111
EGADS : 267 3 Yes 158 160 NA 110 114
EGADS : 268 3 Yes 161 160 NA 110 112
EGADS : 269 3 Yes 159 161 NA 110 113
EGADS : 270 3 Yes 155 159 NA 111 113
EGADS : 271 3 Yes 154 158 NA 111 114
EGADS : 272 3 Yes 157 161 NA 112 113
EGADS : 273 3 Yes 156 160 NA 112 114
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 90.5173952 0 0
EGADS : 2 Yes 90.5173952 0 0
EGADS : 3 Yes 60.5173952 0 0
EGADS : 4 Yes 60.5173952 0 0
EGADS : 5 Yes 90.5173952 29.3018771 0
EGADS : 6 Yes 90.5173952 29.3018771 0
EGADS : 7 Yes 60.5173952 29.3018771 0
EGADS : 8 Yes 60.5173952 29.3018771 0
EGADS : 9 Yes 155.279418 0.556318046 17.8486974
EGADS : 10 Yes 162.754076 0 17.8179957
EGADS : 11 Yes 162.923819 0 18.2706428
EGADS : 12 Yes 156.044413 0.521348839 18.2706428
EGADS : 13 Yes 155.279418 0 17.8486974
EGADS : 14 Yes 156.044413 0 18.2706428
EGADS : 15 Yes 166.073363 0 35.1119946
EGADS : 16 Yes 166.308339 0 34.6929244
EGADS : 17 Yes 169.251074 0 35.1433216
EGADS : 18 Yes 169.082175 0 34.6929244
EGADS : 19 Yes 166.073363 0.227596794 35.1119946
EGADS : 20 Yes 166.308339 0.210212312 34.6929244
EGADS : 21 Yes 162.505711 6.6926087 7.42255789
EGADS : 22 Yes 153.264796 6.72114619 6.73834001
EGADS : 23 Yes 153.930225 7.199099 6.86796425
EGADS : 24 Yes 162.623387 7.31455844 6.87508685
EGADS : 25 Yes 139.227902 5.03861756 7.07099122
EGADS : 26 Yes 165.02399 35.781198 13.6055284
EGADS : 27 Yes 173.282633 35.781198 13.6055284
EGADS : 28 Yes 172.798165 34.4735419 13.3275775
EGADS : 29 Yes 168.724656 34.4225125 13.0211892
EGADS : 30 Yes 160.457816 1.16501909 6.24763245
EGADS : 31 Yes 152.092394 3.29252447 6.00142548
EGADS : 32 Yes 168.960236 34.0035224 12.9505074
EGADS : 33 Yes 172.609156 34.051986 12.953497
EGADS : 34 Yes 153.264796 6.72114619 8.11890743
EGADS : 35 Yes 154.029174 7.14485531 8.17706386
EGADS : 36 Yes 168.724656 34.4225125 13.6122726
EGADS : 37 Yes 156.577382 2.32417494 6.86784347
EGADS : 38 Yes 121.026192 0 0
EGADS : 39 Yes 165.026192 0 7
EGADS : 40 Yes 165.026192 0.5 8.5
EGADS : 41 Yes 121.026192 10 0
EGADS : 42 Yes 165.026192 0 10
EGADS : 43 Yes 159.822328 0 10
EGADS : 44 Yes 137.454662 0 10
EGADS : 45 Yes 121.026192 0 10
EGADS : 46 Yes 169.00177 33.9807538 13.4999966
EGADS : 47 Yes 121.026192 0 0
EGADS : 48 Yes 152.092394 0 6.00142548
EGADS : 49 Yes 160.457816 0 6.24763245
EGADS : 50 Yes 156.577382 0 6.86784347
EGADS : 51 Yes 165.026192 0 8.5
EGADS : 52 Yes 0 0 0
EGADS : 53 Yes 54.9020417 7.00084115 0
EGADS : 54 Yes 97.361045 7.90366896 0
EGADS : 55 Yes 139.227902 0 7.07099122
EGADS : 56 Yes 169.38016 0 35.487551
EGADS : 57 Yes 162.942213 0 35.487551
EGADS : 58 Yes 165.02399 0 13.6055284
EGADS : 59 Yes 173.282633 0 13.6055284
EGADS : 60 Yes 172.798165 0 13.3275775
EGADS : 61 Yes 168.724656 0 13.0211892
EGADS : 62 Yes 153.264796 0 6.73834001
EGADS : 63 Yes 162.505711 0 7.42255789
EGADS : 64 Yes 153.264796 0 8.11890743
EGADS : 65 Yes 168.724656 0 13.6122726
EGADS : 66 Yes 97.361045 0 0
EGADS : 67 Yes 54.9020417 0 0
EGADS : 68 Yes 97.4729837 13.4242561 0
EGADS : 69 Yes 93.4471586 13.4242631 0
EGADS : 70 Yes 93.8409288 32.482011 0
EGADS : 71 Yes 97.8594104 32.482018 0
EGADS : 72 Yes 97.9335611 36.1389817 0
EGADS : 73 Yes 75.3047874 36.1389817 0
EGADS : 74 Yes 93.8409288 32.482011 0
EGADS : 75 Yes 93.4471586 13.4242631 0
EGADS : 76 Yes 168.960236 0 12.9505074
EGADS : 77 Yes 172.609156 0 12.953497
EGADS : 78 Yes 153.930225 0 6.86796425
EGADS : 79 Yes 162.623387 0 6.87508685
EGADS : 80 Yes 154.029174 0 8.17706386
EGADS : 81 Yes 169.00177 0 13.4999966
EGADS : 82 Yes 75.3047874 0 0
EGADS : 83 Yes 97.9335611 0 0
EGADS : 84 Yes 97.8594104 0 0
EGADS : 85 Yes 93.8409288 0 0
EGADS : 86 Yes 93.4471586 0 0
EGADS : 87 Yes 97.4729837 0 0
EGADS : 88 Yes 93.4471586 0 0
EGADS : 89 Yes 93.8409288 0 0
EGADS : 90 Yes 97.1624342 13.7926169 0
EGADS : 91 Yes 93.8265357 13.6735644 0
EGADS : 92 Yes 94.2099771 32.2314198 0
EGADS : 93 Yes 97.6079776 32.3498916 0
EGADS : 94 Yes 100.278023 41.7701593 0
EGADS : 95 Yes 94.7972887 41.7748561 0
EGADS : 96 Yes 107.397556 67.6186586 1.83668579
EGADS : 97 Yes 111.041954 67.6241096 1.25345146
EGADS : 98 Yes 111.257254 68.1412393 1.31307624
EGADS : 99 Yes 107.654637 68.146711 1.88687506
EGADS : 100 Yes 121.207308 95.9421381 4.50820234
EGADS : 101 Yes 122.837313 95.9554542 4.52004059
EGADS : 102 Yes 123.552357 97.6729236 4.7180639
EGADS : 103 Yes 118.391317 97.6729236 3.99272703
EGADS : 104 Yes 121.207308 95.9421381 4.21444802
EGADS : 105 Yes 107.654637 68.146711 0.876544084
EGADS : 106 Yes 107.397556 67.6186586 0.813033541
EGADS : 107 Yes 94.7972887 41.7748561 0
EGADS : 108 Yes 93.9108835 32.2329728 0
EGADS : 109 Yes 93.5781103 13.6748542 0
EGADS : 110 Yes 118.391317 0 3.99272703
EGADS : 111 Yes 123.552357 0 4.7180639
EGADS : 112 Yes 122.837313 0 4.52004059
EGADS : 113 Yes 121.207308 0 4.21444802
EGADS : 114 Yes 107.654637 0 0.876544084
EGADS : 115 Yes 111.257254 0 1.31307624
EGADS : 116 Yes 111.041954 0 1.25345146
EGADS : 117 Yes 107.397556 0 0.813033541
EGADS : 118 Yes 94.7972887 0 0
EGADS : 119 Yes 100.278023 0 0
EGADS : 120 Yes 93.9108835 0 0
EGADS : 121 Yes 97.6079776 0 0
EGADS : 122 Yes 93.5781103 0 0
EGADS : 123 Yes 97.1624342 0 0
EGADS : 124 Yes 93.8265357 0 0
EGADS : 125 Yes 94.2099771 0 0
EGADS : 126 Yes 94.7972887 0 0
EGADS : 127 Yes 107.397556 0 1.83668579
EGADS : 128 Yes 107.654637 0 1.88687506
EGADS : 129 Yes 121.207308 0 4.50820234
EGADS : 130 Yes 100.219054 42.1509694 0
EGADS : 131 Yes 95.2324957 41.963173 0
EGADS : 132 Yes 107.613646 67.3581332 1.77910017
EGADS : 133 Yes 110.892704 67.4707526 0.699981401
EGADS : 134 Yes 111.247925 68.471101 0.828432723
EGADS : 135 Yes 108.034544 68.3613138 1.87771912
EGADS : 136 Yes 121.36809 95.7097324 4.49194275
EGADS : 137 Yes 122.742135 95.7387605 4.2753035
EGADS : 138 Yes 121.327393 95.7291979 4.23513353
EGADS : 139 Yes 107.88707 68.4318513 0.947114671
EGADS : 140 Yes 107.462349 67.4305014 0.82436964
EGADS : 141 Yes 94.9817282 42.0831197 0
EGADS : 142 Yes 121.367879 0 4.23512504
EGADS : 143 Yes 122.701966 0 4.70778241
EGADS : 144 Yes 108.034333 0 0.936789144
EGADS : 145 Yes 111.269456 0 1.85592771
EGADS : 146 Yes 107.462349 0 0.82436964
EGADS : 147 Yes 110.892704 0 0.699981401
EGADS : 148 Yes 94.9817282 0 0
EGADS : 149 Yes 100.219054 0 0
EGADS : 150 Yes 95.2324957 0 0
EGADS : 151 Yes 107.613646 0 1.77910017
EGADS : 152 Yes 107.888388 0 1.86745513
EGADS : 153 Yes 121.327604 0 4.49195125
EGADS : 154 Yes 0 0 1962.43554
EGADS : 155 Yes 0 0 0
EGADS : 156 Yes 0 1953.45847 1962.43554
EGADS : 157 Yes 0 1953.45847 0
EGADS : 158 Yes 2040.09979 0 1962.43554
EGADS : 159 Yes 2040.09979 0 0
EGADS : 160 Yes 2040.09979 1953.45847 1962.43554
EGADS : 161 Yes 2040.09979 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 53.021
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.302
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : 23 CAD geometry 0 STD w/BL
AFLR4 : 24 CAD geometry 0 STD w/BL
AFLR4 : 25 CAD geometry 0 STD w/BL
AFLR4 : 26 CAD geometry 0 STD w/BL
AFLR4 : 27 CAD geometry 0 STD w/BL
AFLR4 : 28 CAD geometry 0 STD w/BL
AFLR4 : 29 CAD geometry 0 STD w/BL
AFLR4 : 30 CAD geometry 0 STD w/BL
AFLR4 : 31 CAD geometry 0 STD w/BL
AFLR4 : 32 CAD geometry 0 STD w/BL
AFLR4 : 33 CAD geometry 0 STD w/BL
AFLR4 : 34 CAD geometry 0 STD w/BL
AFLR4 : 35 CAD geometry 0 STD w/BL
AFLR4 : 36 CAD geometry 0 STD w/BL
AFLR4 : 37 CAD geometry 0 STD w/BL
AFLR4 : 38 CAD geometry 0 STD w/BL
AFLR4 : 39 CAD geometry 0 STD w/BL
AFLR4 : 40 CAD geometry 0 STD w/BL
AFLR4 : 41 CAD geometry 0 STD w/BL
AFLR4 : 42 CAD geometry 0 STD w/BL
AFLR4 : 43 CAD geometry 0 STD w/BL
AFLR4 : 44 CAD geometry 0 STD w/BL
AFLR4 : 45 CAD geometry 0 STD w/BL
AFLR4 : 46 CAD geometry 0 STD w/BL
AFLR4 : 47 CAD geometry 0 STD w/BL
AFLR4 : 48 CAD geometry 0 STD w/BL
AFLR4 : 49 CAD geometry 0 STD w/BL
AFLR4 : 50 CAD geometry 0 STD w/BL
AFLR4 : 51 CAD geometry 0 STD w/BL
AFLR4 : 52 CAD geometry 0 STD w/BL
AFLR4 : 53 CAD geometry 0 STD w/BL
AFLR4 : 54 CAD geometry 0 STD w/BL
AFLR4 : 55 CAD geometry 0 STD w/BL
AFLR4 : 56 CAD geometry 0 STD w/BL
AFLR4 : 57 CAD geometry 0 STD w/BL
AFLR4 : 58 CAD geometry 0 STD w/BL
AFLR4 : 59 CAD geometry 0 STD w/BL
AFLR4 : 60 CAD geometry 0 STD w/BL
AFLR4 : 61 CAD geometry 0 STD w/BL
AFLR4 : 62 CAD geometry 0 STD w/BL
AFLR4 : 63 CAD geometry 0 STD w/BL
AFLR4 : 64 CAD geometry 0 STD w/BL
AFLR4 : 65 CAD geometry 0 STD w/BL
AFLR4 : 66 CAD geometry 0 STD w/BL
AFLR4 : 67 CAD geometry 0 STD w/BL
AFLR4 : 68 CAD geometry 0 STD w/BL
AFLR4 : 69 CAD geometry 0 STD w/BL
AFLR4 : 70 CAD geometry 0 STD w/BL
AFLR4 : 71 CAD geometry 0 STD w/BL
AFLR4 : 72 CAD geometry 0 STD w/BL
AFLR4 : 73 CAD geometry 0 STD w/BL
AFLR4 : 74 CAD geometry 0 STD w/BL
AFLR4 : 75 CAD geometry 0 STD w/BL
AFLR4 : 76 CAD geometry 0 STD w/BL
AFLR4 : 77 CAD geometry 0 STD w/BL
AFLR4 : 78 CAD geometry 0 STD w/BL
AFLR4 : 79 CAD geometry 0 STD w/BL
AFLR4 : 80 CAD geometry 0 STD w/BL
AFLR4 : 81 CAD geometry 0 STD w/BL
AFLR4 : 82 CAD geometry 0 STD w/BL
AFLR4 : 83 CAD geometry 0 STD w/BL
AFLR4 : 84 CAD geometry 0 STD w/BL
AFLR4 : 85 CAD geometry 0 STD w/BL
AFLR4 : 86 CAD geometry 0 STD w/BL
AFLR4 : 87 CAD geometry 0 STD w/BL
AFLR4 : 88 CAD geometry 0 STD w/BL
AFLR4 : 89 CAD geometry 0 STD w/BL
AFLR4 : 90 CAD geometry 0 STD w/BL
AFLR4 : 91 CAD geometry 0 STD w/BL
AFLR4 : 92 CAD geometry 0 STD w/BL
AFLR4 : 93 CAD geometry 0 STD w/BL
AFLR4 : 94 CAD geometry 0 STD w/BL
AFLR4 : 95 CAD geometry 0 STD w/BL
AFLR4 : 96 CAD geometry 0 STD w/BL
AFLR4 : 97 CAD geometry 0 STD w/BL
AFLR4 : 98 CAD geometry 0 STD w/BL
AFLR4 : 99 CAD geometry 0 STD w/BL
AFLR4 : 100 CAD geometry 0 STD w/BL
AFLR4 : 101 CAD geometry 0 STD w/BL
AFLR4 : 102 CAD geometry 0 STD w/BL
AFLR4 : 103 CAD geometry 0 STD w/BL
AFLR4 : 104 CAD geometry 0 STD w/BL
AFLR4 : 105 CAD geometry 0 STD w/BL
AFLR4 : 106 CAD geometry 0 STD w/BL
AFLR4 : 107 CAD geometry 0 STD w/BL
AFLR4 : 108 CAD geometry 0 STD w/BL
AFLR4 : 109 CAD geometry 0 FARFIELD
AFLR4 : 110 CAD geometry 0 FARFIELD
AFLR4 : 111 CAD geometry 0 FARFIELD
AFLR4 : 112 CAD geometry 0 FARFIELD
AFLR4 : 113 CAD geometry 0 FARFIELD
AFLR4 : 114 CAD geometry 0 FARFIELD
AFLR4 : Case has 5 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 23 24 28 29 30 31 33 36 40
AFLR4 : Component 2 includes Definitions 37 38 49 50 51 52 53 54 55 56 57 58
AFLR4 : 61 62 63 64 65 66 67 68 69 70 71 72
AFLR4 : 73 74 75 76 77 78 79 80 81 82 83 84
AFLR4 : 85 86 87 88 89 90 91 92 93 94 95 96
AFLR4 : 97 98 99 100 101 102 103 104 105 106
AFLR4 : Component 3 includes Definitions 15 16 17 18 19 20 21 22 25 26 27 34
AFLR4 : 35 42 43 44 45 46 47 48 59 60
AFLR4 : Component 4 includes Definitions 9 10 11 12 13 14 32 39 41 107 108
AFLR4 : Component 5 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR4 : Define CAD surface definition 25
AFLR4 : Define CAD surface definition 26
AFLR4 : Define CAD surface definition 27
AFLR4 : Define CAD surface definition 28
AFLR4 : Define CAD surface definition 29
AFLR4 : Define CAD surface definition 30
AFLR4 : Define CAD surface definition 31
AFLR4 : Define CAD surface definition 32
AFLR4 : Define CAD surface definition 33
AFLR4 : Define CAD surface definition 34
AFLR4 : Define CAD surface definition 35
AFLR4 : Define CAD surface definition 36
AFLR4 : Define CAD surface definition 37
AFLR4 : Define CAD surface definition 38
AFLR4 : Define CAD surface definition 39
AFLR4 : Define CAD surface definition 40
AFLR4 : Define CAD surface definition 41
AFLR4 : Define CAD surface definition 42
AFLR4 : Define CAD surface definition 43
AFLR4 : Define CAD surface definition 44
AFLR4 : Define CAD surface definition 45
AFLR4 : Define CAD surface definition 46
AFLR4 : Define CAD surface definition 47
AFLR4 : Define CAD surface definition 48
AFLR4 : Define CAD surface definition 49
AFLR4 : Define CAD surface definition 50
AFLR4 : Define CAD surface definition 51
AFLR4 : Define CAD surface definition 52
AFLR4 : Define CAD surface definition 53
AFLR4 : Define CAD surface definition 54
AFLR4 : Define CAD surface definition 55
AFLR4 : Define CAD surface definition 56
AFLR4 : Define CAD surface definition 57
AFLR4 : Define CAD surface definition 58
AFLR4 : Define CAD surface definition 59
AFLR4 : Define CAD surface definition 60
AFLR4 : Define CAD surface definition 61
AFLR4 : Define CAD surface definition 62
AFLR4 : Define CAD surface definition 63
AFLR4 : Define CAD surface definition 64
AFLR4 : Define CAD surface definition 65
AFLR4 : Define CAD surface definition 66
AFLR4 : Define CAD surface definition 67
AFLR4 : Define CAD surface definition 68
AFLR4 : Define CAD surface definition 69
AFLR4 : Define CAD surface definition 70
AFLR4 : Define CAD surface definition 71
AFLR4 : Define CAD surface definition 72
AFLR4 : Define CAD surface definition 73
AFLR4 : Define CAD surface definition 74
AFLR4 : Define CAD surface definition 75
AFLR4 : Define CAD surface definition 76
AFLR4 : Define CAD surface definition 77
AFLR4 : Define CAD surface definition 78
AFLR4 : Define CAD surface definition 79
AFLR4 : Define CAD surface definition 80
AFLR4 : Define CAD surface definition 81
AFLR4 : Define CAD surface definition 82
AFLR4 : Define CAD surface definition 83
AFLR4 : Define CAD surface definition 84
AFLR4 : Define CAD surface definition 85
AFLR4 : Define CAD surface definition 86
AFLR4 : Define CAD surface definition 87
AFLR4 : Define CAD surface definition 88
AFLR4 : Define CAD surface definition 89
AFLR4 : Define CAD surface definition 90
AFLR4 : Define CAD surface definition 91
AFLR4 : Define CAD surface definition 92
AFLR4 : Define CAD surface definition 93
AFLR4 : Define CAD surface definition 94
AFLR4 : Define CAD surface definition 95
AFLR4 : Define CAD surface definition 96
AFLR4 : Define CAD surface definition 97
AFLR4 : Define CAD surface definition 98
AFLR4 : Define CAD surface definition 99
AFLR4 : Define CAD surface definition 100
AFLR4 : Define CAD surface definition 101
AFLR4 : Define CAD surface definition 102
AFLR4 : Define CAD surface definition 103
AFLR4 : Define CAD surface definition 104
AFLR4 : Define CAD surface definition 105
AFLR4 : Define CAD surface definition 106
AFLR4 : Define CAD surface definition 107
AFLR4 : Define CAD surface definition 108
AFLR4 : Define CAD surface definition 109
AFLR4 : Define CAD surface definition 110
AFLR4 : Define CAD surface definition 111
AFLR4 : Define CAD surface definition 112
AFLR4 : Define CAD surface definition 113
AFLR4 : Define CAD surface definition 114
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 339 605 0
AFLR4 : Nodes, Trias,Quads= 362 651 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 319 563 0
AFLR4 : Nodes, Trias,Quads= 284 493 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 340 607 0
AFLR4 : Nodes, Trias,Quads= 362 651 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 321 567 0
AFLR4 : Nodes, Trias,Quads= 284 493 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 340 607 0
AFLR4 : Nodes, Trias,Quads= 362 651 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 321 567 0
AFLR4 : Nodes, Trias,Quads= 284 493 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 339 605 0
AFLR4 : Nodes, Trias,Quads= 362 651 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 319 563 0
AFLR4 : Nodes, Trias,Quads= 284 493 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 15 19 0
AFLR4 : Nodes, Trias,Quads= 9 7 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 15 19 0
AFLR4 : Nodes, Trias,Quads= 9 7 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 47 65 0
AFLR4 : Nodes, Trias,Quads= 27 25 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 24 31 0
AFLR4 : Nodes, Trias,Quads= 23 29 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 24 31 0
AFLR4 : Nodes, Trias,Quads= 22 27 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 47 65 0
AFLR4 : Nodes, Trias,Quads= 27 25 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 51 67 0
AFLR4 : Nodes, Trias,Quads= 58 81 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 1615 3003 0
AFLR4 : Nodes, Trias,Quads= 1188 2149 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 90 127 0
AFLR4 : Nodes, Trias,Quads= 51 49 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 216 367 0
AFLR4 : Nodes, Trias,Quads= 174 283 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 51 67 0
AFLR4 : Nodes, Trias,Quads= 51 67 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 1677 3126 0
AFLR4 : Nodes, Trias,Quads= 1210 2192 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 35 44 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 9 9 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 907 1650 0
AFLR4 : Nodes, Trias,Quads= 569 974 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 3270 6232 0
AFLR4 : Nodes, Trias,Quads= 1907 3506 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 220 375 0
AFLR4 : Nodes, Trias,Quads= 176 287 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 80 108 0
AFLR4 : Nodes, Trias,Quads= 50 48 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 902 1640 0
AFLR4 : Nodes, Trias,Quads= 561 958 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 106 170 0
AFLR4 : Nodes, Trias,Quads= 106 170 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 1586 2835 0
AFLR4 : Nodes, Trias,Quads= 1651 2965 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 3418 6528 0
AFLR4 : Nodes, Trias,Quads= 1888 3468 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 1868 3486 0
AFLR4 : Nodes, Trias,Quads= 1347 2444 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 1025 1836 0
AFLR4 : Nodes, Trias,Quads= 1213 2212 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 1436 2654 0
AFLR4 : Nodes, Trias,Quads= 979 1740 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 1684 3140 0
AFLR4 : Nodes, Trias,Quads= 1216 2204 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 1579 2821 0
AFLR4 : Nodes, Trias,Quads= 1648 2959 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 2154 4060 0
AFLR4 : Nodes, Trias,Quads= 2140 4032 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 2585 4915 0
AFLR4 : Nodes, Trias,Quads= 2189 4123 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 1916 3582 0
AFLR4 : Nodes, Trias,Quads= 1367 2484 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 1026 1838 0
AFLR4 : Nodes, Trias,Quads= 1215 2216 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 47 60 0
AFLR4 : Nodes, Trias,Quads= 32 30 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 35 44 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 9 9 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 59 84 0
AFLR4 : Nodes, Trias,Quads= 32 30 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 41 53 0
AFLR4 : Nodes, Trias,Quads= 48 67 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 51 67 0
AFLR4 : Nodes, Trias,Quads= 50 65 0
AFLR4 : Generate optimal mesh on surface definition 47
AFLR2 : Nodes, Trias,Quads= 80 108 0
AFLR4 : Nodes, Trias,Quads= 50 48 0
AFLR4 : Generate optimal mesh on surface definition 48
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Generate optimal mesh on surface definition 49
AFLR2 : Nodes, Trias,Quads= 2582 4909 0
AFLR4 : Nodes, Trias,Quads= 2199 4143 0
AFLR4 : Generate optimal mesh on surface definition 50
AFLR2 : Nodes, Trias,Quads= 2158 4068 0
AFLR4 : Nodes, Trias,Quads= 2139 4030 0
AFLR4 : Generate optimal mesh on surface definition 51
AFLR2 : Nodes, Trias,Quads= 46 65 0
AFLR4 : Nodes, Trias,Quads= 39 51 0
AFLR4 : Generate optimal mesh on surface definition 52
AFLR2 : Nodes, Trias,Quads= 108 144 0
AFLR4 : Nodes, Trias,Quads= 102 132 0
AFLR4 : Generate optimal mesh on surface definition 53
AFLR2 : Nodes, Trias,Quads= 46 65 0
AFLR4 : Nodes, Trias,Quads= 39 51 0
AFLR4 : Generate optimal mesh on surface definition 54
AFLR2 : Nodes, Trias,Quads= 3787 7224 0
AFLR4 : Nodes, Trias,Quads= 2368 4386 0
AFLR4 : Generate optimal mesh on surface definition 55
AFLR2 : Nodes, Trias,Quads= 3490 6642 0
AFLR4 : Nodes, Trias,Quads= 2094 3850 0
AFLR4 : Generate optimal mesh on surface definition 56
AFLR2 : Nodes, Trias,Quads= 74 114 0
AFLR4 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Generate optimal mesh on surface definition 57
AFLR2 : Nodes, Trias,Quads= 148 206 0
AFLR4 : Nodes, Trias,Quads= 111 132 0
AFLR4 : Generate optimal mesh on surface definition 58
AFLR2 : Nodes, Trias,Quads= 70 107 0
AFLR4 : Nodes, Trias,Quads= 49 65 0
AFLR4 : Generate optimal mesh on surface definition 59
AFLR2 : Nodes, Trias,Quads= 130 209 0
AFLR4 : Nodes, Trias,Quads= 94 137 0
AFLR4 : Generate optimal mesh on surface definition 60
AFLR2 : Nodes, Trias,Quads= 215 365 0
AFLR4 : Nodes, Trias,Quads= 176 287 0
AFLR4 : Generate optimal mesh on surface definition 61
AFLR2 : Nodes, Trias,Quads= 3535 6727 0
AFLR4 : Nodes, Trias,Quads= 2180 4017 0
AFLR4 : Generate optimal mesh on surface definition 62
AFLR2 : Nodes, Trias,Quads= 74 114 0
AFLR4 : Nodes, Trias,Quads= 48 62 0
AFLR4 : Generate optimal mesh on surface definition 63
AFLR2 : Nodes, Trias,Quads= 148 206 0
AFLR4 : Nodes, Trias,Quads= 111 132 0
AFLR4 : Generate optimal mesh on surface definition 64
AFLR2 : Nodes, Trias,Quads= 70 107 0
AFLR4 : Nodes, Trias,Quads= 49 65 0
AFLR4 : Generate optimal mesh on surface definition 65
AFLR2 : Nodes, Trias,Quads= 46 65 0
AFLR4 : Nodes, Trias,Quads= 39 51 0
AFLR4 : Generate optimal mesh on surface definition 66
AFLR2 : Nodes, Trias,Quads= 108 144 0
AFLR4 : Nodes, Trias,Quads= 94 116 0
AFLR4 : Generate optimal mesh on surface definition 67
AFLR2 : Nodes, Trias,Quads= 46 65 0
AFLR4 : Nodes, Trias,Quads= 39 51 0
AFLR4 : Generate optimal mesh on surface definition 68
AFLR2 : Nodes, Trias,Quads= 3573 6801 0
AFLR4 : Nodes, Trias,Quads= 2281 4217 0
AFLR4 : Generate optimal mesh on surface definition 69
AFLR2 : Nodes, Trias,Quads= 245 414 0
AFLR4 : Nodes, Trias,Quads= 224 372 0
AFLR4 : Generate optimal mesh on surface definition 70
AFLR2 : Nodes, Trias,Quads= 50 67 0
AFLR4 : Nodes, Trias,Quads= 51 69 0
AFLR4 : Generate optimal mesh on surface definition 71
AFLR2 : Nodes, Trias,Quads= 114 155 0
AFLR4 : Nodes, Trias,Quads= 78 83 0
AFLR4 : Generate optimal mesh on surface definition 72
AFLR2 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Nodes, Trias,Quads= 31 42 0
AFLR4 : Generate optimal mesh on surface definition 73
AFLR2 : Nodes, Trias,Quads= 39 50 0
AFLR4 : Nodes, Trias,Quads= 42 56 0
AFLR4 : Generate optimal mesh on surface definition 74
AFLR2 : Nodes, Trias,Quads= 157 216 0
AFLR4 : Nodes, Trias,Quads= 141 184 0
AFLR4 : Generate optimal mesh on surface definition 75
AFLR2 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Generate optimal mesh on surface definition 76
AFLR2 : Nodes, Trias,Quads= 36 49 0
AFLR4 : Nodes, Trias,Quads= 21 19 0
AFLR4 : Generate optimal mesh on surface definition 77
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Generate optimal mesh on surface definition 78
AFLR2 : Nodes, Trias,Quads= 148 208 0
AFLR4 : Nodes, Trias,Quads= 86 84 0
AFLR4 : Generate optimal mesh on surface definition 79
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 33 44 0
AFLR4 : Generate optimal mesh on surface definition 80
AFLR2 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Nodes, Trias,Quads= 30 40 0
AFLR4 : Generate optimal mesh on surface definition 81
AFLR2 : Nodes, Trias,Quads= 111 158 0
AFLR4 : Nodes, Trias,Quads= 65 66 0
AFLR4 : Generate optimal mesh on surface definition 82
AFLR2 : Nodes, Trias,Quads= 33 41 0
AFLR4 : Nodes, Trias,Quads= 40 55 0
AFLR4 : Generate optimal mesh on surface definition 83
AFLR2 : Nodes, Trias,Quads= 328 564 0
AFLR4 : Nodes, Trias,Quads= 305 518 0
AFLR4 : Generate optimal mesh on surface definition 84
AFLR2 : Nodes, Trias,Quads= 36 49 0
AFLR4 : Nodes, Trias,Quads= 21 19 0
AFLR4 : Generate optimal mesh on surface definition 85
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 34 45 0
AFLR4 : Generate optimal mesh on surface definition 86
AFLR2 : Nodes, Trias,Quads= 157 216 0
AFLR4 : Nodes, Trias,Quads= 119 140 0
AFLR4 : Generate optimal mesh on surface definition 87
AFLR2 : Nodes, Trias,Quads= 39 51 0
AFLR4 : Nodes, Trias,Quads= 43 59 0
AFLR4 : Generate optimal mesh on surface definition 88
AFLR2 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Nodes, Trias,Quads= 30 40 0
AFLR4 : Generate optimal mesh on surface definition 89
AFLR2 : Nodes, Trias,Quads= 111 158 0
AFLR4 : Nodes, Trias,Quads= 65 66 0
AFLR4 : Generate optimal mesh on surface definition 90
AFLR2 : Nodes, Trias,Quads= 33 41 0
AFLR4 : Nodes, Trias,Quads= 40 55 0
AFLR4 : Generate optimal mesh on surface definition 91
AFLR2 : Nodes, Trias,Quads= 329 566 0
AFLR4 : Nodes, Trias,Quads= 305 518 0
AFLR4 : Generate optimal mesh on surface definition 92
AFLR2 : Nodes, Trias,Quads= 245 414 0
AFLR4 : Nodes, Trias,Quads= 225 374 0
AFLR4 : Generate optimal mesh on surface definition 93
AFLR2 : Nodes, Trias,Quads= 50 67 0
AFLR4 : Nodes, Trias,Quads= 51 69 0
AFLR4 : Generate optimal mesh on surface definition 94
AFLR2 : Nodes, Trias,Quads= 114 155 0
AFLR4 : Nodes, Trias,Quads= 78 83 0
AFLR4 : Generate optimal mesh on surface definition 95
AFLR2 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Nodes, Trias,Quads= 31 42 0
AFLR4 : Generate optimal mesh on surface definition 96
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 35 47 0
AFLR4 : Generate optimal mesh on surface definition 97
AFLR2 : Nodes, Trias,Quads= 148 208 0
AFLR4 : Nodes, Trias,Quads= 112 136 0
AFLR4 : Generate optimal mesh on surface definition 98
AFLR2 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Generate optimal mesh on surface definition 99
AFLR2 : Nodes, Trias,Quads= 251 422 0
AFLR4 : Nodes, Trias,Quads= 208 336 0
AFLR4 : Generate optimal mesh on surface definition 100
AFLR2 : Nodes, Trias,Quads= 332 556 0
AFLR4 : Nodes, Trias,Quads= 250 392 0
AFLR4 : Generate optimal mesh on surface definition 101
AFLR2 : Nodes, Trias,Quads= 295 490 0
AFLR4 : Nodes, Trias,Quads= 216 332 0
AFLR4 : Generate optimal mesh on surface definition 102
AFLR2 : Nodes, Trias,Quads= 207 341 0
AFLR4 : Nodes, Trias,Quads= 174 275 0
AFLR4 : Generate optimal mesh on surface definition 103
AFLR2 : Nodes, Trias,Quads= 327 547 0
AFLR4 : Nodes, Trias,Quads= 240 373 0
AFLR4 : Generate optimal mesh on surface definition 104
AFLR2 : Nodes, Trias,Quads= 208 343 0
AFLR4 : Nodes, Trias,Quads= 173 273 0
AFLR4 : Generate optimal mesh on surface definition 105
AFLR2 : Nodes, Trias,Quads= 248 416 0
AFLR4 : Nodes, Trias,Quads= 208 336 0
AFLR4 : Generate optimal mesh on surface definition 106
AFLR2 : Nodes, Trias,Quads= 297 493 0
AFLR4 : Nodes, Trias,Quads= 225 349 0
AFLR4 : Generate optimal mesh on surface definition 107
AFLR2 : Nodes, Trias,Quads= 40 57 0
AFLR4 : Nodes, Trias,Quads= 30 37 0
AFLR4 : Generate optimal mesh on surface definition 108
AFLR2 : Nodes, Trias,Quads= 40 57 0
AFLR4 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Generate optimal mesh on surface definition 109
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 110
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 111
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 112
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 113
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 114
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 39758 79508 9980
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 39758 79508
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 397 713 0
AFLR4 : Nodes, Trias,Quads= 416 751 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 387 691 0
AFLR4 : Nodes, Trias,Quads= 346 609 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 396 711 0
AFLR4 : Nodes, Trias,Quads= 417 753 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 388 693 0
AFLR4 : Nodes, Trias,Quads= 344 605 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 395 709 0
AFLR4 : Nodes, Trias,Quads= 416 751 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 388 693 0
AFLR4 : Nodes, Trias,Quads= 344 605 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 395 709 0
AFLR4 : Nodes, Trias,Quads= 416 751 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 387 691 0
AFLR4 : Nodes, Trias,Quads= 346 609 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 18 23 0
AFLR4 : Nodes, Trias,Quads= 11 9 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 18 23 0
AFLR4 : Nodes, Trias,Quads= 11 9 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 56 77 0
AFLR4 : Nodes, Trias,Quads= 33 31 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 28 37 0
AFLR4 : Nodes, Trias,Quads= 25 31 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 29 38 0
AFLR4 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 56 77 0
AFLR4 : Nodes, Trias,Quads= 33 31 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 60 80 0
AFLR4 : Nodes, Trias,Quads= 59 78 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 1730 3226 0
AFLR4 : Nodes, Trias,Quads= 1387 2540 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 100 140 0
AFLR4 : Nodes, Trias,Quads= 58 56 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 271 470 0
AFLR4 : Nodes, Trias,Quads= 208 344 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 57 75 0
AFLR4 : Nodes, Trias,Quads= 61 83 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 1821 3408 0
AFLR4 : Nodes, Trias,Quads= 1413 2592 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 38 49 0
AFLR4 : Nodes, Trias,Quads= 25 23 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 15 19 0
AFLR4 : Nodes, Trias,Quads= 15 19 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 1020 1868 0
AFLR4 : Nodes, Trias,Quads= 1567 2962 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 3285 6257 0
AFLR4 : Nodes, Trias,Quads= 2653 4993 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 268 463 0
AFLR4 : Nodes, Trias,Quads= 211 349 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 96 133 0
AFLR4 : Nodes, Trias,Quads= 57 55 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 15 18 0
AFLR4 : Nodes, Trias,Quads= 15 18 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 1004 1837 0
AFLR4 : Nodes, Trias,Quads= 1550 2929 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 106 170 0
AFLR4 : Nodes, Trias,Quads= 116 190 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 1641 2940 0
AFLR4 : Nodes, Trias,Quads= 3186 6030 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 3518 6723 0
AFLR4 : Nodes, Trias,Quads= 2633 4953 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 2078 3899 0
AFLR4 : Nodes, Trias,Quads= 1693 3129 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 1088 1956 0
AFLR4 : Nodes, Trias,Quads= 2728 5236 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 1551 2878 0
AFLR4 : Nodes, Trias,Quads= 1231 2238 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 1791 3350 0
AFLR4 : Nodes, Trias,Quads= 1415 2598 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 1642 2942 0
AFLR4 : Nodes, Trias,Quads= 3182 6022 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 2194 4132 0
AFLR4 : Nodes, Trias,Quads= 2357 4458 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 3014 5761 0
AFLR4 : Nodes, Trias,Quads= 2581 4895 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 2124 3993 0
AFLR4 : Nodes, Trias,Quads= 1733 3211 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 1089 1958 0
AFLR4 : Nodes, Trias,Quads= 2719 5218 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 60 81 0
AFLR4 : Nodes, Trias,Quads= 37 35 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 37 47 0
AFLR4 : Nodes, Trias,Quads= 25 23 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 15 18 0
AFLR4 : Nodes, Trias,Quads= 16 20 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 71 100 0
AFLR4 : Nodes, Trias,Quads= 40 38 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 48 63 0
AFLR4 : Nodes, Trias,Quads= 51 69 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 57 75 0
AFLR4 : Nodes, Trias,Quads= 62 85 0
AFLR4 : Generate optimal mesh on surface definition 47
AFLR2 : Nodes, Trias,Quads= 85 111 0
AFLR4 : Nodes, Trias,Quads= 57 55 0
AFLR4 : Generate optimal mesh on surface definition 48
AFLR2 : Nodes, Trias,Quads= 15 18 0
AFLR4 : Nodes, Trias,Quads= 15 18 0
AFLR4 : Generate optimal mesh on surface definition 49
AFLR2 : Nodes, Trias,Quads= 3046 5824 0
AFLR4 : Nodes, Trias,Quads= 2604 4940 0
AFLR4 : Generate optimal mesh on surface definition 50
AFLR2 : Nodes, Trias,Quads= 2207 4159 0
AFLR4 : Nodes, Trias,Quads= 2346 4437 0
AFLR4 : Generate optimal mesh on surface definition 51
AFLR2 : Nodes, Trias,Quads= 53 77 0
AFLR4 : Nodes, Trias,Quads= 41 53 0
AFLR4 : Generate optimal mesh on surface definition 52
AFLR2 : Nodes, Trias,Quads= 121 160 0
AFLR4 : Nodes, Trias,Quads= 99 116 0
AFLR4 : Generate optimal mesh on surface definition 53
AFLR2 : Nodes, Trias,Quads= 55 80 0
AFLR4 : Nodes, Trias,Quads= 44 58 0
AFLR4 : Generate optimal mesh on surface definition 54
AFLR2 : Nodes, Trias,Quads= 4380 8388 0
AFLR4 : Nodes, Trias,Quads= 2756 5140 0
AFLR4 : Generate optimal mesh on surface definition 55
AFLR2 : Nodes, Trias,Quads= 3996 7635 0
AFLR4 : Nodes, Trias,Quads= 2397 4437 0
AFLR4 : Generate optimal mesh on surface definition 56
AFLR2 : Nodes, Trias,Quads= 78 120 0
AFLR4 : Nodes, Trias,Quads= 51 66 0
AFLR4 : Generate optimal mesh on surface definition 57
AFLR2 : Nodes, Trias,Quads= 164 223 0
AFLR4 : Nodes, Trias,Quads= 162 219 0
AFLR4 : Generate optimal mesh on surface definition 58
AFLR2 : Nodes, Trias,Quads= 73 112 0
AFLR4 : Nodes, Trias,Quads= 48 62 0
AFLR4 : Generate optimal mesh on surface definition 59
AFLR2 : Nodes, Trias,Quads= 175 291 0
AFLR4 : Nodes, Trias,Quads= 161 263 0
AFLR4 : Generate optimal mesh on surface definition 60
AFLR2 : Nodes, Trias,Quads= 260 448 0
AFLR4 : Nodes, Trias,Quads= 208 344 0
AFLR4 : Generate optimal mesh on surface definition 61
AFLR2 : Nodes, Trias,Quads= 4125 7885 0
AFLR4 : Nodes, Trias,Quads= 2505 4645 0
AFLR4 : Generate optimal mesh on surface definition 62
AFLR2 : Nodes, Trias,Quads= 78 120 0
AFLR4 : Nodes, Trias,Quads= 51 66 0
AFLR4 : Generate optimal mesh on surface definition 63
AFLR2 : Nodes, Trias,Quads= 175 244 0
AFLR4 : Nodes, Trias,Quads= 163 220 0
AFLR4 : Generate optimal mesh on surface definition 64
AFLR2 : Nodes, Trias,Quads= 73 112 0
AFLR4 : Nodes, Trias,Quads= 48 62 0
AFLR4 : Generate optimal mesh on surface definition 65
AFLR2 : Nodes, Trias,Quads= 53 77 0
AFLR4 : Nodes, Trias,Quads= 41 53 0
AFLR4 : Generate optimal mesh on surface definition 66
AFLR2 : Nodes, Trias,Quads= 124 169 0
AFLR4 : Nodes, Trias,Quads= 111 143 0
AFLR4 : Generate optimal mesh on surface definition 67
AFLR2 : Nodes, Trias,Quads= 56 82 0
AFLR4 : Nodes, Trias,Quads= 43 56 0
AFLR4 : Generate optimal mesh on surface definition 68
AFLR2 : Nodes, Trias,Quads= 4113 7862 0
AFLR4 : Nodes, Trias,Quads= 2649 4934 0
AFLR4 : Generate optimal mesh on surface definition 69
AFLR2 : Nodes, Trias,Quads= 300 515 0
AFLR4 : Nodes, Trias,Quads= 283 481 0
AFLR4 : Generate optimal mesh on surface definition 70
AFLR2 : Nodes, Trias,Quads= 57 78 0
AFLR4 : Nodes, Trias,Quads= 55 74 0
AFLR4 : Generate optimal mesh on surface definition 71
AFLR2 : Nodes, Trias,Quads= 135 188 0
AFLR4 : Nodes, Trias,Quads= 87 92 0
AFLR4 : Generate optimal mesh on surface definition 72
AFLR2 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Nodes, Trias,Quads= 36 48 0
AFLR4 : Generate optimal mesh on surface definition 73
AFLR2 : Nodes, Trias,Quads= 43 55 0
AFLR4 : Nodes, Trias,Quads= 44 57 0
AFLR4 : Generate optimal mesh on surface definition 74
AFLR2 : Nodes, Trias,Quads= 186 257 0
AFLR4 : Nodes, Trias,Quads= 180 245 0
AFLR4 : Generate optimal mesh on surface definition 75
AFLR2 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Generate optimal mesh on surface definition 76
AFLR2 : Nodes, Trias,Quads= 39 53 0
AFLR4 : Nodes, Trias,Quads= 23 21 0
AFLR4 : Generate optimal mesh on surface definition 77
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Generate optimal mesh on surface definition 78
AFLR2 : Nodes, Trias,Quads= 169 238 0
AFLR4 : Nodes, Trias,Quads= 101 102 0
AFLR4 : Generate optimal mesh on surface definition 79
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 36 48 0
AFLR4 : Generate optimal mesh on surface definition 80
AFLR2 : Nodes, Trias,Quads= 33 43 0
AFLR4 : Nodes, Trias,Quads= 36 49 0
AFLR4 : Generate optimal mesh on surface definition 81
AFLR2 : Nodes, Trias,Quads= 132 188 0
AFLR4 : Nodes, Trias,Quads= 79 82 0
AFLR4 : Generate optimal mesh on surface definition 82
AFLR2 : Nodes, Trias,Quads= 40 51 0
AFLR4 : Nodes, Trias,Quads= 46 63 0
AFLR4 : Generate optimal mesh on surface definition 83
AFLR2 : Nodes, Trias,Quads= 402 701 0
AFLR4 : Nodes, Trias,Quads= 405 707 0
AFLR4 : Generate optimal mesh on surface definition 84
AFLR2 : Nodes, Trias,Quads= 39 53 0
AFLR4 : Nodes, Trias,Quads= 23 21 0
AFLR4 : Generate optimal mesh on surface definition 85
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Generate optimal mesh on surface definition 86
AFLR2 : Nodes, Trias,Quads= 186 260 0
AFLR4 : Nodes, Trias,Quads= 140 168 0
AFLR4 : Generate optimal mesh on surface definition 87
AFLR2 : Nodes, Trias,Quads= 42 54 0
AFLR4 : Nodes, Trias,Quads= 48 66 0
AFLR4 : Generate optimal mesh on surface definition 88
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 37 50 0
AFLR4 : Generate optimal mesh on surface definition 89
AFLR2 : Nodes, Trias,Quads= 132 188 0
AFLR4 : Nodes, Trias,Quads= 79 82 0
AFLR4 : Generate optimal mesh on surface definition 90
AFLR2 : Nodes, Trias,Quads= 40 51 0
AFLR4 : Nodes, Trias,Quads= 45 61 0
AFLR4 : Generate optimal mesh on surface definition 91
AFLR2 : Nodes, Trias,Quads= 401 699 0
AFLR4 : Nodes, Trias,Quads= 404 705 0
AFLR4 : Generate optimal mesh on surface definition 92
AFLR2 : Nodes, Trias,Quads= 293 502 0
AFLR4 : Nodes, Trias,Quads= 277 470 0
AFLR4 : Generate optimal mesh on surface definition 93
AFLR2 : Nodes, Trias,Quads= 57 78 0
AFLR4 : Nodes, Trias,Quads= 55 74 0
AFLR4 : Generate optimal mesh on surface definition 94
AFLR2 : Nodes, Trias,Quads= 135 188 0
AFLR4 : Nodes, Trias,Quads= 87 92 0
AFLR4 : Generate optimal mesh on surface definition 95
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 35 47 0
AFLR4 : Generate optimal mesh on surface definition 96
AFLR2 : Nodes, Trias,Quads= 34 43 0
AFLR4 : Nodes, Trias,Quads= 36 47 0
AFLR4 : Generate optimal mesh on surface definition 97
AFLR2 : Nodes, Trias,Quads= 175 245 0
AFLR4 : Nodes, Trias,Quads= 139 173 0
AFLR4 : Generate optimal mesh on surface definition 98
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Generate optimal mesh on surface definition 99
AFLR2 : Nodes, Trias,Quads= 303 516 0
AFLR4 : Nodes, Trias,Quads= 258 426 0
AFLR4 : Generate optimal mesh on surface definition 100
AFLR2 : Nodes, Trias,Quads= 380 642 0
AFLR4 : Nodes, Trias,Quads= 285 452 0
AFLR4 : Generate optimal mesh on surface definition 101
AFLR2 : Nodes, Trias,Quads= 334 560 0
AFLR4 : Nodes, Trias,Quads= 242 376 0
AFLR4 : Generate optimal mesh on surface definition 102
AFLR2 : Nodes, Trias,Quads= 271 457 0
AFLR4 : Nodes, Trias,Quads= 222 359 0
AFLR4 : Generate optimal mesh on surface definition 103
AFLR2 : Nodes, Trias,Quads= 369 622 0
AFLR4 : Nodes, Trias,Quads= 275 434 0
AFLR4 : Generate optimal mesh on surface definition 104
AFLR2 : Nodes, Trias,Quads= 272 459 0
AFLR4 : Nodes, Trias,Quads= 220 355 0
AFLR4 : Generate optimal mesh on surface definition 105
AFLR2 : Nodes, Trias,Quads= 303 516 0
AFLR4 : Nodes, Trias,Quads= 258 426 0
AFLR4 : Generate optimal mesh on surface definition 106
AFLR2 : Nodes, Trias,Quads= 353 594 0
AFLR4 : Nodes, Trias,Quads= 266 420 0
AFLR4 : Generate optimal mesh on surface definition 107
AFLR2 : Nodes, Trias,Quads= 72 113 0
AFLR4 : Nodes, Trias,Quads= 47 63 0
AFLR4 : Generate optimal mesh on surface definition 108
AFLR2 : Nodes, Trias,Quads= 70 109 0
AFLR4 : Nodes, Trias,Quads= 49 67 0
AFLR4 : Generate optimal mesh on surface definition 109
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 110
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 111
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 112
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 113
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 114
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 54881 109754 10706
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 57112 114216
AFLR4 : Nodes, Trias = 57416 114824
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 779 1451 0
AFLR4 : Nodes, Trias,Quads= 643 1179 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 399 711 0
AFLR4 : Nodes, Trias,Quads= 375 663 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 753 1402 0
AFLR4 : Nodes, Trias,Quads= 682 1260 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 388 692 0
AFLR4 : Nodes, Trias,Quads= 357 630 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 773 1439 0
AFLR4 : Nodes, Trias,Quads= 640 1173 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 400 713 0
AFLR4 : Nodes, Trias,Quads= 373 659 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 751 1398 0
AFLR4 : Nodes, Trias,Quads= 681 1258 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 388 692 0
AFLR4 : Nodes, Trias,Quads= 358 632 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 21 27 0
AFLR4 : Nodes, Trias,Quads= 18 21 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 21 27 0
AFLR4 : Nodes, Trias,Quads= 20 25 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 66 90 0
AFLR4 : Nodes, Trias,Quads= 40 38 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 32 43 0
AFLR4 : Nodes, Trias,Quads= 29 37 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 32 43 0
AFLR4 : Nodes, Trias,Quads= 28 35 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 65 89 0
AFLR4 : Nodes, Trias,Quads= 39 37 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 61 80 0
AFLR4 : Nodes, Trias,Quads= 62 82 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2575 4845 0
AFLR4 : Nodes, Trias,Quads= 2031 3757 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 109 150 0
AFLR4 : Nodes, Trias,Quads= 66 64 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 298 518 0
AFLR4 : Nodes, Trias,Quads= 228 378 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 62 81 0
AFLR4 : Nodes, Trias,Quads= 62 81 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 2640 4977 0
AFLR4 : Nodes, Trias,Quads= 2128 3953 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 39 50 0
AFLR4 : Nodes, Trias,Quads= 26 24 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 19 25 0
AFLR4 : Nodes, Trias,Quads= 19 25 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 2175 4085 0
AFLR4 : Nodes, Trias,Quads= 1917 3569 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 4841 9257 0
AFLR4 : Nodes, Trias,Quads= 3465 6505 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 310 540 0
AFLR4 : Nodes, Trias,Quads= 242 404 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 106 145 0
AFLR4 : Nodes, Trias,Quads= 65 63 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 19 24 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 2233 4200 0
AFLR4 : Nodes, Trias,Quads= 1943 3620 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 106 170 0
AFLR4 : Nodes, Trias,Quads= 120 198 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 3808 7039 0
AFLR4 : Nodes, Trias,Quads= 4844 9111 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 4921 9421 0
AFLR4 : Nodes, Trias,Quads= 3456 6491 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 2589 4890 0
AFLR4 : Nodes, Trias,Quads= 1963 3638 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 2216 4132 0
AFLR4 : Nodes, Trias,Quads= 2617 4934 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 2344 4396 0
AFLR4 : Nodes, Trias,Quads= 1845 3398 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 2657 5011 0
AFLR4 : Nodes, Trias,Quads= 2134 3965 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 3830 7081 0
AFLR4 : Nodes, Trias,Quads= 4876 9173 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 5597 10778 0
AFLR4 : Nodes, Trias,Quads= 3975 7534 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 3935 7561 0
AFLR4 : Nodes, Trias,Quads= 2905 5501 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 2618 4948 0
AFLR4 : Nodes, Trias,Quads= 2017 3746 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 2217 4134 0
AFLR4 : Nodes, Trias,Quads= 2618 4936 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 62 83 0
AFLR4 : Nodes, Trias,Quads= 39 37 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 39 50 0
AFLR4 : Nodes, Trias,Quads= 26 24 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 19 24 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 86 119 0
AFLR4 : Nodes, Trias,Quads= 51 49 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 54 71 0
AFLR4 : Nodes, Trias,Quads= 58 79 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 61 80 0
AFLR4 : Nodes, Trias,Quads= 62 82 0
AFLR4 : Generate optimal mesh on surface definition 47
AFLR2 : Nodes, Trias,Quads= 106 145 0
AFLR4 : Nodes, Trias,Quads= 65 63 0
AFLR4 : Generate optimal mesh on surface definition 48
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 19 24 0
AFLR4 : Generate optimal mesh on surface definition 49
AFLR2 : Nodes, Trias,Quads= 3946 7581 0
AFLR4 : Nodes, Trias,Quads= 2941 5571 0
AFLR4 : Generate optimal mesh on surface definition 50
AFLR2 : Nodes, Trias,Quads= 5414 10410 0
AFLR4 : Nodes, Trias,Quads= 3958 7498 0
AFLR4 : Generate optimal mesh on surface definition 51
AFLR2 : Nodes, Trias,Quads= 62 92 0
AFLR4 : Nodes, Trias,Quads= 45 58 0
AFLR4 : Generate optimal mesh on surface definition 52
AFLR2 : Nodes, Trias,Quads= 127 168 0
AFLR4 : Nodes, Trias,Quads= 120 154 0
AFLR4 : Generate optimal mesh on surface definition 53
AFLR2 : Nodes, Trias,Quads= 58 85 0
AFLR4 : Nodes, Trias,Quads= 44 57 0
AFLR4 : Generate optimal mesh on surface definition 54
AFLR2 : Nodes, Trias,Quads= 5057 9716 0
AFLR4 : Nodes, Trias,Quads= 2994 5590 0
AFLR4 : Generate optimal mesh on surface definition 55
AFLR2 : Nodes, Trias,Quads= 4633 8888 0
AFLR4 : Nodes, Trias,Quads= 2623 4868 0
AFLR4 : Generate optimal mesh on surface definition 56
AFLR2 : Nodes, Trias,Quads= 88 138 0
AFLR4 : Nodes, Trias,Quads= 54 70 0
AFLR4 : Generate optimal mesh on surface definition 57
AFLR2 : Nodes, Trias,Quads= 198 270 0
AFLR4 : Nodes, Trias,Quads= 204 282 0
AFLR4 : Generate optimal mesh on surface definition 58
AFLR2 : Nodes, Trias,Quads= 76 117 0
AFLR4 : Nodes, Trias,Quads= 49 63 0
AFLR4 : Generate optimal mesh on surface definition 59
AFLR2 : Nodes, Trias,Quads= 234 399 0
AFLR4 : Nodes, Trias,Quads= 188 307 0
AFLR4 : Generate optimal mesh on surface definition 60
AFLR2 : Nodes, Trias,Quads= 293 507 0
AFLR4 : Nodes, Trias,Quads= 234 389 0
AFLR4 : Generate optimal mesh on surface definition 61
AFLR2 : Nodes, Trias,Quads= 4681 8974 0
AFLR4 : Nodes, Trias,Quads= 2721 5054 0
AFLR4 : Generate optimal mesh on surface definition 62
AFLR2 : Nodes, Trias,Quads= 87 136 0
AFLR4 : Nodes, Trias,Quads= 54 70 0
AFLR4 : Generate optimal mesh on surface definition 63
AFLR2 : Nodes, Trias,Quads= 205 284 0
AFLR4 : Nodes, Trias,Quads= 195 264 0
AFLR4 : Generate optimal mesh on surface definition 64
AFLR2 : Nodes, Trias,Quads= 76 117 0
AFLR4 : Nodes, Trias,Quads= 50 65 0
AFLR4 : Generate optimal mesh on surface definition 65
AFLR2 : Nodes, Trias,Quads= 62 92 0
AFLR4 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Generate optimal mesh on surface definition 66
AFLR2 : Nodes, Trias,Quads= 138 190 0
AFLR4 : Nodes, Trias,Quads= 127 168 0
AFLR4 : Generate optimal mesh on surface definition 67
AFLR2 : Nodes, Trias,Quads= 62 92 0
AFLR4 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Generate optimal mesh on surface definition 68
AFLR2 : Nodes, Trias,Quads= 4678 8970 0
AFLR4 : Nodes, Trias,Quads= 2893 5400 0
AFLR4 : Generate optimal mesh on surface definition 69
AFLR2 : Nodes, Trias,Quads= 350 608 0
AFLR4 : Nodes, Trias,Quads= 324 556 0
AFLR4 : Generate optimal mesh on surface definition 70
AFLR2 : Nodes, Trias,Quads= 70 101 0
AFLR4 : Nodes, Trias,Quads= 62 85 0
AFLR4 : Generate optimal mesh on surface definition 71
AFLR2 : Nodes, Trias,Quads= 149 207 0
AFLR4 : Nodes, Trias,Quads= 95 99 0
AFLR4 : Generate optimal mesh on surface definition 72
AFLR2 : Nodes, Trias,Quads= 36 46 0
AFLR4 : Nodes, Trias,Quads= 38 50 0
AFLR4 : Generate optimal mesh on surface definition 73
AFLR2 : Nodes, Trias,Quads= 50 67 0
AFLR4 : Nodes, Trias,Quads= 48 63 0
AFLR4 : Generate optimal mesh on surface definition 74
AFLR2 : Nodes, Trias,Quads= 220 305 0
AFLR4 : Nodes, Trias,Quads= 209 283 0
AFLR4 : Generate optimal mesh on surface definition 75
AFLR2 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Generate optimal mesh on surface definition 76
AFLR2 : Nodes, Trias,Quads= 39 50 0
AFLR4 : Nodes, Trias,Quads= 26 24 0
AFLR4 : Generate optimal mesh on surface definition 77
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Generate optimal mesh on surface definition 78
AFLR2 : Nodes, Trias,Quads= 196 279 0
AFLR4 : Nodes, Trias,Quads= 113 113 0
AFLR4 : Generate optimal mesh on surface definition 79
AFLR2 : Nodes, Trias,Quads= 35 45 0
AFLR4 : Nodes, Trias,Quads= 38 51 0
AFLR4 : Generate optimal mesh on surface definition 80
AFLR2 : Nodes, Trias,Quads= 36 46 0
AFLR4 : Nodes, Trias,Quads= 36 46 0
AFLR4 : Generate optimal mesh on surface definition 81
AFLR2 : Nodes, Trias,Quads= 157 225 0
AFLR4 : Nodes, Trias,Quads= 95 101 0
AFLR4 : Generate optimal mesh on surface definition 82
AFLR2 : Nodes, Trias,Quads= 47 63 0
AFLR4 : Nodes, Trias,Quads= 46 61 0
AFLR4 : Generate optimal mesh on surface definition 83
AFLR2 : Nodes, Trias,Quads= 520 923 0
AFLR4 : Nodes, Trias,Quads= 508 899 0
AFLR4 : Generate optimal mesh on surface definition 84
AFLR2 : Nodes, Trias,Quads= 39 50 0
AFLR4 : Nodes, Trias,Quads= 26 24 0
AFLR4 : Generate optimal mesh on surface definition 85
AFLR2 : Nodes, Trias,Quads= 32 41 0
AFLR4 : Nodes, Trias,Quads= 31 39 0
AFLR4 : Generate optimal mesh on surface definition 86
AFLR2 : Nodes, Trias,Quads= 199 273 0
AFLR4 : Nodes, Trias,Quads= 152 179 0
AFLR4 : Generate optimal mesh on surface definition 87
AFLR2 : Nodes, Trias,Quads= 51 69 0
AFLR4 : Nodes, Trias,Quads= 48 63 0
AFLR4 : Generate optimal mesh on surface definition 88
AFLR2 : Nodes, Trias,Quads= 37 47 0
AFLR4 : Nodes, Trias,Quads= 41 55 0
AFLR4 : Generate optimal mesh on surface definition 89
AFLR2 : Nodes, Trias,Quads= 159 229 0
AFLR4 : Nodes, Trias,Quads= 95 101 0
AFLR4 : Generate optimal mesh on surface definition 90
AFLR2 : Nodes, Trias,Quads= 46 61 0
AFLR4 : Nodes, Trias,Quads= 46 61 0
AFLR4 : Generate optimal mesh on surface definition 91
AFLR2 : Nodes, Trias,Quads= 515 913 0
AFLR4 : Nodes, Trias,Quads= 504 891 0
AFLR4 : Generate optimal mesh on surface definition 92
AFLR2 : Nodes, Trias,Quads= 354 616 0
AFLR4 : Nodes, Trias,Quads= 320 548 0
AFLR4 : Generate optimal mesh on surface definition 93
AFLR2 : Nodes, Trias,Quads= 70 101 0
AFLR4 : Nodes, Trias,Quads= 62 85 0
AFLR4 : Generate optimal mesh on surface definition 94
AFLR2 : Nodes, Trias,Quads= 140 190 0
AFLR4 : Nodes, Trias,Quads= 96 102 0
AFLR4 : Generate optimal mesh on surface definition 95
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 35 46 0
AFLR4 : Generate optimal mesh on surface definition 96
AFLR2 : Nodes, Trias,Quads= 36 47 0
AFLR4 : Nodes, Trias,Quads= 37 49 0
AFLR4 : Generate optimal mesh on surface definition 97
AFLR2 : Nodes, Trias,Quads= 204 286 0
AFLR4 : Nodes, Trias,Quads= 165 208 0
AFLR4 : Generate optimal mesh on surface definition 98
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Generate optimal mesh on surface definition 99
AFLR2 : Nodes, Trias,Quads= 344 591 0
AFLR4 : Nodes, Trias,Quads= 292 487 0
AFLR4 : Generate optimal mesh on surface definition 100
AFLR2 : Nodes, Trias,Quads= 442 755 0
AFLR4 : Nodes, Trias,Quads= 340 551 0
AFLR4 : Generate optimal mesh on surface definition 101
AFLR2 : Nodes, Trias,Quads= 377 638 0
AFLR4 : Nodes, Trias,Quads= 268 420 0
AFLR4 : Generate optimal mesh on surface definition 102
AFLR2 : Nodes, Trias,Quads= 327 559 0
AFLR4 : Nodes, Trias,Quads= 273 451 0
AFLR4 : Generate optimal mesh on surface definition 103
AFLR2 : Nodes, Trias,Quads= 419 714 0
AFLR4 : Nodes, Trias,Quads= 304 484 0
AFLR4 : Generate optimal mesh on surface definition 104
AFLR2 : Nodes, Trias,Quads= 326 557 0
AFLR4 : Nodes, Trias,Quads= 271 447 0
AFLR4 : Generate optimal mesh on surface definition 105
AFLR2 : Nodes, Trias,Quads= 345 593 0
AFLR4 : Nodes, Trias,Quads= 292 487 0
AFLR4 : Generate optimal mesh on surface definition 106
AFLR2 : Nodes, Trias,Quads= 409 698 0
AFLR4 : Nodes, Trias,Quads= 301 482 0
AFLR4 : Generate optimal mesh on surface definition 107
AFLR2 : Nodes, Trias,Quads= 89 141 0
AFLR4 : Nodes, Trias,Quads= 66 95 0
AFLR4 : Generate optimal mesh on surface definition 108
AFLR2 : Nodes, Trias,Quads= 94 150 0
AFLR4 : Nodes, Trias,Quads= 67 96 0
AFLR4 : Generate optimal mesh on surface definition 109
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 110
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 111
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 112
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 113
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 114
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 69451 138894 13136
OVERALL : CPU Time = 7.622 seconds
Body 1 (of 4)
Number of nodes = 1866
Number of elements = 3732
Number of triangle elements = 3732
Number of quadrilateral elements = 0
Body 2 (of 4)
Number of nodes = 1861
Number of elements = 3722
Number of triangle elements = 3722
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 65404
Number of elements = 130804
Number of triangle elements = 130804
Number of quadrilateral elements = 0
Body 4 (of 4)
Number of nodes = 320
Number of elements = 636
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 69451
Total number of elements = 138894
Total number of triangle elements = 138894
Total number of quadrilateral elements = 0
real 1m26.294s
user 1m30.751s
sys 0m6.154s
+ status=0
+ set +x
=================================================
data/session07/08_aflr4_InviscidTransport.py passed (as expected)
=================================================
=================================================
09_aflr4_aflr3_InviscidWing.py test;
+ python 09_aflr4_aflr3_InviscidWing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building nacelleOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Nacelle, index = 1
Name = Wing, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Nacelle, index = 1
Name = leftWing, index = 2
Name = riteWing, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 4 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 4 Faces
EGADS : Body 0 has 8 Edges
EGADS : Body 0 has 4 Loops
EGADS : Body 0 has 4 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 4 Faces
EGADS : Body 1 has 8 Edges
EGADS : Body 1 has 4 Loops
EGADS : Body 1 has 4 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 10 Faces
EGADS : Body 2 has 18 Edges
EGADS : Body 2 has 10 Loops
EGADS : Body 2 has 10 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 6 Faces
EGADS : Body 3 has 12 Edges
EGADS : Body 3 has 6 Loops
EGADS : Body 3 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3
EGADS : 2 Yes 0 0 1 0 1 1 4
EGADS : 3 Yes 0 0 1 0 1 1 4
EGADS : 4 Yes 0 0 1 0 1 2 3
EGADS : 5 Yes 1 0 1 0 1 6 7
EGADS : 6 Yes 1 0 1 0 1 5 8
EGADS : 7 Yes 1 0 1 0 1 5 8
EGADS : 8 Yes 1 0 1 0 1 6 7
EGADS : 9 Yes 2 0 1 1 1 10 11 14
EGADS : 10 Yes 2 0 1 1 1 9 12 13
EGADS : 11 Yes 2 0 1 1 1 9 12 16
EGADS : 12 Yes 2 0 1 1 1 10 11 13
EGADS : 13 Yes 2 0 1 1 1 10 12
EGADS : 14 Yes 2 0 1 1 1 9 15 16
EGADS : 15 Yes 2 0 1 1 1 14 17 18
EGADS : 16 Yes 2 0 1 1 1 11 14 17
EGADS : 17 Yes 2 0 1 1 1 15 16 18
EGADS : 18 Yes 2 0 1 1 1 15 17
EGADS : 19 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 20 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 21 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 22 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 23 Yes 3 0 1 NA NA 19 20 21 22
EGADS : 24 Yes 3 0 1 NA NA 19 20 21 22
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 3 2 -4
EGADS : 2 -2 5 1 -6
EGADS : 3 7 4 -8 -3
EGADS : 4 8 6 -7 -5
EGADS : 5 9 12 -10 -11
EGADS : 6 10 14 -9 -13
EGADS : 7 -15 11 16 -12
EGADS : 8 -16 13 15 -14
EGADS : 9 -17 18 19 -20
EGADS : 10 -21 20 22 -23
EGADS : 11 -19 24 17 -25
EGADS : 12 -22 25 21 -26
EGADS : 13 23 26
EGADS : 14 27 29 -28 -18
EGADS : 15 30 32 -31 -29
EGADS : 16 28 33 -27 -24
EGADS : 17 31 34 -30 -33
EGADS : 18 -32 -34
EGADS : 19 35 36 -37 -38
EGADS : 20 -39 42 41 -40
EGADS : 21 43 39 -44 -35
EGADS : 22 -45 37 46 -41
EGADS : 23 38 45 -42 -43
EGADS : 24 -36 44 40 -46
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : 19 19
EGADS : 20 20
EGADS : 21 21
EGADS : 22 22
EGADS : 23 23
EGADS : 24 24
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 3 2 -4
EGADS : 2 Yes -2 5 1 -6
EGADS : 3 Yes 7 4 -8 -3
EGADS : 4 Yes 8 6 -7 -5
EGADS : 5 Yes 9 12 -10 -11
EGADS : 6 Yes 10 14 -9 -13
EGADS : 7 Yes -15 11 16 -12
EGADS : 8 Yes -16 13 15 -14
EGADS : 9 Yes -17 18 19 -20
EGADS : 10 Yes -21 20 22 -23
EGADS : 11 Yes -19 24 17 -25
EGADS : 12 Yes -22 25 21 -26
EGADS : 13 Yes 23 26
EGADS : 14 Yes 27 29 -28 -18
EGADS : 15 Yes 30 32 -31 -29
EGADS : 16 Yes 28 33 -27 -24
EGADS : 17 Yes 31 34 -30 -33
EGADS : 18 Yes -32 -34
EGADS : 19 Yes 35 36 -37 -38
EGADS : 20 Yes -39 42 41 -40
EGADS : 21 Yes 43 39 -44 -35
EGADS : 22 Yes -45 37 46 -41
EGADS : 23 Yes 38 45 -42 -43
EGADS : 24 Yes -36 44 40 -46
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 3 4 1 1 2
EGADS : 3 0 Yes 1 3 1 1 3
EGADS : 4 0 Yes 2 4 1 1 3
EGADS : 5 0 Yes 3 1 1 2 4
EGADS : 6 0 Yes 4 2 1 2 4
EGADS : 7 0 Yes 1 2 1 3 4
EGADS : 8 0 Yes 3 4 1 3 4
EGADS : 9 1 Yes 5 6 1 5 6
EGADS : 10 1 Yes 7 8 1 5 6
EGADS : 11 1 Yes 5 7 1 5 7
EGADS : 12 1 Yes 6 8 1 5 7
EGADS : 13 1 Yes 7 5 1 6 8
EGADS : 14 1 Yes 8 6 1 6 8
EGADS : 15 1 Yes 5 6 1 7 8
EGADS : 16 1 Yes 7 8 1 7 8
EGADS : 17 2 Yes 9 10 1 9 11
EGADS : 18 2 Yes 9 11 1 9 14
EGADS : 19 2 Yes 11 12 1 9 11
EGADS : 20 2 Yes 10 12 1 9 10
EGADS : 21 2 Yes 10 13 1 10 12
EGADS : 22 2 Yes 12 14 1 10 12
EGADS : 23 2 Yes 13 14 1 10 13
EGADS : 24 2 Yes 11 9 1 11 16
EGADS : 25 2 Yes 12 10 1 11 12
EGADS : 26 2 Yes 14 13 1 12 13
EGADS : 27 2 Yes 9 15 1 14 16
EGADS : 28 2 Yes 11 16 1 14 16
EGADS : 29 2 Yes 15 16 1 14 15
EGADS : 30 2 Yes 15 17 1 15 17
EGADS : 31 2 Yes 16 18 1 15 17
EGADS : 32 2 Yes 17 18 1 15 18
EGADS : 33 2 Yes 16 15 1 16 17
EGADS : 34 2 Yes 18 17 1 17 18
EGADS : 35 3 Yes 20 19 NA 19 21
EGADS : 36 3 Yes 19 21 NA 19 24
EGADS : 37 3 Yes 22 21 NA 19 22
EGADS : 38 3 Yes 20 22 NA 19 23
EGADS : 39 3 Yes 24 23 NA 20 21
EGADS : 40 3 Yes 23 25 NA 20 24
EGADS : 41 3 Yes 26 25 NA 20 22
EGADS : 42 3 Yes 24 26 NA 20 23
EGADS : 43 3 Yes 20 24 NA 21 23
EGADS : 44 3 Yes 19 23 NA 21 24
EGADS : 45 3 Yes 22 26 NA 22 23
EGADS : 46 3 Yes 21 25 NA 22 24
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 90.5173952 0 0
EGADS : 2 Yes 90.5173952 0 0
EGADS : 3 Yes 60.5173952 0 0
EGADS : 4 Yes 60.5173952 0 0
EGADS : 5 Yes 90.5173952 29.3018771 0
EGADS : 6 Yes 90.5173952 29.3018771 0
EGADS : 7 Yes 60.5173952 29.3018771 0
EGADS : 8 Yes 60.5173952 29.3018771 0
EGADS : 9 Yes 97.2007855 0 0
EGADS : 10 Yes 97.9335611 0 0
EGADS : 11 Yes 50 0 0
EGADS : 12 Yes 75.3047874 0 0
EGADS : 13 Yes 123.552357 0 4.7180639
EGADS : 14 Yes 118.391317 0 3.99272703
EGADS : 15 Yes 97.9335611 36.1389817 0
EGADS : 16 Yes 75.3047874 36.1389817 0
EGADS : 17 Yes 123.552357 97.6729236 4.7180639
EGADS : 18 Yes 118.391317 97.6729236 3.99272703
EGADS : 19 Yes 0 0 1947.05079
EGADS : 20 Yes 0 0 0
EGADS : 21 Yes 0 1953.45847 1947.05079
EGADS : 22 Yes 0 1953.45847 0
EGADS : 23 Yes 2040.21562 0 1947.05079
EGADS : 24 Yes 2040.21562 0 0
EGADS : 25 Yes 2040.21562 1953.45847 1947.05079
EGADS : 26 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 22.2515
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 2651.51
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 5
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 FARFIELD
AFLR4 : 20 CAD geometry 0 FARFIELD
AFLR4 : 21 CAD geometry 0 FARFIELD
AFLR4 : 22 CAD geometry 0 FARFIELD
AFLR4 : 23 CAD geometry 0 FARFIELD
AFLR4 : 24 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4 : Component 2 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 339 605 0
AFLR4 : Nodes, Trias,Quads= 362 651 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 319 563 0
AFLR4 : Nodes, Trias,Quads= 284 493 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 340 607 0
AFLR4 : Nodes, Trias,Quads= 362 651 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 321 567 0
AFLR4 : Nodes, Trias,Quads= 284 493 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 340 607 0
AFLR4 : Nodes, Trias,Quads= 362 651 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 321 567 0
AFLR4 : Nodes, Trias,Quads= 284 493 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 339 605 0
AFLR4 : Nodes, Trias,Quads= 362 651 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 319 563 0
AFLR4 : Nodes, Trias,Quads= 284 493 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1107 2082 0
AFLR4 : Nodes, Trias,Quads= 685 1238 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 1473 2759 0
AFLR4 : Nodes, Trias,Quads= 721 1255 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 1116 2100 0
AFLR4 : Nodes, Trias,Quads= 671 1210 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 1458 2729 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1108 2084 0
AFLR4 : Nodes, Trias,Quads= 683 1234 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 1488 2789 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 1112 2092 0
AFLR4 : Nodes, Trias,Quads= 653 1174 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 1456 2725 0
AFLR4 : Nodes, Trias,Quads= 708 1229 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 7221 14434 1888
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 7221 14434
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 397 713 0
AFLR4 : Nodes, Trias,Quads= 416 751 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 387 691 0
AFLR4 : Nodes, Trias,Quads= 346 609 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 396 711 0
AFLR4 : Nodes, Trias,Quads= 417 753 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 388 693 0
AFLR4 : Nodes, Trias,Quads= 344 605 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 395 709 0
AFLR4 : Nodes, Trias,Quads= 416 751 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 388 693 0
AFLR4 : Nodes, Trias,Quads= 344 605 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 395 709 0
AFLR4 : Nodes, Trias,Quads= 416 751 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 387 691 0
AFLR4 : Nodes, Trias,Quads= 346 609 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 12796 24695 0
AFLR4 : Nodes, Trias,Quads= 7764 14631 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 29245 57075 0
AFLR4 : Nodes, Trias,Quads= 12448 23481 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12136 23411 0
AFLR4 : Nodes, Trias,Quads= 7447 14033 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 29424 57435 0
AFLR4 : Nodes, Trias,Quads= 12399 23385 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 196 293 0
AFLR4 : Nodes, Trias,Quads= 188 277 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12819 24741 0
AFLR4 : Nodes, Trias,Quads= 7725 14553 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 29449 57483 0
AFLR4 : Nodes, Trias,Quads= 12413 23411 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12144 23427 0
AFLR4 : Nodes, Trias,Quads= 7471 14081 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 29445 57477 0
AFLR4 : Nodes, Trias,Quads= 12478 23543 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 196 293 0
AFLR4 : Nodes, Trias,Quads= 188 277 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 78575 157142 10038
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 78961 157914
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 850 1593 0
AFLR4 : Nodes, Trias,Quads= 754 1401 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 384 685 0
AFLR4 : Nodes, Trias,Quads= 354 625 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 842 1577 0
AFLR4 : Nodes, Trias,Quads= 803 1499 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 384 685 0
AFLR4 : Nodes, Trias,Quads= 351 619 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 837 1566 0
AFLR4 : Nodes, Trias,Quads= 755 1402 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 384 685 0
AFLR4 : Nodes, Trias,Quads= 352 621 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 834 1560 0
AFLR4 : Nodes, Trias,Quads= 806 1504 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 384 685 0
AFLR4 : Nodes, Trias,Quads= 353 623 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 11687 22537 0
AFLR4 : Nodes, Trias,Quads= 9244 17651 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 22200 43075 0
AFLR4 : Nodes, Trias,Quads= 14790 28255 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 11200 21594 0
AFLR4 : Nodes, Trias,Quads= 8943 17080 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 22061 42799 0
AFLR4 : Nodes, Trias,Quads= 14755 28187 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 179 265 0
AFLR4 : Nodes, Trias,Quads= 177 261 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 11697 22557 0
AFLR4 : Nodes, Trias,Quads= 9237 17637 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 22392 43459 0
AFLR4 : Nodes, Trias,Quads= 14703 28081 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 11243 21680 0
AFLR4 : Nodes, Trias,Quads= 8970 17134 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 22235 43146 0
AFLR4 : Nodes, Trias,Quads= 14758 28192 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 184 274 0
AFLR4 : Nodes, Trias,Quads= 179 264 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 95540 191072 9544
OVERALL : CPU Time = 5.982 seconds
Body 1 (of 4)
Number of nodes = 2072
Number of elements = 4144
Number of triangle elements = 4144
Number of quadrilateral elements = 0
Body 2 (of 4)
Number of nodes = 2075
Number of elements = 4150
Number of triangle elements = 4150
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 91373
Number of elements = 182742
Number of triangle elements = 182742
Number of quadrilateral elements = 0
Body 4 (of 4)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 95540
Total number of elements = 191072
Total number of triangle elements = 191072
Total number of quadrilateral elements = 0
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Nacelle
2: Wing
3: Farfield
Finished writing vtk file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Nacelle, index = 1
Name = leftWing, index = 2
Name = riteWing, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Nacelle, index = 1
Name = Wing, index = 2
Name = Farfield, index = 3
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 4 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 4 Faces
EGADS : Body 0 has 8 Edges
EGADS : Body 0 has 4 Loops
EGADS : Body 0 has 4 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 4 Faces
EGADS : Body 1 has 8 Edges
EGADS : Body 1 has 4 Loops
EGADS : Body 1 has 4 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 10 Faces
EGADS : Body 2 has 18 Edges
EGADS : Body 2 has 10 Loops
EGADS : Body 2 has 10 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 6 Faces
EGADS : Body 3 has 12 Edges
EGADS : Body 3 has 6 Loops
EGADS : Body 3 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3
EGADS : 2 Yes 0 0 1 0 1 1 4
EGADS : 3 Yes 0 0 1 0 1 1 4
EGADS : 4 Yes 0 0 1 0 1 2 3
EGADS : 5 Yes 1 0 1 0 1 6 7
EGADS : 6 Yes 1 0 1 0 1 5 8
EGADS : 7 Yes 1 0 1 0 1 5 8
EGADS : 8 Yes 1 0 1 0 1 6 7
EGADS : 9 Yes 2 0 1 1 1 10 11 14
EGADS : 10 Yes 2 0 1 1 1 9 12 13
EGADS : 11 Yes 2 0 1 1 1 9 12 16
EGADS : 12 Yes 2 0 1 1 1 10 11 13
EGADS : 13 Yes 2 0 1 1 1 10 12
EGADS : 14 Yes 2 0 1 1 1 9 15 16
EGADS : 15 Yes 2 0 1 1 1 14 17 18
EGADS : 16 Yes 2 0 1 1 1 11 14 17
EGADS : 17 Yes 2 0 1 1 1 15 16 18
EGADS : 18 Yes 2 0 1 1 1 15 17
EGADS : 19 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 20 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 21 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 22 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 23 Yes 3 0 1 NA NA 19 20 21 22
EGADS : 24 Yes 3 0 1 NA NA 19 20 21 22
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 3 2 -4
EGADS : 2 -2 5 1 -6
EGADS : 3 7 4 -8 -3
EGADS : 4 8 6 -7 -5
EGADS : 5 9 12 -10 -11
EGADS : 6 10 14 -9 -13
EGADS : 7 -15 11 16 -12
EGADS : 8 -16 13 15 -14
EGADS : 9 -17 18 19 -20
EGADS : 10 -21 20 22 -23
EGADS : 11 -19 24 17 -25
EGADS : 12 -22 25 21 -26
EGADS : 13 23 26
EGADS : 14 27 29 -28 -18
EGADS : 15 30 32 -31 -29
EGADS : 16 28 33 -27 -24
EGADS : 17 31 34 -30 -33
EGADS : 18 -32 -34
EGADS : 19 35 36 -37 -38
EGADS : 20 -39 42 41 -40
EGADS : 21 43 39 -44 -35
EGADS : 22 -45 37 46 -41
EGADS : 23 38 45 -42 -43
EGADS : 24 -36 44 40 -46
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : 19 19
EGADS : 20 20
EGADS : 21 21
EGADS : 22 22
EGADS : 23 23
EGADS : 24 24
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 3 2 -4
EGADS : 2 Yes -2 5 1 -6
EGADS : 3 Yes 7 4 -8 -3
EGADS : 4 Yes 8 6 -7 -5
EGADS : 5 Yes 9 12 -10 -11
EGADS : 6 Yes 10 14 -9 -13
EGADS : 7 Yes -15 11 16 -12
EGADS : 8 Yes -16 13 15 -14
EGADS : 9 Yes -17 18 19 -20
EGADS : 10 Yes -21 20 22 -23
EGADS : 11 Yes -19 24 17 -25
EGADS : 12 Yes -22 25 21 -26
EGADS : 13 Yes 23 26
EGADS : 14 Yes 27 29 -28 -18
EGADS : 15 Yes 30 32 -31 -29
EGADS : 16 Yes 28 33 -27 -24
EGADS : 17 Yes 31 34 -30 -33
EGADS : 18 Yes -32 -34
EGADS : 19 Yes 35 36 -37 -38
EGADS : 20 Yes -39 42 41 -40
EGADS : 21 Yes 43 39 -44 -35
EGADS : 22 Yes -45 37 46 -41
EGADS : 23 Yes 38 45 -42 -43
EGADS : 24 Yes -36 44 40 -46
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 3 4 1 1 2
EGADS : 3 0 Yes 1 3 1 1 3
EGADS : 4 0 Yes 2 4 1 1 3
EGADS : 5 0 Yes 3 1 1 2 4
EGADS : 6 0 Yes 4 2 1 2 4
EGADS : 7 0 Yes 1 2 1 3 4
EGADS : 8 0 Yes 3 4 1 3 4
EGADS : 9 1 Yes 5 6 1 5 6
EGADS : 10 1 Yes 7 8 1 5 6
EGADS : 11 1 Yes 5 7 1 5 7
EGADS : 12 1 Yes 6 8 1 5 7
EGADS : 13 1 Yes 7 5 1 6 8
EGADS : 14 1 Yes 8 6 1 6 8
EGADS : 15 1 Yes 5 6 1 7 8
EGADS : 16 1 Yes 7 8 1 7 8
EGADS : 17 2 Yes 9 10 1 9 11
EGADS : 18 2 Yes 9 11 1 9 14
EGADS : 19 2 Yes 11 12 1 9 11
EGADS : 20 2 Yes 10 12 1 9 10
EGADS : 21 2 Yes 10 13 1 10 12
EGADS : 22 2 Yes 12 14 1 10 12
EGADS : 23 2 Yes 13 14 1 10 13
EGADS : 24 2 Yes 11 9 1 11 16
EGADS : 25 2 Yes 12 10 1 11 12
EGADS : 26 2 Yes 14 13 1 12 13
EGADS : 27 2 Yes 9 15 1 14 16
EGADS : 28 2 Yes 11 16 1 14 16
EGADS : 29 2 Yes 15 16 1 14 15
EGADS : 30 2 Yes 15 17 1 15 17
EGADS : 31 2 Yes 16 18 1 15 17
EGADS : 32 2 Yes 17 18 1 15 18
EGADS : 33 2 Yes 16 15 1 16 17
EGADS : 34 2 Yes 18 17 1 17 18
EGADS : 35 3 Yes 20 19 NA 19 21
EGADS : 36 3 Yes 19 21 NA 19 24
EGADS : 37 3 Yes 22 21 NA 19 22
EGADS : 38 3 Yes 20 22 NA 19 23
EGADS : 39 3 Yes 24 23 NA 20 21
EGADS : 40 3 Yes 23 25 NA 20 24
EGADS : 41 3 Yes 26 25 NA 20 22
EGADS : 42 3 Yes 24 26 NA 20 23
EGADS : 43 3 Yes 20 24 NA 21 23
EGADS : 44 3 Yes 19 23 NA 21 24
EGADS : 45 3 Yes 22 26 NA 22 23
EGADS : 46 3 Yes 21 25 NA 22 24
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 90.5173952 0 0
EGADS : 2 Yes 90.5173952 0 0
EGADS : 3 Yes 60.5173952 0 0
EGADS : 4 Yes 60.5173952 0 0
EGADS : 5 Yes 90.5173952 29.3018771 0
EGADS : 6 Yes 90.5173952 29.3018771 0
EGADS : 7 Yes 60.5173952 29.3018771 0
EGADS : 8 Yes 60.5173952 29.3018771 0
EGADS : 9 Yes 97.2007855 0 0
EGADS : 10 Yes 97.9335611 0 0
EGADS : 11 Yes 50 0 0
EGADS : 12 Yes 75.3047874 0 0
EGADS : 13 Yes 123.552357 0 4.7180639
EGADS : 14 Yes 118.391317 0 3.99272703
EGADS : 15 Yes 97.9335611 36.1389817 0
EGADS : 16 Yes 75.3047874 36.1389817 0
EGADS : 17 Yes 123.552357 97.6729236 4.7180639
EGADS : 18 Yes 118.391317 97.6729236 3.99272703
EGADS : 19 Yes 0 0 1947.05079
EGADS : 20 Yes 0 0 0
EGADS : 21 Yes 0 1953.45847 1947.05079
EGADS : 22 Yes 0 1953.45847 0
EGADS : 23 Yes 2040.21562 0 1947.05079
EGADS : 24 Yes 2040.21562 0 0
EGADS : 25 Yes 2040.21562 1953.45847 1947.05079
EGADS : 26 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 22.2515
AFLR4 : Reference Length = 22.2515
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 428.344
AFLR4 : Abs Min Surf Spacing = 0.0556287
AFLR4 : Min Surf Spacing = 0.111257
AFLR4 : Max Surf Spacing = 2.22515
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 STD
AFLR4 : 12 CAD geometry 0 STD
AFLR4 : 13 CAD geometry 0 STD
AFLR4 : 14 CAD geometry 0 STD
AFLR4 : 15 CAD geometry 0 STD
AFLR4 : 16 CAD geometry 0 STD
AFLR4 : 17 CAD geometry 0 STD
AFLR4 : 18 CAD geometry 0 STD
AFLR4 : 19 CAD geometry 0 FARFIELD
AFLR4 : 20 CAD geometry 0 FARFIELD
AFLR4 : 21 CAD geometry 0 FARFIELD
AFLR4 : 22 CAD geometry 0 FARFIELD
AFLR4 : 23 CAD geometry 0 FARFIELD
AFLR4 : 24 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4 : Component 2 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 191072
AFLR43 : Nodes = 95540
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 95540 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 Solid
UG3 : 12 Solid
UG3 : 13 Solid
UG3 : 14 Solid
UG3 : 15 Solid
UG3 : 16 Solid
UG3 : 17 Solid
UG3 : 18 Solid
UG3 : 19 FarField
UG3 : 20 FarField
UG3 : 21 FarField
UG3 : 22 FarField
UG3 : 23 FarField
UG3 : 24 FarField
AFLR3 : CPU Time = 0.351 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 95540 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 19110 113248
AFLR3 IG : Nodes, Elements = 38220 247440
AFLR3 IG : Nodes, Elements = 57330 367745
AFLR3 IG : Nodes, Elements = 76440 520135
AFLR3 IG : Nodes, Elements = 95547 672875
AFLR3 IG : Nodes, Elements = 95547 671480
AFLR3 IG : Nodes, Elements = 95547 671533
AFLR3 IG : Nodes, Elements = 95547 671402
AFLR3 IG : Nodes, Elements = 95540 378462
AFLR3 IG : Nodes, Elements = 95540 378726
AFLR3 IG : Nodes, Elements = 95540 305842
AFLR3 IG : Nodes, Elements = 95540 287127
AFLR3 : CPU Time = 11.548 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 95540 287127
AFLR3 GGi: Nodes, Elements = 95541 287130
AFLR3 GGi: Nodes, Elements = 95541 287141
AFLR3 GGi: Nodes, Elements = 95541 287142
AFLR3 GGi: Nodes, Elements = 95543 287148
AFLR3 GGi: Nodes, Elements = 95543 287205
AFLR3 GGi: Nodes, Elements = 95543 287228
AFLR3 GG : Nodes, Elements = 136408 410551
AFLR3 GG : Nodes, Elements = 136408 573470
AFLR3 GG : Nodes, Elements = 136408 533381
AFLR3 GG : Nodes, Elements = 170819 637623
AFLR3 GG : Nodes, Elements = 170819 773192
AFLR3 GG : Nodes, Elements = 170819 731565
AFLR3 GG : Nodes, Elements = 206009 837914
AFLR3 GG : Nodes, Elements = 206009 978011
AFLR3 GG : Nodes, Elements = 206009 935997
AFLR3 GG : Nodes, Elements = 241032 1041536
AFLR3 GG : Nodes, Elements = 241032 1184601
AFLR3 GG : Nodes, Elements = 241032 1144028
AFLR3 GG : Nodes, Elements = 276099 1249644
AFLR3 GG : Nodes, Elements = 276099 1388535
AFLR3 GG : Nodes, Elements = 276099 1350967
AFLR3 GG : Nodes, Elements = 310846 1455570
AFLR3 GG : Nodes, Elements = 310846 1593212
AFLR3 GG : Nodes, Elements = 310846 1556216
AFLR3 GG : Nodes, Elements = 345374 1660116
AFLR3 GG : Nodes, Elements = 345374 1796669
AFLR3 GG : Nodes, Elements = 345374 1760788
AFLR3 GG : Nodes, Elements = 378925 1861761
AFLR3 GG : Nodes, Elements = 378925 1993110
AFLR3 GG : Nodes, Elements = 378925 1960169
AFLR3 GG : Nodes, Elements = 411461 2058056
AFLR3 GG : Nodes, Elements = 411461 2184587
AFLR3 GG : Nodes, Elements = 411461 2152891
AFLR3 GG : Nodes, Elements = 443112 2248182
AFLR3 GG : Nodes, Elements = 443112 2371784
AFLR3 GG : Nodes, Elements = 443112 2340710
AFLR3 GG : Nodes, Elements = 473548 2432312
AFLR3 GG : Nodes, Elements = 473548 2552093
AFLR3 GG : Nodes, Elements = 473548 2521057
AFLR3 GG : Nodes, Elements = 502892 2609389
AFLR3 GG : Nodes, Elements = 502892 2724830
AFLR3 GG : Nodes, Elements = 502892 2695426
AFLR3 GG : Nodes, Elements = 531293 2780879
AFLR3 GG : Nodes, Elements = 531293 2892730
AFLR3 GG : Nodes, Elements = 531293 2864350
AFLR3 GG : Nodes, Elements = 558794 2947116
AFLR3 GG : Nodes, Elements = 558794 3053977
AFLR3 GG : Nodes, Elements = 558794 3027479
AFLR3 GG : Nodes, Elements = 585079 3106574
AFLR3 GG : Nodes, Elements = 585079 3208642
AFLR3 GG : Nodes, Elements = 585079 3183527
AFLR3 GG : Nodes, Elements = 610505 3260009
AFLR3 GG : Nodes, Elements = 610505 3358804
AFLR3 GG : Nodes, Elements = 610505 3334322
AFLR3 GG : Nodes, Elements = 635099 3408333
AFLR3 GG : Nodes, Elements = 635099 3504302
AFLR3 GG : Nodes, Elements = 635099 3480288
AFLR3 GG : Nodes, Elements = 658851 3551719
AFLR3 GG : Nodes, Elements = 658851 3643539
AFLR3 GG : Nodes, Elements = 658851 3621028
AFLR3 GG : Nodes, Elements = 681666 3689667
AFLR3 GG : Nodes, Elements = 681666 3778766
AFLR3 GG : Nodes, Elements = 681666 3756529
AFLR3 GG : Nodes, Elements = 703837 3823217
AFLR3 GG : Nodes, Elements = 703837 3909372
AFLR3 GG : Nodes, Elements = 703837 3887888
AFLR3 GG : Nodes, Elements = 725158 3951988
AFLR3 GG : Nodes, Elements = 725158 4034454
AFLR3 GG : Nodes, Elements = 725158 4014246
AFLR3 GG : Nodes, Elements = 745652 4075851
AFLR3 GG : Nodes, Elements = 745652 4155349
AFLR3 GG : Nodes, Elements = 745652 4135924
AFLR3 GG : Nodes, Elements = 765434 4195370
AFLR3 GG : Nodes, Elements = 765434 4271915
AFLR3 GG : Nodes, Elements = 765434 4252991
AFLR3 GG : Nodes, Elements = 784582 4310530
AFLR3 GG : Nodes, Elements = 784582 4385833
AFLR3 GG : Nodes, Elements = 784582 4366802
AFLR3 GG : Nodes, Elements = 803082 4422397
AFLR3 GG : Nodes, Elements = 803082 4494089
AFLR3 GG : Nodes, Elements = 803082 4476525
AFLR3 GG : Nodes, Elements = 820791 4529733
AFLR3 GG : Nodes, Elements = 820791 4598745
AFLR3 GG : Nodes, Elements = 820791 4581657
AFLR3 GG : Nodes, Elements = 837830 4632848
AFLR3 GG : Nodes, Elements = 837830 4699294
AFLR3 GG : Nodes, Elements = 837830 4682938
AFLR3 GG : Nodes, Elements = 854503 4733003
AFLR3 GG : Nodes, Elements = 854503 4797490
AFLR3 GG : Nodes, Elements = 854503 4781899
AFLR3 GG : Nodes, Elements = 870424 4829702
AFLR3 GG : Nodes, Elements = 870424 4891624
AFLR3 GG : Nodes, Elements = 870424 4876102
AFLR3 GG : Nodes, Elements = 885805 4922291
AFLR3 GG : Nodes, Elements = 885805 4981472
AFLR3 GG : Nodes, Elements = 885805 4967212
AFLR3 GG : Nodes, Elements = 900588 5011608
AFLR3 GG : Nodes, Elements = 900588 5068491
AFLR3 GG : Nodes, Elements = 900588 5054733
AFLR3 GG : Nodes, Elements = 914877 5097644
AFLR3 GG : Nodes, Elements = 914877 5153115
AFLR3 GG : Nodes, Elements = 914877 5139221
AFLR3 GG : Nodes, Elements = 928570 5180323
AFLR3 GG : Nodes, Elements = 928570 5233321
AFLR3 GG : Nodes, Elements = 928570 5220381
AFLR3 GG : Nodes, Elements = 941719 5259855
AFLR3 GG : Nodes, Elements = 941719 5310534
AFLR3 GG : Nodes, Elements = 941719 5298325
AFLR3 GG : Nodes, Elements = 954683 5337236
AFLR3 GG : Nodes, Elements = 954683 5386713
AFLR3 GG : Nodes, Elements = 954683 5374852
AFLR3 GG : Nodes, Elements = 967367 5412930
AFLR3 GG : Nodes, Elements = 967367 5462247
AFLR3 GG : Nodes, Elements = 967367 5449893
AFLR3 GG : Nodes, Elements = 979708 5486924
AFLR3 GG : Nodes, Elements = 979708 5534306
AFLR3 GG : Nodes, Elements = 979708 5522874
AFLR3 GG : Nodes, Elements = 991642 5558690
AFLR3 GG : Nodes, Elements = 991642 5604904
AFLR3 GG : Nodes, Elements = 991642 5593457
AFLR3 GG : Nodes, Elements = 1003166 5628042
AFLR3 GG : Nodes, Elements = 1003166 5672643
AFLR3 GG : Nodes, Elements = 1003166 5661590
AFLR3 GG : Nodes, Elements = 1014374 5695225
AFLR3 GG : Nodes, Elements = 1014374 5738236
AFLR3 GG : Nodes, Elements = 1014374 5727866
AFLR3 GG : Nodes, Elements = 1025085 5760010
AFLR3 GG : Nodes, Elements = 1025085 5801881
AFLR3 GG : Nodes, Elements = 1025085 5791266
AFLR3 GG : Nodes, Elements = 1035336 5822028
AFLR3 GG : Nodes, Elements = 1035336 5861295
AFLR3 GG : Nodes, Elements = 1035336 5851793
AFLR3 GG : Nodes, Elements = 1044896 5880484
AFLR3 GG : Nodes, Elements = 1044896 5917028
AFLR3 GG : Nodes, Elements = 1044896 5908078
AFLR3 GG : Nodes, Elements = 1053896 5935090
AFLR3 GG : Nodes, Elements = 1053896 5969750
AFLR3 GG : Nodes, Elements = 1053896 5961217
AFLR3 GG : Nodes, Elements = 1062332 5986533
AFLR3 GG : Nodes, Elements = 1062332 6018832
AFLR3 GG : Nodes, Elements = 1062332 6010896
AFLR3 GG : Nodes, Elements = 1070082 6034154
AFLR3 GG : Nodes, Elements = 1070082 6064554
AFLR3 GG : Nodes, Elements = 1070082 6056725
AFLR3 GG : Nodes, Elements = 1077317 6078438
AFLR3 GG : Nodes, Elements = 1077317 6106556
AFLR3 GG : Nodes, Elements = 1077317 6099606
AFLR3 GG : Nodes, Elements = 1083710 6118792
AFLR3 GG : Nodes, Elements = 1083710 6143419
AFLR3 GG : Nodes, Elements = 1083710 6137175
AFLR3 GG : Nodes, Elements = 1089155 6153515
AFLR3 GG : Nodes, Elements = 1089155 6175097
AFLR3 GG : Nodes, Elements = 1089155 6169409
AFLR3 GG : Nodes, Elements = 1093772 6183263
AFLR3 GG : Nodes, Elements = 1093772 6201287
AFLR3 GG : Nodes, Elements = 1093772 6196612
AFLR3 GG : Nodes, Elements = 1097610 6208130
AFLR3 GG : Nodes, Elements = 1097610 6223008
AFLR3 GG : Nodes, Elements = 1097610 6219256
AFLR3 GG : Nodes, Elements = 1100610 6228262
AFLR3 GG : Nodes, Elements = 1100610 6240091
AFLR3 GG : Nodes, Elements = 1100610 6236944
AFLR3 GG : Nodes, Elements = 1102997 6244110
AFLR3 GG : Nodes, Elements = 1102997 6253372
AFLR3 GG : Nodes, Elements = 1102997 6250910
AFLR3 GG : Nodes, Elements = 1104853 6256478
AFLR3 GG : Nodes, Elements = 1104853 6263639
AFLR3 GG : Nodes, Elements = 1104853 6261816
AFLR3 GG : Nodes, Elements = 1106240 6265978
AFLR3 GG : Nodes, Elements = 1106240 6271482
AFLR3 GG : Nodes, Elements = 1106240 6269937
AFLR3 GG : Nodes, Elements = 1107246 6272959
AFLR3 GG : Nodes, Elements = 1107246 6276904
AFLR3 GG : Nodes, Elements = 1107246 6275810
AFLR3 GG : Nodes, Elements = 1107939 6277890
AFLR3 GG : Nodes, Elements = 1107939 6280627
AFLR3 GG : Nodes, Elements = 1107939 6279853
AFLR3 GG : Nodes, Elements = 1108430 6281327
AFLR3 GG : Nodes, Elements = 1108430 6283334
AFLR3 GG : Nodes, Elements = 1108430 6282741
AFLR3 GG : Nodes, Elements = 1108784 6283803
AFLR3 GG : Nodes, Elements = 1108784 6285169
AFLR3 GG : Nodes, Elements = 1108784 6284800
AFLR3 GG : Nodes, Elements = 1108996 6285436
AFLR3 GG : Nodes, Elements = 1108996 6286284
AFLR3 GG : Nodes, Elements = 1108996 6286027
AFLR3 GG : Nodes, Elements = 1109132 6286435
AFLR3 GG : Nodes, Elements = 1109132 6287005
AFLR3 GG : Nodes, Elements = 1109132 6286813
AFLR3 GG : Nodes, Elements = 1109190 6286987
AFLR3 GG : Nodes, Elements = 1109190 6287235
AFLR3 GG : Nodes, Elements = 1109190 6287150
AFLR3 GG : Nodes, Elements = 1109219 6287237
AFLR3 GG : Nodes, Elements = 1109219 6287363
AFLR3 GG : Nodes, Elements = 1109219 6287320
AFLR3 GG : Nodes, Elements = 1109229 6287350
AFLR3 GG : Nodes, Elements = 1109229 6287394
AFLR3 GG : Nodes, Elements = 1109229 6287375
AFLR3 GG : Nodes, Elements = 1109233 6287387
AFLR3 GG : Nodes, Elements = 1109233 6287402
AFLR3 GG : Nodes, Elements = 1109233 6287398
AFLR3 GG : Nodes, Elements = 1109328 6287683
AFLR3 GG : Nodes, Elements = 1109328 6288208
AFLR3 GG : Nodes, Elements = 1109328 6287904
AFLR3 GG : Nodes, Elements = 1109355 6287985
AFLR3 GG : Nodes, Elements = 1109355 6288087
AFLR3 GG : Nodes, Elements = 1109355 6288056
AFLR3 GG : Nodes, Elements = 1109359 6288068
AFLR3 GG : Nodes, Elements = 1109359 6288082
AFLR3 GG : Nodes, Elements = 1109359 6288078
AFLR3 GG : Nodes, Elements = 1109360 6288081
AFLR3 GG : Nodes, Elements = 1109360 6288086
AFLR3 GG : Nodes, Elements = 1109360 6288084
AFLR3 GG : Nodes, Elements = 1109361 6288087
AFLR3 GG : Nodes, Elements = 1109361 6288090
AFLR3 GG : Nodes, Elements = 1109361 6288089
AFLR3 : CPU Time = 3.402 minutes
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 1109361 6288089
AFLR3 QI : Nodes, Elements = 1104673 6261692
AFLR3 QI : Nodes, Elements = 1103868 6257089
AFLR3 QI : Nodes, Elements = 1103699 6256141
AFLR3 QI : Nodes, Elements = 1103677 6256025
AFLR3 QI : Nodes, Elements = 1103674 6256006
AFLR3 QI : Nodes, Elements = 1103674 6278209
AFLR3 QI : Nodes, Elements = 1103674 6255082
AFLR3 QI : Nodes, Elements = 1103674 6244296
AFLR3 QI : Nodes, Elements = 1103674 6246194
AFLR3 QI : Nodes, Elements = 1103674 6242316
AFLR3 QI : Nodes, Elements = 1103674 6241086
AFLR3 QI : Nodes, Elements = 1103674 6242231
AFLR3 QI : Nodes, Elements = 1103674 6240808
AFLR3 QI : Nodes, Elements = 1103674 6240349
AFLR3 QI : Nodes, Elements = 1103674 6241362
AFLR3 QI : Nodes, Elements = 1103674 6240249
AFLR3 QI : Nodes, Elements = 1103674 6239992
AFLR3 QI : Nodes, Elements = 1103674 6240962
AFLR3 QI : Nodes, Elements = 1103674 6239957
AFLR3 QI : Nodes, Elements = 1103674 6239826
AFLR3 : CPU Time = 55.823 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 6239826
UG3 : Min, Max Ang = 5.227 161.3
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 2
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 6239826
UG3 : Min Vol = 1.65e-05
UG3 : Average Vol = 9.56e+03
UG3 : Total-Tet-Vol = 5.96e+10
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 6239826
UG3 : Min, Max Q = 0.0399 1
UG3 : Average Q = 0.909
UG3 : No. Q< 0.1 = 10
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 4.611 minutes
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 6239826
UG3 : Min, Max Ang = 5.227 161.3
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 2
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 6239826
UG3 : Min Vol = 1.65e-05
UG3 : Average Vol = 9.56e+03
UG3 : Total-Tet-Vol = 5.96e+10
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 6239826
UG3 : Min, Max Q = 0.197 1
UG3 : Average Q = 0.872
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 31
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 33
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 35
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 36
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 37
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 38
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 39
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 40
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 41
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 42
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 43
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 44
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 45
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 46
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 19
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 20
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 21
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 22
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 23
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 24
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 19
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 20
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 21
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 22
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 23
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 24
Volume mesh:
Number of nodes = 1103674
Number of elements = 6430898
Number of triangles = 191072
Number of quadrilatarals = 0
Number of tetrahedrals = 6239826
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
real 5m21.254s
user 5m7.707s
sys 0m6.927s
+ status=0
+ set +x
=================================================
data/session07/09_aflr4_aflr3_InviscidWing.py passed (as expected)
=================================================
=================================================
10_aflr4_aflr3_ViscousWing.py test;
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
+ python 10_aflr4_aflr3_ViscousWing.py
MESSAGE:: Building wingOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 6
EGADS : 2 Yes 0 0 1 0 1 1 4 5
EGADS : 3 Yes 0 0 1 0 1 1 4 8
EGADS : 4 Yes 0 0 1 0 1 2 3 5
EGADS : 5 Yes 0 0 1 0 1 2 4
EGADS : 6 Yes 0 0 1 0 1 1 7 8
EGADS : 7 Yes 0 0 1 0 1 6 9 10
EGADS : 8 Yes 0 0 1 0 1 3 6 9
EGADS : 9 Yes 0 0 1 0 1 7 8 10
EGADS : 10 Yes 0 0 1 0 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 2651.51
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 5
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1107 2082 0
AFLR4 : Nodes, Trias,Quads= 685 1238 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1473 2759 0
AFLR4 : Nodes, Trias,Quads= 721 1255 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1116 2100 0
AFLR4 : Nodes, Trias,Quads= 671 1210 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1458 2729 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1108 2084 0
AFLR4 : Nodes, Trias,Quads= 683 1234 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 1488 2789 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1112 2092 0
AFLR4 : Nodes, Trias,Quads= 653 1174 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1456 2725 0
AFLR4 : Nodes, Trias,Quads= 708 1229 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 4933 9858 1312
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 4933 9858
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1115 2096 0
AFLR4 : Nodes, Trias,Quads= 948 1762 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1450 2716 0
AFLR4 : Nodes, Trias,Quads= 1183 2182 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1125 2116 0
AFLR4 : Nodes, Trias,Quads= 936 1738 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1477 2769 0
AFLR4 : Nodes, Trias,Quads= 1165 2145 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 26 35 0
AFLR4 : Nodes, Trias,Quads= 15 13 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1106 2078 0
AFLR4 : Nodes, Trias,Quads= 957 1780 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 1453 2723 0
AFLR4 : Nodes, Trias,Quads= 1179 2175 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1118 2102 0
AFLR4 : Nodes, Trias,Quads= 953 1772 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1477 2770 0
AFLR4 : Nodes, Trias,Quads= 1147 2110 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 26 35 0
AFLR4 : Nodes, Trias,Quads= 15 13 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 7867 15726 1334
OVERALL : CPU Time = 0.378 seconds
Body 1 (of 2)
Number of nodes = 7847
Number of elements = 15690
Number of triangle elements = 15690
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7867
Total number of elements = 15726
Total number of triangle elements = 15726
Total number of quadrilateral elements = 0
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Wing
2: Farfield
Finished writing vtk file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mbl = 1
UG PARAM : nbl = 10
UG PARAM : mblelc = 2
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mbl = 1
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mblelc = 1
UG PARAM : BC_IDs [ 0]= 1
UG PARAM : BC_IDs [ 1]= 2
UG PARAM : BC_IDs [ 2]= 3
UG PARAM : BC_IDs [ 3]= 4
UG PARAM : BC_IDs [ 4]= 5
UG PARAM : BC_IDs [ 5]= 6
UG PARAM : BC_IDs [ 6]= 7
UG PARAM : BC_IDs [ 7]= 8
UG PARAM : BC_IDs [ 8]= 9
UG PARAM : BC_IDs [ 9]= 10
UG PARAM : BC_IDs [10]= 11
UG PARAM : BC_IDs [11]= 12
UG PARAM : BC_IDs [12]= 13
UG PARAM : BC_IDs [13]= 14
UG PARAM : BC_IDs [14]= 15
UG PARAM : BC_IDs [15]= 16
UG PARAM : BL_DS [ 0]= 0.217051
UG PARAM : BL_DS [ 1]= 0.217051
UG PARAM : BL_DS [ 2]= 0.217051
UG PARAM : BL_DS [ 3]= 0.217051
UG PARAM : BL_DS [ 4]= 0.217051
UG PARAM : BL_DS [ 5]= 0.217051
UG PARAM : BL_DS [ 6]= 0.217051
UG PARAM : BL_DS [ 7]= 0.217051
UG PARAM : BL_DS [ 8]= 0.217051
UG PARAM : BL_DS [ 9]= 0.217051
UG PARAM : BL_DS [10]= 0.217051
UG PARAM : BL_DS [11]= 0.217051
UG PARAM : BL_DS [12]= 0.217051
UG PARAM : BL_DS [13]= 0.217051
UG PARAM : BL_DS [14]= 0.217051
UG PARAM : BL_DS [15]= 0.217051
UG PARAM : BL_DEL [ 0]= 2.17051
UG PARAM : BL_DEL [ 1]= 2.17051
UG PARAM : BL_DEL [ 2]= 2.17051
UG PARAM : BL_DEL [ 3]= 2.17051
UG PARAM : BL_DEL [ 4]= 2.17051
UG PARAM : BL_DEL [ 5]= 2.17051
UG PARAM : BL_DEL [ 6]= 2.17051
UG PARAM : BL_DEL [ 7]= 2.17051
UG PARAM : BL_DEL [ 8]= 2.17051
UG PARAM : BL_DEL [ 9]= 2.17051
UG PARAM : BL_DEL [10]= 2.17051
UG PARAM : BL_DEL [11]= 2.17051
UG PARAM : BL_DEL [12]= 2.17051
UG PARAM : BL_DEL [13]= 2.17051
UG PARAM : BL_DEL [14]= 2.17051
UG PARAM : BL_DEL [15]= 2.17051
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 6
EGADS : 2 Yes 0 0 1 0 1 1 4 5
EGADS : 3 Yes 0 0 1 0 1 1 4 8
EGADS : 4 Yes 0 0 1 0 1 2 3 5
EGADS : 5 Yes 0 0 1 0 1 2 4
EGADS : 6 Yes 0 0 1 0 1 1 7 8
EGADS : 7 Yes 0 0 1 0 1 6 9 10
EGADS : 8 Yes 0 0 1 0 1 3 6 9
EGADS : 9 Yes 0 0 1 0 1 7 8 10
EGADS : 10 Yes 0 0 1 0 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 13.1976
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 428.309
AFLR4 : Abs Min Surf Spacing = 0.032994
AFLR4 : Min Surf Spacing = 0.065988
AFLR4 : Max Surf Spacing = 1.31976
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 15726
AFLR43 : Nodes = 7867
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mbl = 1
UG PARAM : nbl = 10
UG PARAM : mblelc = 2
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mbl = 1
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mblelc = 1
UG PARAM : BC_IDs [ 0]= 1
UG PARAM : BC_IDs [ 1]= 2
UG PARAM : BC_IDs [ 2]= 3
UG PARAM : BC_IDs [ 3]= 4
UG PARAM : BC_IDs [ 4]= 5
UG PARAM : BC_IDs [ 5]= 6
UG PARAM : BC_IDs [ 6]= 7
UG PARAM : BC_IDs [ 7]= 8
UG PARAM : BC_IDs [ 8]= 9
UG PARAM : BC_IDs [ 9]= 10
UG PARAM : BC_IDs [10]= 11
UG PARAM : BC_IDs [11]= 12
UG PARAM : BC_IDs [12]= 13
UG PARAM : BC_IDs [13]= 14
UG PARAM : BC_IDs [14]= 15
UG PARAM : BC_IDs [15]= 16
UG PARAM : BL_DS [ 0]= 0.217051
UG PARAM : BL_DS [ 1]= 0.217051
UG PARAM : BL_DS [ 2]= 0.217051
UG PARAM : BL_DS [ 3]= 0.217051
UG PARAM : BL_DS [ 4]= 0.217051
UG PARAM : BL_DS [ 5]= 0.217051
UG PARAM : BL_DS [ 6]= 0.217051
UG PARAM : BL_DS [ 7]= 0.217051
UG PARAM : BL_DS [ 8]= 0.217051
UG PARAM : BL_DS [ 9]= 0.217051
UG PARAM : BL_DS [10]= 0.217051
UG PARAM : BL_DS [11]= 0.217051
UG PARAM : BL_DS [12]= 0.217051
UG PARAM : BL_DS [13]= 0.217051
UG PARAM : BL_DS [14]= 0.217051
UG PARAM : BL_DS [15]= 0.217051
UG PARAM : BL_DEL [ 0]= 2.17051
UG PARAM : BL_DEL [ 1]= 2.17051
UG PARAM : BL_DEL [ 2]= 2.17051
UG PARAM : BL_DEL [ 3]= 2.17051
UG PARAM : BL_DEL [ 4]= 2.17051
UG PARAM : BL_DEL [ 5]= 2.17051
UG PARAM : BL_DEL [ 6]= 2.17051
UG PARAM : BL_DEL [ 7]= 2.17051
UG PARAM : BL_DEL [ 8]= 2.17051
UG PARAM : BL_DEL [ 9]= 2.17051
UG PARAM : BL_DEL [10]= 2.17051
UG PARAM : BL_DEL [11]= 2.17051
UG PARAM : BL_DEL [12]= 2.17051
UG PARAM : BL_DEL [13]= 2.17051
UG PARAM : BL_DEL [14]= 2.17051
UG PARAM : BL_DEL [15]= 2.17051
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 7867 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid w/BL
UG3 : 2 Solid w/BL
UG3 : 3 Solid w/BL
UG3 : 4 Solid w/BL
UG3 : 5 Solid w/BL
UG3 : 6 Solid w/BL
UG3 : 7 Solid w/BL
UG3 : 8 Solid w/BL
UG3 : 9 Solid w/BL
UG3 : 10 Solid w/BL
UG3 : 11 FarField
UG3 : 12 FarField
UG3 : 13 FarField
UG3 : 14 FarField
UG3 : 15 FarField
UG3 : 16 FarField
AFLR3 : CPU Time = 0.023 seconds
AFLR3 : DONE
ANBL3 : ---------------------------------------
ANBL3 : ANBL3 LIBRARY
ANBL3 : ADVANCING-NORMAL
ANBL3 : BOUNDARY-LAYER (BL)
ANBL3 : STRUCTURED-LAYER (SL)
ANBL3 : SPECIFIED NORMAL SPACING (SNS)
ANBL3 : TETRAHEDRAL/PENTAHEDRAL GRID GENERATOR
ANBL3 : Version Number 9.34.2
ANBL3 : Version Date 03/10/23 @ 04:32PM
ANBL3 : Compile OS Darwin 22.6.0 x86_64
ANBL3 : Compile Date 11/01/23 @ 12:20PM
ANBL3 : Copyright 1994-2021, D.L. Marcum
ANBL3 : ---------------------------------------
ANBL3 BLC: BL BOUNDARY CONDITIONS CHECK
ANBL3 BLC: Nodes, Elements = 7867 0
ANBL3 : CPU Time = 0.017 seconds
ANBL3 : DONE
ANBL3 BLG: BL NODE GENERATION
ANBL3 BLG: Nodes, Layer = 0 0
ANBL3 BLG: Nodes, Layer = 15694 2
ANBL3 BLG: Nodes, Layer = 23541 3
ANBL3 BLG: Nodes, Layer = 31384 4
ANBL3 BLG: Nodes, Layer = 39209 5
ANBL3 BLG: Nodes, Layer = 47034 6
ANBL3 BLG: Nodes, Layer = 62668 8
ANBL3 BLG: Nodes, Layer = 70485 9
ANBL3 BLG: Nodes, Layer = 78298 10
ANBL3 BLG: Nodes, Layer = 86108 11
ANBL3 : CPU Time = 4.084 seconds
ANBL3 : DONE
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 7867 0
AFLR3 : CPU Time = 0.012 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 7867 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1574 11548
AFLR3 IG : Nodes, Elements = 3148 23433
AFLR3 IG : Nodes, Elements = 4722 34747
AFLR3 IG : Nodes, Elements = 6296 47989
AFLR3 IG : Nodes, Elements = 7870 61771
AFLR3 IG : Nodes, Elements = 7874 61704
AFLR3 IG : Nodes, Elements = 7874 61705
AFLR3 IG : Nodes, Elements = 7874 61620
AFLR3 IG : Nodes, Elements = 7874 61703
AFLR3 IG : Nodes, Elements = 7874 61495
AFLR3 IG : Nodes, Elements = 7874 61496
AFLR3 IG : Nodes, Elements = 7867 38596
AFLR3 IG : Nodes, Elements = 7867 38782
AFLR3 IG : Nodes, Elements = 7867 29846
AFLR3 IG : Nodes, Elements = 7867 25854
AFLR3 : CPU Time = 0.379 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 7867 25854
AFLR3 GG : Nodes, Elements = 10937 35181
AFLR3 GG : Nodes, Elements = 10937 46901
AFLR3 GG : Nodes, Elements = 10937 42992
AFLR3 GG : Nodes, Elements = 13491 50995
AFLR3 GG : Nodes, Elements = 13491 61245
AFLR3 GG : Nodes, Elements = 13491 57321
AFLR3 GG : Nodes, Elements = 16586 66820
AFLR3 GG : Nodes, Elements = 16586 79524
AFLR3 GG : Nodes, Elements = 16586 75473
AFLR3 GG : Nodes, Elements = 19702 84956
AFLR3 GG : Nodes, Elements = 19702 97713
AFLR3 GG : Nodes, Elements = 19702 93907
AFLR3 GG : Nodes, Elements = 22862 103501
AFLR3 GG : Nodes, Elements = 22862 116278
AFLR3 GG : Nodes, Elements = 22862 112708
AFLR3 GG : Nodes, Elements = 25966 122101
AFLR3 GG : Nodes, Elements = 25966 134533
AFLR3 GG : Nodes, Elements = 25966 131184
AFLR3 GG : Nodes, Elements = 29094 140634
AFLR3 GG : Nodes, Elements = 29094 152868
AFLR3 GG : Nodes, Elements = 29094 149663
AFLR3 GG : Nodes, Elements = 32148 158884
AFLR3 GG : Nodes, Elements = 32148 171160
AFLR3 GG : Nodes, Elements = 32148 167888
AFLR3 GG : Nodes, Elements = 35096 176780
AFLR3 GG : Nodes, Elements = 35096 188437
AFLR3 GG : Nodes, Elements = 35096 185289
AFLR3 GG : Nodes, Elements = 37921 193821
AFLR3 GG : Nodes, Elements = 37921 205051
AFLR3 GG : Nodes, Elements = 37921 202109
AFLR3 GG : Nodes, Elements = 40600 210174
AFLR3 GG : Nodes, Elements = 40600 220760
AFLR3 GG : Nodes, Elements = 40600 217997
AFLR3 GG : Nodes, Elements = 43121 225594
AFLR3 GG : Nodes, Elements = 43121 235553
AFLR3 GG : Nodes, Elements = 43121 233075
AFLR3 GG : Nodes, Elements = 45550 240384
AFLR3 GG : Nodes, Elements = 45550 249946
AFLR3 GG : Nodes, Elements = 45550 247498
AFLR3 GG : Nodes, Elements = 47861 254455
AFLR3 GG : Nodes, Elements = 47861 263545
AFLR3 GG : Nodes, Elements = 47861 261218
AFLR3 GG : Nodes, Elements = 50001 267656
AFLR3 GG : Nodes, Elements = 50001 276103
AFLR3 GG : Nodes, Elements = 50001 274015
AFLR3 GG : Nodes, Elements = 52057 280202
AFLR3 GG : Nodes, Elements = 52057 288215
AFLR3 GG : Nodes, Elements = 52057 286177
AFLR3 GG : Nodes, Elements = 53968 291927
AFLR3 GG : Nodes, Elements = 53968 299418
AFLR3 GG : Nodes, Elements = 53968 297519
AFLR3 GG : Nodes, Elements = 55797 303017
AFLR3 GG : Nodes, Elements = 55797 310220
AFLR3 GG : Nodes, Elements = 55797 308413
AFLR3 GG : Nodes, Elements = 57514 313575
AFLR3 GG : Nodes, Elements = 57514 320309
AFLR3 GG : Nodes, Elements = 57514 318605
AFLR3 GG : Nodes, Elements = 59138 323487
AFLR3 GG : Nodes, Elements = 59138 329878
AFLR3 GG : Nodes, Elements = 59138 328288
AFLR3 GG : Nodes, Elements = 60665 332879
AFLR3 GG : Nodes, Elements = 60665 338849
AFLR3 GG : Nodes, Elements = 60665 337396
AFLR3 GG : Nodes, Elements = 62088 341681
AFLR3 GG : Nodes, Elements = 62088 347262
AFLR3 GG : Nodes, Elements = 62088 345875
AFLR3 GG : Nodes, Elements = 63415 349869
AFLR3 GG : Nodes, Elements = 63415 355081
AFLR3 GG : Nodes, Elements = 63415 353749
AFLR3 GG : Nodes, Elements = 64681 357555
AFLR3 GG : Nodes, Elements = 64681 362539
AFLR3 GG : Nodes, Elements = 64681 361280
AFLR3 GG : Nodes, Elements = 65896 364937
AFLR3 GG : Nodes, Elements = 65896 369721
AFLR3 GG : Nodes, Elements = 65896 368510
AFLR3 GG : Nodes, Elements = 67015 371873
AFLR3 GG : Nodes, Elements = 67015 376277
AFLR3 GG : Nodes, Elements = 67015 375206
AFLR3 GG : Nodes, Elements = 68063 378354
AFLR3 GG : Nodes, Elements = 68063 382406
AFLR3 GG : Nodes, Elements = 68063 381404
AFLR3 GG : Nodes, Elements = 69051 384371
AFLR3 GG : Nodes, Elements = 69051 388233
AFLR3 GG : Nodes, Elements = 69051 387236
AFLR3 GG : Nodes, Elements = 69962 389972
AFLR3 GG : Nodes, Elements = 69962 393606
AFLR3 GG : Nodes, Elements = 69962 392683
AFLR3 GG : Nodes, Elements = 70813 395239
AFLR3 GG : Nodes, Elements = 70813 398541
AFLR3 GG : Nodes, Elements = 70813 397699
AFLR3 GG : Nodes, Elements = 71605 400080
AFLR3 GG : Nodes, Elements = 71605 403145
AFLR3 GG : Nodes, Elements = 71605 402371
AFLR3 GG : Nodes, Elements = 72325 404534
AFLR3 GG : Nodes, Elements = 72325 407380
AFLR3 GG : Nodes, Elements = 72325 406682
AFLR3 GG : Nodes, Elements = 72949 408557
AFLR3 GG : Nodes, Elements = 72949 411007
AFLR3 GG : Nodes, Elements = 72949 410361
AFLR3 GG : Nodes, Elements = 73486 411973
AFLR3 GG : Nodes, Elements = 73486 414144
AFLR3 GG : Nodes, Elements = 73486 413559
AFLR3 GG : Nodes, Elements = 73944 414934
AFLR3 GG : Nodes, Elements = 73944 416807
AFLR3 GG : Nodes, Elements = 73944 416302
AFLR3 GG : Nodes, Elements = 74335 417475
AFLR3 GG : Nodes, Elements = 74335 419040
AFLR3 GG : Nodes, Elements = 74335 418581
AFLR3 GG : Nodes, Elements = 74664 419570
AFLR3 GG : Nodes, Elements = 74664 420885
AFLR3 GG : Nodes, Elements = 74664 420532
AFLR3 GG : Nodes, Elements = 74936 421350
AFLR3 GG : Nodes, Elements = 74936 422382
AFLR3 GG : Nodes, Elements = 74936 422107
AFLR3 GG : Nodes, Elements = 75170 422810
AFLR3 GG : Nodes, Elements = 75170 423744
AFLR3 GG : Nodes, Elements = 75170 423506
AFLR3 GG : Nodes, Elements = 75376 424125
AFLR3 GG : Nodes, Elements = 75376 424899
AFLR3 GG : Nodes, Elements = 75376 424685
AFLR3 GG : Nodes, Elements = 75544 425189
AFLR3 GG : Nodes, Elements = 75544 425885
AFLR3 GG : Nodes, Elements = 75544 425693
AFLR3 GG : Nodes, Elements = 75685 426117
AFLR3 GG : Nodes, Elements = 75685 426656
AFLR3 GG : Nodes, Elements = 75685 426519
AFLR3 GG : Nodes, Elements = 75771 426777
AFLR3 GG : Nodes, Elements = 75771 427115
AFLR3 GG : Nodes, Elements = 75771 427006
AFLR3 GG : Nodes, Elements = 75832 427190
AFLR3 GG : Nodes, Elements = 75832 427467
AFLR3 GG : Nodes, Elements = 75832 427374
AFLR3 GG : Nodes, Elements = 75870 427488
AFLR3 GG : Nodes, Elements = 75870 427649
AFLR3 GG : Nodes, Elements = 75870 427583
AFLR3 GG : Nodes, Elements = 75892 427649
AFLR3 GG : Nodes, Elements = 75892 427761
AFLR3 GG : Nodes, Elements = 75892 427712
AFLR3 GG : Nodes, Elements = 75900 427736
AFLR3 GG : Nodes, Elements = 75900 427785
AFLR3 GG : Nodes, Elements = 75900 427761
AFLR3 GG : Nodes, Elements = 75905 427776
AFLR3 GG : Nodes, Elements = 75905 427798
AFLR3 GG : Nodes, Elements = 75905 427787
AFLR3 GG : Nodes, Elements = 75907 427793
AFLR3 GG : Nodes, Elements = 75907 427800
AFLR3 GG : Nodes, Elements = 75907 427797
AFLR3 GG : Nodes, Elements = 75908 427800
AFLR3 GG : Nodes, Elements = 75908 427803
AFLR3 GG : Nodes, Elements = 75908 427802
AFLR3 GG : Nodes, Elements = 75912 427814
AFLR3 GG : Nodes, Elements = 75912 427836
AFLR3 GG : Nodes, Elements = 75912 427826
AFLR3 : CPU Time = 6.444 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 75912 427826
AFLR3 QI : Nodes, Elements = 75488 425463
AFLR3 QI : Nodes, Elements = 75435 425168
AFLR3 QI : Nodes, Elements = 75432 425150
AFLR3 QI : Nodes, Elements = 75432 427355
AFLR3 QI : Nodes, Elements = 75432 424919
AFLR3 QI : Nodes, Elements = 75432 423819
AFLR3 QI : Nodes, Elements = 75432 425898
AFLR3 QI : Nodes, Elements = 75432 423890
AFLR3 QI : Nodes, Elements = 75432 423752
AFLR3 QI : Nodes, Elements = 75432 424639
AFLR3 QI : Nodes, Elements = 75432 423702
AFLR3 QI : Nodes, Elements = 75432 423576
AFLR3 QI : Nodes, Elements = 75432 424262
AFLR3 QI : Nodes, Elements = 75432 423581
AFLR3 QI : Nodes, Elements = 75432 423504
AFLR3 QI : Nodes, Elements = 75432 424154
AFLR3 QI : Nodes, Elements = 75432 423540
AFLR3 QI : Nodes, Elements = 75432 423475
AFLR3 QI : Nodes, Elements = 75432 423466
AFLR3 : CPU Time = 2.008 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 75432 423466
AFLR3 : CPU Time = 0.074 seconds
AFLR3 : DONE
ANBL3 BLM: BL VOLUME GRID MERGE
ANBL3 BLM: Nodes, Elements = 75432 423466
UG3 : OUTPUT GRID
UG3 : Grid File Name = .tmp.b8.ugrid
UG3 : Quad Surface Faces= 0
UG3 : Tria Surface Faces= 15726
UG3 : Nodes = 153693
UG3 : Total Elements = 580087
UG3 : Hex Elements = 0
UG3 : Pent_5 Elements = 147
UG3 : Pent_6 Elements = 156367
UG3 : Tet Elements = 423573
ANBL3 BLM: Nodes, Elements = 153693 892968
ANBL3 BLM: Nodes, Elements = 153693 107
ANBL3 : CPU Time = 0.351 seconds
ANBL3 : DONE
OVERALL : CPU Time = 13.583 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 423573
UG3 : Min, Max Ang = 0.03393 179.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 32
UG3 : No. Angle>179.9 = 1
UG3 : No. Pyramid Elems = 147
UG3 : Min, Max Ang = 8.861 172.3
UG3 : Average Angle = 80.9
UG3 : No. Angle>160.0 = 12
UG3 : No. Angle>179.9 = 0
UG3 : No. Prism Elems = 156367
UG3 : Min, Max Ang = 9.482 174.2
UG3 : Average Angle = 80
UG3 : No. Angle>160.0 = 421
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 423573
UG3 : Min Vol = 8.4e-05
UG3 : Average Vol = 1.41e+05
UG3 : Total-Tet-Vol = 5.96e+10
UG3 : No. Vol<TOL = 0
UG3 : No. Pyramid Elems = 147
UG3 : Min Vol = 0.00545
UG3 : Average Vol = 0.074
UG3 : Total-Pyramid-Vol = 10.9
UG3 : No. Vol<TOL = 0
UG3 : No. Prism Elems = 156367
UG3 : Min Vol = 0.0139
UG3 : Average Vol = 0.165
UG3 : Total-Prism-Vol = 2.58e+04
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 423573
UG3 : Min, Max Q = 0.00273 1
UG3 : Average Q = 0.854
UG3 : No. Q< 0.1 = 10
UG3 : No. Q< 0.01 = 1
UG3 : No. Pyramid Elems = 147
UG3 : Min, Max Q = 0.259 1
UG3 : Average Q = 0.754
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : No. Prism Elems = 156367
UG3 : Min, Max Q = 0.353 1
UG3 : Average Q = 0.907
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
Number of nodes = 153693
Number of elements = 595813
Number of triangles = 15726
Number of quadrilatarals = 0
Number of tetrahedrals = 423573
Number of pyramids = 147
Number of prisms = 156367
Number of hexahedrals = 0
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
real 0m20.611s
user 0m16.547s
sys 0m3.189s
+ status=0
+ set +x
=================================================
data/session07/10_aflr4_aflr3_ViscousWing.py passed (as expected)
=================================================
=================================================
11_aflr4_aflr3_ViscousWingPod.py test;
+ python 11_aflr4_aflr3_ViscousWingPod.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building nacelleOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Nacelle, index = 1
Name = Wing, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Nacelle, index = 1
Name = leftWing, index = 2
Name = riteWing, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 4 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 4 Faces
EGADS : Body 0 has 8 Edges
EGADS : Body 0 has 4 Loops
EGADS : Body 0 has 4 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 4 Faces
EGADS : Body 1 has 8 Edges
EGADS : Body 1 has 4 Loops
EGADS : Body 1 has 4 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 10 Faces
EGADS : Body 2 has 18 Edges
EGADS : Body 2 has 10 Loops
EGADS : Body 2 has 10 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 6 Faces
EGADS : Body 3 has 12 Edges
EGADS : Body 3 has 6 Loops
EGADS : Body 3 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3
EGADS : 2 Yes 0 0 1 0 1 1 4
EGADS : 3 Yes 0 0 1 0 1 1 4
EGADS : 4 Yes 0 0 1 0 1 2 3
EGADS : 5 Yes 1 0 1 0 1 6 7
EGADS : 6 Yes 1 0 1 0 1 5 8
EGADS : 7 Yes 1 0 1 0 1 5 8
EGADS : 8 Yes 1 0 1 0 1 6 7
EGADS : 9 Yes 2 0 1 0 1 10 11 14
EGADS : 10 Yes 2 0 1 0 1 9 12 13
EGADS : 11 Yes 2 0 1 0 1 9 12 16
EGADS : 12 Yes 2 0 1 0 1 10 11 13
EGADS : 13 Yes 2 0 1 0 1 10 12
EGADS : 14 Yes 2 0 1 0 1 9 15 16
EGADS : 15 Yes 2 0 1 0 1 14 17 18
EGADS : 16 Yes 2 0 1 0 1 11 14 17
EGADS : 17 Yes 2 0 1 0 1 15 16 18
EGADS : 18 Yes 2 0 1 0 1 15 17
EGADS : 19 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 20 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 21 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 22 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 23 Yes 3 0 1 NA NA 19 20 21 22
EGADS : 24 Yes 3 0 1 NA NA 19 20 21 22
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 3 2 -4
EGADS : 2 -2 5 1 -6
EGADS : 3 7 4 -8 -3
EGADS : 4 8 6 -7 -5
EGADS : 5 9 12 -10 -11
EGADS : 6 10 14 -9 -13
EGADS : 7 -15 11 16 -12
EGADS : 8 -16 13 15 -14
EGADS : 9 -17 18 19 -20
EGADS : 10 -21 20 22 -23
EGADS : 11 -19 24 17 -25
EGADS : 12 -22 25 21 -26
EGADS : 13 23 26
EGADS : 14 27 29 -28 -18
EGADS : 15 30 32 -31 -29
EGADS : 16 28 33 -27 -24
EGADS : 17 31 34 -30 -33
EGADS : 18 -32 -34
EGADS : 19 35 36 -37 -38
EGADS : 20 -39 42 41 -40
EGADS : 21 43 39 -44 -35
EGADS : 22 -45 37 46 -41
EGADS : 23 38 45 -42 -43
EGADS : 24 -36 44 40 -46
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : 19 19
EGADS : 20 20
EGADS : 21 21
EGADS : 22 22
EGADS : 23 23
EGADS : 24 24
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 3 2 -4
EGADS : 2 Yes -2 5 1 -6
EGADS : 3 Yes 7 4 -8 -3
EGADS : 4 Yes 8 6 -7 -5
EGADS : 5 Yes 9 12 -10 -11
EGADS : 6 Yes 10 14 -9 -13
EGADS : 7 Yes -15 11 16 -12
EGADS : 8 Yes -16 13 15 -14
EGADS : 9 Yes -17 18 19 -20
EGADS : 10 Yes -21 20 22 -23
EGADS : 11 Yes -19 24 17 -25
EGADS : 12 Yes -22 25 21 -26
EGADS : 13 Yes 23 26
EGADS : 14 Yes 27 29 -28 -18
EGADS : 15 Yes 30 32 -31 -29
EGADS : 16 Yes 28 33 -27 -24
EGADS : 17 Yes 31 34 -30 -33
EGADS : 18 Yes -32 -34
EGADS : 19 Yes 35 36 -37 -38
EGADS : 20 Yes -39 42 41 -40
EGADS : 21 Yes 43 39 -44 -35
EGADS : 22 Yes -45 37 46 -41
EGADS : 23 Yes 38 45 -42 -43
EGADS : 24 Yes -36 44 40 -46
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 3 4 1 1 2
EGADS : 3 0 Yes 1 3 1 1 3
EGADS : 4 0 Yes 2 4 1 1 3
EGADS : 5 0 Yes 3 1 1 2 4
EGADS : 6 0 Yes 4 2 1 2 4
EGADS : 7 0 Yes 1 2 1 3 4
EGADS : 8 0 Yes 3 4 1 3 4
EGADS : 9 1 Yes 5 6 1 5 6
EGADS : 10 1 Yes 7 8 1 5 6
EGADS : 11 1 Yes 5 7 1 5 7
EGADS : 12 1 Yes 6 8 1 5 7
EGADS : 13 1 Yes 7 5 1 6 8
EGADS : 14 1 Yes 8 6 1 6 8
EGADS : 15 1 Yes 5 6 1 7 8
EGADS : 16 1 Yes 7 8 1 7 8
EGADS : 17 2 Yes 9 10 1 9 11
EGADS : 18 2 Yes 9 11 1 9 14
EGADS : 19 2 Yes 11 12 1 9 11
EGADS : 20 2 Yes 10 12 1 9 10
EGADS : 21 2 Yes 10 13 1 10 12
EGADS : 22 2 Yes 12 14 1 10 12
EGADS : 23 2 Yes 13 14 1 10 13
EGADS : 24 2 Yes 11 9 1 11 16
EGADS : 25 2 Yes 12 10 1 11 12
EGADS : 26 2 Yes 14 13 1 12 13
EGADS : 27 2 Yes 9 15 1 14 16
EGADS : 28 2 Yes 11 16 1 14 16
EGADS : 29 2 Yes 15 16 1 14 15
EGADS : 30 2 Yes 15 17 1 15 17
EGADS : 31 2 Yes 16 18 1 15 17
EGADS : 32 2 Yes 17 18 1 15 18
EGADS : 33 2 Yes 16 15 1 16 17
EGADS : 34 2 Yes 18 17 1 17 18
EGADS : 35 3 Yes 20 19 NA 19 21
EGADS : 36 3 Yes 19 21 NA 19 24
EGADS : 37 3 Yes 22 21 NA 19 22
EGADS : 38 3 Yes 20 22 NA 19 23
EGADS : 39 3 Yes 24 23 NA 20 21
EGADS : 40 3 Yes 23 25 NA 20 24
EGADS : 41 3 Yes 26 25 NA 20 22
EGADS : 42 3 Yes 24 26 NA 20 23
EGADS : 43 3 Yes 20 24 NA 21 23
EGADS : 44 3 Yes 19 23 NA 21 24
EGADS : 45 3 Yes 22 26 NA 22 23
EGADS : 46 3 Yes 21 25 NA 22 24
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 90.5173952 0 0
EGADS : 2 Yes 90.5173952 0 0
EGADS : 3 Yes 60.5173952 0 0
EGADS : 4 Yes 60.5173952 0 0
EGADS : 5 Yes 90.5173952 29.3018771 0
EGADS : 6 Yes 90.5173952 29.3018771 0
EGADS : 7 Yes 60.5173952 29.3018771 0
EGADS : 8 Yes 60.5173952 29.3018771 0
EGADS : 9 Yes 97.2007855 0 0
EGADS : 10 Yes 97.9335611 0 0
EGADS : 11 Yes 50 0 0
EGADS : 12 Yes 75.3047874 0 0
EGADS : 13 Yes 123.552357 0 4.7180639
EGADS : 14 Yes 118.391317 0 3.99272703
EGADS : 15 Yes 97.9335611 36.1389817 0
EGADS : 16 Yes 75.3047874 36.1389817 0
EGADS : 17 Yes 123.552357 97.6729236 4.7180639
EGADS : 18 Yes 118.391317 97.6729236 3.99272703
EGADS : 19 Yes 0 0 1947.05079
EGADS : 20 Yes 0 0 0
EGADS : 21 Yes 0 1953.45847 1947.05079
EGADS : 22 Yes 0 1953.45847 0
EGADS : 23 Yes 2040.21562 0 1947.05079
EGADS : 24 Yes 2040.21562 0 0
EGADS : 25 Yes 2040.21562 1953.45847 1947.05079
EGADS : 26 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 22.2515
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 5303.02
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 10
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 FARFIELD
AFLR4 : 20 CAD geometry 0 FARFIELD
AFLR4 : 21 CAD geometry 0 FARFIELD
AFLR4 : 22 CAD geometry 0 FARFIELD
AFLR4 : 23 CAD geometry 0 FARFIELD
AFLR4 : 24 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4 : Component 2 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 146 247 0
AFLR4 : Nodes, Trias,Quads= 151 257 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 129 213 0
AFLR4 : Nodes, Trias,Quads= 115 185 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 146 247 0
AFLR4 : Nodes, Trias,Quads= 150 255 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 129 213 0
AFLR4 : Nodes, Trias,Quads= 116 187 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 146 247 0
AFLR4 : Nodes, Trias,Quads= 150 255 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 129 213 0
AFLR4 : Nodes, Trias,Quads= 116 187 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 146 247 0
AFLR4 : Nodes, Trias,Quads= 151 257 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 129 213 0
AFLR4 : Nodes, Trias,Quads= 115 185 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 427 774 0
AFLR4 : Nodes, Trias,Quads= 333 586 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 610 1113 0
AFLR4 : Nodes, Trias,Quads= 325 543 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 457 833 0
AFLR4 : Nodes, Trias,Quads= 324 567 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 586 1065 0
AFLR4 : Nodes, Trias,Quads= 313 519 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 11 12 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 428 776 0
AFLR4 : Nodes, Trias,Quads= 336 592 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 616 1125 0
AFLR4 : Nodes, Trias,Quads= 323 539 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 456 831 0
AFLR4 : Nodes, Trias,Quads= 332 583 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 585 1063 0
AFLR4 : Nodes, Trias,Quads= 314 521 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 11 12 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 3125 6242 1118
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 3125 6242
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 220 383 0
AFLR4 : Nodes, Trias,Quads= 219 381 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 204 351 0
AFLR4 : Nodes, Trias,Quads= 177 297 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 224 391 0
AFLR4 : Nodes, Trias,Quads= 219 381 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 205 353 0
AFLR4 : Nodes, Trias,Quads= 178 299 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 224 391 0
AFLR4 : Nodes, Trias,Quads= 219 381 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 205 353 0
AFLR4 : Nodes, Trias,Quads= 178 299 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 220 383 0
AFLR4 : Nodes, Trias,Quads= 219 381 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 204 351 0
AFLR4 : Nodes, Trias,Quads= 177 297 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 504 921 0
AFLR4 : Nodes, Trias,Quads= 447 807 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 638 1166 0
AFLR4 : Nodes, Trias,Quads= 470 830 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 522 956 0
AFLR4 : Nodes, Trias,Quads= 452 816 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 609 1109 0
AFLR4 : Nodes, Trias,Quads= 463 817 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 11 12 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 500 913 0
AFLR4 : Nodes, Trias,Quads= 451 815 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 637 1164 0
AFLR4 : Nodes, Trias,Quads= 481 852 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 521 954 0
AFLR4 : Nodes, Trias,Quads= 452 816 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 609 1109 0
AFLR4 : Nodes, Trias,Quads= 462 815 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 11 12 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 4670 9332 1276
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 5096 10184
AFLR4 : Nodes, Trias = 5178 10348
AFLR4 : Nodes, Trias = 5178 10348
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 525 968 0
AFLR4 : Nodes, Trias,Quads= 454 826 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 200 342 0
AFLR4 : Nodes, Trias,Quads= 189 320 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 517 952 0
AFLR4 : Nodes, Trias,Quads= 522 962 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 200 342 0
AFLR4 : Nodes, Trias,Quads= 192 326 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 516 950 0
AFLR4 : Nodes, Trias,Quads= 455 828 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 200 342 0
AFLR4 : Nodes, Trias,Quads= 192 326 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 523 964 0
AFLR4 : Nodes, Trias,Quads= 518 954 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 200 342 0
AFLR4 : Nodes, Trias,Quads= 190 322 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 578 1062 0
AFLR4 : Nodes, Trias,Quads= 525 956 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 742 1369 0
AFLR4 : Nodes, Trias,Quads= 509 903 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 579 1064 0
AFLR4 : Nodes, Trias,Quads= 758 1422 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 708 1302 0
AFLR4 : Nodes, Trias,Quads= 508 902 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 575 1056 0
AFLR4 : Nodes, Trias,Quads= 528 962 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 722 1330 0
AFLR4 : Nodes, Trias,Quads= 529 944 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 580 1066 0
AFLR4 : Nodes, Trias,Quads= 749 1404 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 694 1275 0
AFLR4 : Nodes, Trias,Quads= 498 883 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 6648 13288 1424
OVERALL : CPU Time = 0.999 seconds
Body 1 (of 4)
Number of nodes = 1217
Number of elements = 2434
Number of triangle elements = 2434
Number of quadrilateral elements = 0
Body 2 (of 4)
Number of nodes = 1215
Number of elements = 2430
Number of triangle elements = 2430
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 4196
Number of elements = 8388
Number of triangle elements = 8388
Number of quadrilateral elements = 0
Body 4 (of 4)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 6648
Total number of elements = 13288
Total number of triangle elements = 13288
Total number of quadrilateral elements = 0
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Nacelle
2: Wing
3: Farfield
Finished writing vtk file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Nacelle, index = 1
Name = leftWing, index = 2
Name = riteWing, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Nacelle, index = 1
Name = Wing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Nacelle
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mbl = 1
UG PARAM : nbl = 10
UG PARAM : mblelc = 2
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mbl = 1
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mblelc = 1
UG PARAM : BC_IDs [ 0]= 1
UG PARAM : BC_IDs [ 1]= 2
UG PARAM : BC_IDs [ 2]= 3
UG PARAM : BC_IDs [ 3]= 4
UG PARAM : BC_IDs [ 4]= 5
UG PARAM : BC_IDs [ 5]= 6
UG PARAM : BC_IDs [ 6]= 7
UG PARAM : BC_IDs [ 7]= 8
UG PARAM : BC_IDs [ 8]= 9
UG PARAM : BC_IDs [ 9]= 10
UG PARAM : BC_IDs [10]= 11
UG PARAM : BC_IDs [11]= 12
UG PARAM : BC_IDs [12]= 13
UG PARAM : BC_IDs [13]= 14
UG PARAM : BC_IDs [14]= 15
UG PARAM : BC_IDs [15]= 16
UG PARAM : BC_IDs [16]= 17
UG PARAM : BC_IDs [17]= 18
UG PARAM : BC_IDs [18]= 19
UG PARAM : BC_IDs [19]= 20
UG PARAM : BC_IDs [20]= 21
UG PARAM : BC_IDs [21]= 22
UG PARAM : BC_IDs [22]= 23
UG PARAM : BC_IDs [23]= 24
UG PARAM : BL_DS [ 0]= 0.434102
UG PARAM : BL_DS [ 1]= 0.434102
UG PARAM : BL_DS [ 2]= 0.434102
UG PARAM : BL_DS [ 3]= 0.434102
UG PARAM : BL_DS [ 4]= 0.434102
UG PARAM : BL_DS [ 5]= 0.434102
UG PARAM : BL_DS [ 6]= 0.434102
UG PARAM : BL_DS [ 7]= 0.434102
UG PARAM : BL_DS [ 8]= 0.217051
UG PARAM : BL_DS [ 9]= 0.217051
UG PARAM : BL_DS [10]= 0.217051
UG PARAM : BL_DS [11]= 0.217051
UG PARAM : BL_DS [12]= 0.217051
UG PARAM : BL_DS [13]= 0.217051
UG PARAM : BL_DS [14]= 0.217051
UG PARAM : BL_DS [15]= 0.217051
UG PARAM : BL_DS [16]= 0.217051
UG PARAM : BL_DS [17]= 0.217051
UG PARAM : BL_DS [18]= 0
UG PARAM : BL_DS [19]= 0
UG PARAM : BL_DS [20]= 0
UG PARAM : BL_DS [21]= 0
UG PARAM : BL_DS [22]= 0
UG PARAM : BL_DS [23]= 0
UG PARAM : BL_DEL [ 0]= 2.17051
UG PARAM : BL_DEL [ 1]= 2.17051
UG PARAM : BL_DEL [ 2]= 2.17051
UG PARAM : BL_DEL [ 3]= 2.17051
UG PARAM : BL_DEL [ 4]= 2.17051
UG PARAM : BL_DEL [ 5]= 2.17051
UG PARAM : BL_DEL [ 6]= 2.17051
UG PARAM : BL_DEL [ 7]= 2.17051
UG PARAM : BL_DEL [ 8]= 2.17051
UG PARAM : BL_DEL [ 9]= 2.17051
UG PARAM : BL_DEL [10]= 2.17051
UG PARAM : BL_DEL [11]= 2.17051
UG PARAM : BL_DEL [12]= 2.17051
UG PARAM : BL_DEL [13]= 2.17051
UG PARAM : BL_DEL [14]= 2.17051
UG PARAM : BL_DEL [15]= 2.17051
UG PARAM : BL_DEL [16]= 2.17051
UG PARAM : BL_DEL [17]= 2.17051
UG PARAM : BL_DEL [18]= 0
UG PARAM : BL_DEL [19]= 0
UG PARAM : BL_DEL [20]= 0
UG PARAM : BL_DEL [21]= 0
UG PARAM : BL_DEL [22]= 0
UG PARAM : BL_DEL [23]= 0
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 4 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 4 Faces
EGADS : Body 0 has 8 Edges
EGADS : Body 0 has 4 Loops
EGADS : Body 0 has 4 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 4 Faces
EGADS : Body 1 has 8 Edges
EGADS : Body 1 has 4 Loops
EGADS : Body 1 has 4 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 10 Faces
EGADS : Body 2 has 18 Edges
EGADS : Body 2 has 10 Loops
EGADS : Body 2 has 10 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 6 Faces
EGADS : Body 3 has 12 Edges
EGADS : Body 3 has 6 Loops
EGADS : Body 3 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3
EGADS : 2 Yes 0 0 1 0 1 1 4
EGADS : 3 Yes 0 0 1 0 1 1 4
EGADS : 4 Yes 0 0 1 0 1 2 3
EGADS : 5 Yes 1 0 1 0 1 6 7
EGADS : 6 Yes 1 0 1 0 1 5 8
EGADS : 7 Yes 1 0 1 0 1 5 8
EGADS : 8 Yes 1 0 1 0 1 6 7
EGADS : 9 Yes 2 0 1 0 1 10 11 14
EGADS : 10 Yes 2 0 1 0 1 9 12 13
EGADS : 11 Yes 2 0 1 0 1 9 12 16
EGADS : 12 Yes 2 0 1 0 1 10 11 13
EGADS : 13 Yes 2 0 1 0 1 10 12
EGADS : 14 Yes 2 0 1 0 1 9 15 16
EGADS : 15 Yes 2 0 1 0 1 14 17 18
EGADS : 16 Yes 2 0 1 0 1 11 14 17
EGADS : 17 Yes 2 0 1 0 1 15 16 18
EGADS : 18 Yes 2 0 1 0 1 15 17
EGADS : 19 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 20 Yes 3 0 1 NA NA 21 22 23 24
EGADS : 21 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 22 Yes 3 0 1 NA NA 19 20 23 24
EGADS : 23 Yes 3 0 1 NA NA 19 20 21 22
EGADS : 24 Yes 3 0 1 NA NA 19 20 21 22
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 3 2 -4
EGADS : 2 -2 5 1 -6
EGADS : 3 7 4 -8 -3
EGADS : 4 8 6 -7 -5
EGADS : 5 9 12 -10 -11
EGADS : 6 10 14 -9 -13
EGADS : 7 -15 11 16 -12
EGADS : 8 -16 13 15 -14
EGADS : 9 -17 18 19 -20
EGADS : 10 -21 20 22 -23
EGADS : 11 -19 24 17 -25
EGADS : 12 -22 25 21 -26
EGADS : 13 23 26
EGADS : 14 27 29 -28 -18
EGADS : 15 30 32 -31 -29
EGADS : 16 28 33 -27 -24
EGADS : 17 31 34 -30 -33
EGADS : 18 -32 -34
EGADS : 19 35 36 -37 -38
EGADS : 20 -39 42 41 -40
EGADS : 21 43 39 -44 -35
EGADS : 22 -45 37 46 -41
EGADS : 23 38 45 -42 -43
EGADS : 24 -36 44 40 -46
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : 19 19
EGADS : 20 20
EGADS : 21 21
EGADS : 22 22
EGADS : 23 23
EGADS : 24 24
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 3 2 -4
EGADS : 2 Yes -2 5 1 -6
EGADS : 3 Yes 7 4 -8 -3
EGADS : 4 Yes 8 6 -7 -5
EGADS : 5 Yes 9 12 -10 -11
EGADS : 6 Yes 10 14 -9 -13
EGADS : 7 Yes -15 11 16 -12
EGADS : 8 Yes -16 13 15 -14
EGADS : 9 Yes -17 18 19 -20
EGADS : 10 Yes -21 20 22 -23
EGADS : 11 Yes -19 24 17 -25
EGADS : 12 Yes -22 25 21 -26
EGADS : 13 Yes 23 26
EGADS : 14 Yes 27 29 -28 -18
EGADS : 15 Yes 30 32 -31 -29
EGADS : 16 Yes 28 33 -27 -24
EGADS : 17 Yes 31 34 -30 -33
EGADS : 18 Yes -32 -34
EGADS : 19 Yes 35 36 -37 -38
EGADS : 20 Yes -39 42 41 -40
EGADS : 21 Yes 43 39 -44 -35
EGADS : 22 Yes -45 37 46 -41
EGADS : 23 Yes 38 45 -42 -43
EGADS : 24 Yes -36 44 40 -46
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 3 4 1 1 2
EGADS : 3 0 Yes 1 3 1 1 3
EGADS : 4 0 Yes 2 4 1 1 3
EGADS : 5 0 Yes 3 1 1 2 4
EGADS : 6 0 Yes 4 2 1 2 4
EGADS : 7 0 Yes 1 2 1 3 4
EGADS : 8 0 Yes 3 4 1 3 4
EGADS : 9 1 Yes 5 6 1 5 6
EGADS : 10 1 Yes 7 8 1 5 6
EGADS : 11 1 Yes 5 7 1 5 7
EGADS : 12 1 Yes 6 8 1 5 7
EGADS : 13 1 Yes 7 5 1 6 8
EGADS : 14 1 Yes 8 6 1 6 8
EGADS : 15 1 Yes 5 6 1 7 8
EGADS : 16 1 Yes 7 8 1 7 8
EGADS : 17 2 Yes 9 10 1 9 11
EGADS : 18 2 Yes 9 11 1 9 14
EGADS : 19 2 Yes 11 12 1 9 11
EGADS : 20 2 Yes 10 12 1 9 10
EGADS : 21 2 Yes 10 13 1 10 12
EGADS : 22 2 Yes 12 14 1 10 12
EGADS : 23 2 Yes 13 14 1 10 13
EGADS : 24 2 Yes 11 9 1 11 16
EGADS : 25 2 Yes 12 10 1 11 12
EGADS : 26 2 Yes 14 13 1 12 13
EGADS : 27 2 Yes 9 15 1 14 16
EGADS : 28 2 Yes 11 16 1 14 16
EGADS : 29 2 Yes 15 16 1 14 15
EGADS : 30 2 Yes 15 17 1 15 17
EGADS : 31 2 Yes 16 18 1 15 17
EGADS : 32 2 Yes 17 18 1 15 18
EGADS : 33 2 Yes 16 15 1 16 17
EGADS : 34 2 Yes 18 17 1 17 18
EGADS : 35 3 Yes 20 19 NA 19 21
EGADS : 36 3 Yes 19 21 NA 19 24
EGADS : 37 3 Yes 22 21 NA 19 22
EGADS : 38 3 Yes 20 22 NA 19 23
EGADS : 39 3 Yes 24 23 NA 20 21
EGADS : 40 3 Yes 23 25 NA 20 24
EGADS : 41 3 Yes 26 25 NA 20 22
EGADS : 42 3 Yes 24 26 NA 20 23
EGADS : 43 3 Yes 20 24 NA 21 23
EGADS : 44 3 Yes 19 23 NA 21 24
EGADS : 45 3 Yes 22 26 NA 22 23
EGADS : 46 3 Yes 21 25 NA 22 24
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 90.5173952 0 0
EGADS : 2 Yes 90.5173952 0 0
EGADS : 3 Yes 60.5173952 0 0
EGADS : 4 Yes 60.5173952 0 0
EGADS : 5 Yes 90.5173952 29.3018771 0
EGADS : 6 Yes 90.5173952 29.3018771 0
EGADS : 7 Yes 60.5173952 29.3018771 0
EGADS : 8 Yes 60.5173952 29.3018771 0
EGADS : 9 Yes 97.2007855 0 0
EGADS : 10 Yes 97.9335611 0 0
EGADS : 11 Yes 50 0 0
EGADS : 12 Yes 75.3047874 0 0
EGADS : 13 Yes 123.552357 0 4.7180639
EGADS : 14 Yes 118.391317 0 3.99272703
EGADS : 15 Yes 97.9335611 36.1389817 0
EGADS : 16 Yes 75.3047874 36.1389817 0
EGADS : 17 Yes 123.552357 97.6729236 4.7180639
EGADS : 18 Yes 118.391317 97.6729236 3.99272703
EGADS : 19 Yes 0 0 1947.05079
EGADS : 20 Yes 0 0 0
EGADS : 21 Yes 0 1953.45847 1947.05079
EGADS : 22 Yes 0 1953.45847 0
EGADS : 23 Yes 2040.21562 0 1947.05079
EGADS : 24 Yes 2040.21562 0 0
EGADS : 25 Yes 2040.21562 1953.45847 1947.05079
EGADS : 26 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 22.2515
AFLR4 : Reference Length = 22.2515
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 428.344
AFLR4 : Abs Min Surf Spacing = 0.0556287
AFLR4 : Min Surf Spacing = 0.111257
AFLR4 : Max Surf Spacing = 2.22515
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 FARFIELD
AFLR4 : 20 CAD geometry 0 FARFIELD
AFLR4 : 21 CAD geometry 0 FARFIELD
AFLR4 : 22 CAD geometry 0 FARFIELD
AFLR4 : 23 CAD geometry 0 FARFIELD
AFLR4 : 24 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4 : Component 2 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 13288
AFLR43 : Nodes = 6648
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mbl = 1
UG PARAM : nbl = 10
UG PARAM : mblelc = 2
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mbl = 1
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mblelc = 1
UG PARAM : BC_IDs [ 0]= 1
UG PARAM : BC_IDs [ 1]= 2
UG PARAM : BC_IDs [ 2]= 3
UG PARAM : BC_IDs [ 3]= 4
UG PARAM : BC_IDs [ 4]= 5
UG PARAM : BC_IDs [ 5]= 6
UG PARAM : BC_IDs [ 6]= 7
UG PARAM : BC_IDs [ 7]= 8
UG PARAM : BC_IDs [ 8]= 9
UG PARAM : BC_IDs [ 9]= 10
UG PARAM : BC_IDs [10]= 11
UG PARAM : BC_IDs [11]= 12
UG PARAM : BC_IDs [12]= 13
UG PARAM : BC_IDs [13]= 14
UG PARAM : BC_IDs [14]= 15
UG PARAM : BC_IDs [15]= 16
UG PARAM : BC_IDs [16]= 17
UG PARAM : BC_IDs [17]= 18
UG PARAM : BC_IDs [18]= 19
UG PARAM : BC_IDs [19]= 20
UG PARAM : BC_IDs [20]= 21
UG PARAM : BC_IDs [21]= 22
UG PARAM : BC_IDs [22]= 23
UG PARAM : BC_IDs [23]= 24
UG PARAM : BL_DS [ 0]= 0.434102
UG PARAM : BL_DS [ 1]= 0.434102
UG PARAM : BL_DS [ 2]= 0.434102
UG PARAM : BL_DS [ 3]= 0.434102
UG PARAM : BL_DS [ 4]= 0.434102
UG PARAM : BL_DS [ 5]= 0.434102
UG PARAM : BL_DS [ 6]= 0.434102
UG PARAM : BL_DS [ 7]= 0.434102
UG PARAM : BL_DS [ 8]= 0.217051
UG PARAM : BL_DS [ 9]= 0.217051
UG PARAM : BL_DS [10]= 0.217051
UG PARAM : BL_DS [11]= 0.217051
UG PARAM : BL_DS [12]= 0.217051
UG PARAM : BL_DS [13]= 0.217051
UG PARAM : BL_DS [14]= 0.217051
UG PARAM : BL_DS [15]= 0.217051
UG PARAM : BL_DS [16]= 0.217051
UG PARAM : BL_DS [17]= 0.217051
UG PARAM : BL_DS [18]= 0
UG PARAM : BL_DS [19]= 0
UG PARAM : BL_DS [20]= 0
UG PARAM : BL_DS [21]= 0
UG PARAM : BL_DS [22]= 0
UG PARAM : BL_DS [23]= 0
UG PARAM : BL_DEL [ 0]= 2.17051
UG PARAM : BL_DEL [ 1]= 2.17051
UG PARAM : BL_DEL [ 2]= 2.17051
UG PARAM : BL_DEL [ 3]= 2.17051
UG PARAM : BL_DEL [ 4]= 2.17051
UG PARAM : BL_DEL [ 5]= 2.17051
UG PARAM : BL_DEL [ 6]= 2.17051
UG PARAM : BL_DEL [ 7]= 2.17051
UG PARAM : BL_DEL [ 8]= 2.17051
UG PARAM : BL_DEL [ 9]= 2.17051
UG PARAM : BL_DEL [10]= 2.17051
UG PARAM : BL_DEL [11]= 2.17051
UG PARAM : BL_DEL [12]= 2.17051
UG PARAM : BL_DEL [13]= 2.17051
UG PARAM : BL_DEL [14]= 2.17051
UG PARAM : BL_DEL [15]= 2.17051
UG PARAM : BL_DEL [16]= 2.17051
UG PARAM : BL_DEL [17]= 2.17051
UG PARAM : BL_DEL [18]= 0
UG PARAM : BL_DEL [19]= 0
UG PARAM : BL_DEL [20]= 0
UG PARAM : BL_DEL [21]= 0
UG PARAM : BL_DEL [22]= 0
UG PARAM : BL_DEL [23]= 0
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 6648 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid w/BL
UG3 : 2 Solid w/BL
UG3 : 3 Solid w/BL
UG3 : 4 Solid w/BL
UG3 : 5 Solid w/BL
UG3 : 6 Solid w/BL
UG3 : 7 Solid w/BL
UG3 : 8 Solid w/BL
UG3 : 9 Solid w/BL
UG3 : 10 Solid w/BL
UG3 : 11 Solid w/BL
UG3 : 12 Solid w/BL
UG3 : 13 Solid w/BL
UG3 : 14 Solid w/BL
UG3 : 15 Solid w/BL
UG3 : 16 Solid w/BL
UG3 : 17 Solid w/BL
UG3 : 18 Solid w/BL
UG3 : 19 FarField
UG3 : 20 FarField
UG3 : 21 FarField
UG3 : 22 FarField
UG3 : 23 FarField
UG3 : 24 FarField
AFLR3 : CPU Time = 0.019 seconds
AFLR3 : DONE
ANBL3 : ---------------------------------------
ANBL3 : ANBL3 LIBRARY
ANBL3 : ADVANCING-NORMAL
ANBL3 : BOUNDARY-LAYER (BL)
ANBL3 : STRUCTURED-LAYER (SL)
ANBL3 : SPECIFIED NORMAL SPACING (SNS)
ANBL3 : TETRAHEDRAL/PENTAHEDRAL GRID GENERATOR
ANBL3 : Version Number 9.34.2
ANBL3 : Version Date 03/10/23 @ 04:32PM
ANBL3 : Compile OS Darwin 22.6.0 x86_64
ANBL3 : Compile Date 11/01/23 @ 12:20PM
ANBL3 : Copyright 1994-2021, D.L. Marcum
ANBL3 : ---------------------------------------
ANBL3 BLC: BL BOUNDARY CONDITIONS CHECK
ANBL3 BLC: Nodes, Elements = 6648 0
ANBL3 : CPU Time = 0.016 seconds
ANBL3 : DONE
ANBL3 BLG: BL NODE GENERATION
ANBL3 BLG: Nodes, Layer = 0 0
ANBL3 BLG: Nodes, Layer = 13236 2
ANBL3 BLG: Nodes, Layer = 19803 3
ANBL3 BLG: Nodes, Layer = 25869 4
ANBL3 BLG: Nodes, Layer = 31554 5
ANBL3 BLG: Nodes, Layer = 37022 6
ANBL3 BLG: Nodes, Layer = 42307 7
ANBL3 BLG: Nodes, Layer = 47280 8
ANBL3 BLG: Nodes, Layer = 51732 9
ANBL3 BLG: Nodes, Layer = 55961 10
ANBL3 BLG: Nodes, Layer = 60010 11
ANBL3 : CPU Time = 4.464 seconds
ANBL3 : DONE
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 6648 0
AFLR3 : CPU Time = 0.010 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 6648 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1332 8500
AFLR3 IG : Nodes, Elements = 2664 17268
AFLR3 IG : Nodes, Elements = 3996 25716
AFLR3 IG : Nodes, Elements = 5328 35137
AFLR3 IG : Nodes, Elements = 6655 45684
AFLR3 IG : Nodes, Elements = 6655 45691
AFLR3 IG : Nodes, Elements = 6655 45677
AFLR3 IG : Nodes, Elements = 6655 47449
AFLR3 IG : Nodes, Elements = 6655 45093
AFLR3 IG : Nodes, Elements = 6655 45152
AFLR3 IG : Nodes, Elements = 6655 45155
AFLR3 IG : Nodes, Elements = 6655 45768
AFLR3 IG : Nodes, Elements = 6655 45737
AFLR3 IG : Nodes, Elements = 6655 44251
AFLR3 IG : Nodes, Elements = 6655 44706
AFLR3 IG : Nodes, Elements = 6655 44254
AFLR3 IG : Nodes, Elements = 6655 44573
AFLR3 IG : Nodes, Elements = 6655 44558
AFLR3 IG : Nodes, Elements = 6655 44110
AFLR3 IG : Nodes, Elements = 6655 44112
AFLR3 IG : Nodes, Elements = 6655 44383
AFLR3 IG : Nodes, Elements = 6655 44114
AFLR3 IG : Nodes, Elements = 6655 44328
AFLR3 IG : Nodes, Elements = 6655 44320
AFLR3 IG : Nodes, Elements = 6655 44107
AFLR3 IG : Nodes, Elements = 6655 44368
AFLR3 IG : Nodes, Elements = 6655 44097
AFLR3 IG : Nodes, Elements = 6655 44313
AFLR3 IG : Nodes, Elements = 6655 44294
AFLR3 IG : Nodes, Elements = 6655 44081
AFLR3 IG : Nodes, Elements = 6655 44308
AFLR3 IG : Nodes, Elements = 6655 44086
AFLR3 IG : Nodes, Elements = 6655 44281
AFLR3 IG : Nodes, Elements = 6655 44265
AFLR3 IG : Nodes, Elements = 6655 44089
AFLR3 IG : Nodes, Elements = 6655 44090
AFLR3 IG : Nodes, Elements = 6655 44293
AFLR3 IG : Nodes, Elements = 6655 44085
AFLR3 IG : Nodes, Elements = 6655 44257
AFLR3 IG : Nodes, Elements = 6655 44241
AFLR3 IG : Nodes, Elements = 6655 44088
AFLR3 IG : Nodes, Elements = 6655 44309
AFLR3 IG : Nodes, Elements = 6655 44124
AFLR3 IG : Nodes, Elements = 6655 44202
AFLR3 IG : Nodes, Elements = 6655 44194
AFLR3 IG : Nodes, Elements = 6655 44087
AFLR3 IG : Nodes, Elements = 6655 44178
AFLR3 IG : Nodes, Elements = 6655 44100
AFLR3 IG : Nodes, Elements = 6655 44102
AFLR3 IG : Nodes, Elements = 6655 44115
AFLR3 IG : Nodes, Elements = 6655 44114
AFLR3 IG : Nodes, Elements = 6655 44096
AFLR3 IG : Nodes, Elements = 6655 44107
AFLR3 IG : Nodes, Elements = 6655 44092
AFLR3 IG : Nodes, Elements = 6655 44108
AFLR3 IG : Nodes, Elements = 6655 44107
AFLR3 IG : Nodes, Elements = 6655 44088
AFLR3 IG : Nodes, Elements = 6655 44134
AFLR3 IG : Nodes, Elements = 6655 44089
AFLR3 IG : Nodes, Elements = 6655 44090
AFLR3 IG : Nodes, Elements = 6648 24873
AFLR3 IG : Nodes, Elements = 6648 26298
AFLR3 IG : Nodes, Elements = 6648 23129
AFLR3 IG : Nodes, Elements = 6648 22296
AFLR3 : CPU Time = 1.433 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6648 22296
AFLR3 GG : Nodes, Elements = 8390 27587
AFLR3 GG : Nodes, Elements = 8390 32978
AFLR3 GG : Nodes, Elements = 8390 31071
AFLR3 GG : Nodes, Elements = 8390 30643
AFLR3 GG : Nodes, Elements = 10061 35733
AFLR3 GG : Nodes, Elements = 10061 42842
AFLR3 GG : Nodes, Elements = 10061 40740
AFLR3 GG : Nodes, Elements = 10061 40350
AFLR3 GG : Nodes, Elements = 11845 45778
AFLR3 GG : Nodes, Elements = 11845 53560
AFLR3 GG : Nodes, Elements = 11845 51473
AFLR3 GG : Nodes, Elements = 11845 51073
AFLR3 GG : Nodes, Elements = 13690 56654
AFLR3 GG : Nodes, Elements = 13690 64443
AFLR3 GG : Nodes, Elements = 13690 62339
AFLR3 GG : Nodes, Elements = 13690 61910
AFLR3 GG : Nodes, Elements = 15589 67667
AFLR3 GG : Nodes, Elements = 15589 75797
AFLR3 GG : Nodes, Elements = 15589 73648
AFLR3 GG : Nodes, Elements = 15589 73231
AFLR3 GG : Nodes, Elements = 17448 78855
AFLR3 GG : Nodes, Elements = 17448 86736
AFLR3 GG : Nodes, Elements = 17448 84618
AFLR3 GG : Nodes, Elements = 17448 84221
AFLR3 GG : Nodes, Elements = 19322 89886
AFLR3 GG : Nodes, Elements = 19322 97889
AFLR3 GG : Nodes, Elements = 19322 95803
AFLR3 GG : Nodes, Elements = 19322 95413
AFLR3 GG : Nodes, Elements = 21164 100976
AFLR3 GG : Nodes, Elements = 21164 108784
AFLR3 GG : Nodes, Elements = 21164 106726
AFLR3 GG : Nodes, Elements = 21164 106343
AFLR3 GG : Nodes, Elements = 22954 111745
AFLR3 GG : Nodes, Elements = 22954 119252
AFLR3 GG : Nodes, Elements = 22954 117363
AFLR3 GG : Nodes, Elements = 22954 117012
AFLR3 GG : Nodes, Elements = 24733 122389
AFLR3 GG : Nodes, Elements = 24733 129894
AFLR3 GG : Nodes, Elements = 24733 127889
AFLR3 GG : Nodes, Elements = 24733 127580
AFLR3 GG : Nodes, Elements = 26406 132639
AFLR3 GG : Nodes, Elements = 26406 139745
AFLR3 GG : Nodes, Elements = 26406 137899
AFLR3 GG : Nodes, Elements = 26406 137582
AFLR3 GG : Nodes, Elements = 28047 142535
AFLR3 GG : Nodes, Elements = 28047 149540
AFLR3 GG : Nodes, Elements = 28047 147684
AFLR3 GG : Nodes, Elements = 28047 147375
AFLR3 GG : Nodes, Elements = 29585 152017
AFLR3 GG : Nodes, Elements = 29585 158541
AFLR3 GG : Nodes, Elements = 29585 156850
AFLR3 GG : Nodes, Elements = 29585 156556
AFLR3 GG : Nodes, Elements = 31083 161072
AFLR3 GG : Nodes, Elements = 31083 167399
AFLR3 GG : Nodes, Elements = 31083 165803
AFLR3 GG : Nodes, Elements = 31083 165502
AFLR3 GG : Nodes, Elements = 32509 169801
AFLR3 GG : Nodes, Elements = 32509 175881
AFLR3 GG : Nodes, Elements = 32509 174304
AFLR3 GG : Nodes, Elements = 32509 174050
AFLR3 GG : Nodes, Elements = 33852 178099
AFLR3 GG : Nodes, Elements = 33852 183710
AFLR3 GG : Nodes, Elements = 33852 182299
AFLR3 GG : Nodes, Elements = 33852 182043
AFLR3 GG : Nodes, Elements = 35140 185929
AFLR3 GG : Nodes, Elements = 35140 191381
AFLR3 GG : Nodes, Elements = 35140 189982
AFLR3 GG : Nodes, Elements = 35140 189730
AFLR3 GG : Nodes, Elements = 36375 193455
AFLR3 GG : Nodes, Elements = 36375 198691
AFLR3 GG : Nodes, Elements = 36375 197347
AFLR3 GG : Nodes, Elements = 36375 197110
AFLR3 GG : Nodes, Elements = 37561 200694
AFLR3 GG : Nodes, Elements = 37561 205779
AFLR3 GG : Nodes, Elements = 37561 204472
AFLR3 GG : Nodes, Elements = 37561 204224
AFLR3 GG : Nodes, Elements = 38688 207623
AFLR3 GG : Nodes, Elements = 38688 212355
AFLR3 GG : Nodes, Elements = 38688 211115
AFLR3 GG : Nodes, Elements = 38688 210922
AFLR3 GG : Nodes, Elements = 39762 214161
AFLR3 GG : Nodes, Elements = 39762 218708
AFLR3 GG : Nodes, Elements = 39762 217510
AFLR3 GG : Nodes, Elements = 39762 217304
AFLR3 GG : Nodes, Elements = 40796 220422
AFLR3 GG : Nodes, Elements = 40796 224873
AFLR3 GG : Nodes, Elements = 40796 223735
AFLR3 GG : Nodes, Elements = 40796 223497
AFLR3 GG : Nodes, Elements = 41777 226458
AFLR3 GG : Nodes, Elements = 41777 230679
AFLR3 GG : Nodes, Elements = 41777 229521
AFLR3 GG : Nodes, Elements = 41777 229337
AFLR3 GG : Nodes, Elements = 42715 232162
AFLR3 GG : Nodes, Elements = 42715 236153
AFLR3 GG : Nodes, Elements = 42715 235132
AFLR3 GG : Nodes, Elements = 42715 234925
AFLR3 GG : Nodes, Elements = 43621 237659
AFLR3 GG : Nodes, Elements = 43621 241515
AFLR3 GG : Nodes, Elements = 43621 240542
AFLR3 GG : Nodes, Elements = 43621 240342
AFLR3 GG : Nodes, Elements = 44474 242918
AFLR3 GG : Nodes, Elements = 44474 246565
AFLR3 GG : Nodes, Elements = 44474 245591
AFLR3 GG : Nodes, Elements = 44474 245425
AFLR3 GG : Nodes, Elements = 45307 247936
AFLR3 GG : Nodes, Elements = 45307 251540
AFLR3 GG : Nodes, Elements = 45307 250575
AFLR3 GG : Nodes, Elements = 45307 250387
AFLR3 GG : Nodes, Elements = 46087 252736
AFLR3 GG : Nodes, Elements = 46087 256111
AFLR3 GG : Nodes, Elements = 46087 255227
AFLR3 GG : Nodes, Elements = 46087 255043
AFLR3 GG : Nodes, Elements = 46853 257350
AFLR3 GG : Nodes, Elements = 46853 260595
AFLR3 GG : Nodes, Elements = 46853 259772
AFLR3 GG : Nodes, Elements = 46853 259624
AFLR3 GG : Nodes, Elements = 47566 261778
AFLR3 GG : Nodes, Elements = 47566 264797
AFLR3 GG : Nodes, Elements = 47566 264023
AFLR3 GG : Nodes, Elements = 47566 263895
AFLR3 GG : Nodes, Elements = 48273 266018
AFLR3 GG : Nodes, Elements = 48273 269024
AFLR3 GG : Nodes, Elements = 48273 268253
AFLR3 GG : Nodes, Elements = 48273 268073
AFLR3 GG : Nodes, Elements = 48946 270104
AFLR3 GG : Nodes, Elements = 48946 273009
AFLR3 GG : Nodes, Elements = 48946 272229
AFLR3 GG : Nodes, Elements = 48946 272101
AFLR3 GG : Nodes, Elements = 49600 274068
AFLR3 GG : Nodes, Elements = 49600 276854
AFLR3 GG : Nodes, Elements = 49600 276154
AFLR3 GG : Nodes, Elements = 49600 276025
AFLR3 GG : Nodes, Elements = 50211 277867
AFLR3 GG : Nodes, Elements = 50211 280468
AFLR3 GG : Nodes, Elements = 50211 279797
AFLR3 GG : Nodes, Elements = 50211 279661
AFLR3 GG : Nodes, Elements = 50835 281538
AFLR3 GG : Nodes, Elements = 50835 284205
AFLR3 GG : Nodes, Elements = 50835 283495
AFLR3 GG : Nodes, Elements = 50835 283365
AFLR3 GG : Nodes, Elements = 51411 285095
AFLR3 GG : Nodes, Elements = 51411 287544
AFLR3 GG : Nodes, Elements = 51411 286926
AFLR3 GG : Nodes, Elements = 51411 286815
AFLR3 GG : Nodes, Elements = 51973 288507
AFLR3 GG : Nodes, Elements = 51973 290881
AFLR3 GG : Nodes, Elements = 51973 290287
AFLR3 GG : Nodes, Elements = 51973 290169
AFLR3 GG : Nodes, Elements = 52518 291808
AFLR3 GG : Nodes, Elements = 52518 294101
AFLR3 GG : Nodes, Elements = 52518 293544
AFLR3 GG : Nodes, Elements = 52518 293422
AFLR3 GG : Nodes, Elements = 53036 294983
AFLR3 GG : Nodes, Elements = 53036 297218
AFLR3 GG : Nodes, Elements = 53036 296627
AFLR3 GG : Nodes, Elements = 53036 296494
AFLR3 GG : Nodes, Elements = 53557 298063
AFLR3 GG : Nodes, Elements = 53557 300277
AFLR3 GG : Nodes, Elements = 53557 299705
AFLR3 GG : Nodes, Elements = 53557 299601
AFLR3 GG : Nodes, Elements = 54058 301109
AFLR3 GG : Nodes, Elements = 54058 303243
AFLR3 GG : Nodes, Elements = 54058 302706
AFLR3 GG : Nodes, Elements = 54058 302616
AFLR3 GG : Nodes, Elements = 54529 304030
AFLR3 GG : Nodes, Elements = 54529 306043
AFLR3 GG : Nodes, Elements = 54529 305527
AFLR3 GG : Nodes, Elements = 54529 305423
AFLR3 GG : Nodes, Elements = 55005 306853
AFLR3 GG : Nodes, Elements = 55005 308905
AFLR3 GG : Nodes, Elements = 55005 308373
AFLR3 GG : Nodes, Elements = 55005 308271
AFLR3 GG : Nodes, Elements = 55437 309568
AFLR3 GG : Nodes, Elements = 55437 311435
AFLR3 GG : Nodes, Elements = 55437 310947
AFLR3 GG : Nodes, Elements = 55437 310847
AFLR3 GG : Nodes, Elements = 55835 312046
AFLR3 GG : Nodes, Elements = 55835 313731
AFLR3 GG : Nodes, Elements = 55835 313309
AFLR3 GG : Nodes, Elements = 55835 313218
AFLR3 GG : Nodes, Elements = 56200 314313
AFLR3 GG : Nodes, Elements = 56200 315892
AFLR3 GG : Nodes, Elements = 56200 315458
AFLR3 GG : Nodes, Elements = 56200 315374
AFLR3 GG : Nodes, Elements = 56513 316314
AFLR3 GG : Nodes, Elements = 56513 317696
AFLR3 GG : Nodes, Elements = 56513 317309
AFLR3 GG : Nodes, Elements = 56513 317225
AFLR3 GG : Nodes, Elements = 56808 318110
AFLR3 GG : Nodes, Elements = 56808 319419
AFLR3 GG : Nodes, Elements = 56808 319055
AFLR3 GG : Nodes, Elements = 56808 318983
AFLR3 GG : Nodes, Elements = 57038 319674
AFLR3 GG : Nodes, Elements = 57038 320691
AFLR3 GG : Nodes, Elements = 57038 320396
AFLR3 GG : Nodes, Elements = 57038 320320
AFLR3 GG : Nodes, Elements = 57252 320962
AFLR3 GG : Nodes, Elements = 57252 321930
AFLR3 GG : Nodes, Elements = 57252 321630
AFLR3 GG : Nodes, Elements = 57252 321578
AFLR3 GG : Nodes, Elements = 57432 322118
AFLR3 GG : Nodes, Elements = 57432 322954
AFLR3 GG : Nodes, Elements = 57432 322715
AFLR3 GG : Nodes, Elements = 57432 322656
AFLR3 GG : Nodes, Elements = 57562 323046
AFLR3 GG : Nodes, Elements = 57562 323640
AFLR3 GG : Nodes, Elements = 57562 323454
AFLR3 GG : Nodes, Elements = 57562 323414
AFLR3 GG : Nodes, Elements = 57657 323699
AFLR3 GG : Nodes, Elements = 57657 324184
AFLR3 GG : Nodes, Elements = 57657 324004
AFLR3 GG : Nodes, Elements = 57657 323967
AFLR3 GG : Nodes, Elements = 57720 324156
AFLR3 GG : Nodes, Elements = 57720 324499
AFLR3 GG : Nodes, Elements = 57720 324361
AFLR3 GG : Nodes, Elements = 57720 324342
AFLR3 GG : Nodes, Elements = 57761 324465
AFLR3 GG : Nodes, Elements = 57761 324656
AFLR3 GG : Nodes, Elements = 57761 324587
AFLR3 GG : Nodes, Elements = 57761 324574
AFLR3 GG : Nodes, Elements = 57797 324682
AFLR3 GG : Nodes, Elements = 57797 324868
AFLR3 GG : Nodes, Elements = 57797 324807
AFLR3 GG : Nodes, Elements = 57797 324787
AFLR3 GG : Nodes, Elements = 57821 324859
AFLR3 GG : Nodes, Elements = 57821 324968
AFLR3 GG : Nodes, Elements = 57821 324929
AFLR3 GG : Nodes, Elements = 57821 324923
AFLR3 GG : Nodes, Elements = 57843 324989
AFLR3 GG : Nodes, Elements = 57843 325095
AFLR3 GG : Nodes, Elements = 57843 325049
AFLR3 GG : Nodes, Elements = 57843 325045
AFLR3 GG : Nodes, Elements = 57853 325075
AFLR3 GG : Nodes, Elements = 57853 325137
AFLR3 GG : Nodes, Elements = 57853 325110
AFLR3 GG : Nodes, Elements = 57853 325107
AFLR3 GG : Nodes, Elements = 57862 325134
AFLR3 GG : Nodes, Elements = 57862 325195
AFLR3 GG : Nodes, Elements = 57862 325164
AFLR3 GG : Nodes, Elements = 57862 325156
AFLR3 GG : Nodes, Elements = 57864 325162
AFLR3 GG : Nodes, Elements = 57864 325178
AFLR3 GG : Nodes, Elements = 57864 325165
AFLR3 GG : Nodes, Elements = 57864 325164
AFLR3 GG : Nodes, Elements = 57866 325170
AFLR3 GG : Nodes, Elements = 57866 325185
AFLR3 GG : Nodes, Elements = 57866 325175
AFLR3 GG : Nodes, Elements = 57866 325174
AFLR3 GG : Nodes, Elements = 57867 325177
AFLR3 GG : Nodes, Elements = 57867 325189
AFLR3 GG : Nodes, Elements = 57867 325182
AFLR3 GG : Nodes, Elements = 57867 325181
AFLR3 GG : Nodes, Elements = 57869 325187
AFLR3 GG : Nodes, Elements = 57869 325203
AFLR3 GG : Nodes, Elements = 57869 325198
AFLR3 GG : Nodes, Elements = 57869 325195
AFLR3 GG : Nodes, Elements = 57879 325225
AFLR3 GG : Nodes, Elements = 57879 325274
AFLR3 GG : Nodes, Elements = 57879 325255
AFLR3 GG : Nodes, Elements = 57879 325252
AFLR3 GG : Nodes, Elements = 57883 325264
AFLR3 GG : Nodes, Elements = 57883 325288
AFLR3 GG : Nodes, Elements = 57883 325280
AFLR3 GG : Nodes, Elements = 57886 325289
AFLR3 GG : Nodes, Elements = 57886 325307
AFLR3 GG : Nodes, Elements = 57886 325299
AFLR3 GG : Nodes, Elements = 57886 325293
AFLR3 : CPU Time = 6.245 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 57886 325293
AFLR3 QI : Nodes, Elements = 56601 318069
AFLR3 QI : Nodes, Elements = 56394 316891
AFLR3 QI : Nodes, Elements = 56384 316837
AFLR3 QI : Nodes, Elements = 56384 320490
AFLR3 QI : Nodes, Elements = 56384 316651
AFLR3 QI : Nodes, Elements = 56384 316122
AFLR3 QI : Nodes, Elements = 56384 317204
AFLR3 QI : Nodes, Elements = 56384 316201
AFLR3 QI : Nodes, Elements = 56384 315876
AFLR3 QI : Nodes, Elements = 56384 316733
AFLR3 QI : Nodes, Elements = 56384 315999
AFLR3 QI : Nodes, Elements = 56384 315861
AFLR3 QI : Nodes, Elements = 56384 316752
AFLR3 QI : Nodes, Elements = 56384 316025
AFLR3 QI : Nodes, Elements = 56384 315827
AFLR3 QI : Nodes, Elements = 56384 316618
AFLR3 QI : Nodes, Elements = 56384 315981
AFLR3 QI : Nodes, Elements = 56384 315804
AFLR3 QI : Nodes, Elements = 56384 315779
AFLR3 QI : Nodes, Elements = 56398 315840
AFLR3 QI : Nodes, Elements = 56398 316599
AFLR3 QI : Nodes, Elements = 56398 316015
AFLR3 QI : Nodes, Elements = 56398 315864
AFLR3 QI : Nodes, Elements = 56398 316591
AFLR3 QI : Nodes, Elements = 56398 315993
AFLR3 QI : Nodes, Elements = 56398 315852
AFLR3 : CPU Time = 1.981 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 56398 315852
AFLR3 QRG: Nodes, Elements = 56403 315876
AFLR3 QRG: Nodes, Elements = 56406 315890
AFLR3 QRG: Nodes, Elements = 56425 315992
AFLR3 QRG: Nodes, Elements = 56441 316082
AFLR3 : CPU Time = 0.048 seconds
AFLR3 : DONE
ANBL3 BLM: BL VOLUME GRID MERGE
ANBL3 BLM: Nodes, Elements = 56441 316082
UG3 : OUTPUT GRID
UG3 : Grid File Name = .tmp.b8.ugrid
UG3 : Quad Surface Faces= 0
UG3 : Tria Surface Faces= 13288
UG3 : Nodes = 109823
UG3 : Total Elements = 425492
UG3 : Hex Elements = 0
UG3 : Pent_5 Elements = 2793
UG3 : Pent_6 Elements = 104033
UG3 : Tet Elements = 318666
ANBL3 BLM: Nodes, Elements = 109823 636351
ANBL3 BLM: Nodes, Elements = 109823 2584
ANBL3 : CPU Time = 0.301 seconds
ANBL3 : DONE
OVERALL : CPU Time = 15.117 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 318666
UG3 : Min, Max Ang = 0.8537 178.7
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 290
UG3 : No. Angle>179.9 = 0
UG3 : No. Pyramid Elems = 2793
UG3 : Min, Max Ang = 7.032 171.7
UG3 : Average Angle = 82.6
UG3 : No. Angle>160.0 = 56
UG3 : No. Angle>179.9 = 0
UG3 : No. Prism Elems = 104033
UG3 : Min, Max Ang = 6.792 174.6
UG3 : Average Angle = 80.1
UG3 : No. Angle>160.0 = 561
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 318666
UG3 : Min Vol = 0.000481
UG3 : Average Vol = 1.87e+05
UG3 : Total-Tet-Vol = 5.96e+10
UG3 : No. Vol<TOL = 0
UG3 : No. Pyramid Elems = 2793
UG3 : Min Vol = 0.0167
UG3 : Average Vol = 0.25
UG3 : Total-Pyramid-Vol = 699
UG3 : No. Vol<TOL = 0
UG3 : No. Prism Elems = 104033
UG3 : Min Vol = 0.0144
UG3 : Average Vol = 0.37
UG3 : Total-Prism-Vol = 3.84e+04
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 318666
UG3 : Min, Max Q = 0.0647 1
UG3 : Average Q = 0.852
UG3 : No. Q< 0.1 = 25
UG3 : No. Q< 0.01 = 0
UG3 : No. Pyramid Elems = 2793
UG3 : Min, Max Q = 0.26 1
UG3 : Average Q = 0.793
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : No. Prism Elems = 104033
UG3 : Min, Max Q = 0.279 1
UG3 : Average Q = 0.902
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 31
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 33
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 35
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 36
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 37
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 38
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 39
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 40
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 41
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 42
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 43
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 44
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 45
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 46
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 19
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 20
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 21
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 22
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 23
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 24
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 19
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 20
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 21
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 22
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 23
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 24
Volume mesh:
Number of nodes = 109823
Number of elements = 438780
Number of triangles = 13288
Number of quadrilatarals = 0
Number of tetrahedrals = 318666
Number of pyramids = 2793
Number of prisms = 104033
Number of hexahedrals = 0
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
real 0m22.901s
user 0m19.333s
sys 0m3.063s
+ status=0
+ set +x
=================================================
data/session07/11_aflr4_aflr3_ViscousWingPod.py passed (as expected)
=================================================
=================================================
12_aflr4_aflr3_ViscousTransport.py test;
+ python 12_aflr4_aflr3_ViscousTransport.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building wingHinges
MESSAGE:: Building pylonOml
MESSAGE:: Building nacelleOml
MESSAGE:: Building htailOml
MESSAGE:: Building htailHinges
MESSAGE:: Building vtailOml
MESSAGE:: Building vtailHinges
MESSAGE:: Building fuseOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = Fuselage, index = 1
Name = Wing, index = 2
Name = Htail, index = 3
Name = Pylon, index = 4
Name = Vtail, index = 5
Name = Nacelle, index = 6
Name = Control, index = 7
Name = Farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 9
Name = Fuselage, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = Htail, index = 4
Name = Pylon, index = 5
Name = Vtail, index = 6
Name = Nacelle, index = 7
Name = Control, index = 8
Name = Farfield, index = 9
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 11 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 67 Faces
EGADS : Body 0 has 176 Edges
EGADS : Body 0 has 71 Loops
EGADS : Body 0 has 107 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 5 Faces
EGADS : Body 1 has 9 Edges
EGADS : Body 1 has 5 Loops
EGADS : Body 1 has 6 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 5 Faces
EGADS : Body 2 has 9 Edges
EGADS : Body 2 has 5 Loops
EGADS : Body 2 has 6 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 5 Faces
EGADS : Body 3 has 9 Edges
EGADS : Body 3 has 5 Loops
EGADS : Body 3 has 6 Nodes
EGADS : Body 4 is a SolidBody
EGADS : Body 4 has 1 Shells
EGADS : Body 4 has 5 Faces
EGADS : Body 4 has 9 Edges
EGADS : Body 4 has 5 Loops
EGADS : Body 4 has 6 Nodes
EGADS : Body 5 is a SolidBody
EGADS : Body 5 has 1 Shells
EGADS : Body 5 has 5 Faces
EGADS : Body 5 has 9 Edges
EGADS : Body 5 has 5 Loops
EGADS : Body 5 has 6 Nodes
EGADS : Body 6 is a SolidBody
EGADS : Body 6 has 1 Shells
EGADS : Body 6 has 5 Faces
EGADS : Body 6 has 9 Edges
EGADS : Body 6 has 5 Loops
EGADS : Body 6 has 6 Nodes
EGADS : Body 7 is a SolidBody
EGADS : Body 7 has 1 Shells
EGADS : Body 7 has 5 Faces
EGADS : Body 7 has 9 Edges
EGADS : Body 7 has 5 Loops
EGADS : Body 7 has 6 Nodes
EGADS : Body 8 is a SolidBody
EGADS : Body 8 has 1 Shells
EGADS : Body 8 has 5 Faces
EGADS : Body 8 has 9 Edges
EGADS : Body 8 has 5 Loops
EGADS : Body 8 has 6 Nodes
EGADS : Body 9 is a SolidBody
EGADS : Body 9 has 1 Shells
EGADS : Body 9 has 5 Faces
EGADS : Body 9 has 9 Edges
EGADS : Body 9 has 5 Loops
EGADS : Body 9 has 6 Nodes
EGADS : Body 10 is a SolidBody
EGADS : Body 10 has 1 Shells
EGADS : Body 10 has 6 Faces
EGADS : Body 10 has 12 Edges
EGADS : Body 10 has 6 Loops
EGADS : Body 10 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 6
EGADS : 2 Yes 0 0 1 0 1 1 7 8 9 10
EGADS : 3 Yes 0 0 1 0 1 1 8 11 12 13 14
EGADS : 4 Yes 0 0 1 0 1 1 7 12
EGADS : 5 Yes 0 0 1 0 1 1 6 15 16 17 18
EGADS : 6 Yes 0 0 1 0 1 1 5 15 16 17 19
EGADS : 20 21
EGADS : 7 Yes 0 0 1 0 1 2 4 22
EGADS : 8 Yes 0 0 1 0 1 2 3 11 22 23 24
EGADS : 9 Yes 0 0 1 0 1 2 10 25 26 27 28
EGADS : 29 30
EGADS : 10 Yes 0 0 1 0 1 2 9 26 27 28 31
EGADS : 11 Yes 0 0 1 0 1 3 8 12 22
EGADS : 12 Yes 0 0 1 0 1 3 4 11 13 14 22
EGADS : 32
EGADS : 13 Yes 0 0 1 0 1 3 12 14 33 34 35
EGADS : 36
EGADS : 14 Yes 0 0 1 0 1 3 12 13 33 34 35
EGADS : 36
EGADS : 15 Yes 0 0 1 0 1 5 6 16
EGADS : 16 Yes 0 0 1 0 1 5 6 15 17
EGADS : 17 Yes 0 0 1 0 1 5 6 16
EGADS : 18 Yes 0 0 1 0 1 5 19 37 38 39 40
EGADS : 41 42 43
EGADS : 19 Yes 0 0 1 0 1 6 18 37 38 39 40
EGADS : 41 42 43
EGADS : 20 Yes 0 0 1 0 1 6 21 44
EGADS : 21 Yes 0 0 1 0 1 6 20 45
EGADS : 22 Yes 0 0 1 0 1 7 8 11 12 23 24
EGADS : 46
EGADS : 23 Yes 0 0 1 0 1 8 22 24 47 48 49
EGADS : 50
EGADS : 24 Yes 0 0 1 0 1 8 22 23 47 48 49
EGADS : 50
EGADS : 25 Yes 0 0 1 0 1 9 31 51 52 53 54
EGADS : 55 56 57
EGADS : 26 Yes 0 0 1 0 1 9 10 27
EGADS : 27 Yes 0 0 1 0 1 9 10 26 28
EGADS : 28 Yes 0 0 1 0 1 9 10 27
EGADS : 29 Yes 0 0 1 0 1 9 30 58
EGADS : 30 Yes 0 0 1 0 1 9 29 59
EGADS : 31 Yes 0 0 1 0 1 10 25 51 52 53
EGADS : 54 55 56 57
EGADS : 32 Yes 0 0 1 0 1 12 46 60 61 62
EGADS : 63
EGADS : 33 Yes 0 0 1 0 1 13 14 34
EGADS : 34 Yes 0 0 1 0 1 13 14 33 35
EGADS : 35 Yes 0 0 1 0 1 13 14 34
EGADS : 36 Yes 0 0 1 0 1 13 14
EGADS : 37 Yes 0 0 1 0 1 18 19 38
EGADS : 38 Yes 0 0 1 0 1 18 19 37 39
EGADS : 39 Yes 0 0 1 0 1 18 19 38
EGADS : 40 Yes 0 0 1 0 1 18 19 41
EGADS : 41 Yes 0 0 1 0 1 18 19 40 42
EGADS : 42 Yes 0 0 1 0 1 18 19 41
EGADS : 43 Yes 0 0 1 0 1 18 19
EGADS : 44 Yes 0 0 1 0 1 20 45 64
EGADS : 45 Yes 0 0 1 0 1 21 44 65
EGADS : 46 Yes 0 0 1 0 1 22 32 60 61 62
EGADS : 63
EGADS : 47 Yes 0 0 1 0 1 23 24
EGADS : 48 Yes 0 0 1 0 1 23 24 49
EGADS : 49 Yes 0 0 1 0 1 23 24 48 50
EGADS : 50 Yes 0 0 1 0 1 23 24 49
EGADS : 51 Yes 0 0 1 0 1 25 31
EGADS : 52 Yes 0 0 1 0 1 25 31 53
EGADS : 53 Yes 0 0 1 0 1 25 31 52 54
EGADS : 54 Yes 0 0 1 0 1 25 31 53
EGADS : 55 Yes 0 0 1 0 1 25 31 56
EGADS : 56 Yes 0 0 1 0 1 25 31 55 57
EGADS : 57 Yes 0 0 1 0 1 25 31 56
EGADS : 58 Yes 0 0 1 0 1 29 59 66
EGADS : 59 Yes 0 0 1 0 1 30 58 67
EGADS : 60 Yes 0 0 1 0 1 32 46 61
EGADS : 61 Yes 0 0 1 0 1 32 46 60 62
EGADS : 62 Yes 0 0 1 0 1 32 46 61
EGADS : 63 Yes 0 0 1 0 1 32 46
EGADS : 64 Yes 0 0 1 0 1 44 65
EGADS : 65 Yes 0 0 1 0 1 45 64
EGADS : 66 Yes 0 0 1 0 1 58 67
EGADS : 67 Yes 0 0 1 0 1 59 66
EGADS : 68 Yes 1 0 1 0 1 69 70 71 72
EGADS : 69 Yes 1 0 1 0 1 68 70 72
EGADS : 70 Yes 1 0 1 0 1 68 69 71 72
EGADS : 71 Yes 1 0 1 0 1 68 70 72
EGADS : 72 Yes 1 0 1 0 1 68 69 70 71
EGADS : 73 Yes 2 0 1 0 1 74 75 76 77
EGADS : 74 Yes 2 0 1 0 1 73 75 77
EGADS : 75 Yes 2 0 1 0 1 73 74 76 77
EGADS : 76 Yes 2 0 1 0 1 73 75 77
EGADS : 77 Yes 2 0 1 0 1 73 74 75 76
EGADS : 78 Yes 3 0 1 0 1 79 80 81 82
EGADS : 79 Yes 3 0 1 0 1 78 80 82
EGADS : 80 Yes 3 0 1 0 1 78 79 81 82
EGADS : 81 Yes 3 0 1 0 1 78 80 82
EGADS : 82 Yes 3 0 1 0 1 78 79 80 81
EGADS : 83 Yes 4 0 1 0 1 84 85 86 87
EGADS : 84 Yes 4 0 1 0 1 83 85 86 87
EGADS : 85 Yes 4 0 1 0 1 83 84 86
EGADS : 86 Yes 4 0 1 0 1 83 84 85 87
EGADS : 87 Yes 4 0 1 0 1 83 84 86
EGADS : 88 Yes 5 0 1 0 1 89 90 91 92
EGADS : 89 Yes 5 0 1 0 1 88 90 91 92
EGADS : 90 Yes 5 0 1 0 1 88 89 91
EGADS : 91 Yes 5 0 1 0 1 88 89 90 92
EGADS : 92 Yes 5 0 1 0 1 88 89 91
EGADS : 93 Yes 6 0 1 0 1 94 95 96 97
EGADS : 94 Yes 6 0 1 0 1 93 95 97
EGADS : 95 Yes 6 0 1 0 1 93 94 96 97
EGADS : 96 Yes 6 0 1 0 1 93 95 97
EGADS : 97 Yes 6 0 1 0 1 93 94 95 96
EGADS : 98 Yes 7 0 1 0 1 99 100 101 102
EGADS : 99 Yes 7 0 1 0 1 98 100 101 102
EGADS : 100 Yes 7 0 1 0 1 98 99 101
EGADS : 101 Yes 7 0 1 0 1 98 99 100 102
EGADS : 102 Yes 7 0 1 0 1 98 99 101
EGADS : 103 Yes 8 0 1 0 1 104 105 106 107
EGADS : 104 Yes 8 0 1 0 1 103 105 106 107
EGADS : 105 Yes 8 0 1 0 1 103 104 106
EGADS : 106 Yes 8 0 1 0 1 103 104 105 107
EGADS : 107 Yes 8 0 1 0 1 103 104 106
EGADS : 108 Yes 9 0 1 0 1 109 110 111 112
EGADS : 109 Yes 9 0 1 0 1 108 110 111 112
EGADS : 110 Yes 9 0 1 0 1 108 109 111
EGADS : 111 Yes 9 0 1 0 1 108 109 110 112
EGADS : 112 Yes 9 0 1 0 1 108 109 111
EGADS : 113 Yes 10 0 1 NA NA 115 116 117 118
EGADS : 114 Yes 10 0 1 NA NA 115 116 117 118
EGADS : 115 Yes 10 0 1 NA NA 113 114 117 118
EGADS : 116 Yes 10 0 1 NA NA 113 114 117 118
EGADS : 117 Yes 10 0 1 NA NA 113 114 115 116
EGADS : 118 Yes 10 0 1 NA NA 113 114 115 116
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 4 3 -2 -5 -6
EGADS : 2 -7 9 1 -8 10 11
EGADS : 3 -12 2 17 -16 -15 14 -13
EGADS : 4 -3 18 19 -20
EGADS : 5 21 -22 23 24 25 26 -27 5
EGADS : 6 27 28 -25 29 -30 -31 -21 6 32 33
EGADS : 7 -19 34 7 -35
EGADS : 8 -36 8 12 -40 -39 38 37
EGADS : 9 -41 -10 47 46 45 -44 43 -42 48 49
EGADS : 10 -47 -11 41 -53 -43 -52 -51 50
EGADS : 11 13 54 55 40
EGADS : 12 -17 20 60 59 58 -54 -14 -57 -56
EGADS : 13 61 -62 63 64 65 66 -67 57 15
EGADS : 14 67 68 -65 69 -70 -71 -61 16 56
EGADS : 15 31 72 22
EGADS : 16 30 73 -23 -72
EGADS : 17 -73 -29 -24
EGADS : 18 74 -75 76 77 78 -79 80 81 82 83 -84 -26
EGADS : 19 84 85 -82 86 -87 -88 -78 89 -90 -91 -74 -28
EGADS : 20 -92 94 -32 -93
EGADS : 21 -94 95 93 -33
EGADS : 22 -60 35 36 98 97 39 -55 -58 96
EGADS : 23 -99 -98 -37 105 104 103 -102 101 -100
EGADS : 24 -105 -38 -97 99 -109 -101 -108 -107 106
EGADS : 25 -110 42 120 119 118 -117 116 115 114 -113 112 -111
EGADS : 26 44 121 52
EGADS : 27 -45 122 51 -121
EGADS : 28 -122 -46 -50
EGADS : 29 123 124 -48 -125
EGADS : 30 125 -49 -124 -126
EGADS : 31 -120 53 110 -133 -112 -132 -131 130 -116 -129 -128 127
EGADS : 32 -134 -59 140 -139 -138 -137 -136 135
EGADS : 33 71 141 62
EGADS : 34 70 142 -63 -141
EGADS : 35 -142 -69 -64
EGADS : 36 -66 -68
EGADS : 37 91 143 75
EGADS : 38 90 144 -76 -143
EGADS : 39 -144 -89 -77
EGADS : 40 88 145 79
EGADS : 41 87 146 -80 -145
EGADS : 42 -146 -86 -81
EGADS : 43 -83 -85
EGADS : 44 147 92 148 149 -150 -151
EGADS : 45 -147 153 150 -152 -148 -95
EGADS : 46 -140 -96 134 157 156 -155 138 -154
EGADS : 47 109 100
EGADS : 48 102 158 108
EGADS : 49 -103 159 107 -158
EGADS : 50 -159 -104 -106
EGADS : 51 133 111
EGADS : 52 113 160 132
EGADS : 53 -114 161 131 -160
EGADS : 54 -161 -115 -130
EGADS : 55 117 162 129
EGADS : 56 -118 163 128 -162
EGADS : 57 -163 -119 -127
EGADS : 58 164 -123 165 166 -167 -168
EGADS : 59 -164 170 167 -169 -165 126
EGADS : 60 -135 171 -157
EGADS : 61 136 172 -156 -171
EGADS : 62 -172 137 155
EGADS : 63 139 154
EGADS : 64 -149 173 151 -174
EGADS : 65 152 174 -153 -173
EGADS : 66 -166 175 168 -176
EGADS : 67 169 176 -170 -175
EGADS : 68 -177 180 179 -178
EGADS : 69 181 182 177
EGADS : 70 178 183 -184 -181
EGADS : 71 -179 -185 -183
EGADS : 72 -180 -182 184 185
EGADS : 73 -186 189 188 -187
EGADS : 74 190 191 186
EGADS : 75 187 192 -193 -190
EGADS : 76 -188 -194 -192
EGADS : 77 -189 -191 193 194
EGADS : 78 -195 198 197 -196
EGADS : 79 199 200 195
EGADS : 80 196 201 -202 -199
EGADS : 81 -197 -203 -201
EGADS : 82 -198 -200 202 203
EGADS : 83 204 -205 -206 207
EGADS : 84 208 209 -210 -204
EGADS : 85 211 205 210
EGADS : 86 -209 212 206 -211
EGADS : 87 -208 -207 -212
EGADS : 88 213 -214 -215 216
EGADS : 89 217 218 -219 -213
EGADS : 90 220 214 219
EGADS : 91 -218 221 215 -220
EGADS : 92 -217 -216 -221
EGADS : 93 -222 -223 224 225
EGADS : 94 226 222 227
EGADS : 95 -228 229 223 -226
EGADS : 96 -230 -224 -229
EGADS : 97 -225 230 228 -227
EGADS : 98 231 234 -233 -232
EGADS : 99 -231 -237 236 235
EGADS : 100 238 237 232
EGADS : 101 233 239 -236 -238
EGADS : 102 -234 -235 -239
EGADS : 103 240 -241 -242 243
EGADS : 104 -240 244 245 -246
EGADS : 105 247 241 246
EGADS : 106 -245 248 242 -247
EGADS : 107 -244 -243 -248
EGADS : 108 -249 -252 251 250
EGADS : 109 -253 249 255 -254
EGADS : 110 256 -255 -250
EGADS : 111 -251 257 254 -256
EGADS : 112 252 253 -257
EGADS : 113 258 259 -260 -261
EGADS : 114 -262 265 264 -263
EGADS : 115 266 262 -267 -258
EGADS : 116 -268 260 269 -264
EGADS : 117 261 268 -265 -266
EGADS : 118 -259 267 263 -269
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1 2
EGADS : 2 3 4
EGADS : 3 5
EGADS : 4 6
EGADS : 5 7
EGADS : 6 8 9
EGADS : 7 10
EGADS : 8 11
EGADS : 9 12 13
EGADS : 10 14
EGADS : 11 15
EGADS : 12 16
EGADS : 13 17
EGADS : 14 18
EGADS : 15 19
EGADS : 16 20
EGADS : 17 21
EGADS : 18 22
EGADS : 19 23
EGADS : 20 24
EGADS : 21 25
EGADS : 22 26
EGADS : 23 27
EGADS : 24 28
EGADS : 25 29
EGADS : 26 30
EGADS : 27 31
EGADS : 28 32
EGADS : 29 33
EGADS : 30 34
EGADS : 31 35
EGADS : 32 36
EGADS : 33 37
EGADS : 34 38
EGADS : 35 39
EGADS : 36 40
EGADS : 37 41
EGADS : 38 42
EGADS : 39 43
EGADS : 40 44
EGADS : 41 45
EGADS : 42 46
EGADS : 43 47
EGADS : 44 48
EGADS : 45 49
EGADS : 46 50
EGADS : 47 51
EGADS : 48 52
EGADS : 49 53
EGADS : 50 54
EGADS : 51 55
EGADS : 52 56
EGADS : 53 57
EGADS : 54 58
EGADS : 55 59
EGADS : 56 60
EGADS : 57 61
EGADS : 58 62
EGADS : 59 63
EGADS : 60 64
EGADS : 61 65
EGADS : 62 66
EGADS : 63 67
EGADS : 64 68
EGADS : 65 69
EGADS : 66 70
EGADS : 67 71
EGADS : 68 72
EGADS : 69 73
EGADS : 70 74
EGADS : 71 75
EGADS : 72 76
EGADS : 73 77
EGADS : 74 78
EGADS : 75 79
EGADS : 76 80
EGADS : 77 81
EGADS : 78 82
EGADS : 79 83
EGADS : 80 84
EGADS : 81 85
EGADS : 82 86
EGADS : 83 87
EGADS : 84 88
EGADS : 85 89
EGADS : 86 90
EGADS : 87 91
EGADS : 88 92
EGADS : 89 93
EGADS : 90 94
EGADS : 91 95
EGADS : 92 96
EGADS : 93 97
EGADS : 94 98
EGADS : 95 99
EGADS : 96 100
EGADS : 97 101
EGADS : 98 102
EGADS : 99 103
EGADS : 100 104
EGADS : 101 105
EGADS : 102 106
EGADS : 103 107
EGADS : 104 108
EGADS : 105 109
EGADS : 106 110
EGADS : 107 111
EGADS : 108 112
EGADS : 109 113
EGADS : 110 114
EGADS : 111 115
EGADS : 112 116
EGADS : 113 117
EGADS : 114 118
EGADS : 115 119
EGADS : 116 120
EGADS : 117 121
EGADS : 118 122
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 4 3 -2
EGADS : 2 Yes -5 -6
EGADS : 3 Yes -7 9 1 -8
EGADS : 4 Yes 10 11
EGADS : 5 Yes -12 2 17 -16 -15 14 -13
EGADS : 6 Yes -3 18 19 -20
EGADS : 7 Yes 21 -22 23 24 25 26 -27 5
EGADS : 8 Yes 27 28 -25 29 -30 -31 -21 6
EGADS : 9 Yes 32 33
EGADS : 10 Yes -19 34 7 -35
EGADS : 11 Yes -36 8 12 -40 -39 38 37
EGADS : 12 Yes -41 -10 47 46 45 -44 43 -42
EGADS : 13 Yes 48 49
EGADS : 14 Yes -47 -11 41 -53 -43 -52 -51 50
EGADS : 15 Yes 13 54 55 40
EGADS : 16 Yes -17 20 60 59 58 -54 -14 -57 -56
EGADS : 17 Yes 61 -62 63 64 65 66 -67 57 15
EGADS : 18 Yes 67 68 -65 69 -70 -71 -61 16 56
EGADS : 19 Yes 31 72 22
EGADS : 20 Yes 30 73 -23 -72
EGADS : 21 Yes -73 -29 -24
EGADS : 22 Yes 74 -75 76 77 78 -79 80 81 82 83 -84 -26
EGADS : 23 Yes 84 85 -82 86 -87 -88 -78 89 -90 -91 -74 -28
EGADS : 24 Yes -92 94 -32 -93
EGADS : 25 Yes -94 95 93 -33
EGADS : 26 Yes -60 35 36 98 97 39 -55 -58 96
EGADS : 27 Yes -99 -98 -37 105 104 103 -102 101 -100
EGADS : 28 Yes -105 -38 -97 99 -109 -101 -108 -107 106
EGADS : 29 Yes -110 42 120 119 118 -117 116 115 114 -113 112 -111
EGADS : 30 Yes 44 121 52
EGADS : 31 Yes -45 122 51 -121
EGADS : 32 Yes -122 -46 -50
EGADS : 33 Yes 123 124 -48 -125
EGADS : 34 Yes 125 -49 -124 -126
EGADS : 35 Yes -120 53 110 -133 -112 -132 -131 130 -116 -129 -128
EGADS : 127
EGADS : 36 Yes -134 -59 140 -139 -138 -137 -136 135
EGADS : 37 Yes 71 141 62
EGADS : 38 Yes 70 142 -63 -141
EGADS : 39 Yes -142 -69 -64
EGADS : 40 Yes -66 -68
EGADS : 41 Yes 91 143 75
EGADS : 42 Yes 90 144 -76 -143
EGADS : 43 Yes -144 -89 -77
EGADS : 44 Yes 88 145 79
EGADS : 45 Yes 87 146 -80 -145
EGADS : 46 Yes -146 -86 -81
EGADS : 47 Yes -83 -85
EGADS : 48 Yes 147 92 148 149 -150 -151
EGADS : 49 Yes -147 153 150 -152 -148 -95
EGADS : 50 Yes -140 -96 134 157 156 -155 138 -154
EGADS : 51 Yes 109 100
EGADS : 52 Yes 102 158 108
EGADS : 53 Yes -103 159 107 -158
EGADS : 54 Yes -159 -104 -106
EGADS : 55 Yes 133 111
EGADS : 56 Yes 113 160 132
EGADS : 57 Yes -114 161 131 -160
EGADS : 58 Yes -161 -115 -130
EGADS : 59 Yes 117 162 129
EGADS : 60 Yes -118 163 128 -162
EGADS : 61 Yes -163 -119 -127
EGADS : 62 Yes 164 -123 165 166 -167 -168
EGADS : 63 Yes -164 170 167 -169 -165 126
EGADS : 64 Yes -135 171 -157
EGADS : 65 Yes 136 172 -156 -171
EGADS : 66 Yes -172 137 155
EGADS : 67 Yes 139 154
EGADS : 68 Yes -149 173 151 -174
EGADS : 69 Yes 152 174 -153 -173
EGADS : 70 Yes -166 175 168 -176
EGADS : 71 Yes 169 176 -170 -175
EGADS : 72 Yes -177 180 179 -178
EGADS : 73 Yes 181 182 177
EGADS : 74 Yes 178 183 -184 -181
EGADS : 75 Yes -179 -185 -183
EGADS : 76 Yes -180 -182 184 185
EGADS : 77 Yes -186 189 188 -187
EGADS : 78 Yes 190 191 186
EGADS : 79 Yes 187 192 -193 -190
EGADS : 80 Yes -188 -194 -192
EGADS : 81 Yes -189 -191 193 194
EGADS : 82 Yes -195 198 197 -196
EGADS : 83 Yes 199 200 195
EGADS : 84 Yes 196 201 -202 -199
EGADS : 85 Yes -197 -203 -201
EGADS : 86 Yes -198 -200 202 203
EGADS : 87 Yes 204 -205 -206 207
EGADS : 88 Yes 208 209 -210 -204
EGADS : 89 Yes 211 205 210
EGADS : 90 Yes -209 212 206 -211
EGADS : 91 Yes -208 -207 -212
EGADS : 92 Yes 213 -214 -215 216
EGADS : 93 Yes 217 218 -219 -213
EGADS : 94 Yes 220 214 219
EGADS : 95 Yes -218 221 215 -220
EGADS : 96 Yes -217 -216 -221
EGADS : 97 Yes -222 -223 224 225
EGADS : 98 Yes 226 222 227
EGADS : 99 Yes -228 229 223 -226
EGADS : 100 Yes -230 -224 -229
EGADS : 101 Yes -225 230 228 -227
EGADS : 102 Yes 231 234 -233 -232
EGADS : 103 Yes -231 -237 236 235
EGADS : 104 Yes 238 237 232
EGADS : 105 Yes 233 239 -236 -238
EGADS : 106 Yes -234 -235 -239
EGADS : 107 Yes 240 -241 -242 243
EGADS : 108 Yes -240 244 245 -246
EGADS : 109 Yes 247 241 246
EGADS : 110 Yes -245 248 242 -247
EGADS : 111 Yes -244 -243 -248
EGADS : 112 Yes -249 -252 251 250
EGADS : 113 Yes -253 249 255 -254
EGADS : 114 Yes 256 -255 -250
EGADS : 115 Yes -251 257 254 -256
EGADS : 116 Yes 252 253 -257
EGADS : 117 Yes 258 259 -260 -261
EGADS : 118 Yes -262 265 264 -263
EGADS : 119 Yes 266 262 -267 -258
EGADS : 120 Yes -268 260 269 -264
EGADS : 121 Yes 261 268 -265 -266
EGADS : 122 Yes -259 267 263 -269
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 2 3 1 1 3
EGADS : 3 0 Yes 1 3 1 1 4
EGADS : 4 0 DEGEN 1 1 - 1
EGADS : 5 0 Yes 4 5 1 1 5
EGADS : 6 0 Yes 5 4 1 1 6
EGADS : 7 0 Yes 1 6 1 2 7
EGADS : 8 0 Yes 6 2 1 2 8
EGADS : 9 0 DEGEN 1 1 - 2
EGADS : 10 0 Yes 7 8 1 2 9
EGADS : 11 0 Yes 8 7 1 2 10
EGADS : 12 0 Yes 2 9 1 3 8
EGADS : 13 0 Yes 9 10 1 3 11
EGADS : 14 0 Yes 11 10 1 3 12
EGADS : 15 0 Yes 11 12 1 3 13
EGADS : 16 0 Yes 12 13 1 3 14
EGADS : 17 0 Yes 3 13 1 3 12
EGADS : 18 0 DEGEN 1 1 - 4
EGADS : 19 0 Yes 1 14 1 4 7
EGADS : 20 0 Yes 3 14 1 4 12
EGADS : 21 0 Yes 5 15 1 5 6
EGADS : 22 0 Yes 16 15 1 5 15
EGADS : 23 0 Yes 16 17 1 5 16
EGADS : 24 0 Yes 17 18 1 5 17
EGADS : 25 0 Yes 18 19 1 5 6
EGADS : 26 0 Yes 19 20 1 5 18
EGADS : 27 0 Yes 4 20 1 5 6
EGADS : 28 0 Yes 20 19 1 6 19
EGADS : 29 0 Yes 18 21 1 6 17
EGADS : 30 0 Yes 22 21 1 6 16
EGADS : 31 0 Yes 15 22 1 6 15
EGADS : 32 0 Yes 23 24 1 6 20
EGADS : 33 0 Yes 24 23 1 6 21
EGADS : 34 0 DEGEN 1 1 - 7
EGADS : 35 0 Yes 14 6 1 7 22
EGADS : 36 0 Yes 6 25 1 8 22
EGADS : 37 0 Yes 26 25 1 8 23
EGADS : 38 0 Yes 27 26 1 8 24
EGADS : 39 0 Yes 27 28 1 8 22
EGADS : 40 0 Yes 28 9 1 8 11
EGADS : 41 0 Yes 8 29 1 9 10
EGADS : 42 0 Yes 29 30 1 9 25
EGADS : 43 0 Yes 31 30 1 9 10
EGADS : 44 0 Yes 31 32 1 9 26
EGADS : 45 0 Yes 33 32 1 9 27
EGADS : 46 0 Yes 34 33 1 9 28
EGADS : 47 0 Yes 7 34 1 9 10
EGADS : 48 0 Yes 35 36 1 9 29
EGADS : 49 0 Yes 36 35 1 9 30
EGADS : 50 0 Yes 37 34 1 10 28
EGADS : 51 0 Yes 37 38 1 10 27
EGADS : 52 0 Yes 38 31 1 10 26
EGADS : 53 0 Yes 30 29 1 10 31
EGADS : 54 0 Yes 10 39 1 11 12
EGADS : 55 0 Yes 39 28 1 11 22
EGADS : 56 0 Yes 13 40 1 12 14
EGADS : 57 0 Yes 40 11 1 12 13
EGADS : 58 0 Yes 41 39 1 12 22
EGADS : 59 0 Yes 42 41 1 12 32
EGADS : 60 0 Yes 14 42 1 12 22
EGADS : 61 0 Yes 12 43 1 13 14
EGADS : 62 0 Yes 44 43 1 13 33
EGADS : 63 0 Yes 44 45 1 13 34
EGADS : 64 0 Yes 45 46 1 13 35
EGADS : 65 0 Yes 46 47 1 13 14
EGADS : 66 0 Yes 47 48 1 13 36
EGADS : 67 0 Yes 40 48 1 13 14
EGADS : 68 0 Yes 48 47 1 14 36
EGADS : 69 0 Yes 46 49 1 14 35
EGADS : 70 0 Yes 50 49 1 14 34
EGADS : 71 0 Yes 43 50 1 14 33
EGADS : 72 0 Yes 22 16 1 15 16
EGADS : 73 0 Yes 21 17 1 16 17
EGADS : 74 0 Yes 19 51 1 18 19
EGADS : 75 0 Yes 52 51 1 18 37
EGADS : 76 0 Yes 52 53 1 18 38
EGADS : 77 0 Yes 53 54 1 18 39
EGADS : 78 0 Yes 54 55 1 18 19
EGADS : 79 0 Yes 56 55 1 18 40
EGADS : 80 0 Yes 56 57 1 18 41
EGADS : 81 0 Yes 57 58 1 18 42
EGADS : 82 0 Yes 58 59 1 18 19
EGADS : 83 0 Yes 59 60 1 18 43
EGADS : 84 0 Yes 20 60 1 18 19
EGADS : 85 0 Yes 60 59 1 19 43
EGADS : 86 0 Yes 58 61 1 19 42
EGADS : 87 0 Yes 62 61 1 19 41
EGADS : 88 0 Yes 55 62 1 19 40
EGADS : 89 0 Yes 54 63 1 19 39
EGADS : 90 0 Yes 64 63 1 19 38
EGADS : 91 0 Yes 51 64 1 19 37
EGADS : 92 0 Yes 65 66 1 20 44
EGADS : 93 0 Yes 66 23 1 20 21
EGADS : 94 0 Yes 65 24 1 20 21
EGADS : 95 0 Yes 65 66 1 21 45
EGADS : 96 0 Yes 41 42 1 22 46
EGADS : 97 0 Yes 67 27 1 22 24
EGADS : 98 0 Yes 25 67 1 22 23
EGADS : 99 0 Yes 67 68 1 23 24
EGADS : 100 0 Yes 68 69 1 23 47
EGADS : 101 0 Yes 70 69 1 23 24
EGADS : 102 0 Yes 70 71 1 23 48
EGADS : 103 0 Yes 72 71 1 23 49
EGADS : 104 0 Yes 73 72 1 23 50
EGADS : 105 0 Yes 26 73 1 23 24
EGADS : 106 0 Yes 74 73 1 24 50
EGADS : 107 0 Yes 74 75 1 24 49
EGADS : 108 0 Yes 75 70 1 24 48
EGADS : 109 0 Yes 69 68 1 24 47
EGADS : 110 0 Yes 29 76 1 25 31
EGADS : 111 0 Yes 76 77 1 25 51
EGADS : 112 0 Yes 78 77 1 25 31
EGADS : 113 0 Yes 78 79 1 25 52
EGADS : 114 0 Yes 80 79 1 25 53
EGADS : 115 0 Yes 81 80 1 25 54
EGADS : 116 0 Yes 82 81 1 25 31
EGADS : 117 0 Yes 82 83 1 25 55
EGADS : 118 0 Yes 84 83 1 25 56
EGADS : 119 0 Yes 85 84 1 25 57
EGADS : 120 0 Yes 30 85 1 25 31
EGADS : 121 0 Yes 32 38 1 26 27
EGADS : 122 0 Yes 33 37 1 27 28
EGADS : 123 0 Yes 86 87 1 29 58
EGADS : 124 0 Yes 87 36 1 29 30
EGADS : 125 0 Yes 86 35 1 29 30
EGADS : 126 0 Yes 86 87 1 30 59
EGADS : 127 0 Yes 88 85 1 31 57
EGADS : 128 0 Yes 88 89 1 31 56
EGADS : 129 0 Yes 89 82 1 31 55
EGADS : 130 0 Yes 90 81 1 31 54
EGADS : 131 0 Yes 90 91 1 31 53
EGADS : 132 0 Yes 91 78 1 31 52
EGADS : 133 0 Yes 77 76 1 31 51
EGADS : 134 0 Yes 41 92 1 32 46
EGADS : 135 0 Yes 93 92 1 32 60
EGADS : 136 0 Yes 93 94 1 32 61
EGADS : 137 0 Yes 94 95 1 32 62
EGADS : 138 0 Yes 95 96 1 32 46
EGADS : 139 0 Yes 96 97 1 32 63
EGADS : 140 0 Yes 42 97 1 32 46
EGADS : 141 0 Yes 50 44 1 33 34
EGADS : 142 0 Yes 49 45 1 34 35
EGADS : 143 0 Yes 64 52 1 37 38
EGADS : 144 0 Yes 63 53 1 38 39
EGADS : 145 0 Yes 62 56 1 40 41
EGADS : 146 0 Yes 61 57 1 41 42
EGADS : 147 0 Yes 98 65 1 44 45
EGADS : 148 0 Yes 66 99 1 44 45
EGADS : 149 0 Yes 99 100 1 44 64
EGADS : 150 0 Yes 101 100 1 44 45
EGADS : 151 0 Yes 98 101 1 44 64
EGADS : 152 0 Yes 99 100 1 45 65
EGADS : 153 0 Yes 98 101 1 45 65
EGADS : 154 0 Yes 97 96 1 46 63
EGADS : 155 0 Yes 95 102 1 46 62
EGADS : 156 0 Yes 103 102 1 46 61
EGADS : 157 0 Yes 92 103 1 46 60
EGADS : 158 0 Yes 71 75 1 48 49
EGADS : 159 0 Yes 72 74 1 49 50
EGADS : 160 0 Yes 79 91 1 52 53
EGADS : 161 0 Yes 80 90 1 53 54
EGADS : 162 0 Yes 83 89 1 55 56
EGADS : 163 0 Yes 84 88 1 56 57
EGADS : 164 0 Yes 104 87 1 58 59
EGADS : 165 0 Yes 86 105 1 58 59
EGADS : 166 0 Yes 105 106 1 58 66
EGADS : 167 0 Yes 107 106 1 58 59
EGADS : 168 0 Yes 104 107 1 58 66
EGADS : 169 0 Yes 105 106 1 59 67
EGADS : 170 0 Yes 104 107 1 59 67
EGADS : 171 0 Yes 93 103 1 60 61
EGADS : 172 0 Yes 94 102 1 61 62
EGADS : 173 0 Yes 99 98 1 64 65
EGADS : 174 0 Yes 100 101 1 64 65
EGADS : 175 0 Yes 105 104 1 66 67
EGADS : 176 0 Yes 106 107 1 66 67
EGADS : 177 1 Yes 108 109 1 68 69
EGADS : 178 1 Yes 109 110 1 68 70
EGADS : 179 1 Yes 111 110 1 68 71
EGADS : 180 1 Yes 108 111 1 68 72
EGADS : 181 1 Yes 109 112 1 69 70
EGADS : 182 1 Yes 112 108 1 69 72
EGADS : 183 1 Yes 110 113 1 70 71
EGADS : 184 1 Yes 112 113 1 70 72
EGADS : 185 1 Yes 113 111 1 71 72
EGADS : 186 2 Yes 114 115 1 73 74
EGADS : 187 2 Yes 115 116 1 73 75
EGADS : 188 2 Yes 117 116 1 73 76
EGADS : 189 2 Yes 114 117 1 73 77
EGADS : 190 2 Yes 115 118 1 74 75
EGADS : 191 2 Yes 118 114 1 74 77
EGADS : 192 2 Yes 116 119 1 75 76
EGADS : 193 2 Yes 118 119 1 75 77
EGADS : 194 2 Yes 119 117 1 76 77
EGADS : 195 3 Yes 120 121 1 78 79
EGADS : 196 3 Yes 121 122 1 78 80
EGADS : 197 3 Yes 123 122 1 78 81
EGADS : 198 3 Yes 120 123 1 78 82
EGADS : 199 3 Yes 121 124 1 79 80
EGADS : 200 3 Yes 124 120 1 79 82
EGADS : 201 3 Yes 122 125 1 80 81
EGADS : 202 3 Yes 124 125 1 80 82
EGADS : 203 3 Yes 125 123 1 81 82
EGADS : 204 4 Yes 126 127 1 83 84
EGADS : 205 4 Yes 128 127 1 83 85
EGADS : 206 4 Yes 129 128 1 83 86
EGADS : 207 4 Yes 129 126 1 83 87
EGADS : 208 4 Yes 126 130 1 84 87
EGADS : 209 4 Yes 130 131 1 84 86
EGADS : 210 4 Yes 127 131 1 84 85
EGADS : 211 4 Yes 131 128 1 85 86
EGADS : 212 4 Yes 130 129 1 86 87
EGADS : 213 5 Yes 132 133 1 88 89
EGADS : 214 5 Yes 134 133 1 88 90
EGADS : 215 5 Yes 135 134 1 88 91
EGADS : 216 5 Yes 135 132 1 88 92
EGADS : 217 5 Yes 132 136 1 89 92
EGADS : 218 5 Yes 136 137 1 89 91
EGADS : 219 5 Yes 133 137 1 89 90
EGADS : 220 5 Yes 137 134 1 90 91
EGADS : 221 5 Yes 136 135 1 91 92
EGADS : 222 6 Yes 138 139 1 93 94
EGADS : 223 6 Yes 140 138 1 93 95
EGADS : 224 6 Yes 140 141 1 93 96
EGADS : 225 6 Yes 141 139 1 93 97
EGADS : 226 6 Yes 142 138 1 94 95
EGADS : 227 6 Yes 139 142 1 94 97
EGADS : 228 6 Yes 143 142 1 95 97
EGADS : 229 6 Yes 143 140 1 95 96
EGADS : 230 6 Yes 141 143 1 96 97
EGADS : 231 7 Yes 144 145 1 98 99
EGADS : 232 7 Yes 144 146 1 98 100
EGADS : 233 7 Yes 146 147 1 98 101
EGADS : 234 7 Yes 145 147 1 98 102
EGADS : 235 7 Yes 148 145 1 99 102
EGADS : 236 7 Yes 149 148 1 99 101
EGADS : 237 7 Yes 149 144 1 99 100
EGADS : 238 7 Yes 146 149 1 100 101
EGADS : 239 7 Yes 147 148 1 101 102
EGADS : 240 8 Yes 150 151 1 103 104
EGADS : 241 8 Yes 152 151 1 103 105
EGADS : 242 8 Yes 153 152 1 103 106
EGADS : 243 8 Yes 153 150 1 103 107
EGADS : 244 8 Yes 150 154 1 104 107
EGADS : 245 8 Yes 154 155 1 104 106
EGADS : 246 8 Yes 151 155 1 104 105
EGADS : 247 8 Yes 155 152 1 105 106
EGADS : 248 8 Yes 154 153 1 106 107
EGADS : 249 9 Yes 156 157 1 108 109
EGADS : 250 9 Yes 158 157 1 108 110
EGADS : 251 9 Yes 159 158 1 108 111
EGADS : 252 9 Yes 159 156 1 108 112
EGADS : 253 9 Yes 156 160 1 109 112
EGADS : 254 9 Yes 160 161 1 109 111
EGADS : 255 9 Yes 157 161 1 109 110
EGADS : 256 9 Yes 158 161 1 110 111
EGADS : 257 9 Yes 159 160 1 111 112
EGADS : 258 10 Yes 163 162 NA 113 115
EGADS : 259 10 Yes 162 164 NA 113 118
EGADS : 260 10 Yes 165 164 NA 113 116
EGADS : 261 10 Yes 163 165 NA 113 117
EGADS : 262 10 Yes 167 166 NA 114 115
EGADS : 263 10 Yes 166 168 NA 114 118
EGADS : 264 10 Yes 169 168 NA 114 116
EGADS : 265 10 Yes 167 169 NA 114 117
EGADS : 266 10 Yes 163 167 NA 115 117
EGADS : 267 10 Yes 162 166 NA 115 118
EGADS : 268 10 Yes 165 169 NA 116 117
EGADS : 269 10 Yes 164 168 NA 116 118
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 121.026192 0 0
EGADS : 3 Yes 121.026192 10 0
EGADS : 4 Yes 54.9020417 7.00084115 0
EGADS : 5 Yes 97.361045 7.90366896 0
EGADS : 6 Yes 121.026192 0 0
EGADS : 7 Yes 97.361045 0 0
EGADS : 8 Yes 54.9020417 0 0
EGADS : 9 Yes 165.026192 0 7
EGADS : 10 Yes 165.026192 0.5 8.5
EGADS : 11 Yes 156.577382 2.32417494 6.86784347
EGADS : 12 Yes 160.457816 1.16501909 6.24763245
EGADS : 13 Yes 152.092394 3.29252447 6.00142548
EGADS : 14 Yes 121.026192 0 10
EGADS : 15 Yes 97.4729828 13.4242093 0
EGADS : 16 Yes 93.4296648 13.4242093 0
EGADS : 17 Yes 93.813734 32.4820648 0
EGADS : 18 Yes 97.8594113 32.4820648 0
EGADS : 19 Yes 97.9335611 36.1389817 0
EGADS : 20 Yes 75.3047874 36.1389817 0
EGADS : 21 Yes 93.813734 32.4820648 0
EGADS : 22 Yes 93.4296648 13.4242093 0
EGADS : 23 Yes 72.4759225 29.3018771 0
EGADS : 24 Yes 83.5054156 29.3018771 0
EGADS : 25 Yes 152.092394 0 6.00142548
EGADS : 26 Yes 160.457816 0 6.24763245
EGADS : 27 Yes 156.577382 0 6.86784347
EGADS : 28 Yes 165.026192 0 8.5
EGADS : 29 Yes 75.3047874 0 0
EGADS : 30 Yes 97.9335611 0 0
EGADS : 31 Yes 97.8594113 0 0
EGADS : 32 Yes 93.813734 0 0
EGADS : 33 Yes 93.4296648 0 0
EGADS : 34 Yes 97.4729828 0 0
EGADS : 35 Yes 72.4759225 0 0
EGADS : 36 Yes 83.5054156 0 0
EGADS : 37 Yes 93.4296648 0 0
EGADS : 38 Yes 93.813734 0 0
EGADS : 39 Yes 165.026192 0 10
EGADS : 40 Yes 139.227902 5.03861756 7.07099122
EGADS : 41 Yes 159.822328 0 10
EGADS : 42 Yes 137.454662 0 10
EGADS : 43 Yes 162.492237 6.6562396 7.4148274
EGADS : 44 Yes 153.156875 6.6562396 8.10980625
EGADS : 45 Yes 168.687412 34.4921381 13.6297335
EGADS : 46 Yes 172.805054 34.4921381 13.3315303
EGADS : 47 Yes 173.282633 35.781198 13.6055284
EGADS : 48 Yes 165.02399 35.781198 13.6055284
EGADS : 49 Yes 168.687412 34.4921381 13.033327
EGADS : 50 Yes 153.156875 6.6562396 6.71984855
EGADS : 51 Yes 100.269362 41.7493571 0
EGADS : 52 Yes 94.7284993 41.7493571 0
EGADS : 53 Yes 107.349293 67.6443173 1.84589548
EGADS : 54 Yes 111.050367 67.6443173 1.25578139
EGADS : 55 Yes 111.248847 68.1210465 1.31074802
EGADS : 56 Yes 107.581644 68.1210465 1.89111513
EGADS : 57 Yes 121.153699 95.9694651 4.50848923
EGADS : 58 Yes 122.843146 95.9694651 4.52165604
EGADS : 59 Yes 123.552357 97.6729236 4.7180639
EGADS : 60 Yes 118.391317 97.6729236 3.99272703
EGADS : 61 Yes 121.153699 95.9694651 4.20550678
EGADS : 62 Yes 107.581644 68.1210465 0.865881946
EGADS : 63 Yes 107.349293 67.6443173 0.808537183
EGADS : 64 Yes 94.7284993 41.7493571 0
EGADS : 65 Yes 79.4370049 29.3018771 0
EGADS : 66 Yes 70.524066 29.3018771 0
EGADS : 67 Yes 139.227902 0 7.07099122
EGADS : 68 Yes 165.02399 0 13.6055284
EGADS : 69 Yes 173.282633 0 13.6055284
EGADS : 70 Yes 172.805054 0 13.3315303
EGADS : 71 Yes 168.687412 0 13.033327
EGADS : 72 Yes 153.156875 0 6.71984855
EGADS : 73 Yes 162.492237 0 7.4148274
EGADS : 74 Yes 153.156875 0 8.10980625
EGADS : 75 Yes 168.687412 0 13.6297335
EGADS : 76 Yes 118.391317 0 3.99272703
EGADS : 77 Yes 123.552357 0 4.7180639
EGADS : 78 Yes 122.843146 0 4.52165604
EGADS : 79 Yes 121.153699 0 4.20550678
EGADS : 80 Yes 107.581644 0 0.865881946
EGADS : 81 Yes 111.248847 0 1.31074802
EGADS : 82 Yes 111.050367 0 1.25578139
EGADS : 83 Yes 107.349293 0 0.808537183
EGADS : 84 Yes 94.7284993 0 0
EGADS : 85 Yes 100.269362 0 0
EGADS : 86 Yes 70.524066 0 0
EGADS : 87 Yes 79.4370049 0 0
EGADS : 88 Yes 94.7284993 0 0
EGADS : 89 Yes 107.349293 0 1.84589548
EGADS : 90 Yes 107.581644 0 1.89111513
EGADS : 91 Yes 121.153699 0 4.50848923
EGADS : 92 Yes 160.542569 0 11.9206428
EGADS : 93 Yes 151.486032 0.673415422 11.9206428
EGADS : 94 Yes 165.862466 0.235428105 34.9229244
EGADS : 95 Yes 169.168425 0 34.9229244
EGADS : 96 Yes 169.38016 0 35.487551
EGADS : 97 Yes 162.942213 0 35.487551
EGADS : 98 Yes 90.5173952 29.3018771 0
EGADS : 99 Yes 60.5173952 29.3018771 0
EGADS : 100 Yes 60.5173952 29.3018771 0
EGADS : 101 Yes 90.5173952 29.3018771 0
EGADS : 102 Yes 165.862466 0 34.9229244
EGADS : 103 Yes 151.486032 0 11.9206428
EGADS : 104 Yes 90.5173952 0 0
EGADS : 105 Yes 60.5173952 0 0
EGADS : 106 Yes 60.5173952 0 0
EGADS : 107 Yes 90.5173952 0 0
EGADS : 108 Yes 111.321903 0 1.86654259
EGADS : 109 Yes 108.055298 0 0.93793256
EGADS : 110 Yes 121.33061 0 4.22828065
EGADS : 111 Yes 122.700876 0 4.71377572
EGADS : 112 Yes 107.907885 0 1.87632098
EGADS : 113 Yes 121.289329 0 4.49106118
EGADS : 114 Yes 100.394138 0 0
EGADS : 115 Yes 95.1284577 0 0
EGADS : 116 Yes 107.505559 0 0.813039939
EGADS : 117 Yes 110.968457 0 0.689237814
EGADS : 118 Yes 95.3800953 0 0
EGADS : 119 Yes 107.657908 0 1.77558767
EGADS : 120 Yes 97.2857328 0 0
EGADS : 121 Yes 93.6847537 0 0
EGADS : 122 Yes 94.0587466 0 0
EGADS : 123 Yes 97.7824572 0 0
EGADS : 124 Yes 93.9345512 0 0
EGADS : 125 Yes 94.3601422 0 0
EGADS : 126 Yes 97.2857328 13.7821489 0
EGADS : 127 Yes 97.7824572 32.3393376 0
EGADS : 128 Yes 94.3601422 32.2302343 0
EGADS : 129 Yes 93.9345512 13.6726922 0
EGADS : 130 Yes 93.6847537 13.6742093 0
EGADS : 131 Yes 94.0587466 32.2320648 0
EGADS : 132 Yes 100.394138 42.0879216 0
EGADS : 133 Yes 110.968457 67.4483237 0.689237814
EGADS : 134 Yes 107.657908 67.3218336 1.77558767
EGADS : 135 Yes 95.3800953 41.8796344 0
EGADS : 136 Yes 95.1284577 41.9993571 0
EGADS : 137 Yes 107.505559 67.3943173 0.813039939
EGADS : 138 Yes 121.330781 95.7095395 4.49106118
EGADS : 139 Yes 122.742253 95.7419985 4.26970731
EGADS : 140 Yes 108.055908 68.3356022 1.87632098
EGADS : 141 Yes 111.300912 68.4526045 0.818951249
EGADS : 142 Yes 121.289158 95.7293907 4.22828065
EGADS : 143 Yes 107.907275 68.4064908 0.93793256
EGADS : 144 Yes 162.652062 0 6.87525931
EGADS : 145 Yes 172.609142 0 12.9541609
EGADS : 146 Yes 153.959016 0 6.86654493
EGADS : 147 Yes 168.960275 0 12.950503
EGADS : 148 Yes 169.001731 0 13.500001
EGADS : 149 Yes 154.05778 0 8.17566644
EGADS : 150 Yes 162.652062 7.30770007 6.87525931
EGADS : 151 Yes 172.609142 34.0557129 12.9541609
EGADS : 152 Yes 169.001731 33.980789 13.500001
EGADS : 153 Yes 154.05778 7.12920153 8.17566644
EGADS : 154 Yes 153.959016 7.18327767 6.86654493
EGADS : 155 Yes 168.960275 34.0034872 12.950503
EGADS : 156 Yes 160.730069 0 12.4206428
EGADS : 157 Yes 168.980925 0 34.4229244
EGADS : 158 Yes 166.139589 0.215327731 34.4229244
EGADS : 159 Yes 152.388156 0.632183325 12.4206428
EGADS : 160 Yes 152.388156 0 12.4206428
EGADS : 161 Yes 166.139589 0 34.4229244
EGADS : 162 Yes 0 0 1962.43554
EGADS : 163 Yes 0 0 0
EGADS : 164 Yes 0 1953.45847 1962.43554
EGADS : 165 Yes 0 1953.45847 0
EGADS : 166 Yes 2040.09979 0 1962.43554
EGADS : 167 Yes 2040.09979 0 0
EGADS : 168 Yes 2040.09979 1953.45847 1962.43554
EGADS : 169 Yes 2040.09979 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 53.021
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 3181.81
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 6
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : 23 CAD geometry 0 STD w/BL
AFLR4 : 24 CAD geometry 0 STD w/BL
AFLR4 : 25 CAD geometry 0 STD w/BL
AFLR4 : 26 CAD geometry 0 STD w/BL
AFLR4 : 27 CAD geometry 0 STD w/BL
AFLR4 : 28 CAD geometry 0 STD w/BL
AFLR4 : 29 CAD geometry 0 STD w/BL
AFLR4 : 30 CAD geometry 0 STD w/BL
AFLR4 : 31 CAD geometry 0 STD w/BL
AFLR4 : 32 CAD geometry 0 STD w/BL
AFLR4 : 33 CAD geometry 0 STD w/BL
AFLR4 : 34 CAD geometry 0 STD w/BL
AFLR4 : 35 CAD geometry 0 STD w/BL
AFLR4 : 36 CAD geometry 0 STD w/BL
AFLR4 : 37 CAD geometry 0 STD w/BL
AFLR4 : 38 CAD geometry 0 STD w/BL
AFLR4 : 39 CAD geometry 0 STD w/BL
AFLR4 : 40 CAD geometry 0 STD w/BL
AFLR4 : 41 CAD geometry 0 STD w/BL
AFLR4 : 42 CAD geometry 0 STD w/BL
AFLR4 : 43 CAD geometry 0 STD w/BL
AFLR4 : 44 CAD geometry 0 STD w/BL
AFLR4 : 45 CAD geometry 0 STD w/BL
AFLR4 : 46 CAD geometry 0 STD w/BL
AFLR4 : 47 CAD geometry 0 STD w/BL
AFLR4 : 48 CAD geometry 0 STD w/BL
AFLR4 : 49 CAD geometry 0 STD w/BL
AFLR4 : 50 CAD geometry 0 STD w/BL
AFLR4 : 51 CAD geometry 0 STD w/BL
AFLR4 : 52 CAD geometry 0 STD w/BL
AFLR4 : 53 CAD geometry 0 STD w/BL
AFLR4 : 54 CAD geometry 0 STD w/BL
AFLR4 : 55 CAD geometry 0 STD w/BL
AFLR4 : 56 CAD geometry 0 STD w/BL
AFLR4 : 57 CAD geometry 0 STD w/BL
AFLR4 : 58 CAD geometry 0 STD w/BL
AFLR4 : 59 CAD geometry 0 STD w/BL
AFLR4 : 60 CAD geometry 0 STD w/BL
AFLR4 : 61 CAD geometry 0 STD w/BL
AFLR4 : 62 CAD geometry 0 STD w/BL
AFLR4 : 63 CAD geometry 0 STD w/BL
AFLR4 : 64 CAD geometry 0 STD w/BL
AFLR4 : 65 CAD geometry 0 STD w/BL
AFLR4 : 66 CAD geometry 0 STD w/BL
AFLR4 : 67 CAD geometry 0 STD w/BL
AFLR4 : 68 CAD geometry 0 STD w/BL
AFLR4 : 69 CAD geometry 0 STD w/BL
AFLR4 : 70 CAD geometry 0 STD w/BL
AFLR4 : 71 CAD geometry 0 STD w/BL
AFLR4 : 72 CAD geometry 0 STD w/BL
AFLR4 : 73 CAD geometry 0 STD w/BL
AFLR4 : 74 CAD geometry 0 STD w/BL
AFLR4 : 75 CAD geometry 0 STD w/BL
AFLR4 : 76 CAD geometry 0 STD w/BL
AFLR4 : 77 CAD geometry 0 STD w/BL
AFLR4 : 78 CAD geometry 0 STD w/BL
AFLR4 : 79 CAD geometry 0 STD w/BL
AFLR4 : 80 CAD geometry 0 STD w/BL
AFLR4 : 81 CAD geometry 0 STD w/BL
AFLR4 : 82 CAD geometry 0 STD w/BL
AFLR4 : 83 CAD geometry 0 STD w/BL
AFLR4 : 84 CAD geometry 0 STD w/BL
AFLR4 : 85 CAD geometry 0 STD w/BL
AFLR4 : 86 CAD geometry 0 STD w/BL
AFLR4 : 87 CAD geometry 0 STD w/BL
AFLR4 : 88 CAD geometry 0 STD w/BL
AFLR4 : 89 CAD geometry 0 STD w/BL
AFLR4 : 90 CAD geometry 0 STD w/BL
AFLR4 : 91 CAD geometry 0 STD w/BL
AFLR4 : 92 CAD geometry 0 STD w/BL
AFLR4 : 93 CAD geometry 0 STD w/BL
AFLR4 : 94 CAD geometry 0 STD w/BL
AFLR4 : 95 CAD geometry 0 STD w/BL
AFLR4 : 96 CAD geometry 0 STD w/BL
AFLR4 : 97 CAD geometry 0 STD w/BL
AFLR4 : 98 CAD geometry 0 STD w/BL
AFLR4 : 99 CAD geometry 0 STD w/BL
AFLR4 : 100 CAD geometry 0 STD w/BL
AFLR4 : 101 CAD geometry 0 STD w/BL
AFLR4 : 102 CAD geometry 0 STD w/BL
AFLR4 : 103 CAD geometry 0 STD w/BL
AFLR4 : 104 CAD geometry 0 STD w/BL
AFLR4 : 105 CAD geometry 0 STD w/BL
AFLR4 : 106 CAD geometry 0 STD w/BL
AFLR4 : 107 CAD geometry 0 STD w/BL
AFLR4 : 108 CAD geometry 0 STD w/BL
AFLR4 : 109 CAD geometry 0 STD w/BL
AFLR4 : 110 CAD geometry 0 STD w/BL
AFLR4 : 111 CAD geometry 0 STD w/BL
AFLR4 : 112 CAD geometry 0 STD w/BL
AFLR4 : 113 CAD geometry 0 FARFIELD
AFLR4 : 114 CAD geometry 0 FARFIELD
AFLR4 : 115 CAD geometry 0 FARFIELD
AFLR4 : 116 CAD geometry 0 FARFIELD
AFLR4 : 117 CAD geometry 0 FARFIELD
AFLR4 : 118 CAD geometry 0 FARFIELD
AFLR4 : Case has 10 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 7 8 11 12 22
AFLR4 : Component 2 includes Definitions 5 6 9 10 15 16 17 18 19 25 26 27 28
AFLR4 : 31 37 38 39 40 41 42 43 51 52 53 54
AFLR4 : 55 56 57 68 69 70 71 72 73 77 78 82
AFLR4 : 83 84 88 89 93 97
AFLR4 : Component 3 includes Definitions 13 14 23 24 33 34 35 36 47 48 49 50
AFLR4 : 74 75 76 98 99 103 104
AFLR4 : Component 4 includes Definitions 32 46 60 61 62 63 79 80 81 108 109
AFLR4 : Component 5 includes Definitions 44 45 58 59 64 65 66 67 85 86 87
AFLR4 : Component 6 includes Definitions 20 21 29 30 90 91 92
AFLR4 : Component 7 includes Definitions 94 95 96
AFLR4 : Component 8 includes Definitions 100 101 102
AFLR4 : Component 9 includes Definitions 105 106 107
AFLR4 : Component 10 includes Definitions 110 111 112
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR4 : Define CAD surface definition 25
AFLR4 : Define CAD surface definition 26
AFLR4 : Define CAD surface definition 27
AFLR4 : Define CAD surface definition 28
AFLR4 : Define CAD surface definition 29
AFLR4 : Define CAD surface definition 30
AFLR4 : Define CAD surface definition 31
AFLR4 : Define CAD surface definition 32
AFLR4 : Define CAD surface definition 33
AFLR4 : Define CAD surface definition 34
AFLR4 : Define CAD surface definition 35
AFLR4 : Define CAD surface definition 36
AFLR4 : Define CAD surface definition 37
AFLR4 : Define CAD surface definition 38
AFLR4 : Define CAD surface definition 39
AFLR4 : Define CAD surface definition 40
AFLR4 : Define CAD surface definition 41
AFLR4 : Define CAD surface definition 42
AFLR4 : Define CAD surface definition 43
AFLR4 : Define CAD surface definition 44
AFLR4 : Define CAD surface definition 45
AFLR4 : Define CAD surface definition 46
AFLR4 : Define CAD surface definition 47
AFLR4 : Define CAD surface definition 48
AFLR4 : Define CAD surface definition 49
AFLR4 : Define CAD surface definition 50
AFLR4 : Define CAD surface definition 51
AFLR4 : Define CAD surface definition 52
AFLR4 : Define CAD surface definition 53
AFLR4 : Define CAD surface definition 54
AFLR4 : Define CAD surface definition 55
AFLR4 : Define CAD surface definition 56
AFLR4 : Define CAD surface definition 57
AFLR4 : Define CAD surface definition 58
AFLR4 : Define CAD surface definition 59
AFLR4 : Define CAD surface definition 60
AFLR4 : Define CAD surface definition 61
AFLR4 : Define CAD surface definition 62
AFLR4 : Define CAD surface definition 63
AFLR4 : Define CAD surface definition 64
AFLR4 : Define CAD surface definition 65
AFLR4 : Define CAD surface definition 66
AFLR4 : Define CAD surface definition 67
AFLR4 : Define CAD surface definition 68
AFLR4 : Define CAD surface definition 69
AFLR4 : Define CAD surface definition 70
AFLR4 : Define CAD surface definition 71
AFLR4 : Define CAD surface definition 72
AFLR4 : Define CAD surface definition 73
AFLR4 : Define CAD surface definition 74
AFLR4 : Define CAD surface definition 75
AFLR4 : Define CAD surface definition 76
AFLR4 : Define CAD surface definition 77
AFLR4 : Define CAD surface definition 78
AFLR4 : Define CAD surface definition 79
AFLR4 : Define CAD surface definition 80
AFLR4 : Define CAD surface definition 81
AFLR4 : Define CAD surface definition 82
AFLR4 : Define CAD surface definition 83
AFLR4 : Define CAD surface definition 84
AFLR4 : Define CAD surface definition 85
AFLR4 : Define CAD surface definition 86
AFLR4 : Define CAD surface definition 87
AFLR4 : Define CAD surface definition 88
AFLR4 : Define CAD surface definition 89
AFLR4 : Define CAD surface definition 90
AFLR4 : Define CAD surface definition 91
AFLR4 : Define CAD surface definition 92
AFLR4 : Define CAD surface definition 93
AFLR4 : Define CAD surface definition 94
AFLR4 : Define CAD surface definition 95
AFLR4 : Define CAD surface definition 96
AFLR4 : Define CAD surface definition 97
AFLR4 : Define CAD surface definition 98
AFLR4 : Define CAD surface definition 99
AFLR4 : Define CAD surface definition 100
AFLR4 : Define CAD surface definition 101
AFLR4 : Define CAD surface definition 102
AFLR4 : Define CAD surface definition 103
AFLR4 : Define CAD surface definition 104
AFLR4 : Define CAD surface definition 105
AFLR4 : Define CAD surface definition 106
AFLR4 : Define CAD surface definition 107
AFLR4 : Define CAD surface definition 108
AFLR4 : Define CAD surface definition 109
AFLR4 : Define CAD surface definition 110
AFLR4 : Define CAD surface definition 111
AFLR4 : Define CAD surface definition 112
AFLR4 : Define CAD surface definition 113
AFLR4 : Define CAD surface definition 114
AFLR4 : Define CAD surface definition 115
AFLR4 : Define CAD surface definition 116
AFLR4 : Define CAD surface definition 117
AFLR4 : Define CAD surface definition 118
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 201 301 0
AFLR4 : Nodes, Trias,Quads= 184 267 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 201 301 0
AFLR4 : Nodes, Trias,Quads= 183 265 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 148 243 0
AFLR4 : Nodes, Trias,Quads= 92 131 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 125 184 0
AFLR4 : Nodes, Trias,Quads= 134 202 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 730 1326 0
AFLR4 : Nodes, Trias,Quads= 627 1120 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 868 1583 0
AFLR4 : Nodes, Trias,Quads= 655 1157 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 125 184 0
AFLR4 : Nodes, Trias,Quads= 133 200 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 148 243 0
AFLR4 : Nodes, Trias,Quads= 91 129 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 860 1567 0
AFLR4 : Nodes, Trias,Quads= 651 1149 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 728 1322 0
AFLR4 : Nodes, Trias,Quads= 631 1128 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 17 20 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 334 576 0
AFLR4 : Nodes, Trias,Quads= 211 330 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 851 1557 0
AFLR4 : Nodes, Trias,Quads= 537 929 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 833 1521 0
AFLR4 : Nodes, Trias,Quads= 543 941 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 22 28 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 67 88 0
AFLR4 : Nodes, Trias,Quads= 46 46 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 1997 3751 0
AFLR4 : Nodes, Trias,Quads= 1162 2081 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 2014 3782 0
AFLR4 : Nodes, Trias,Quads= 1149 2052 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 51 73 0
AFLR4 : Nodes, Trias,Quads= 44 59 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 48 68 0
AFLR4 : Nodes, Trias,Quads= 43 58 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 355 618 0
AFLR4 : Nodes, Trias,Quads= 213 334 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 820 1495 0
AFLR4 : Nodes, Trias,Quads= 540 935 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 861 1577 0
AFLR4 : Nodes, Trias,Quads= 543 941 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 2005 3764 0
AFLR4 : Nodes, Trias,Quads= 1146 2046 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 66 86 0
AFLR4 : Nodes, Trias,Quads= 46 46 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 22 28 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 47 66 0
AFLR4 : Nodes, Trias,Quads= 43 58 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 49 69 0
AFLR4 : Nodes, Trias,Quads= 44 59 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 1993 3743 0
AFLR4 : Nodes, Trias,Quads= 1177 2111 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 728 1310 0
AFLR4 : Nodes, Trias,Quads= 449 752 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 21 20 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 100 132 0
AFLR4 : Nodes, Trias,Quads= 67 66 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 29 36 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 79 105 0
AFLR4 : Nodes, Trias,Quads= 54 55 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 35 47 0
AFLR4 : Nodes, Trias,Quads= 24 25 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 35 47 0
AFLR4 : Nodes, Trias,Quads= 24 25 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 121 160 0
AFLR4 : Nodes, Trias,Quads= 83 84 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 17 20 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 361 650 0
AFLR4 : Nodes, Trias,Quads= 381 690 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 363 654 0
AFLR4 : Nodes, Trias,Quads= 378 684 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 725 1304 0
AFLR4 : Nodes, Trias,Quads= 446 746 0
AFLR4 : Generate optimal mesh on surface definition 47
AFLR2 : Nodes, Trias,Quads= 29 36 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 48
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 49
AFLR2 : Nodes, Trias,Quads= 100 132 0
AFLR4 : Nodes, Trias,Quads= 67 66 0
AFLR4 : Generate optimal mesh on surface definition 50
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 21 20 0
AFLR4 : Generate optimal mesh on surface definition 51
AFLR2 : Nodes, Trias,Quads= 17 20 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 52
AFLR2 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 53
AFLR2 : Nodes, Trias,Quads= 121 160 0
AFLR4 : Nodes, Trias,Quads= 83 84 0
AFLR4 : Generate optimal mesh on surface definition 54
AFLR2 : Nodes, Trias,Quads= 35 47 0
AFLR4 : Nodes, Trias,Quads= 24 25 0
AFLR4 : Generate optimal mesh on surface definition 55
AFLR2 : Nodes, Trias,Quads= 35 47 0
AFLR4 : Nodes, Trias,Quads= 24 25 0
AFLR4 : Generate optimal mesh on surface definition 56
AFLR2 : Nodes, Trias,Quads= 79 105 0
AFLR4 : Nodes, Trias,Quads= 54 55 0
AFLR4 : Generate optimal mesh on surface definition 57
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 58
AFLR2 : Nodes, Trias,Quads= 360 648 0
AFLR4 : Nodes, Trias,Quads= 380 688 0
AFLR4 : Generate optimal mesh on surface definition 59
AFLR2 : Nodes, Trias,Quads= 360 648 0
AFLR4 : Nodes, Trias,Quads= 379 686 0
AFLR4 : Generate optimal mesh on surface definition 60
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 61
AFLR2 : Nodes, Trias,Quads= 97 128 0
AFLR4 : Nodes, Trias,Quads= 65 64 0
AFLR4 : Generate optimal mesh on surface definition 62
AFLR2 : Nodes, Trias,Quads= 42 54 0
AFLR4 : Nodes, Trias,Quads= 32 34 0
AFLR4 : Generate optimal mesh on surface definition 63
AFLR2 : Nodes, Trias,Quads= 35 44 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 64
AFLR2 : Nodes, Trias,Quads= 235 406 0
AFLR4 : Nodes, Trias,Quads= 211 358 0
AFLR4 : Generate optimal mesh on surface definition 65
AFLR2 : Nodes, Trias,Quads= 235 406 0
AFLR4 : Nodes, Trias,Quads= 211 358 0
AFLR4 : Generate optimal mesh on surface definition 66
AFLR2 : Nodes, Trias,Quads= 235 406 0
AFLR4 : Nodes, Trias,Quads= 211 358 0
AFLR4 : Generate optimal mesh on surface definition 67
AFLR2 : Nodes, Trias,Quads= 235 406 0
AFLR4 : Nodes, Trias,Quads= 211 358 0
AFLR4 : Generate optimal mesh on surface definition 68
AFLR2 : Nodes, Trias,Quads= 206 330 0
AFLR4 : Nodes, Trias,Quads= 151 220 0
AFLR4 : Generate optimal mesh on surface definition 69
AFLR2 : Nodes, Trias,Quads= 22 29 0
AFLR4 : Nodes, Trias,Quads= 13 11 0
AFLR4 : Generate optimal mesh on surface definition 70
AFLR2 : Nodes, Trias,Quads= 127 168 0
AFLR4 : Nodes, Trias,Quads= 87 88 0
AFLR4 : Generate optimal mesh on surface definition 71
AFLR2 : Nodes, Trias,Quads= 25 32 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 72
AFLR2 : Nodes, Trias,Quads= 208 333 0
AFLR4 : Nodes, Trias,Quads= 157 231 0
AFLR4 : Generate optimal mesh on surface definition 73
AFLR2 : Nodes, Trias,Quads= 119 185 0
AFLR4 : Nodes, Trias,Quads= 98 143 0
AFLR4 : Generate optimal mesh on surface definition 74
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 75
AFLR2 : Nodes, Trias,Quads= 79 104 0
AFLR4 : Nodes, Trias,Quads= 55 56 0
AFLR4 : Generate optimal mesh on surface definition 76
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 77
AFLR2 : Nodes, Trias,Quads= 119 185 0
AFLR4 : Nodes, Trias,Quads= 100 147 0
AFLR4 : Generate optimal mesh on surface definition 78
AFLR2 : Nodes, Trias,Quads= 106 165 0
AFLR4 : Nodes, Trias,Quads= 97 147 0
AFLR4 : Generate optimal mesh on surface definition 79
AFLR2 : Nodes, Trias,Quads= 22 28 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 80
AFLR2 : Nodes, Trias,Quads= 68 89 0
AFLR4 : Nodes, Trias,Quads= 47 47 0
AFLR4 : Generate optimal mesh on surface definition 81
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 82
AFLR2 : Nodes, Trias,Quads= 111 174 0
AFLR4 : Nodes, Trias,Quads= 103 158 0
AFLR4 : Generate optimal mesh on surface definition 83
AFLR2 : Nodes, Trias,Quads= 110 172 0
AFLR4 : Nodes, Trias,Quads= 103 158 0
AFLR4 : Generate optimal mesh on surface definition 84
AFLR2 : Nodes, Trias,Quads= 106 165 0
AFLR4 : Nodes, Trias,Quads= 97 147 0
AFLR4 : Generate optimal mesh on surface definition 85
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 86
AFLR2 : Nodes, Trias,Quads= 69 91 0
AFLR4 : Nodes, Trias,Quads= 47 47 0
AFLR4 : Generate optimal mesh on surface definition 87
AFLR2 : Nodes, Trias,Quads= 22 28 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 88
AFLR2 : Nodes, Trias,Quads= 119 185 0
AFLR4 : Nodes, Trias,Quads= 100 147 0
AFLR4 : Generate optimal mesh on surface definition 89
AFLR2 : Nodes, Trias,Quads= 120 187 0
AFLR4 : Nodes, Trias,Quads= 98 143 0
AFLR4 : Generate optimal mesh on surface definition 90
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 91
AFLR2 : Nodes, Trias,Quads= 79 104 0
AFLR4 : Nodes, Trias,Quads= 55 56 0
AFLR4 : Generate optimal mesh on surface definition 92
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 93
AFLR2 : Nodes, Trias,Quads= 207 331 0
AFLR4 : Nodes, Trias,Quads= 155 227 0
AFLR4 : Generate optimal mesh on surface definition 94
AFLR2 : Nodes, Trias,Quads= 25 32 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 95
AFLR2 : Nodes, Trias,Quads= 127 168 0
AFLR4 : Nodes, Trias,Quads= 87 88 0
AFLR4 : Generate optimal mesh on surface definition 96
AFLR2 : Nodes, Trias,Quads= 22 29 0
AFLR4 : Nodes, Trias,Quads= 13 11 0
AFLR4 : Generate optimal mesh on surface definition 97
AFLR2 : Nodes, Trias,Quads= 207 332 0
AFLR4 : Nodes, Trias,Quads= 152 222 0
AFLR4 : Generate optimal mesh on surface definition 98
AFLR2 : Nodes, Trias,Quads= 229 388 0
AFLR4 : Nodes, Trias,Quads= 171 272 0
AFLR4 : Generate optimal mesh on surface definition 99
AFLR2 : Nodes, Trias,Quads= 227 384 0
AFLR4 : Nodes, Trias,Quads= 172 274 0
AFLR4 : Generate optimal mesh on surface definition 100
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 21 20 0
AFLR4 : Generate optimal mesh on surface definition 101
AFLR2 : Nodes, Trias,Quads= 100 132 0
AFLR4 : Nodes, Trias,Quads= 67 66 0
AFLR4 : Generate optimal mesh on surface definition 102
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 21 20 0
AFLR4 : Generate optimal mesh on surface definition 103
AFLR2 : Nodes, Trias,Quads= 225 380 0
AFLR4 : Nodes, Trias,Quads= 172 274 0
AFLR4 : Generate optimal mesh on surface definition 104
AFLR2 : Nodes, Trias,Quads= 228 386 0
AFLR4 : Nodes, Trias,Quads= 172 274 0
AFLR4 : Generate optimal mesh on surface definition 105
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 21 20 0
AFLR4 : Generate optimal mesh on surface definition 106
AFLR2 : Nodes, Trias,Quads= 100 132 0
AFLR4 : Nodes, Trias,Quads= 67 66 0
AFLR4 : Generate optimal mesh on surface definition 107
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 21 20 0
AFLR4 : Generate optimal mesh on surface definition 108
AFLR2 : Nodes, Trias,Quads= 244 418 0
AFLR4 : Nodes, Trias,Quads= 180 290 0
AFLR4 : Generate optimal mesh on surface definition 109
AFLR2 : Nodes, Trias,Quads= 245 420 0
AFLR4 : Nodes, Trias,Quads= 180 290 0
AFLR4 : Generate optimal mesh on surface definition 110
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 21 20 0
AFLR4 : Generate optimal mesh on surface definition 111
AFLR2 : Nodes, Trias,Quads= 100 132 0
AFLR4 : Nodes, Trias,Quads= 67 66 0
AFLR4 : Generate optimal mesh on surface definition 112
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 21 20 0
AFLR4 : Generate optimal mesh on surface definition 113
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 114
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 115
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 116
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 117
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 118
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 14992 29948 6594
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 14992 29948
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 221 333 0
AFLR4 : Nodes, Trias,Quads= 306 503 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 217 326 0
AFLR4 : Nodes, Trias,Quads= 291 474 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 193 323 0
AFLR4 : Nodes, Trias,Quads= 128 193 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 149 226 0
AFLR4 : Nodes, Trias,Quads= 165 258 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 764 1394 0
AFLR4 : Nodes, Trias,Quads= 758 1382 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 882 1611 0
AFLR4 : Nodes, Trias,Quads= 823 1493 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 150 228 0
AFLR4 : Nodes, Trias,Quads= 161 250 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 192 321 0
AFLR4 : Nodes, Trias,Quads= 124 185 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 855 1559 0
AFLR4 : Nodes, Trias,Quads= 812 1473 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 764 1395 0
AFLR4 : Nodes, Trias,Quads= 760 1387 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 14 14 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 399 695 0
AFLR4 : Nodes, Trias,Quads= 325 547 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 873 1599 0
AFLR4 : Nodes, Trias,Quads= 615 1083 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 858 1570 0
AFLR4 : Nodes, Trias,Quads= 606 1066 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 62 80 0
AFLR4 : Nodes, Trias,Quads= 42 40 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 2052 3855 0
AFLR4 : Nodes, Trias,Quads= 1330 2411 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 2043 3837 0
AFLR4 : Nodes, Trias,Quads= 1290 2331 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 75 115 0
AFLR4 : Nodes, Trias,Quads= 52 69 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 70 106 0
AFLR4 : Nodes, Trias,Quads= 50 66 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 433 763 0
AFLR4 : Nodes, Trias,Quads= 326 549 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 851 1556 0
AFLR4 : Nodes, Trias,Quads= 602 1058 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 880 1613 0
AFLR4 : Nodes, Trias,Quads= 627 1107 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 2033 3817 0
AFLR4 : Nodes, Trias,Quads= 1281 2313 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 61 79 0
AFLR4 : Nodes, Trias,Quads= 41 39 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 20 25 0
AFLR4 : Nodes, Trias,Quads= 13 11 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 64 96 0
AFLR4 : Nodes, Trias,Quads= 47 62 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 66 99 0
AFLR4 : Nodes, Trias,Quads= 49 65 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 2044 3840 0
AFLR4 : Nodes, Trias,Quads= 1321 2394 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 749 1351 0
AFLR4 : Nodes, Trias,Quads= 492 837 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 102 137 0
AFLR4 : Nodes, Trias,Quads= 65 63 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 28 36 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 79 105 0
AFLR4 : Nodes, Trias,Quads= 52 51 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 25 26 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 25 26 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 133 181 0
AFLR4 : Nodes, Trias,Quads= 84 83 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 25 32 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 490 896 0
AFLR4 : Nodes, Trias,Quads= 448 812 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 486 888 0
AFLR4 : Nodes, Trias,Quads= 442 800 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 739 1330 0
AFLR4 : Nodes, Trias,Quads= 479 810 0
AFLR4 : Generate optimal mesh on surface definition 47
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 48
AFLR2 : Nodes, Trias,Quads= 27 34 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 49
AFLR2 : Nodes, Trias,Quads= 97 127 0
AFLR4 : Nodes, Trias,Quads= 65 63 0
AFLR4 : Generate optimal mesh on surface definition 50
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 51
AFLR2 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 52
AFLR2 : Nodes, Trias,Quads= 23 29 0
AFLR4 : Nodes, Trias,Quads= 15 13 0
AFLR4 : Generate optimal mesh on surface definition 53
AFLR2 : Nodes, Trias,Quads= 133 183 0
AFLR4 : Nodes, Trias,Quads= 82 81 0
AFLR4 : Generate optimal mesh on surface definition 54
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 25 26 0
AFLR4 : Generate optimal mesh on surface definition 55
AFLR2 : Nodes, Trias,Quads= 34 44 0
AFLR4 : Nodes, Trias,Quads= 25 26 0
AFLR4 : Generate optimal mesh on surface definition 56
AFLR2 : Nodes, Trias,Quads= 80 107 0
AFLR4 : Nodes, Trias,Quads= 53 53 0
AFLR4 : Generate optimal mesh on surface definition 57
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 58
AFLR2 : Nodes, Trias,Quads= 456 830 0
AFLR4 : Nodes, Trias,Quads= 432 782 0
AFLR4 : Generate optimal mesh on surface definition 59
AFLR2 : Nodes, Trias,Quads= 452 822 0
AFLR4 : Nodes, Trias,Quads= 419 756 0
AFLR4 : Generate optimal mesh on surface definition 60
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 61
AFLR2 : Nodes, Trias,Quads= 89 117 0
AFLR4 : Nodes, Trias,Quads= 59 57 0
AFLR4 : Generate optimal mesh on surface definition 62
AFLR2 : Nodes, Trias,Quads= 37 47 0
AFLR4 : Nodes, Trias,Quads= 28 29 0
AFLR4 : Generate optimal mesh on surface definition 63
AFLR2 : Nodes, Trias,Quads= 45 61 0
AFLR4 : Nodes, Trias,Quads= 27 25 0
AFLR4 : Generate optimal mesh on surface definition 64
AFLR2 : Nodes, Trias,Quads= 316 558 0
AFLR4 : Nodes, Trias,Quads= 274 474 0
AFLR4 : Generate optimal mesh on surface definition 65
AFLR2 : Nodes, Trias,Quads= 315 556 0
AFLR4 : Nodes, Trias,Quads= 275 476 0
AFLR4 : Generate optimal mesh on surface definition 66
AFLR2 : Nodes, Trias,Quads= 316 558 0
AFLR4 : Nodes, Trias,Quads= 274 474 0
AFLR4 : Generate optimal mesh on surface definition 67
AFLR2 : Nodes, Trias,Quads= 315 556 0
AFLR4 : Nodes, Trias,Quads= 275 476 0
AFLR4 : Generate optimal mesh on surface definition 68
AFLR2 : Nodes, Trias,Quads= 224 362 0
AFLR4 : Nodes, Trias,Quads= 175 264 0
AFLR4 : Generate optimal mesh on surface definition 69
AFLR2 : Nodes, Trias,Quads= 22 29 0
AFLR4 : Nodes, Trias,Quads= 13 11 0
AFLR4 : Generate optimal mesh on surface definition 70
AFLR2 : Nodes, Trias,Quads= 147 205 0
AFLR4 : Nodes, Trias,Quads= 88 87 0
AFLR4 : Generate optimal mesh on surface definition 71
AFLR2 : Nodes, Trias,Quads= 25 32 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 72
AFLR2 : Nodes, Trias,Quads= 234 380 0
AFLR4 : Nodes, Trias,Quads= 187 286 0
AFLR4 : Generate optimal mesh on surface definition 73
AFLR2 : Nodes, Trias,Quads= 122 191 0
AFLR4 : Nodes, Trias,Quads= 107 161 0
AFLR4 : Generate optimal mesh on surface definition 74
AFLR2 : Nodes, Trias,Quads= 19 24 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 75
AFLR2 : Nodes, Trias,Quads= 78 103 0
AFLR4 : Nodes, Trias,Quads= 52 51 0
AFLR4 : Generate optimal mesh on surface definition 76
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 77
AFLR2 : Nodes, Trias,Quads= 126 198 0
AFLR4 : Nodes, Trias,Quads= 112 170 0
AFLR4 : Generate optimal mesh on surface definition 78
AFLR2 : Nodes, Trias,Quads= 116 183 0
AFLR4 : Nodes, Trias,Quads= 109 169 0
AFLR4 : Generate optimal mesh on surface definition 79
AFLR2 : Nodes, Trias,Quads= 22 28 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 80
AFLR2 : Nodes, Trias,Quads= 68 90 0
AFLR4 : Nodes, Trias,Quads= 47 48 0
AFLR4 : Generate optimal mesh on surface definition 81
AFLR2 : Nodes, Trias,Quads= 19 24 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 82
AFLR2 : Nodes, Trias,Quads= 118 187 0
AFLR4 : Nodes, Trias,Quads= 111 173 0
AFLR4 : Generate optimal mesh on surface definition 83
AFLR2 : Nodes, Trias,Quads= 117 185 0
AFLR4 : Nodes, Trias,Quads= 111 173 0
AFLR4 : Generate optimal mesh on surface definition 84
AFLR2 : Nodes, Trias,Quads= 115 181 0
AFLR4 : Nodes, Trias,Quads= 109 169 0
AFLR4 : Generate optimal mesh on surface definition 85
AFLR2 : Nodes, Trias,Quads= 19 24 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 86
AFLR2 : Nodes, Trias,Quads= 68 90 0
AFLR4 : Nodes, Trias,Quads= 47 48 0
AFLR4 : Generate optimal mesh on surface definition 87
AFLR2 : Nodes, Trias,Quads= 22 28 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 88
AFLR2 : Nodes, Trias,Quads= 125 196 0
AFLR4 : Nodes, Trias,Quads= 111 168 0
AFLR4 : Generate optimal mesh on surface definition 89
AFLR2 : Nodes, Trias,Quads= 122 191 0
AFLR4 : Nodes, Trias,Quads= 107 161 0
AFLR4 : Generate optimal mesh on surface definition 90
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 91
AFLR2 : Nodes, Trias,Quads= 78 103 0
AFLR4 : Nodes, Trias,Quads= 52 51 0
AFLR4 : Generate optimal mesh on surface definition 92
AFLR2 : Nodes, Trias,Quads= 19 24 0
AFLR4 : Nodes, Trias,Quads= 12 10 0
AFLR4 : Generate optimal mesh on surface definition 93
AFLR2 : Nodes, Trias,Quads= 233 378 0
AFLR4 : Nodes, Trias,Quads= 187 286 0
AFLR4 : Generate optimal mesh on surface definition 94
AFLR2 : Nodes, Trias,Quads= 25 32 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 95
AFLR2 : Nodes, Trias,Quads= 148 207 0
AFLR4 : Nodes, Trias,Quads= 88 87 0
AFLR4 : Generate optimal mesh on surface definition 96
AFLR2 : Nodes, Trias,Quads= 22 29 0
AFLR4 : Nodes, Trias,Quads= 13 11 0
AFLR4 : Generate optimal mesh on surface definition 97
AFLR2 : Nodes, Trias,Quads= 229 372 0
AFLR4 : Nodes, Trias,Quads= 175 264 0
AFLR4 : Generate optimal mesh on surface definition 98
AFLR2 : Nodes, Trias,Quads= 236 401 0
AFLR4 : Nodes, Trias,Quads= 200 329 0
AFLR4 : Generate optimal mesh on surface definition 99
AFLR2 : Nodes, Trias,Quads= 243 414 0
AFLR4 : Nodes, Trias,Quads= 204 336 0
AFLR4 : Generate optimal mesh on surface definition 100
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 101
AFLR2 : Nodes, Trias,Quads= 108 149 0
AFLR4 : Nodes, Trias,Quads= 66 65 0
AFLR4 : Generate optimal mesh on surface definition 102
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 103
AFLR2 : Nodes, Trias,Quads= 241 410 0
AFLR4 : Nodes, Trias,Quads= 204 336 0
AFLR4 : Generate optimal mesh on surface definition 104
AFLR2 : Nodes, Trias,Quads= 238 405 0
AFLR4 : Nodes, Trias,Quads= 201 331 0
AFLR4 : Generate optimal mesh on surface definition 105
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 106
AFLR2 : Nodes, Trias,Quads= 108 149 0
AFLR4 : Nodes, Trias,Quads= 66 65 0
AFLR4 : Generate optimal mesh on surface definition 107
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 108
AFLR2 : Nodes, Trias,Quads= 241 412 0
AFLR4 : Nodes, Trias,Quads= 200 330 0
AFLR4 : Generate optimal mesh on surface definition 109
AFLR2 : Nodes, Trias,Quads= 243 416 0
AFLR4 : Nodes, Trias,Quads= 202 334 0
AFLR4 : Generate optimal mesh on surface definition 110
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 111
AFLR2 : Nodes, Trias,Quads= 97 128 0
AFLR4 : Nodes, Trias,Quads= 64 62 0
AFLR4 : Generate optimal mesh on surface definition 112
AFLR2 : Nodes, Trias,Quads= 31 40 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 113
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 114
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 115
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 116
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 117
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 118
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 17838 35640 6838
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 19585 39134
AFLR4 : Nodes, Trias = 20717 41398
AFLR4 : Nodes, Trias = 21827 43618
AFLR4 : Nodes, Trias = 22762 45488
AFLR4 : Nodes, Trias = 23524 47012
AFLR4 : Nodes, Trias = 23924 47812
AFLR4 : Nodes, Trias = 24008 47980
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 799 1346 0
AFLR4 : Nodes, Trias,Quads= 1156 2060 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 696 1157 0
AFLR4 : Nodes, Trias,Quads= 935 1635 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 610 1103 0
AFLR4 : Nodes, Trias,Quads= 437 757 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 366 622 0
AFLR4 : Nodes, Trias,Quads= 483 856 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 2301 4380 0
AFLR4 : Nodes, Trias,Quads= 1586 2950 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 2447 4630 0
AFLR4 : Nodes, Trias,Quads= 2254 4244 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 364 618 0
AFLR4 : Nodes, Trias,Quads= 481 852 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 605 1093 0
AFLR4 : Nodes, Trias,Quads= 430 743 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1819 3421 0
AFLR4 : Nodes, Trias,Quads= 1634 3051 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 2023 3844 0
AFLR4 : Nodes, Trias,Quads= 1336 2470 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 18 22 0
AFLR4 : Nodes, Trias,Quads= 14 14 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 1422 2644 0
AFLR4 : Nodes, Trias,Quads= 870 1540 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1664 3096 0
AFLR4 : Nodes, Trias,Quads= 1398 2564 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1898 3542 0
AFLR4 : Nodes, Trias,Quads= 1705 3156 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 238 386 0
AFLR4 : Nodes, Trias,Quads= 284 478 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 21 27 0
AFLR4 : Nodes, Trias,Quads= 14 13 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 2433 4570 0
AFLR4 : Nodes, Trias,Quads= 1882 3468 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 2560 4813 0
AFLR4 : Nodes, Trias,Quads= 2080 3853 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 539 977 0
AFLR4 : Nodes, Trias,Quads= 320 539 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 463 833 0
AFLR4 : Nodes, Trias,Quads= 270 447 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 1538 2877 0
AFLR4 : Nodes, Trias,Quads= 860 1521 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 1881 3508 0
AFLR4 : Nodes, Trias,Quads= 1684 3114 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 1853 3463 0
AFLR4 : Nodes, Trias,Quads= 1608 2973 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 2397 4507 0
AFLR4 : Nodes, Trias,Quads= 1662 3037 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 21 27 0
AFLR4 : Nodes, Trias,Quads= 14 13 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 60 78 0
AFLR4 : Nodes, Trias,Quads= 41 40 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 20 25 0
AFLR4 : Nodes, Trias,Quads= 13 11 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 485 875 0
AFLR4 : Nodes, Trias,Quads= 288 481 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 514 928 0
AFLR4 : Nodes, Trias,Quads= 306 512 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 2168 4078 0
AFLR4 : Nodes, Trias,Quads= 1399 2540 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 1770 3290 0
AFLR4 : Nodes, Trias,Quads= 1381 2512 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 222 379 0
AFLR4 : Nodes, Trias,Quads= 332 599 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 266 407 0
AFLR4 : Nodes, Trias,Quads= 330 535 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 46 63 0
AFLR4 : Nodes, Trias,Quads= 31 33 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 37 48 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 20 25 0
AFLR4 : Nodes, Trias,Quads= 14 13 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 82 109 0
AFLR4 : Nodes, Trias,Quads= 65 75 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 73 108 0
AFLR4 : Nodes, Trias,Quads= 113 188 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 72 105 0
AFLR4 : Nodes, Trias,Quads= 112 185 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 309 473 0
AFLR4 : Nodes, Trias,Quads= 366 587 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 51 70 0
AFLR4 : Nodes, Trias,Quads= 47 62 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 27 34 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 1065 2004 0
AFLR4 : Nodes, Trias,Quads= 926 1726 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 965 1808 0
AFLR4 : Nodes, Trias,Quads= 885 1648 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 1738 3231 0
AFLR4 : Nodes, Trias,Quads= 1352 2459 0
AFLR4 : Generate optimal mesh on surface definition 47
AFLR2 : Nodes, Trias,Quads= 37 48 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 48
AFLR2 : Nodes, Trias,Quads= 46 63 0
AFLR4 : Nodes, Trias,Quads= 32 35 0
AFLR4 : Generate optimal mesh on surface definition 49
AFLR2 : Nodes, Trias,Quads= 374 609 0
AFLR4 : Nodes, Trias,Quads= 524 909 0
AFLR4 : Generate optimal mesh on surface definition 50
AFLR2 : Nodes, Trias,Quads= 187 313 0
AFLR4 : Nodes, Trias,Quads= 268 475 0
AFLR4 : Generate optimal mesh on surface definition 51
AFLR2 : Nodes, Trias,Quads= 26 32 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 52
AFLR2 : Nodes, Trias,Quads= 23 29 0
AFLR4 : Nodes, Trias,Quads= 15 13 0
AFLR4 : Generate optimal mesh on surface definition 53
AFLR2 : Nodes, Trias,Quads= 145 204 0
AFLR4 : Nodes, Trias,Quads= 85 84 0
AFLR4 : Generate optimal mesh on surface definition 54
AFLR2 : Nodes, Trias,Quads= 35 45 0
AFLR4 : Nodes, Trias,Quads= 26 27 0
AFLR4 : Generate optimal mesh on surface definition 55
AFLR2 : Nodes, Trias,Quads= 101 154 0
AFLR4 : Nodes, Trias,Quads= 138 228 0
AFLR4 : Generate optimal mesh on surface definition 56
AFLR2 : Nodes, Trias,Quads= 125 175 0
AFLR4 : Nodes, Trias,Quads= 131 187 0
AFLR4 : Generate optimal mesh on surface definition 57
AFLR2 : Nodes, Trias,Quads= 20 25 0
AFLR4 : Nodes, Trias,Quads= 14 13 0
AFLR4 : Generate optimal mesh on surface definition 58
AFLR2 : Nodes, Trias,Quads= 1009 1895 0
AFLR4 : Nodes, Trias,Quads= 903 1683 0
AFLR4 : Generate optimal mesh on surface definition 59
AFLR2 : Nodes, Trias,Quads= 1035 1945 0
AFLR4 : Nodes, Trias,Quads= 919 1713 0
AFLR4 : Generate optimal mesh on surface definition 60
AFLR2 : Nodes, Trias,Quads= 232 398 0
AFLR4 : Nodes, Trias,Quads= 358 650 0
AFLR4 : Generate optimal mesh on surface definition 61
AFLR2 : Nodes, Trias,Quads= 347 567 0
AFLR4 : Nodes, Trias,Quads= 474 821 0
AFLR4 : Generate optimal mesh on surface definition 62
AFLR2 : Nodes, Trias,Quads= 44 60 0
AFLR4 : Nodes, Trias,Quads= 30 32 0
AFLR4 : Generate optimal mesh on surface definition 63
AFLR2 : Nodes, Trias,Quads= 48 64 0
AFLR4 : Nodes, Trias,Quads= 30 28 0
AFLR4 : Generate optimal mesh on surface definition 64
AFLR2 : Nodes, Trias,Quads= 314 553 0
AFLR4 : Nodes, Trias,Quads= 288 501 0
AFLR4 : Generate optimal mesh on surface definition 65
AFLR2 : Nodes, Trias,Quads= 316 557 0
AFLR4 : Nodes, Trias,Quads= 296 517 0
AFLR4 : Generate optimal mesh on surface definition 66
AFLR2 : Nodes, Trias,Quads= 315 555 0
AFLR4 : Nodes, Trias,Quads= 286 497 0
AFLR4 : Generate optimal mesh on surface definition 67
AFLR2 : Nodes, Trias,Quads= 316 557 0
AFLR4 : Nodes, Trias,Quads= 297 519 0
AFLR4 : Generate optimal mesh on surface definition 68
AFLR2 : Nodes, Trias,Quads= 237 385 0
AFLR4 : Nodes, Trias,Quads= 183 277 0
AFLR4 : Generate optimal mesh on surface definition 69
AFLR2 : Nodes, Trias,Quads= 22 29 0
AFLR4 : Nodes, Trias,Quads= 13 11 0
AFLR4 : Generate optimal mesh on surface definition 70
AFLR2 : Nodes, Trias,Quads= 152 215 0
AFLR4 : Nodes, Trias,Quads= 87 85 0
AFLR4 : Generate optimal mesh on surface definition 71
AFLR2 : Nodes, Trias,Quads= 25 32 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 72
AFLR2 : Nodes, Trias,Quads= 252 413 0
AFLR4 : Nodes, Trias,Quads= 197 303 0
AFLR4 : Generate optimal mesh on surface definition 73
AFLR2 : Nodes, Trias,Quads= 728 1314 0
AFLR4 : Nodes, Trias,Quads= 730 1318 0
AFLR4 : Generate optimal mesh on surface definition 74
AFLR2 : Nodes, Trias,Quads= 112 179 0
AFLR4 : Nodes, Trias,Quads= 109 173 0
AFLR4 : Generate optimal mesh on surface definition 75
AFLR2 : Nodes, Trias,Quads= 678 1184 0
AFLR4 : Nodes, Trias,Quads= 654 1136 0
AFLR4 : Generate optimal mesh on surface definition 76
AFLR2 : Nodes, Trias,Quads= 380 680 0
AFLR4 : Nodes, Trias,Quads= 374 668 0
AFLR4 : Generate optimal mesh on surface definition 77
AFLR2 : Nodes, Trias,Quads= 722 1303 0
AFLR4 : Nodes, Trias,Quads= 733 1325 0
AFLR4 : Generate optimal mesh on surface definition 78
AFLR2 : Nodes, Trias,Quads= 259 441 0
AFLR4 : Nodes, Trias,Quads= 274 471 0
AFLR4 : Generate optimal mesh on surface definition 79
AFLR2 : Nodes, Trias,Quads= 25 32 0
AFLR4 : Nodes, Trias,Quads= 17 16 0
AFLR4 : Generate optimal mesh on surface definition 80
AFLR2 : Nodes, Trias,Quads= 175 268 0
AFLR4 : Nodes, Trias,Quads= 153 224 0
AFLR4 : Generate optimal mesh on surface definition 81
AFLR2 : Nodes, Trias,Quads= 90 140 0
AFLR4 : Nodes, Trias,Quads= 85 130 0
AFLR4 : Generate optimal mesh on surface definition 82
AFLR2 : Nodes, Trias,Quads= 264 451 0
AFLR4 : Nodes, Trias,Quads= 273 469 0
AFLR4 : Generate optimal mesh on surface definition 83
AFLR2 : Nodes, Trias,Quads= 557 997 0
AFLR4 : Nodes, Trias,Quads= 599 1081 0
AFLR4 : Generate optimal mesh on surface definition 84
AFLR2 : Nodes, Trias,Quads= 498 880 0
AFLR4 : Nodes, Trias,Quads= 589 1062 0
AFLR4 : Generate optimal mesh on surface definition 85
AFLR2 : Nodes, Trias,Quads= 89 138 0
AFLR4 : Nodes, Trias,Quads= 85 130 0
AFLR4 : Generate optimal mesh on surface definition 86
AFLR2 : Nodes, Trias,Quads= 508 870 0
AFLR4 : Nodes, Trias,Quads= 467 788 0
AFLR4 : Generate optimal mesh on surface definition 87
AFLR2 : Nodes, Trias,Quads= 104 163 0
AFLR4 : Nodes, Trias,Quads= 94 143 0
AFLR4 : Generate optimal mesh on surface definition 88
AFLR2 : Nodes, Trias,Quads= 716 1291 0
AFLR4 : Nodes, Trias,Quads= 728 1315 0
AFLR4 : Generate optimal mesh on surface definition 89
AFLR2 : Nodes, Trias,Quads= 742 1342 0
AFLR4 : Nodes, Trias,Quads= 735 1328 0
AFLR4 : Generate optimal mesh on surface definition 90
AFLR2 : Nodes, Trias,Quads= 377 674 0
AFLR4 : Nodes, Trias,Quads= 374 668 0
AFLR4 : Generate optimal mesh on surface definition 91
AFLR2 : Nodes, Trias,Quads= 679 1186 0
AFLR4 : Nodes, Trias,Quads= 653 1134 0
AFLR4 : Generate optimal mesh on surface definition 92
AFLR2 : Nodes, Trias,Quads= 114 183 0
AFLR4 : Nodes, Trias,Quads= 109 173 0
AFLR4 : Generate optimal mesh on surface definition 93
AFLR2 : Nodes, Trias,Quads= 804 1439 0
AFLR4 : Nodes, Trias,Quads= 683 1197 0
AFLR4 : Generate optimal mesh on surface definition 94
AFLR2 : Nodes, Trias,Quads= 68 98 0
AFLR4 : Nodes, Trias,Quads= 59 80 0
AFLR4 : Generate optimal mesh on surface definition 95
AFLR2 : Nodes, Trias,Quads= 689 1178 0
AFLR4 : Nodes, Trias,Quads= 600 1000 0
AFLR4 : Generate optimal mesh on surface definition 96
AFLR2 : Nodes, Trias,Quads= 348 619 0
AFLR4 : Nodes, Trias,Quads= 344 611 0
AFLR4 : Generate optimal mesh on surface definition 97
AFLR2 : Nodes, Trias,Quads= 736 1300 0
AFLR4 : Nodes, Trias,Quads= 694 1216 0
AFLR4 : Generate optimal mesh on surface definition 98
AFLR2 : Nodes, Trias,Quads= 1092 2013 0
AFLR4 : Nodes, Trias,Quads= 863 1555 0
AFLR4 : Generate optimal mesh on surface definition 99
AFLR2 : Nodes, Trias,Quads= 997 1831 0
AFLR4 : Nodes, Trias,Quads= 824 1485 0
AFLR4 : Generate optimal mesh on surface definition 100
AFLR2 : Nodes, Trias,Quads= 617 1124 0
AFLR4 : Nodes, Trias,Quads= 635 1160 0
AFLR4 : Generate optimal mesh on surface definition 101
AFLR2 : Nodes, Trias,Quads= 773 1355 0
AFLR4 : Nodes, Trias,Quads= 701 1211 0
AFLR4 : Generate optimal mesh on surface definition 102
AFLR2 : Nodes, Trias,Quads= 80 117 0
AFLR4 : Nodes, Trias,Quads= 69 95 0
AFLR4 : Generate optimal mesh on surface definition 103
AFLR2 : Nodes, Trias,Quads= 908 1659 0
AFLR4 : Nodes, Trias,Quads= 765 1373 0
AFLR4 : Generate optimal mesh on surface definition 104
AFLR2 : Nodes, Trias,Quads= 1055 1943 0
AFLR4 : Nodes, Trias,Quads= 827 1487 0
AFLR4 : Generate optimal mesh on surface definition 105
AFLR2 : Nodes, Trias,Quads= 80 117 0
AFLR4 : Nodes, Trias,Quads= 69 95 0
AFLR4 : Generate optimal mesh on surface definition 106
AFLR2 : Nodes, Trias,Quads= 670 1159 0
AFLR4 : Nodes, Trias,Quads= 578 975 0
AFLR4 : Generate optimal mesh on surface definition 107
AFLR2 : Nodes, Trias,Quads= 616 1122 0
AFLR4 : Nodes, Trias,Quads= 631 1152 0
AFLR4 : Generate optimal mesh on surface definition 108
AFLR2 : Nodes, Trias,Quads= 1009 1861 0
AFLR4 : Nodes, Trias,Quads= 712 1267 0
AFLR4 : Generate optimal mesh on surface definition 109
AFLR2 : Nodes, Trias,Quads= 1012 1867 0
AFLR4 : Nodes, Trias,Quads= 709 1261 0
AFLR4 : Generate optimal mesh on surface definition 110
AFLR2 : Nodes, Trias,Quads= 51 69 0
AFLR4 : Nodes, Trias,Quads= 41 49 0
AFLR4 : Generate optimal mesh on surface definition 111
AFLR2 : Nodes, Trias,Quads= 734 1294 0
AFLR4 : Nodes, Trias,Quads= 745 1316 0
AFLR4 : Generate optimal mesh on surface definition 112
AFLR2 : Nodes, Trias,Quads= 565 1023 0
AFLR4 : Nodes, Trias,Quads= 597 1087 0
AFLR4 : Generate optimal mesh on surface definition 113
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 114
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 115
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 116
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 117
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 118
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 51880 103724 12318
OVERALL : CPU Time = 7.322 seconds
Body 1 (of 11)
Number of nodes = 34785
Number of elements = 69574
Number of triangle elements = 69574
Number of quadrilateral elements = 0
Body 2 (of 11)
Number of nodes = 347
Number of elements = 690
Number of triangle elements = 690
Number of quadrilateral elements = 0
Body 3 (of 11)
Number of nodes = 2312
Number of elements = 4620
Number of triangle elements = 4620
Number of quadrilateral elements = 0
Body 4 (of 11)
Number of nodes = 657
Number of elements = 1310
Number of triangle elements = 1310
Number of quadrilateral elements = 0
Body 5 (of 11)
Number of nodes = 1604
Number of elements = 3204
Number of triangle elements = 3204
Number of quadrilateral elements = 0
Body 6 (of 11)
Number of nodes = 2311
Number of elements = 4618
Number of triangle elements = 4618
Number of quadrilateral elements = 0
Body 7 (of 11)
Number of nodes = 2054
Number of elements = 4104
Number of triangle elements = 4104
Number of quadrilateral elements = 0
Body 8 (of 11)
Number of nodes = 2755
Number of elements = 5506
Number of triangle elements = 5506
Number of quadrilateral elements = 0
Body 9 (of 11)
Number of nodes = 2543
Number of elements = 5082
Number of triangle elements = 5082
Number of quadrilateral elements = 0
Body 10 (of 11)
Number of nodes = 2492
Number of elements = 4980
Number of triangle elements = 4980
Number of quadrilateral elements = 0
Body 11 (of 11)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 51880
Total number of elements = 103724
Total number of triangle elements = 103724
Total number of quadrilateral elements = 0
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Fuselage
2: Wing
3: Htail
4: Pylon
5: Vtail
6: Nacelle
7: Control
8: Farfield
Finished writing vtk file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 9
Name = Fuselage, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = Htail, index = 4
Name = Pylon, index = 5
Name = Vtail, index = 6
Name = Nacelle, index = 7
Name = Control, index = 8
Name = Farfield, index = 9
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = Fuselage, index = 1
Name = Wing, index = 2
Name = Htail, index = 3
Name = Pylon, index = 4
Name = Vtail, index = 5
Name = Nacelle, index = 6
Name = Control, index = 7
Name = Farfield, index = 8
Getting mesh sizing parameters
Mesh sizing name - Control
Mesh sizing name - Fuselage
Mesh sizing name - Htail
Mesh sizing name - Nacelle
Mesh sizing name - Pylon
Mesh sizing name - Vtail
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mbl = 1
UG PARAM : nbl = 5
UG PARAM : mblelc = 2
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mbl = 1
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mblelc = 1
UG PARAM : BC_IDs [ 0]= 1
UG PARAM : BC_IDs [ 1]= 2
UG PARAM : BC_IDs [ 2]= 3
UG PARAM : BC_IDs [ 3]= 4
UG PARAM : BC_IDs [ 4]= 5
UG PARAM : BC_IDs [ 5]= 6
UG PARAM : BC_IDs [ 6]= 7
UG PARAM : BC_IDs [ 7]= 8
UG PARAM : BC_IDs [ 8]= 9
UG PARAM : BC_IDs [ 9]= 10
UG PARAM : BC_IDs [10]= 11
UG PARAM : BC_IDs [11]= 12
UG PARAM : BC_IDs [12]= 13
UG PARAM : BC_IDs [13]= 14
UG PARAM : BC_IDs [14]= 15
UG PARAM : BC_IDs [15]= 16
UG PARAM : BC_IDs [16]= 17
UG PARAM : BC_IDs [17]= 18
UG PARAM : BC_IDs [18]= 19
UG PARAM : BC_IDs [19]= 20
UG PARAM : BC_IDs [20]= 21
UG PARAM : BC_IDs [21]= 22
UG PARAM : BC_IDs [22]= 23
UG PARAM : BC_IDs [23]= 24
UG PARAM : BC_IDs [24]= 25
UG PARAM : BC_IDs [25]= 26
UG PARAM : BC_IDs [26]= 27
UG PARAM : BC_IDs [27]= 28
UG PARAM : BC_IDs [28]= 29
UG PARAM : BC_IDs [29]= 30
UG PARAM : BC_IDs [30]= 31
UG PARAM : BC_IDs [31]= 32
UG PARAM : BC_IDs [32]= 33
UG PARAM : BC_IDs [33]= 34
UG PARAM : BC_IDs [34]= 35
UG PARAM : BC_IDs [35]= 36
UG PARAM : BC_IDs [36]= 37
UG PARAM : BC_IDs [37]= 38
UG PARAM : BC_IDs [38]= 39
UG PARAM : BC_IDs [39]= 40
UG PARAM : BC_IDs [40]= 41
UG PARAM : BC_IDs [41]= 42
UG PARAM : BC_IDs [42]= 43
UG PARAM : BC_IDs [43]= 44
UG PARAM : BC_IDs [44]= 45
UG PARAM : BC_IDs [45]= 46
UG PARAM : BC_IDs [46]= 47
UG PARAM : BC_IDs [47]= 48
UG PARAM : BC_IDs [48]= 49
UG PARAM : BC_IDs [49]= 50
UG PARAM : BC_IDs [50]= 51
UG PARAM : BC_IDs [51]= 52
UG PARAM : BC_IDs [52]= 53
UG PARAM : BC_IDs [53]= 54
UG PARAM : BC_IDs [54]= 55
UG PARAM : BC_IDs [55]= 56
UG PARAM : BC_IDs [56]= 57
UG PARAM : BC_IDs [57]= 58
UG PARAM : BC_IDs [58]= 59
UG PARAM : BC_IDs [59]= 60
UG PARAM : BC_IDs [60]= 61
UG PARAM : BC_IDs [61]= 62
UG PARAM : BC_IDs [62]= 63
UG PARAM : BC_IDs [63]= 64
UG PARAM : BC_IDs [64]= 65
UG PARAM : BC_IDs [65]= 66
UG PARAM : BC_IDs [66]= 67
UG PARAM : BC_IDs [67]= 68
UG PARAM : BC_IDs [68]= 69
UG PARAM : BC_IDs [69]= 70
UG PARAM : BC_IDs [70]= 71
UG PARAM : BC_IDs [71]= 72
UG PARAM : BC_IDs [72]= 73
UG PARAM : BC_IDs [73]= 74
UG PARAM : BC_IDs [74]= 75
UG PARAM : BC_IDs [75]= 76
UG PARAM : BC_IDs [76]= 77
UG PARAM : BC_IDs [77]= 78
UG PARAM : BC_IDs [78]= 79
UG PARAM : BC_IDs [79]= 80
UG PARAM : BC_IDs [80]= 81
UG PARAM : BC_IDs [81]= 82
UG PARAM : BC_IDs [82]= 83
UG PARAM : BC_IDs [83]= 84
UG PARAM : BC_IDs [84]= 85
UG PARAM : BC_IDs [85]= 86
UG PARAM : BC_IDs [86]= 87
UG PARAM : BC_IDs [87]= 88
UG PARAM : BC_IDs [88]= 89
UG PARAM : BC_IDs [89]= 90
UG PARAM : BC_IDs [90]= 91
UG PARAM : BC_IDs [91]= 92
UG PARAM : BC_IDs [92]= 93
UG PARAM : BC_IDs [93]= 94
UG PARAM : BC_IDs [94]= 95
UG PARAM : BC_IDs [95]= 96
UG PARAM : BC_IDs [96]= 97
UG PARAM : BC_IDs [97]= 98
UG PARAM : BC_IDs [98]= 99
UG PARAM : BC_IDs [99]= 100
UG PARAM : BC_IDs [117]= 118
UG PARAM : BL_DS [ 0]= 0.434102
UG PARAM : BL_DS [ 1]= 0.434102
UG PARAM : BL_DS [ 2]= 0.434102
UG PARAM : BL_DS [ 3]= 0.434102
UG PARAM : BL_DS [ 4]= 0.434102
UG PARAM : BL_DS [ 5]= 0.434102
UG PARAM : BL_DS [ 6]= 0.434102
UG PARAM : BL_DS [ 7]= 0.434102
UG PARAM : BL_DS [ 8]= 0.434102
UG PARAM : BL_DS [ 9]= 0.434102
UG PARAM : BL_DS [10]= 0.434102
UG PARAM : BL_DS [11]= 0.434102
UG PARAM : BL_DS [12]= 0.434102
UG PARAM : BL_DS [13]= 0.434102
UG PARAM : BL_DS [14]= 0.434102
UG PARAM : BL_DS [15]= 0.434102
UG PARAM : BL_DS [16]= 0.434102
UG PARAM : BL_DS [17]= 0.434102
UG PARAM : BL_DS [18]= 0.434102
UG PARAM : BL_DS [19]= 0.434102
UG PARAM : BL_DS [20]= 0.434102
UG PARAM : BL_DS [21]= 0.434102
UG PARAM : BL_DS [22]= 0.434102
UG PARAM : BL_DS [23]= 0.434102
UG PARAM : BL_DS [24]= 0.434102
UG PARAM : BL_DS [25]= 0.434102
UG PARAM : BL_DS [26]= 0.434102
UG PARAM : BL_DS [27]= 0.434102
UG PARAM : BL_DS [28]= 0.434102
UG PARAM : BL_DS [29]= 0.434102
UG PARAM : BL_DS [30]= 0.434102
UG PARAM : BL_DS [31]= 0.434102
UG PARAM : BL_DS [32]= 0.434102
UG PARAM : BL_DS [33]= 0.434102
UG PARAM : BL_DS [34]= 0.434102
UG PARAM : BL_DS [35]= 0.434102
UG PARAM : BL_DS [36]= 0.434102
UG PARAM : BL_DS [37]= 0.434102
UG PARAM : BL_DS [38]= 0.434102
UG PARAM : BL_DS [39]= 0.434102
UG PARAM : BL_DS [40]= 0.434102
UG PARAM : BL_DS [41]= 0.434102
UG PARAM : BL_DS [42]= 0.434102
UG PARAM : BL_DS [43]= 0.434102
UG PARAM : BL_DS [44]= 0.434102
UG PARAM : BL_DS [45]= 0.434102
UG PARAM : BL_DS [46]= 0.434102
UG PARAM : BL_DS [47]= 0.434102
UG PARAM : BL_DS [48]= 0.434102
UG PARAM : BL_DS [49]= 0.434102
UG PARAM : BL_DS [50]= 0.434102
UG PARAM : BL_DS [51]= 0.434102
UG PARAM : BL_DS [52]= 0.434102
UG PARAM : BL_DS [53]= 0.434102
UG PARAM : BL_DS [54]= 0.434102
UG PARAM : BL_DS [55]= 0.434102
UG PARAM : BL_DS [56]= 0.434102
UG PARAM : BL_DS [57]= 0.434102
UG PARAM : BL_DS [58]= 0.434102
UG PARAM : BL_DS [59]= 0.434102
UG PARAM : BL_DS [60]= 0.434102
UG PARAM : BL_DS [61]= 0.434102
UG PARAM : BL_DS [62]= 0.434102
UG PARAM : BL_DS [63]= 0.434102
UG PARAM : BL_DS [64]= 0.434102
UG PARAM : BL_DS [65]= 0.434102
UG PARAM : BL_DS [66]= 0.434102
UG PARAM : BL_DS [67]= 0.434102
UG PARAM : BL_DS [68]= 0.217051
UG PARAM : BL_DS [69]= 0.217051
UG PARAM : BL_DS [70]= 0.217051
UG PARAM : BL_DS [71]= 0.434102
UG PARAM : BL_DS [72]= 0.434102
UG PARAM : BL_DS [73]= 0.217051
UG PARAM : BL_DS [74]= 0.217051
UG PARAM : BL_DS [75]= 0.217051
UG PARAM : BL_DS [76]= 0.434102
UG PARAM : BL_DS [77]= 0.434102
UG PARAM : BL_DS [78]= 0.217051
UG PARAM : BL_DS [79]= 0.217051
UG PARAM : BL_DS [80]= 0.217051
UG PARAM : BL_DS [81]= 0.434102
UG PARAM : BL_DS [82]= 0.434102
UG PARAM : BL_DS [83]= 0.434102
UG PARAM : BL_DS [84]= 0.217051
UG PARAM : BL_DS [85]= 0.217051
UG PARAM : BL_DS [86]= 0.217051
UG PARAM : BL_DS [87]= 0.434102
UG PARAM : BL_DS [88]= 0.434102
UG PARAM : BL_DS [89]= 0.217051
UG PARAM : BL_DS [90]= 0.217051
UG PARAM : BL_DS [91]= 0.217051
UG PARAM : BL_DS [92]= 0.434102
UG PARAM : BL_DS [93]= 0.217051
UG PARAM : BL_DS [94]= 0.217051
UG PARAM : BL_DS [95]= 0.217051
UG PARAM : BL_DS [96]= 0.434102
UG PARAM : BL_DS [97]= 0.434102
UG PARAM : BL_DS [98]= 0.434102
UG PARAM : BL_DS [99]= 0.217051
UG PARAM : BL_DS [117]= 0
UG PARAM : BL_DEL [ 0]= 2.17051
UG PARAM : BL_DEL [ 1]= 2.17051
UG PARAM : BL_DEL [ 2]= 2.17051
UG PARAM : BL_DEL [ 3]= 2.17051
UG PARAM : BL_DEL [ 4]= 2.17051
UG PARAM : BL_DEL [ 5]= 2.17051
UG PARAM : BL_DEL [ 6]= 2.17051
UG PARAM : BL_DEL [ 7]= 2.17051
UG PARAM : BL_DEL [ 8]= 2.17051
UG PARAM : BL_DEL [ 9]= 2.17051
UG PARAM : BL_DEL [10]= 2.17051
UG PARAM : BL_DEL [11]= 2.17051
UG PARAM : BL_DEL [12]= 2.17051
UG PARAM : BL_DEL [13]= 2.17051
UG PARAM : BL_DEL [14]= 2.17051
UG PARAM : BL_DEL [15]= 2.17051
UG PARAM : BL_DEL [16]= 2.17051
UG PARAM : BL_DEL [17]= 2.17051
UG PARAM : BL_DEL [18]= 2.17051
UG PARAM : BL_DEL [19]= 2.17051
UG PARAM : BL_DEL [20]= 2.17051
UG PARAM : BL_DEL [21]= 2.17051
UG PARAM : BL_DEL [22]= 2.17051
UG PARAM : BL_DEL [23]= 2.17051
UG PARAM : BL_DEL [24]= 2.17051
UG PARAM : BL_DEL [25]= 2.17051
UG PARAM : BL_DEL [26]= 2.17051
UG PARAM : BL_DEL [27]= 2.17051
UG PARAM : BL_DEL [28]= 2.17051
UG PARAM : BL_DEL [29]= 2.17051
UG PARAM : BL_DEL [30]= 2.17051
UG PARAM : BL_DEL [31]= 2.17051
UG PARAM : BL_DEL [32]= 2.17051
UG PARAM : BL_DEL [33]= 2.17051
UG PARAM : BL_DEL [34]= 2.17051
UG PARAM : BL_DEL [35]= 2.17051
UG PARAM : BL_DEL [36]= 2.17051
UG PARAM : BL_DEL [37]= 2.17051
UG PARAM : BL_DEL [38]= 2.17051
UG PARAM : BL_DEL [39]= 2.17051
UG PARAM : BL_DEL [40]= 2.17051
UG PARAM : BL_DEL [41]= 2.17051
UG PARAM : BL_DEL [42]= 2.17051
UG PARAM : BL_DEL [43]= 2.17051
UG PARAM : BL_DEL [44]= 2.17051
UG PARAM : BL_DEL [45]= 2.17051
UG PARAM : BL_DEL [46]= 2.17051
UG PARAM : BL_DEL [47]= 2.17051
UG PARAM : BL_DEL [48]= 2.17051
UG PARAM : BL_DEL [49]= 2.17051
UG PARAM : BL_DEL [50]= 2.17051
UG PARAM : BL_DEL [51]= 2.17051
UG PARAM : BL_DEL [52]= 2.17051
UG PARAM : BL_DEL [53]= 2.17051
UG PARAM : BL_DEL [54]= 2.17051
UG PARAM : BL_DEL [55]= 2.17051
UG PARAM : BL_DEL [56]= 2.17051
UG PARAM : BL_DEL [57]= 2.17051
UG PARAM : BL_DEL [58]= 2.17051
UG PARAM : BL_DEL [59]= 2.17051
UG PARAM : BL_DEL [60]= 2.17051
UG PARAM : BL_DEL [61]= 2.17051
UG PARAM : BL_DEL [62]= 2.17051
UG PARAM : BL_DEL [63]= 2.17051
UG PARAM : BL_DEL [64]= 2.17051
UG PARAM : BL_DEL [65]= 2.17051
UG PARAM : BL_DEL [66]= 2.17051
UG PARAM : BL_DEL [67]= 2.17051
UG PARAM : BL_DEL [68]= 2.17051
UG PARAM : BL_DEL [69]= 2.17051
UG PARAM : BL_DEL [70]= 2.17051
UG PARAM : BL_DEL [71]= 2.17051
UG PARAM : BL_DEL [72]= 2.17051
UG PARAM : BL_DEL [73]= 2.17051
UG PARAM : BL_DEL [74]= 2.17051
UG PARAM : BL_DEL [75]= 2.17051
UG PARAM : BL_DEL [76]= 2.17051
UG PARAM : BL_DEL [77]= 2.17051
UG PARAM : BL_DEL [78]= 2.17051
UG PARAM : BL_DEL [79]= 2.17051
UG PARAM : BL_DEL [80]= 2.17051
UG PARAM : BL_DEL [81]= 2.17051
UG PARAM : BL_DEL [82]= 2.17051
UG PARAM : BL_DEL [83]= 2.17051
UG PARAM : BL_DEL [84]= 2.17051
UG PARAM : BL_DEL [85]= 2.17051
UG PARAM : BL_DEL [86]= 2.17051
UG PARAM : BL_DEL [87]= 2.17051
UG PARAM : BL_DEL [88]= 2.17051
UG PARAM : BL_DEL [89]= 2.17051
UG PARAM : BL_DEL [90]= 2.17051
UG PARAM : BL_DEL [91]= 2.17051
UG PARAM : BL_DEL [92]= 2.17051
UG PARAM : BL_DEL [93]= 2.17051
UG PARAM : BL_DEL [94]= 2.17051
UG PARAM : BL_DEL [95]= 2.17051
UG PARAM : BL_DEL [96]= 2.17051
UG PARAM : BL_DEL [97]= 2.17051
UG PARAM : BL_DEL [98]= 2.17051
UG PARAM : BL_DEL [99]= 2.17051
UG PARAM : BL_DEL [117]= 0
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 11 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 67 Faces
EGADS : Body 0 has 176 Edges
EGADS : Body 0 has 71 Loops
EGADS : Body 0 has 107 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 5 Faces
EGADS : Body 1 has 9 Edges
EGADS : Body 1 has 5 Loops
EGADS : Body 1 has 6 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 5 Faces
EGADS : Body 2 has 9 Edges
EGADS : Body 2 has 5 Loops
EGADS : Body 2 has 6 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 5 Faces
EGADS : Body 3 has 9 Edges
EGADS : Body 3 has 5 Loops
EGADS : Body 3 has 6 Nodes
EGADS : Body 4 is a SolidBody
EGADS : Body 4 has 1 Shells
EGADS : Body 4 has 5 Faces
EGADS : Body 4 has 9 Edges
EGADS : Body 4 has 5 Loops
EGADS : Body 4 has 6 Nodes
EGADS : Body 5 is a SolidBody
EGADS : Body 5 has 1 Shells
EGADS : Body 5 has 5 Faces
EGADS : Body 5 has 9 Edges
EGADS : Body 5 has 5 Loops
EGADS : Body 5 has 6 Nodes
EGADS : Body 6 is a SolidBody
EGADS : Body 6 has 1 Shells
EGADS : Body 6 has 5 Faces
EGADS : Body 6 has 9 Edges
EGADS : Body 6 has 5 Loops
EGADS : Body 6 has 6 Nodes
EGADS : Body 7 is a SolidBody
EGADS : Body 7 has 1 Shells
EGADS : Body 7 has 5 Faces
EGADS : Body 7 has 9 Edges
EGADS : Body 7 has 5 Loops
EGADS : Body 7 has 6 Nodes
EGADS : Body 8 is a SolidBody
EGADS : Body 8 has 1 Shells
EGADS : Body 8 has 5 Faces
EGADS : Body 8 has 9 Edges
EGADS : Body 8 has 5 Loops
EGADS : Body 8 has 6 Nodes
EGADS : Body 9 is a SolidBody
EGADS : Body 9 has 1 Shells
EGADS : Body 9 has 5 Faces
EGADS : Body 9 has 9 Edges
EGADS : Body 9 has 5 Loops
EGADS : Body 9 has 6 Nodes
EGADS : Body 10 is a SolidBody
EGADS : Body 10 has 1 Shells
EGADS : Body 10 has 6 Faces
EGADS : Body 10 has 12 Edges
EGADS : Body 10 has 6 Loops
EGADS : Body 10 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 6
EGADS : 2 Yes 0 0 1 0 1 1 7 8 9 10
EGADS : 3 Yes 0 0 1 0 1 1 8 11 12 13 14
EGADS : 4 Yes 0 0 1 0 1 1 7 12
EGADS : 5 Yes 0 0 1 0 1 1 6 15 16 17 18
EGADS : 6 Yes 0 0 1 0 1 1 5 15 16 17 19
EGADS : 20 21
EGADS : 7 Yes 0 0 1 0 1 2 4 22
EGADS : 8 Yes 0 0 1 0 1 2 3 11 22 23 24
EGADS : 9 Yes 0 0 1 0 1 2 10 25 26 27 28
EGADS : 29 30
EGADS : 10 Yes 0 0 1 0 1 2 9 26 27 28 31
EGADS : 11 Yes 0 0 1 0 1 3 8 12 22
EGADS : 12 Yes 0 0 1 0 1 3 4 11 13 14 22
EGADS : 32
EGADS : 13 Yes 0 0 1 0 1 3 12 14 33 34 35
EGADS : 36
EGADS : 14 Yes 0 0 1 0 1 3 12 13 33 34 35
EGADS : 36
EGADS : 15 Yes 0 0 1 0 1 5 6 16
EGADS : 16 Yes 0 0 1 0 1 5 6 15 17
EGADS : 17 Yes 0 0 1 0 1 5 6 16
EGADS : 18 Yes 0 0 1 0 1 5 19 37 38 39 40
EGADS : 41 42 43
EGADS : 19 Yes 0 0 1 0 1 6 18 37 38 39 40
EGADS : 41 42 43
EGADS : 20 Yes 0 0 1 0 1 6 21 44
EGADS : 21 Yes 0 0 1 0 1 6 20 45
EGADS : 22 Yes 0 0 1 0 1 7 8 11 12 23 24
EGADS : 46
EGADS : 23 Yes 0 0 1 0 1 8 22 24 47 48 49
EGADS : 50
EGADS : 24 Yes 0 0 1 0 1 8 22 23 47 48 49
EGADS : 50
EGADS : 25 Yes 0 0 1 0 1 9 31 51 52 53 54
EGADS : 55 56 57
EGADS : 26 Yes 0 0 1 0 1 9 10 27
EGADS : 27 Yes 0 0 1 0 1 9 10 26 28
EGADS : 28 Yes 0 0 1 0 1 9 10 27
EGADS : 29 Yes 0 0 1 0 1 9 30 58
EGADS : 30 Yes 0 0 1 0 1 9 29 59
EGADS : 31 Yes 0 0 1 0 1 10 25 51 52 53
EGADS : 54 55 56 57
EGADS : 32 Yes 0 0 1 0 1 12 46 60 61 62
EGADS : 63
EGADS : 33 Yes 0 0 1 0 1 13 14 34
EGADS : 34 Yes 0 0 1 0 1 13 14 33 35
EGADS : 35 Yes 0 0 1 0 1 13 14 34
EGADS : 36 Yes 0 0 1 0 1 13 14
EGADS : 37 Yes 0 0 1 0 1 18 19 38
EGADS : 38 Yes 0 0 1 0 1 18 19 37 39
EGADS : 39 Yes 0 0 1 0 1 18 19 38
EGADS : 40 Yes 0 0 1 0 1 18 19 41
EGADS : 41 Yes 0 0 1 0 1 18 19 40 42
EGADS : 42 Yes 0 0 1 0 1 18 19 41
EGADS : 43 Yes 0 0 1 0 1 18 19
EGADS : 44 Yes 0 0 1 0 1 20 45 64
EGADS : 45 Yes 0 0 1 0 1 21 44 65
EGADS : 46 Yes 0 0 1 0 1 22 32 60 61 62
EGADS : 63
EGADS : 47 Yes 0 0 1 0 1 23 24
EGADS : 48 Yes 0 0 1 0 1 23 24 49
EGADS : 49 Yes 0 0 1 0 1 23 24 48 50
EGADS : 50 Yes 0 0 1 0 1 23 24 49
EGADS : 51 Yes 0 0 1 0 1 25 31
EGADS : 52 Yes 0 0 1 0 1 25 31 53
EGADS : 53 Yes 0 0 1 0 1 25 31 52 54
EGADS : 54 Yes 0 0 1 0 1 25 31 53
EGADS : 55 Yes 0 0 1 0 1 25 31 56
EGADS : 56 Yes 0 0 1 0 1 25 31 55 57
EGADS : 57 Yes 0 0 1 0 1 25 31 56
EGADS : 58 Yes 0 0 1 0 1 29 59 66
EGADS : 59 Yes 0 0 1 0 1 30 58 67
EGADS : 60 Yes 0 0 1 0 1 32 46 61
EGADS : 61 Yes 0 0 1 0 1 32 46 60 62
EGADS : 62 Yes 0 0 1 0 1 32 46 61
EGADS : 63 Yes 0 0 1 0 1 32 46
EGADS : 64 Yes 0 0 1 0 1 44 65
EGADS : 65 Yes 0 0 1 0 1 45 64
EGADS : 66 Yes 0 0 1 0 1 58 67
EGADS : 67 Yes 0 0 1 0 1 59 66
EGADS : 68 Yes 1 0 1 0 1 69 70 71 72
EGADS : 69 Yes 1 0 1 0 1 68 70 72
EGADS : 70 Yes 1 0 1 0 1 68 69 71 72
EGADS : 71 Yes 1 0 1 0 1 68 70 72
EGADS : 72 Yes 1 0 1 0 1 68 69 70 71
EGADS : 73 Yes 2 0 1 0 1 74 75 76 77
EGADS : 74 Yes 2 0 1 0 1 73 75 77
EGADS : 75 Yes 2 0 1 0 1 73 74 76 77
EGADS : 76 Yes 2 0 1 0 1 73 75 77
EGADS : 77 Yes 2 0 1 0 1 73 74 75 76
EGADS : 78 Yes 3 0 1 0 1 79 80 81 82
EGADS : 79 Yes 3 0 1 0 1 78 80 82
EGADS : 80 Yes 3 0 1 0 1 78 79 81 82
EGADS : 81 Yes 3 0 1 0 1 78 80 82
EGADS : 82 Yes 3 0 1 0 1 78 79 80 81
EGADS : 83 Yes 4 0 1 0 1 84 85 86 87
EGADS : 84 Yes 4 0 1 0 1 83 85 86 87
EGADS : 85 Yes 4 0 1 0 1 83 84 86
EGADS : 86 Yes 4 0 1 0 1 83 84 85 87
EGADS : 87 Yes 4 0 1 0 1 83 84 86
EGADS : 88 Yes 5 0 1 0 1 89 90 91 92
EGADS : 89 Yes 5 0 1 0 1 88 90 91 92
EGADS : 90 Yes 5 0 1 0 1 88 89 91
EGADS : 91 Yes 5 0 1 0 1 88 89 90 92
EGADS : 92 Yes 5 0 1 0 1 88 89 91
EGADS : 93 Yes 6 0 1 0 1 94 95 96 97
EGADS : 94 Yes 6 0 1 0 1 93 95 97
EGADS : 95 Yes 6 0 1 0 1 93 94 96 97
EGADS : 96 Yes 6 0 1 0 1 93 95 97
EGADS : 97 Yes 6 0 1 0 1 93 94 95 96
EGADS : 98 Yes 7 0 1 0 1 99 100 101 102
EGADS : 99 Yes 7 0 1 0 1 98 100 101 102
EGADS : 100 Yes 7 0 1 0 1 98 99 101
EGADS : 101 Yes 7 0 1 0 1 98 99 100 102
EGADS : 102 Yes 7 0 1 0 1 98 99 101
EGADS : 103 Yes 8 0 1 0 1 104 105 106 107
EGADS : 104 Yes 8 0 1 0 1 103 105 106 107
EGADS : 105 Yes 8 0 1 0 1 103 104 106
EGADS : 106 Yes 8 0 1 0 1 103 104 105 107
EGADS : 107 Yes 8 0 1 0 1 103 104 106
EGADS : 108 Yes 9 0 1 0 1 109 110 111 112
EGADS : 109 Yes 9 0 1 0 1 108 110 111 112
EGADS : 110 Yes 9 0 1 0 1 108 109 111
EGADS : 111 Yes 9 0 1 0 1 108 109 110 112
EGADS : 112 Yes 9 0 1 0 1 108 109 111
EGADS : 113 Yes 10 0 1 NA NA 115 116 117 118
EGADS : 114 Yes 10 0 1 NA NA 115 116 117 118
EGADS : 115 Yes 10 0 1 NA NA 113 114 117 118
EGADS : 116 Yes 10 0 1 NA NA 113 114 117 118
EGADS : 117 Yes 10 0 1 NA NA 113 114 115 116
EGADS : 118 Yes 10 0 1 NA NA 113 114 115 116
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 4 3 -2 -5 -6
EGADS : 2 -7 9 1 -8 10 11
EGADS : 3 -12 2 17 -16 -15 14 -13
EGADS : 4 -3 18 19 -20
EGADS : 5 21 -22 23 24 25 26 -27 5
EGADS : 6 27 28 -25 29 -30 -31 -21 6 32 33
EGADS : 7 -19 34 7 -35
EGADS : 8 -36 8 12 -40 -39 38 37
EGADS : 9 -41 -10 47 46 45 -44 43 -42 48 49
EGADS : 10 -47 -11 41 -53 -43 -52 -51 50
EGADS : 11 13 54 55 40
EGADS : 12 -17 20 60 59 58 -54 -14 -57 -56
EGADS : 13 61 -62 63 64 65 66 -67 57 15
EGADS : 14 67 68 -65 69 -70 -71 -61 16 56
EGADS : 15 31 72 22
EGADS : 16 30 73 -23 -72
EGADS : 17 -73 -29 -24
EGADS : 18 74 -75 76 77 78 -79 80 81 82 83 -84 -26
EGADS : 19 84 85 -82 86 -87 -88 -78 89 -90 -91 -74 -28
EGADS : 20 -92 94 -32 -93
EGADS : 21 -94 95 93 -33
EGADS : 22 -60 35 36 98 97 39 -55 -58 96
EGADS : 23 -99 -98 -37 105 104 103 -102 101 -100
EGADS : 24 -105 -38 -97 99 -109 -101 -108 -107 106
EGADS : 25 -110 42 120 119 118 -117 116 115 114 -113 112 -111
EGADS : 26 44 121 52
EGADS : 27 -45 122 51 -121
EGADS : 28 -122 -46 -50
EGADS : 29 123 124 -48 -125
EGADS : 30 125 -49 -124 -126
EGADS : 31 -120 53 110 -133 -112 -132 -131 130 -116 -129 -128 127
EGADS : 32 -134 -59 140 -139 -138 -137 -136 135
EGADS : 33 71 141 62
EGADS : 34 70 142 -63 -141
EGADS : 35 -142 -69 -64
EGADS : 36 -66 -68
EGADS : 37 91 143 75
EGADS : 38 90 144 -76 -143
EGADS : 39 -144 -89 -77
EGADS : 40 88 145 79
EGADS : 41 87 146 -80 -145
EGADS : 42 -146 -86 -81
EGADS : 43 -83 -85
EGADS : 44 147 92 148 149 -150 -151
EGADS : 45 -147 153 150 -152 -148 -95
EGADS : 46 -140 -96 134 157 156 -155 138 -154
EGADS : 47 109 100
EGADS : 48 102 158 108
EGADS : 49 -103 159 107 -158
EGADS : 50 -159 -104 -106
EGADS : 51 133 111
EGADS : 52 113 160 132
EGADS : 53 -114 161 131 -160
EGADS : 54 -161 -115 -130
EGADS : 55 117 162 129
EGADS : 56 -118 163 128 -162
EGADS : 57 -163 -119 -127
EGADS : 58 164 -123 165 166 -167 -168
EGADS : 59 -164 170 167 -169 -165 126
EGADS : 60 -135 171 -157
EGADS : 61 136 172 -156 -171
EGADS : 62 -172 137 155
EGADS : 63 139 154
EGADS : 64 -149 173 151 -174
EGADS : 65 152 174 -153 -173
EGADS : 66 -166 175 168 -176
EGADS : 67 169 176 -170 -175
EGADS : 68 -177 180 179 -178
EGADS : 69 181 182 177
EGADS : 70 178 183 -184 -181
EGADS : 71 -179 -185 -183
EGADS : 72 -180 -182 184 185
EGADS : 73 -186 189 188 -187
EGADS : 74 190 191 186
EGADS : 75 187 192 -193 -190
EGADS : 76 -188 -194 -192
EGADS : 77 -189 -191 193 194
EGADS : 78 -195 198 197 -196
EGADS : 79 199 200 195
EGADS : 80 196 201 -202 -199
EGADS : 81 -197 -203 -201
EGADS : 82 -198 -200 202 203
EGADS : 83 204 -205 -206 207
EGADS : 84 208 209 -210 -204
EGADS : 85 211 205 210
EGADS : 86 -209 212 206 -211
EGADS : 87 -208 -207 -212
EGADS : 88 213 -214 -215 216
EGADS : 89 217 218 -219 -213
EGADS : 90 220 214 219
EGADS : 91 -218 221 215 -220
EGADS : 92 -217 -216 -221
EGADS : 93 -222 -223 224 225
EGADS : 94 226 222 227
EGADS : 95 -228 229 223 -226
EGADS : 96 -230 -224 -229
EGADS : 97 -225 230 228 -227
EGADS : 98 231 234 -233 -232
EGADS : 99 -231 -237 236 235
EGADS : 100 238 237 232
EGADS : 101 233 239 -236 -238
EGADS : 102 -234 -235 -239
EGADS : 103 240 -241 -242 243
EGADS : 104 -240 244 245 -246
EGADS : 105 247 241 246
EGADS : 106 -245 248 242 -247
EGADS : 107 -244 -243 -248
EGADS : 108 -249 -252 251 250
EGADS : 109 -253 249 255 -254
EGADS : 110 256 -255 -250
EGADS : 111 -251 257 254 -256
EGADS : 112 252 253 -257
EGADS : 113 258 259 -260 -261
EGADS : 114 -262 265 264 -263
EGADS : 115 266 262 -267 -258
EGADS : 116 -268 260 269 -264
EGADS : 117 261 268 -265 -266
EGADS : 118 -259 267 263 -269
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1 2
EGADS : 2 3 4
EGADS : 3 5
EGADS : 4 6
EGADS : 5 7
EGADS : 6 8 9
EGADS : 7 10
EGADS : 8 11
EGADS : 9 12 13
EGADS : 10 14
EGADS : 11 15
EGADS : 12 16
EGADS : 13 17
EGADS : 14 18
EGADS : 15 19
EGADS : 16 20
EGADS : 17 21
EGADS : 18 22
EGADS : 19 23
EGADS : 20 24
EGADS : 21 25
EGADS : 22 26
EGADS : 23 27
EGADS : 24 28
EGADS : 25 29
EGADS : 26 30
EGADS : 27 31
EGADS : 28 32
EGADS : 29 33
EGADS : 30 34
EGADS : 31 35
EGADS : 32 36
EGADS : 33 37
EGADS : 34 38
EGADS : 35 39
EGADS : 36 40
EGADS : 37 41
EGADS : 38 42
EGADS : 39 43
EGADS : 40 44
EGADS : 41 45
EGADS : 42 46
EGADS : 43 47
EGADS : 44 48
EGADS : 45 49
EGADS : 46 50
EGADS : 47 51
EGADS : 48 52
EGADS : 49 53
EGADS : 50 54
EGADS : 51 55
EGADS : 52 56
EGADS : 53 57
EGADS : 54 58
EGADS : 55 59
EGADS : 56 60
EGADS : 57 61
EGADS : 58 62
EGADS : 59 63
EGADS : 60 64
EGADS : 61 65
EGADS : 62 66
EGADS : 63 67
EGADS : 64 68
EGADS : 65 69
EGADS : 66 70
EGADS : 67 71
EGADS : 68 72
EGADS : 69 73
EGADS : 70 74
EGADS : 71 75
EGADS : 72 76
EGADS : 73 77
EGADS : 74 78
EGADS : 75 79
EGADS : 76 80
EGADS : 77 81
EGADS : 78 82
EGADS : 79 83
EGADS : 80 84
EGADS : 81 85
EGADS : 82 86
EGADS : 83 87
EGADS : 84 88
EGADS : 85 89
EGADS : 86 90
EGADS : 87 91
EGADS : 88 92
EGADS : 89 93
EGADS : 90 94
EGADS : 91 95
EGADS : 92 96
EGADS : 93 97
EGADS : 94 98
EGADS : 95 99
EGADS : 96 100
EGADS : 97 101
EGADS : 98 102
EGADS : 99 103
EGADS : 100 104
EGADS : 101 105
EGADS : 102 106
EGADS : 103 107
EGADS : 104 108
EGADS : 105 109
EGADS : 106 110
EGADS : 107 111
EGADS : 108 112
EGADS : 109 113
EGADS : 110 114
EGADS : 111 115
EGADS : 112 116
EGADS : 113 117
EGADS : 114 118
EGADS : 115 119
EGADS : 116 120
EGADS : 117 121
EGADS : 118 122
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 4 3 -2
EGADS : 2 Yes -5 -6
EGADS : 3 Yes -7 9 1 -8
EGADS : 4 Yes 10 11
EGADS : 5 Yes -12 2 17 -16 -15 14 -13
EGADS : 6 Yes -3 18 19 -20
EGADS : 7 Yes 21 -22 23 24 25 26 -27 5
EGADS : 8 Yes 27 28 -25 29 -30 -31 -21 6
EGADS : 9 Yes 32 33
EGADS : 10 Yes -19 34 7 -35
EGADS : 11 Yes -36 8 12 -40 -39 38 37
EGADS : 12 Yes -41 -10 47 46 45 -44 43 -42
EGADS : 13 Yes 48 49
EGADS : 14 Yes -47 -11 41 -53 -43 -52 -51 50
EGADS : 15 Yes 13 54 55 40
EGADS : 16 Yes -17 20 60 59 58 -54 -14 -57 -56
EGADS : 17 Yes 61 -62 63 64 65 66 -67 57 15
EGADS : 18 Yes 67 68 -65 69 -70 -71 -61 16 56
EGADS : 19 Yes 31 72 22
EGADS : 20 Yes 30 73 -23 -72
EGADS : 21 Yes -73 -29 -24
EGADS : 22 Yes 74 -75 76 77 78 -79 80 81 82 83 -84 -26
EGADS : 23 Yes 84 85 -82 86 -87 -88 -78 89 -90 -91 -74 -28
EGADS : 24 Yes -92 94 -32 -93
EGADS : 25 Yes -94 95 93 -33
EGADS : 26 Yes -60 35 36 98 97 39 -55 -58 96
EGADS : 27 Yes -99 -98 -37 105 104 103 -102 101 -100
EGADS : 28 Yes -105 -38 -97 99 -109 -101 -108 -107 106
EGADS : 29 Yes -110 42 120 119 118 -117 116 115 114 -113 112 -111
EGADS : 30 Yes 44 121 52
EGADS : 31 Yes -45 122 51 -121
EGADS : 32 Yes -122 -46 -50
EGADS : 33 Yes 123 124 -48 -125
EGADS : 34 Yes 125 -49 -124 -126
EGADS : 35 Yes -120 53 110 -133 -112 -132 -131 130 -116 -129 -128
EGADS : 127
EGADS : 36 Yes -134 -59 140 -139 -138 -137 -136 135
EGADS : 37 Yes 71 141 62
EGADS : 38 Yes 70 142 -63 -141
EGADS : 39 Yes -142 -69 -64
EGADS : 40 Yes -66 -68
EGADS : 41 Yes 91 143 75
EGADS : 42 Yes 90 144 -76 -143
EGADS : 43 Yes -144 -89 -77
EGADS : 44 Yes 88 145 79
EGADS : 45 Yes 87 146 -80 -145
EGADS : 46 Yes -146 -86 -81
EGADS : 47 Yes -83 -85
EGADS : 48 Yes 147 92 148 149 -150 -151
EGADS : 49 Yes -147 153 150 -152 -148 -95
EGADS : 50 Yes -140 -96 134 157 156 -155 138 -154
EGADS : 51 Yes 109 100
EGADS : 52 Yes 102 158 108
EGADS : 53 Yes -103 159 107 -158
EGADS : 54 Yes -159 -104 -106
EGADS : 55 Yes 133 111
EGADS : 56 Yes 113 160 132
EGADS : 57 Yes -114 161 131 -160
EGADS : 58 Yes -161 -115 -130
EGADS : 59 Yes 117 162 129
EGADS : 60 Yes -118 163 128 -162
EGADS : 61 Yes -163 -119 -127
EGADS : 62 Yes 164 -123 165 166 -167 -168
EGADS : 63 Yes -164 170 167 -169 -165 126
EGADS : 64 Yes -135 171 -157
EGADS : 65 Yes 136 172 -156 -171
EGADS : 66 Yes -172 137 155
EGADS : 67 Yes 139 154
EGADS : 68 Yes -149 173 151 -174
EGADS : 69 Yes 152 174 -153 -173
EGADS : 70 Yes -166 175 168 -176
EGADS : 71 Yes 169 176 -170 -175
EGADS : 72 Yes -177 180 179 -178
EGADS : 73 Yes 181 182 177
EGADS : 74 Yes 178 183 -184 -181
EGADS : 75 Yes -179 -185 -183
EGADS : 76 Yes -180 -182 184 185
EGADS : 77 Yes -186 189 188 -187
EGADS : 78 Yes 190 191 186
EGADS : 79 Yes 187 192 -193 -190
EGADS : 80 Yes -188 -194 -192
EGADS : 81 Yes -189 -191 193 194
EGADS : 82 Yes -195 198 197 -196
EGADS : 83 Yes 199 200 195
EGADS : 84 Yes 196 201 -202 -199
EGADS : 85 Yes -197 -203 -201
EGADS : 86 Yes -198 -200 202 203
EGADS : 87 Yes 204 -205 -206 207
EGADS : 88 Yes 208 209 -210 -204
EGADS : 89 Yes 211 205 210
EGADS : 90 Yes -209 212 206 -211
EGADS : 91 Yes -208 -207 -212
EGADS : 92 Yes 213 -214 -215 216
EGADS : 93 Yes 217 218 -219 -213
EGADS : 94 Yes 220 214 219
EGADS : 95 Yes -218 221 215 -220
EGADS : 96 Yes -217 -216 -221
EGADS : 97 Yes -222 -223 224 225
EGADS : 98 Yes 226 222 227
EGADS : 99 Yes -228 229 223 -226
EGADS : 100 Yes -230 -224 -229
EGADS : 101 Yes -225 230 228 -227
EGADS : 102 Yes 231 234 -233 -232
EGADS : 103 Yes -231 -237 236 235
EGADS : 104 Yes 238 237 232
EGADS : 105 Yes 233 239 -236 -238
EGADS : 106 Yes -234 -235 -239
EGADS : 107 Yes 240 -241 -242 243
EGADS : 108 Yes -240 244 245 -246
EGADS : 109 Yes 247 241 246
EGADS : 110 Yes -245 248 242 -247
EGADS : 111 Yes -244 -243 -248
EGADS : 112 Yes -249 -252 251 250
EGADS : 113 Yes -253 249 255 -254
EGADS : 114 Yes 256 -255 -250
EGADS : 115 Yes -251 257 254 -256
EGADS : 116 Yes 252 253 -257
EGADS : 117 Yes 258 259 -260 -261
EGADS : 118 Yes -262 265 264 -263
EGADS : 119 Yes 266 262 -267 -258
EGADS : 120 Yes -268 260 269 -264
EGADS : 121 Yes 261 268 -265 -266
EGADS : 122 Yes -259 267 263 -269
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 2 3 1 1 3
EGADS : 3 0 Yes 1 3 1 1 4
EGADS : 4 0 DEGEN 1 1 - 1
EGADS : 5 0 Yes 4 5 1 1 5
EGADS : 6 0 Yes 5 4 1 1 6
EGADS : 7 0 Yes 1 6 1 2 7
EGADS : 8 0 Yes 6 2 1 2 8
EGADS : 9 0 DEGEN 1 1 - 2
EGADS : 10 0 Yes 7 8 1 2 9
EGADS : 11 0 Yes 8 7 1 2 10
EGADS : 12 0 Yes 2 9 1 3 8
EGADS : 13 0 Yes 9 10 1 3 11
EGADS : 14 0 Yes 11 10 1 3 12
EGADS : 15 0 Yes 11 12 1 3 13
EGADS : 16 0 Yes 12 13 1 3 14
EGADS : 17 0 Yes 3 13 1 3 12
EGADS : 18 0 DEGEN 1 1 - 4
EGADS : 19 0 Yes 1 14 1 4 7
EGADS : 20 0 Yes 3 14 1 4 12
EGADS : 21 0 Yes 5 15 1 5 6
EGADS : 22 0 Yes 16 15 1 5 15
EGADS : 23 0 Yes 16 17 1 5 16
EGADS : 24 0 Yes 17 18 1 5 17
EGADS : 25 0 Yes 18 19 1 5 6
EGADS : 26 0 Yes 19 20 1 5 18
EGADS : 27 0 Yes 4 20 1 5 6
EGADS : 28 0 Yes 20 19 1 6 19
EGADS : 29 0 Yes 18 21 1 6 17
EGADS : 30 0 Yes 22 21 1 6 16
EGADS : 31 0 Yes 15 22 1 6 15
EGADS : 32 0 Yes 23 24 1 6 20
EGADS : 33 0 Yes 24 23 1 6 21
EGADS : 34 0 DEGEN 1 1 - 7
EGADS : 35 0 Yes 14 6 1 7 22
EGADS : 36 0 Yes 6 25 1 8 22
EGADS : 37 0 Yes 26 25 1 8 23
EGADS : 38 0 Yes 27 26 1 8 24
EGADS : 39 0 Yes 27 28 1 8 22
EGADS : 40 0 Yes 28 9 1 8 11
EGADS : 41 0 Yes 8 29 1 9 10
EGADS : 42 0 Yes 29 30 1 9 25
EGADS : 43 0 Yes 31 30 1 9 10
EGADS : 44 0 Yes 31 32 1 9 26
EGADS : 45 0 Yes 33 32 1 9 27
EGADS : 46 0 Yes 34 33 1 9 28
EGADS : 47 0 Yes 7 34 1 9 10
EGADS : 48 0 Yes 35 36 1 9 29
EGADS : 49 0 Yes 36 35 1 9 30
EGADS : 50 0 Yes 37 34 1 10 28
EGADS : 51 0 Yes 37 38 1 10 27
EGADS : 52 0 Yes 38 31 1 10 26
EGADS : 53 0 Yes 30 29 1 10 31
EGADS : 54 0 Yes 10 39 1 11 12
EGADS : 55 0 Yes 39 28 1 11 22
EGADS : 56 0 Yes 13 40 1 12 14
EGADS : 57 0 Yes 40 11 1 12 13
EGADS : 58 0 Yes 41 39 1 12 22
EGADS : 59 0 Yes 42 41 1 12 32
EGADS : 60 0 Yes 14 42 1 12 22
EGADS : 61 0 Yes 12 43 1 13 14
EGADS : 62 0 Yes 44 43 1 13 33
EGADS : 63 0 Yes 44 45 1 13 34
EGADS : 64 0 Yes 45 46 1 13 35
EGADS : 65 0 Yes 46 47 1 13 14
EGADS : 66 0 Yes 47 48 1 13 36
EGADS : 67 0 Yes 40 48 1 13 14
EGADS : 68 0 Yes 48 47 1 14 36
EGADS : 69 0 Yes 46 49 1 14 35
EGADS : 70 0 Yes 50 49 1 14 34
EGADS : 71 0 Yes 43 50 1 14 33
EGADS : 72 0 Yes 22 16 1 15 16
EGADS : 73 0 Yes 21 17 1 16 17
EGADS : 74 0 Yes 19 51 1 18 19
EGADS : 75 0 Yes 52 51 1 18 37
EGADS : 76 0 Yes 52 53 1 18 38
EGADS : 77 0 Yes 53 54 1 18 39
EGADS : 78 0 Yes 54 55 1 18 19
EGADS : 79 0 Yes 56 55 1 18 40
EGADS : 80 0 Yes 56 57 1 18 41
EGADS : 81 0 Yes 57 58 1 18 42
EGADS : 82 0 Yes 58 59 1 18 19
EGADS : 83 0 Yes 59 60 1 18 43
EGADS : 84 0 Yes 20 60 1 18 19
EGADS : 85 0 Yes 60 59 1 19 43
EGADS : 86 0 Yes 58 61 1 19 42
EGADS : 87 0 Yes 62 61 1 19 41
EGADS : 88 0 Yes 55 62 1 19 40
EGADS : 89 0 Yes 54 63 1 19 39
EGADS : 90 0 Yes 64 63 1 19 38
EGADS : 91 0 Yes 51 64 1 19 37
EGADS : 92 0 Yes 65 66 1 20 44
EGADS : 93 0 Yes 66 23 1 20 21
EGADS : 94 0 Yes 65 24 1 20 21
EGADS : 95 0 Yes 65 66 1 21 45
EGADS : 96 0 Yes 41 42 1 22 46
EGADS : 97 0 Yes 67 27 1 22 24
EGADS : 98 0 Yes 25 67 1 22 23
EGADS : 99 0 Yes 67 68 1 23 24
EGADS : 100 0 Yes 68 69 1 23 47
EGADS : 101 0 Yes 70 69 1 23 24
EGADS : 102 0 Yes 70 71 1 23 48
EGADS : 103 0 Yes 72 71 1 23 49
EGADS : 104 0 Yes 73 72 1 23 50
EGADS : 105 0 Yes 26 73 1 23 24
EGADS : 106 0 Yes 74 73 1 24 50
EGADS : 107 0 Yes 74 75 1 24 49
EGADS : 108 0 Yes 75 70 1 24 48
EGADS : 109 0 Yes 69 68 1 24 47
EGADS : 110 0 Yes 29 76 1 25 31
EGADS : 111 0 Yes 76 77 1 25 51
EGADS : 112 0 Yes 78 77 1 25 31
EGADS : 113 0 Yes 78 79 1 25 52
EGADS : 114 0 Yes 80 79 1 25 53
EGADS : 115 0 Yes 81 80 1 25 54
EGADS : 116 0 Yes 82 81 1 25 31
EGADS : 117 0 Yes 82 83 1 25 55
EGADS : 118 0 Yes 84 83 1 25 56
EGADS : 119 0 Yes 85 84 1 25 57
EGADS : 120 0 Yes 30 85 1 25 31
EGADS : 121 0 Yes 32 38 1 26 27
EGADS : 122 0 Yes 33 37 1 27 28
EGADS : 123 0 Yes 86 87 1 29 58
EGADS : 124 0 Yes 87 36 1 29 30
EGADS : 125 0 Yes 86 35 1 29 30
EGADS : 126 0 Yes 86 87 1 30 59
EGADS : 127 0 Yes 88 85 1 31 57
EGADS : 128 0 Yes 88 89 1 31 56
EGADS : 129 0 Yes 89 82 1 31 55
EGADS : 130 0 Yes 90 81 1 31 54
EGADS : 131 0 Yes 90 91 1 31 53
EGADS : 132 0 Yes 91 78 1 31 52
EGADS : 133 0 Yes 77 76 1 31 51
EGADS : 134 0 Yes 41 92 1 32 46
EGADS : 135 0 Yes 93 92 1 32 60
EGADS : 136 0 Yes 93 94 1 32 61
EGADS : 137 0 Yes 94 95 1 32 62
EGADS : 138 0 Yes 95 96 1 32 46
EGADS : 139 0 Yes 96 97 1 32 63
EGADS : 140 0 Yes 42 97 1 32 46
EGADS : 141 0 Yes 50 44 1 33 34
EGADS : 142 0 Yes 49 45 1 34 35
EGADS : 143 0 Yes 64 52 1 37 38
EGADS : 144 0 Yes 63 53 1 38 39
EGADS : 145 0 Yes 62 56 1 40 41
EGADS : 146 0 Yes 61 57 1 41 42
EGADS : 147 0 Yes 98 65 1 44 45
EGADS : 148 0 Yes 66 99 1 44 45
EGADS : 149 0 Yes 99 100 1 44 64
EGADS : 150 0 Yes 101 100 1 44 45
EGADS : 151 0 Yes 98 101 1 44 64
EGADS : 152 0 Yes 99 100 1 45 65
EGADS : 153 0 Yes 98 101 1 45 65
EGADS : 154 0 Yes 97 96 1 46 63
EGADS : 155 0 Yes 95 102 1 46 62
EGADS : 156 0 Yes 103 102 1 46 61
EGADS : 157 0 Yes 92 103 1 46 60
EGADS : 158 0 Yes 71 75 1 48 49
EGADS : 159 0 Yes 72 74 1 49 50
EGADS : 160 0 Yes 79 91 1 52 53
EGADS : 161 0 Yes 80 90 1 53 54
EGADS : 162 0 Yes 83 89 1 55 56
EGADS : 163 0 Yes 84 88 1 56 57
EGADS : 164 0 Yes 104 87 1 58 59
EGADS : 165 0 Yes 86 105 1 58 59
EGADS : 166 0 Yes 105 106 1 58 66
EGADS : 167 0 Yes 107 106 1 58 59
EGADS : 168 0 Yes 104 107 1 58 66
EGADS : 169 0 Yes 105 106 1 59 67
EGADS : 170 0 Yes 104 107 1 59 67
EGADS : 171 0 Yes 93 103 1 60 61
EGADS : 172 0 Yes 94 102 1 61 62
EGADS : 173 0 Yes 99 98 1 64 65
EGADS : 174 0 Yes 100 101 1 64 65
EGADS : 175 0 Yes 105 104 1 66 67
EGADS : 176 0 Yes 106 107 1 66 67
EGADS : 177 1 Yes 108 109 1 68 69
EGADS : 178 1 Yes 109 110 1 68 70
EGADS : 179 1 Yes 111 110 1 68 71
EGADS : 180 1 Yes 108 111 1 68 72
EGADS : 181 1 Yes 109 112 1 69 70
EGADS : 182 1 Yes 112 108 1 69 72
EGADS : 183 1 Yes 110 113 1 70 71
EGADS : 184 1 Yes 112 113 1 70 72
EGADS : 185 1 Yes 113 111 1 71 72
EGADS : 186 2 Yes 114 115 1 73 74
EGADS : 187 2 Yes 115 116 1 73 75
EGADS : 188 2 Yes 117 116 1 73 76
EGADS : 189 2 Yes 114 117 1 73 77
EGADS : 190 2 Yes 115 118 1 74 75
EGADS : 191 2 Yes 118 114 1 74 77
EGADS : 192 2 Yes 116 119 1 75 76
EGADS : 193 2 Yes 118 119 1 75 77
EGADS : 194 2 Yes 119 117 1 76 77
EGADS : 195 3 Yes 120 121 1 78 79
EGADS : 196 3 Yes 121 122 1 78 80
EGADS : 197 3 Yes 123 122 1 78 81
EGADS : 198 3 Yes 120 123 1 78 82
EGADS : 199 3 Yes 121 124 1 79 80
EGADS : 200 3 Yes 124 120 1 79 82
EGADS : 201 3 Yes 122 125 1 80 81
EGADS : 202 3 Yes 124 125 1 80 82
EGADS : 203 3 Yes 125 123 1 81 82
EGADS : 204 4 Yes 126 127 1 83 84
EGADS : 205 4 Yes 128 127 1 83 85
EGADS : 206 4 Yes 129 128 1 83 86
EGADS : 207 4 Yes 129 126 1 83 87
EGADS : 208 4 Yes 126 130 1 84 87
EGADS : 209 4 Yes 130 131 1 84 86
EGADS : 210 4 Yes 127 131 1 84 85
EGADS : 211 4 Yes 131 128 1 85 86
EGADS : 212 4 Yes 130 129 1 86 87
EGADS : 213 5 Yes 132 133 1 88 89
EGADS : 214 5 Yes 134 133 1 88 90
EGADS : 215 5 Yes 135 134 1 88 91
EGADS : 216 5 Yes 135 132 1 88 92
EGADS : 217 5 Yes 132 136 1 89 92
EGADS : 218 5 Yes 136 137 1 89 91
EGADS : 219 5 Yes 133 137 1 89 90
EGADS : 220 5 Yes 137 134 1 90 91
EGADS : 221 5 Yes 136 135 1 91 92
EGADS : 222 6 Yes 138 139 1 93 94
EGADS : 223 6 Yes 140 138 1 93 95
EGADS : 224 6 Yes 140 141 1 93 96
EGADS : 225 6 Yes 141 139 1 93 97
EGADS : 226 6 Yes 142 138 1 94 95
EGADS : 227 6 Yes 139 142 1 94 97
EGADS : 228 6 Yes 143 142 1 95 97
EGADS : 229 6 Yes 143 140 1 95 96
EGADS : 230 6 Yes 141 143 1 96 97
EGADS : 231 7 Yes 144 145 1 98 99
EGADS : 232 7 Yes 144 146 1 98 100
EGADS : 233 7 Yes 146 147 1 98 101
EGADS : 234 7 Yes 145 147 1 98 102
EGADS : 235 7 Yes 148 145 1 99 102
EGADS : 236 7 Yes 149 148 1 99 101
EGADS : 237 7 Yes 149 144 1 99 100
EGADS : 238 7 Yes 146 149 1 100 101
EGADS : 239 7 Yes 147 148 1 101 102
EGADS : 240 8 Yes 150 151 1 103 104
EGADS : 241 8 Yes 152 151 1 103 105
EGADS : 242 8 Yes 153 152 1 103 106
EGADS : 243 8 Yes 153 150 1 103 107
EGADS : 244 8 Yes 150 154 1 104 107
EGADS : 245 8 Yes 154 155 1 104 106
EGADS : 246 8 Yes 151 155 1 104 105
EGADS : 247 8 Yes 155 152 1 105 106
EGADS : 248 8 Yes 154 153 1 106 107
EGADS : 249 9 Yes 156 157 1 108 109
EGADS : 250 9 Yes 158 157 1 108 110
EGADS : 251 9 Yes 159 158 1 108 111
EGADS : 252 9 Yes 159 156 1 108 112
EGADS : 253 9 Yes 156 160 1 109 112
EGADS : 254 9 Yes 160 161 1 109 111
EGADS : 255 9 Yes 157 161 1 109 110
EGADS : 256 9 Yes 158 161 1 110 111
EGADS : 257 9 Yes 159 160 1 111 112
EGADS : 258 10 Yes 163 162 NA 113 115
EGADS : 259 10 Yes 162 164 NA 113 118
EGADS : 260 10 Yes 165 164 NA 113 116
EGADS : 261 10 Yes 163 165 NA 113 117
EGADS : 262 10 Yes 167 166 NA 114 115
EGADS : 263 10 Yes 166 168 NA 114 118
EGADS : 264 10 Yes 169 168 NA 114 116
EGADS : 265 10 Yes 167 169 NA 114 117
EGADS : 266 10 Yes 163 167 NA 115 117
EGADS : 267 10 Yes 162 166 NA 115 118
EGADS : 268 10 Yes 165 169 NA 116 117
EGADS : 269 10 Yes 164 168 NA 116 118
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 121.026192 0 0
EGADS : 3 Yes 121.026192 10 0
EGADS : 4 Yes 54.9020417 7.00084115 0
EGADS : 5 Yes 97.361045 7.90366896 0
EGADS : 6 Yes 121.026192 0 0
EGADS : 7 Yes 97.361045 0 0
EGADS : 8 Yes 54.9020417 0 0
EGADS : 9 Yes 165.026192 0 7
EGADS : 10 Yes 165.026192 0.5 8.5
EGADS : 11 Yes 156.577382 2.32417494 6.86784347
EGADS : 12 Yes 160.457816 1.16501909 6.24763245
EGADS : 13 Yes 152.092394 3.29252447 6.00142548
EGADS : 14 Yes 121.026192 0 10
EGADS : 15 Yes 97.4729828 13.4242093 0
EGADS : 16 Yes 93.4296648 13.4242093 0
EGADS : 17 Yes 93.813734 32.4820648 0
EGADS : 18 Yes 97.8594113 32.4820648 0
EGADS : 19 Yes 97.9335611 36.1389817 0
EGADS : 20 Yes 75.3047874 36.1389817 0
EGADS : 21 Yes 93.813734 32.4820648 0
EGADS : 22 Yes 93.4296648 13.4242093 0
EGADS : 23 Yes 72.4759225 29.3018771 0
EGADS : 24 Yes 83.5054156 29.3018771 0
EGADS : 25 Yes 152.092394 0 6.00142548
EGADS : 26 Yes 160.457816 0 6.24763245
EGADS : 27 Yes 156.577382 0 6.86784347
EGADS : 28 Yes 165.026192 0 8.5
EGADS : 29 Yes 75.3047874 0 0
EGADS : 30 Yes 97.9335611 0 0
EGADS : 31 Yes 97.8594113 0 0
EGADS : 32 Yes 93.813734 0 0
EGADS : 33 Yes 93.4296648 0 0
EGADS : 34 Yes 97.4729828 0 0
EGADS : 35 Yes 72.4759225 0 0
EGADS : 36 Yes 83.5054156 0 0
EGADS : 37 Yes 93.4296648 0 0
EGADS : 38 Yes 93.813734 0 0
EGADS : 39 Yes 165.026192 0 10
EGADS : 40 Yes 139.227902 5.03861756 7.07099122
EGADS : 41 Yes 159.822328 0 10
EGADS : 42 Yes 137.454662 0 10
EGADS : 43 Yes 162.492237 6.6562396 7.4148274
EGADS : 44 Yes 153.156875 6.6562396 8.10980625
EGADS : 45 Yes 168.687412 34.4921381 13.6297335
EGADS : 46 Yes 172.805054 34.4921381 13.3315303
EGADS : 47 Yes 173.282633 35.781198 13.6055284
EGADS : 48 Yes 165.02399 35.781198 13.6055284
EGADS : 49 Yes 168.687412 34.4921381 13.033327
EGADS : 50 Yes 153.156875 6.6562396 6.71984855
EGADS : 51 Yes 100.269362 41.7493571 0
EGADS : 52 Yes 94.7284993 41.7493571 0
EGADS : 53 Yes 107.349293 67.6443173 1.84589548
EGADS : 54 Yes 111.050367 67.6443173 1.25578139
EGADS : 55 Yes 111.248847 68.1210465 1.31074802
EGADS : 56 Yes 107.581644 68.1210465 1.89111513
EGADS : 57 Yes 121.153699 95.9694651 4.50848923
EGADS : 58 Yes 122.843146 95.9694651 4.52165604
EGADS : 59 Yes 123.552357 97.6729236 4.7180639
EGADS : 60 Yes 118.391317 97.6729236 3.99272703
EGADS : 61 Yes 121.153699 95.9694651 4.20550678
EGADS : 62 Yes 107.581644 68.1210465 0.865881946
EGADS : 63 Yes 107.349293 67.6443173 0.808537183
EGADS : 64 Yes 94.7284993 41.7493571 0
EGADS : 65 Yes 79.4370049 29.3018771 0
EGADS : 66 Yes 70.524066 29.3018771 0
EGADS : 67 Yes 139.227902 0 7.07099122
EGADS : 68 Yes 165.02399 0 13.6055284
EGADS : 69 Yes 173.282633 0 13.6055284
EGADS : 70 Yes 172.805054 0 13.3315303
EGADS : 71 Yes 168.687412 0 13.033327
EGADS : 72 Yes 153.156875 0 6.71984855
EGADS : 73 Yes 162.492237 0 7.4148274
EGADS : 74 Yes 153.156875 0 8.10980625
EGADS : 75 Yes 168.687412 0 13.6297335
EGADS : 76 Yes 118.391317 0 3.99272703
EGADS : 77 Yes 123.552357 0 4.7180639
EGADS : 78 Yes 122.843146 0 4.52165604
EGADS : 79 Yes 121.153699 0 4.20550678
EGADS : 80 Yes 107.581644 0 0.865881946
EGADS : 81 Yes 111.248847 0 1.31074802
EGADS : 82 Yes 111.050367 0 1.25578139
EGADS : 83 Yes 107.349293 0 0.808537183
EGADS : 84 Yes 94.7284993 0 0
EGADS : 85 Yes 100.269362 0 0
EGADS : 86 Yes 70.524066 0 0
EGADS : 87 Yes 79.4370049 0 0
EGADS : 88 Yes 94.7284993 0 0
EGADS : 89 Yes 107.349293 0 1.84589548
EGADS : 90 Yes 107.581644 0 1.89111513
EGADS : 91 Yes 121.153699 0 4.50848923
EGADS : 92 Yes 160.542569 0 11.9206428
EGADS : 93 Yes 151.486032 0.673415422 11.9206428
EGADS : 94 Yes 165.862466 0.235428105 34.9229244
EGADS : 95 Yes 169.168425 0 34.9229244
EGADS : 96 Yes 169.38016 0 35.487551
EGADS : 97 Yes 162.942213 0 35.487551
EGADS : 98 Yes 90.5173952 29.3018771 0
EGADS : 99 Yes 60.5173952 29.3018771 0
EGADS : 100 Yes 60.5173952 29.3018771 0
EGADS : 101 Yes 90.5173952 29.3018771 0
EGADS : 102 Yes 165.862466 0 34.9229244
EGADS : 103 Yes 151.486032 0 11.9206428
EGADS : 104 Yes 90.5173952 0 0
EGADS : 105 Yes 60.5173952 0 0
EGADS : 106 Yes 60.5173952 0 0
EGADS : 107 Yes 90.5173952 0 0
EGADS : 108 Yes 111.321903 0 1.86654259
EGADS : 109 Yes 108.055298 0 0.93793256
EGADS : 110 Yes 121.33061 0 4.22828065
EGADS : 111 Yes 122.700876 0 4.71377572
EGADS : 112 Yes 107.907885 0 1.87632098
EGADS : 113 Yes 121.289329 0 4.49106118
EGADS : 114 Yes 100.394138 0 0
EGADS : 115 Yes 95.1284577 0 0
EGADS : 116 Yes 107.505559 0 0.813039939
EGADS : 117 Yes 110.968457 0 0.689237814
EGADS : 118 Yes 95.3800953 0 0
EGADS : 119 Yes 107.657908 0 1.77558767
EGADS : 120 Yes 97.2857328 0 0
EGADS : 121 Yes 93.6847537 0 0
EGADS : 122 Yes 94.0587466 0 0
EGADS : 123 Yes 97.7824572 0 0
EGADS : 124 Yes 93.9345512 0 0
EGADS : 125 Yes 94.3601422 0 0
EGADS : 126 Yes 97.2857328 13.7821489 0
EGADS : 127 Yes 97.7824572 32.3393376 0
EGADS : 128 Yes 94.3601422 32.2302343 0
EGADS : 129 Yes 93.9345512 13.6726922 0
EGADS : 130 Yes 93.6847537 13.6742093 0
EGADS : 131 Yes 94.0587466 32.2320648 0
EGADS : 132 Yes 100.394138 42.0879216 0
EGADS : 133 Yes 110.968457 67.4483237 0.689237814
EGADS : 134 Yes 107.657908 67.3218336 1.77558767
EGADS : 135 Yes 95.3800953 41.8796344 0
EGADS : 136 Yes 95.1284577 41.9993571 0
EGADS : 137 Yes 107.505559 67.3943173 0.813039939
EGADS : 138 Yes 121.330781 95.7095395 4.49106118
EGADS : 139 Yes 122.742253 95.7419985 4.26970731
EGADS : 140 Yes 108.055908 68.3356022 1.87632098
EGADS : 141 Yes 111.300912 68.4526045 0.818951249
EGADS : 142 Yes 121.289158 95.7293907 4.22828065
EGADS : 143 Yes 107.907275 68.4064908 0.93793256
EGADS : 144 Yes 162.652062 0 6.87525931
EGADS : 145 Yes 172.609142 0 12.9541609
EGADS : 146 Yes 153.959016 0 6.86654493
EGADS : 147 Yes 168.960275 0 12.950503
EGADS : 148 Yes 169.001731 0 13.500001
EGADS : 149 Yes 154.05778 0 8.17566644
EGADS : 150 Yes 162.652062 7.30770007 6.87525931
EGADS : 151 Yes 172.609142 34.0557129 12.9541609
EGADS : 152 Yes 169.001731 33.980789 13.500001
EGADS : 153 Yes 154.05778 7.12920153 8.17566644
EGADS : 154 Yes 153.959016 7.18327767 6.86654493
EGADS : 155 Yes 168.960275 34.0034872 12.950503
EGADS : 156 Yes 160.730069 0 12.4206428
EGADS : 157 Yes 168.980925 0 34.4229244
EGADS : 158 Yes 166.139589 0.215327731 34.4229244
EGADS : 159 Yes 152.388156 0.632183325 12.4206428
EGADS : 160 Yes 152.388156 0 12.4206428
EGADS : 161 Yes 166.139589 0 34.4229244
EGADS : 162 Yes 0 0 1962.43554
EGADS : 163 Yes 0 0 0
EGADS : 164 Yes 0 1953.45847 1962.43554
EGADS : 165 Yes 0 1953.45847 0
EGADS : 166 Yes 2040.09979 0 1962.43554
EGADS : 167 Yes 2040.09979 0 0
EGADS : 168 Yes 2040.09979 1953.45847 1962.43554
EGADS : 169 Yes 2040.09979 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 53.021
AFLR4 : Reference Length = 53.021
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 428.462
AFLR4 : Abs Min Surf Spacing = 0.132552
AFLR4 : Min Surf Spacing = 0.265105
AFLR4 : Max Surf Spacing = 5.3021
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : 23 CAD geometry 0 STD w/BL
AFLR4 : 24 CAD geometry 0 STD w/BL
AFLR4 : 25 CAD geometry 0 STD w/BL
AFLR4 : 26 CAD geometry 0 STD w/BL
AFLR4 : 27 CAD geometry 0 STD w/BL
AFLR4 : 28 CAD geometry 0 STD w/BL
AFLR4 : 29 CAD geometry 0 STD w/BL
AFLR4 : 30 CAD geometry 0 STD w/BL
AFLR4 : 31 CAD geometry 0 STD w/BL
AFLR4 : 32 CAD geometry 0 STD w/BL
AFLR4 : 33 CAD geometry 0 STD w/BL
AFLR4 : 34 CAD geometry 0 STD w/BL
AFLR4 : 35 CAD geometry 0 STD w/BL
AFLR4 : 36 CAD geometry 0 STD w/BL
AFLR4 : 37 CAD geometry 0 STD w/BL
AFLR4 : 38 CAD geometry 0 STD w/BL
AFLR4 : 39 CAD geometry 0 STD w/BL
AFLR4 : 40 CAD geometry 0 STD w/BL
AFLR4 : 41 CAD geometry 0 STD w/BL
AFLR4 : 42 CAD geometry 0 STD w/BL
AFLR4 : 43 CAD geometry 0 STD w/BL
AFLR4 : 44 CAD geometry 0 STD w/BL
AFLR4 : 45 CAD geometry 0 STD w/BL
AFLR4 : 46 CAD geometry 0 STD w/BL
AFLR4 : 47 CAD geometry 0 STD w/BL
AFLR4 : 48 CAD geometry 0 STD w/BL
AFLR4 : 49 CAD geometry 0 STD w/BL
AFLR4 : 50 CAD geometry 0 STD w/BL
AFLR4 : 51 CAD geometry 0 STD w/BL
AFLR4 : 52 CAD geometry 0 STD w/BL
AFLR4 : 53 CAD geometry 0 STD w/BL
AFLR4 : 54 CAD geometry 0 STD w/BL
AFLR4 : 55 CAD geometry 0 STD w/BL
AFLR4 : 56 CAD geometry 0 STD w/BL
AFLR4 : 57 CAD geometry 0 STD w/BL
AFLR4 : 58 CAD geometry 0 STD w/BL
AFLR4 : 59 CAD geometry 0 STD w/BL
AFLR4 : 60 CAD geometry 0 STD w/BL
AFLR4 : 61 CAD geometry 0 STD w/BL
AFLR4 : 62 CAD geometry 0 STD w/BL
AFLR4 : 63 CAD geometry 0 STD w/BL
AFLR4 : 64 CAD geometry 0 STD w/BL
AFLR4 : 65 CAD geometry 0 STD w/BL
AFLR4 : 66 CAD geometry 0 STD w/BL
AFLR4 : 67 CAD geometry 0 STD w/BL
AFLR4 : 68 CAD geometry 0 STD w/BL
AFLR4 : 69 CAD geometry 0 STD w/BL
AFLR4 : 70 CAD geometry 0 STD w/BL
AFLR4 : 71 CAD geometry 0 STD w/BL
AFLR4 : 72 CAD geometry 0 STD w/BL
AFLR4 : 73 CAD geometry 0 STD w/BL
AFLR4 : 74 CAD geometry 0 STD w/BL
AFLR4 : 75 CAD geometry 0 STD w/BL
AFLR4 : 76 CAD geometry 0 STD w/BL
AFLR4 : 77 CAD geometry 0 STD w/BL
AFLR4 : 78 CAD geometry 0 STD w/BL
AFLR4 : 79 CAD geometry 0 STD w/BL
AFLR4 : 80 CAD geometry 0 STD w/BL
AFLR4 : 81 CAD geometry 0 STD w/BL
AFLR4 : 82 CAD geometry 0 STD w/BL
AFLR4 : 83 CAD geometry 0 STD w/BL
AFLR4 : 84 CAD geometry 0 STD w/BL
AFLR4 : 85 CAD geometry 0 STD w/BL
AFLR4 : 86 CAD geometry 0 STD w/BL
AFLR4 : 87 CAD geometry 0 STD w/BL
AFLR4 : 88 CAD geometry 0 STD w/BL
AFLR4 : 89 CAD geometry 0 STD w/BL
AFLR4 : 90 CAD geometry 0 STD w/BL
AFLR4 : 91 CAD geometry 0 STD w/BL
AFLR4 : 92 CAD geometry 0 STD w/BL
AFLR4 : 93 CAD geometry 0 STD w/BL
AFLR4 : 94 CAD geometry 0 STD w/BL
AFLR4 : 95 CAD geometry 0 STD w/BL
AFLR4 : 96 CAD geometry 0 STD w/BL
AFLR4 : 97 CAD geometry 0 STD w/BL
AFLR4 : 98 CAD geometry 0 STD w/BL
AFLR4 : 99 CAD geometry 0 STD w/BL
AFLR4 : 100 CAD geometry 0 STD w/BL
AFLR4 : 101 CAD geometry 0 STD w/BL
AFLR4 : 102 CAD geometry 0 STD w/BL
AFLR4 : 103 CAD geometry 0 STD w/BL
AFLR4 : 104 CAD geometry 0 STD w/BL
AFLR4 : 105 CAD geometry 0 STD w/BL
AFLR4 : 106 CAD geometry 0 STD w/BL
AFLR4 : 107 CAD geometry 0 STD w/BL
AFLR4 : 108 CAD geometry 0 STD w/BL
AFLR4 : 109 CAD geometry 0 STD w/BL
AFLR4 : 110 CAD geometry 0 STD w/BL
AFLR4 : 111 CAD geometry 0 STD w/BL
AFLR4 : 112 CAD geometry 0 STD w/BL
AFLR4 : 113 CAD geometry 0 FARFIELD
AFLR4 : 114 CAD geometry 0 FARFIELD
AFLR4 : 115 CAD geometry 0 FARFIELD
AFLR4 : 116 CAD geometry 0 FARFIELD
AFLR4 : 117 CAD geometry 0 FARFIELD
AFLR4 : 118 CAD geometry 0 FARFIELD
AFLR4 : Case has 10 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 7 8 11 12 22
AFLR4 : Component 2 includes Definitions 5 6 9 10 15 16 17 18 19 25 26 27 28
AFLR4 : 31 37 38 39 40 41 42 43 51 52 53 54
AFLR4 : 55 56 57 68 69 70 71 72 73 77 78 82
AFLR4 : 83 84 88 89 93 97
AFLR4 : Component 3 includes Definitions 13 14 23 24 33 34 35 36 47 48 49 50
AFLR4 : 74 75 76 98 99 103 104
AFLR4 : Component 4 includes Definitions 32 46 60 61 62 63 79 80 81 108 109
AFLR4 : Component 5 includes Definitions 44 45 58 59 64 65 66 67 85 86 87
AFLR4 : Component 6 includes Definitions 20 21 29 30 90 91 92
AFLR4 : Component 7 includes Definitions 94 95 96
AFLR4 : Component 8 includes Definitions 100 101 102
AFLR4 : Component 9 includes Definitions 105 106 107
AFLR4 : Component 10 includes Definitions 110 111 112
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR4 : Define CAD surface definition 25
AFLR4 : Define CAD surface definition 26
AFLR4 : Define CAD surface definition 27
AFLR4 : Define CAD surface definition 28
AFLR4 : Define CAD surface definition 29
AFLR4 : Define CAD surface definition 30
AFLR4 : Define CAD surface definition 31
AFLR4 : Define CAD surface definition 32
AFLR4 : Define CAD surface definition 33
AFLR4 : Define CAD surface definition 34
AFLR4 : Define CAD surface definition 35
AFLR4 : Define CAD surface definition 36
AFLR4 : Define CAD surface definition 37
AFLR4 : Define CAD surface definition 38
AFLR4 : Define CAD surface definition 39
AFLR4 : Define CAD surface definition 40
AFLR4 : Define CAD surface definition 41
AFLR4 : Define CAD surface definition 42
AFLR4 : Define CAD surface definition 43
AFLR4 : Define CAD surface definition 44
AFLR4 : Define CAD surface definition 45
AFLR4 : Define CAD surface definition 46
AFLR4 : Define CAD surface definition 47
AFLR4 : Define CAD surface definition 48
AFLR4 : Define CAD surface definition 49
AFLR4 : Define CAD surface definition 50
AFLR4 : Define CAD surface definition 51
AFLR4 : Define CAD surface definition 52
AFLR4 : Define CAD surface definition 53
AFLR4 : Define CAD surface definition 54
AFLR4 : Define CAD surface definition 55
AFLR4 : Define CAD surface definition 56
AFLR4 : Define CAD surface definition 57
AFLR4 : Define CAD surface definition 58
AFLR4 : Define CAD surface definition 59
AFLR4 : Define CAD surface definition 60
AFLR4 : Define CAD surface definition 61
AFLR4 : Define CAD surface definition 62
AFLR4 : Define CAD surface definition 63
AFLR4 : Define CAD surface definition 64
AFLR4 : Define CAD surface definition 65
AFLR4 : Define CAD surface definition 66
AFLR4 : Define CAD surface definition 67
AFLR4 : Define CAD surface definition 68
AFLR4 : Define CAD surface definition 69
AFLR4 : Define CAD surface definition 70
AFLR4 : Define CAD surface definition 71
AFLR4 : Define CAD surface definition 72
AFLR4 : Define CAD surface definition 73
AFLR4 : Define CAD surface definition 74
AFLR4 : Define CAD surface definition 75
AFLR4 : Define CAD surface definition 76
AFLR4 : Define CAD surface definition 77
AFLR4 : Define CAD surface definition 78
AFLR4 : Define CAD surface definition 79
AFLR4 : Define CAD surface definition 80
AFLR4 : Define CAD surface definition 81
AFLR4 : Define CAD surface definition 82
AFLR4 : Define CAD surface definition 83
AFLR4 : Define CAD surface definition 84
AFLR4 : Define CAD surface definition 85
AFLR4 : Define CAD surface definition 86
AFLR4 : Define CAD surface definition 87
AFLR4 : Define CAD surface definition 88
AFLR4 : Define CAD surface definition 89
AFLR4 : Define CAD surface definition 90
AFLR4 : Define CAD surface definition 91
AFLR4 : Define CAD surface definition 92
AFLR4 : Define CAD surface definition 93
AFLR4 : Define CAD surface definition 94
AFLR4 : Define CAD surface definition 95
AFLR4 : Define CAD surface definition 96
AFLR4 : Define CAD surface definition 97
AFLR4 : Define CAD surface definition 98
AFLR4 : Define CAD surface definition 99
AFLR4 : Define CAD surface definition 100
AFLR4 : Define CAD surface definition 101
AFLR4 : Define CAD surface definition 102
AFLR4 : Define CAD surface definition 103
AFLR4 : Define CAD surface definition 104
AFLR4 : Define CAD surface definition 105
AFLR4 : Define CAD surface definition 106
AFLR4 : Define CAD surface definition 107
AFLR4 : Define CAD surface definition 108
AFLR4 : Define CAD surface definition 109
AFLR4 : Define CAD surface definition 110
AFLR4 : Define CAD surface definition 111
AFLR4 : Define CAD surface definition 112
AFLR4 : Define CAD surface definition 113
AFLR4 : Define CAD surface definition 114
AFLR4 : Define CAD surface definition 115
AFLR4 : Define CAD surface definition 116
AFLR4 : Define CAD surface definition 117
AFLR4 : Define CAD surface definition 118
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 103724
AFLR43 : Nodes = 51880
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mbl = 1
UG PARAM : nbl = 5
UG PARAM : mblelc = 2
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mbl = 1
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mblelc = 1
UG PARAM : BC_IDs [ 0]= 1
UG PARAM : BC_IDs [ 1]= 2
UG PARAM : BC_IDs [ 2]= 3
UG PARAM : BC_IDs [ 3]= 4
UG PARAM : BC_IDs [ 4]= 5
UG PARAM : BC_IDs [ 5]= 6
UG PARAM : BC_IDs [ 6]= 7
UG PARAM : BC_IDs [ 7]= 8
UG PARAM : BC_IDs [ 8]= 9
UG PARAM : BC_IDs [ 9]= 10
UG PARAM : BC_IDs [10]= 11
UG PARAM : BC_IDs [11]= 12
UG PARAM : BC_IDs [12]= 13
UG PARAM : BC_IDs [13]= 14
UG PARAM : BC_IDs [14]= 15
UG PARAM : BC_IDs [15]= 16
UG PARAM : BC_IDs [16]= 17
UG PARAM : BC_IDs [17]= 18
UG PARAM : BC_IDs [18]= 19
UG PARAM : BC_IDs [19]= 20
UG PARAM : BC_IDs [20]= 21
UG PARAM : BC_IDs [21]= 22
UG PARAM : BC_IDs [22]= 23
UG PARAM : BC_IDs [23]= 24
UG PARAM : BC_IDs [24]= 25
UG PARAM : BC_IDs [25]= 26
UG PARAM : BC_IDs [26]= 27
UG PARAM : BC_IDs [27]= 28
UG PARAM : BC_IDs [28]= 29
UG PARAM : BC_IDs [29]= 30
UG PARAM : BC_IDs [30]= 31
UG PARAM : BC_IDs [31]= 32
UG PARAM : BC_IDs [32]= 33
UG PARAM : BC_IDs [33]= 34
UG PARAM : BC_IDs [34]= 35
UG PARAM : BC_IDs [35]= 36
UG PARAM : BC_IDs [36]= 37
UG PARAM : BC_IDs [37]= 38
UG PARAM : BC_IDs [38]= 39
UG PARAM : BC_IDs [39]= 40
UG PARAM : BC_IDs [40]= 41
UG PARAM : BC_IDs [41]= 42
UG PARAM : BC_IDs [42]= 43
UG PARAM : BC_IDs [43]= 44
UG PARAM : BC_IDs [44]= 45
UG PARAM : BC_IDs [45]= 46
UG PARAM : BC_IDs [46]= 47
UG PARAM : BC_IDs [47]= 48
UG PARAM : BC_IDs [48]= 49
UG PARAM : BC_IDs [49]= 50
UG PARAM : BC_IDs [50]= 51
UG PARAM : BC_IDs [51]= 52
UG PARAM : BC_IDs [52]= 53
UG PARAM : BC_IDs [53]= 54
UG PARAM : BC_IDs [54]= 55
UG PARAM : BC_IDs [55]= 56
UG PARAM : BC_IDs [56]= 57
UG PARAM : BC_IDs [57]= 58
UG PARAM : BC_IDs [58]= 59
UG PARAM : BC_IDs [59]= 60
UG PARAM : BC_IDs [60]= 61
UG PARAM : BC_IDs [61]= 62
UG PARAM : BC_IDs [62]= 63
UG PARAM : BC_IDs [63]= 64
UG PARAM : BC_IDs [64]= 65
UG PARAM : BC_IDs [65]= 66
UG PARAM : BC_IDs [66]= 67
UG PARAM : BC_IDs [67]= 68
UG PARAM : BC_IDs [68]= 69
UG PARAM : BC_IDs [69]= 70
UG PARAM : BC_IDs [70]= 71
UG PARAM : BC_IDs [71]= 72
UG PARAM : BC_IDs [72]= 73
UG PARAM : BC_IDs [73]= 74
UG PARAM : BC_IDs [74]= 75
UG PARAM : BC_IDs [75]= 76
UG PARAM : BC_IDs [76]= 77
UG PARAM : BC_IDs [77]= 78
UG PARAM : BC_IDs [78]= 79
UG PARAM : BC_IDs [79]= 80
UG PARAM : BC_IDs [80]= 81
UG PARAM : BC_IDs [81]= 82
UG PARAM : BC_IDs [82]= 83
UG PARAM : BC_IDs [83]= 84
UG PARAM : BC_IDs [84]= 85
UG PARAM : BC_IDs [85]= 86
UG PARAM : BC_IDs [86]= 87
UG PARAM : BC_IDs [87]= 88
UG PARAM : BC_IDs [88]= 89
UG PARAM : BC_IDs [89]= 90
UG PARAM : BC_IDs [90]= 91
UG PARAM : BC_IDs [91]= 92
UG PARAM : BC_IDs [92]= 93
UG PARAM : BC_IDs [93]= 94
UG PARAM : BC_IDs [94]= 95
UG PARAM : BC_IDs [95]= 96
UG PARAM : BC_IDs [96]= 97
UG PARAM : BC_IDs [97]= 98
UG PARAM : BC_IDs [98]= 99
UG PARAM : BC_IDs [99]= 100
UG PARAM : BC_IDs [117]= 118
UG PARAM : BL_DS [ 0]= 0.434102
UG PARAM : BL_DS [ 1]= 0.434102
UG PARAM : BL_DS [ 2]= 0.434102
UG PARAM : BL_DS [ 3]= 0.434102
UG PARAM : BL_DS [ 4]= 0.434102
UG PARAM : BL_DS [ 5]= 0.434102
UG PARAM : BL_DS [ 6]= 0.434102
UG PARAM : BL_DS [ 7]= 0.434102
UG PARAM : BL_DS [ 8]= 0.434102
UG PARAM : BL_DS [ 9]= 0.434102
UG PARAM : BL_DS [10]= 0.434102
UG PARAM : BL_DS [11]= 0.434102
UG PARAM : BL_DS [12]= 0.434102
UG PARAM : BL_DS [13]= 0.434102
UG PARAM : BL_DS [14]= 0.434102
UG PARAM : BL_DS [15]= 0.434102
UG PARAM : BL_DS [16]= 0.434102
UG PARAM : BL_DS [17]= 0.434102
UG PARAM : BL_DS [18]= 0.434102
UG PARAM : BL_DS [19]= 0.434102
UG PARAM : BL_DS [20]= 0.434102
UG PARAM : BL_DS [21]= 0.434102
UG PARAM : BL_DS [22]= 0.434102
UG PARAM : BL_DS [23]= 0.434102
UG PARAM : BL_DS [24]= 0.434102
UG PARAM : BL_DS [25]= 0.434102
UG PARAM : BL_DS [26]= 0.434102
UG PARAM : BL_DS [27]= 0.434102
UG PARAM : BL_DS [28]= 0.434102
UG PARAM : BL_DS [29]= 0.434102
UG PARAM : BL_DS [30]= 0.434102
UG PARAM : BL_DS [31]= 0.434102
UG PARAM : BL_DS [32]= 0.434102
UG PARAM : BL_DS [33]= 0.434102
UG PARAM : BL_DS [34]= 0.434102
UG PARAM : BL_DS [35]= 0.434102
UG PARAM : BL_DS [36]= 0.434102
UG PARAM : BL_DS [37]= 0.434102
UG PARAM : BL_DS [38]= 0.434102
UG PARAM : BL_DS [39]= 0.434102
UG PARAM : BL_DS [40]= 0.434102
UG PARAM : BL_DS [41]= 0.434102
UG PARAM : BL_DS [42]= 0.434102
UG PARAM : BL_DS [43]= 0.434102
UG PARAM : BL_DS [44]= 0.434102
UG PARAM : BL_DS [45]= 0.434102
UG PARAM : BL_DS [46]= 0.434102
UG PARAM : BL_DS [47]= 0.434102
UG PARAM : BL_DS [48]= 0.434102
UG PARAM : BL_DS [49]= 0.434102
UG PARAM : BL_DS [50]= 0.434102
UG PARAM : BL_DS [51]= 0.434102
UG PARAM : BL_DS [52]= 0.434102
UG PARAM : BL_DS [53]= 0.434102
UG PARAM : BL_DS [54]= 0.434102
UG PARAM : BL_DS [55]= 0.434102
UG PARAM : BL_DS [56]= 0.434102
UG PARAM : BL_DS [57]= 0.434102
UG PARAM : BL_DS [58]= 0.434102
UG PARAM : BL_DS [59]= 0.434102
UG PARAM : BL_DS [60]= 0.434102
UG PARAM : BL_DS [61]= 0.434102
UG PARAM : BL_DS [62]= 0.434102
UG PARAM : BL_DS [63]= 0.434102
UG PARAM : BL_DS [64]= 0.434102
UG PARAM : BL_DS [65]= 0.434102
UG PARAM : BL_DS [66]= 0.434102
UG PARAM : BL_DS [67]= 0.434102
UG PARAM : BL_DS [68]= 0.217051
UG PARAM : BL_DS [69]= 0.217051
UG PARAM : BL_DS [70]= 0.217051
UG PARAM : BL_DS [71]= 0.434102
UG PARAM : BL_DS [72]= 0.434102
UG PARAM : BL_DS [73]= 0.217051
UG PARAM : BL_DS [74]= 0.217051
UG PARAM : BL_DS [75]= 0.217051
UG PARAM : BL_DS [76]= 0.434102
UG PARAM : BL_DS [77]= 0.434102
UG PARAM : BL_DS [78]= 0.217051
UG PARAM : BL_DS [79]= 0.217051
UG PARAM : BL_DS [80]= 0.217051
UG PARAM : BL_DS [81]= 0.434102
UG PARAM : BL_DS [82]= 0.434102
UG PARAM : BL_DS [83]= 0.434102
UG PARAM : BL_DS [84]= 0.217051
UG PARAM : BL_DS [85]= 0.217051
UG PARAM : BL_DS [86]= 0.217051
UG PARAM : BL_DS [87]= 0.434102
UG PARAM : BL_DS [88]= 0.434102
UG PARAM : BL_DS [89]= 0.217051
UG PARAM : BL_DS [90]= 0.217051
UG PARAM : BL_DS [91]= 0.217051
UG PARAM : BL_DS [92]= 0.434102
UG PARAM : BL_DS [93]= 0.217051
UG PARAM : BL_DS [94]= 0.217051
UG PARAM : BL_DS [95]= 0.217051
UG PARAM : BL_DS [96]= 0.434102
UG PARAM : BL_DS [97]= 0.434102
UG PARAM : BL_DS [98]= 0.434102
UG PARAM : BL_DS [99]= 0.217051
UG PARAM : BL_DS [117]= 0
UG PARAM : BL_DEL [ 0]= 2.17051
UG PARAM : BL_DEL [ 1]= 2.17051
UG PARAM : BL_DEL [ 2]= 2.17051
UG PARAM : BL_DEL [ 3]= 2.17051
UG PARAM : BL_DEL [ 4]= 2.17051
UG PARAM : BL_DEL [ 5]= 2.17051
UG PARAM : BL_DEL [ 6]= 2.17051
UG PARAM : BL_DEL [ 7]= 2.17051
UG PARAM : BL_DEL [ 8]= 2.17051
UG PARAM : BL_DEL [ 9]= 2.17051
UG PARAM : BL_DEL [10]= 2.17051
UG PARAM : BL_DEL [11]= 2.17051
UG PARAM : BL_DEL [12]= 2.17051
UG PARAM : BL_DEL [13]= 2.17051
UG PARAM : BL_DEL [14]= 2.17051
UG PARAM : BL_DEL [15]= 2.17051
UG PARAM : BL_DEL [16]= 2.17051
UG PARAM : BL_DEL [17]= 2.17051
UG PARAM : BL_DEL [18]= 2.17051
UG PARAM : BL_DEL [19]= 2.17051
UG PARAM : BL_DEL [20]= 2.17051
UG PARAM : BL_DEL [21]= 2.17051
UG PARAM : BL_DEL [22]= 2.17051
UG PARAM : BL_DEL [23]= 2.17051
UG PARAM : BL_DEL [24]= 2.17051
UG PARAM : BL_DEL [25]= 2.17051
UG PARAM : BL_DEL [26]= 2.17051
UG PARAM : BL_DEL [27]= 2.17051
UG PARAM : BL_DEL [28]= 2.17051
UG PARAM : BL_DEL [29]= 2.17051
UG PARAM : BL_DEL [30]= 2.17051
UG PARAM : BL_DEL [31]= 2.17051
UG PARAM : BL_DEL [32]= 2.17051
UG PARAM : BL_DEL [33]= 2.17051
UG PARAM : BL_DEL [34]= 2.17051
UG PARAM : BL_DEL [35]= 2.17051
UG PARAM : BL_DEL [36]= 2.17051
UG PARAM : BL_DEL [37]= 2.17051
UG PARAM : BL_DEL [38]= 2.17051
UG PARAM : BL_DEL [39]= 2.17051
UG PARAM : BL_DEL [40]= 2.17051
UG PARAM : BL_DEL [41]= 2.17051
UG PARAM : BL_DEL [42]= 2.17051
UG PARAM : BL_DEL [43]= 2.17051
UG PARAM : BL_DEL [44]= 2.17051
UG PARAM : BL_DEL [45]= 2.17051
UG PARAM : BL_DEL [46]= 2.17051
UG PARAM : BL_DEL [47]= 2.17051
UG PARAM : BL_DEL [48]= 2.17051
UG PARAM : BL_DEL [49]= 2.17051
UG PARAM : BL_DEL [50]= 2.17051
UG PARAM : BL_DEL [51]= 2.17051
UG PARAM : BL_DEL [52]= 2.17051
UG PARAM : BL_DEL [53]= 2.17051
UG PARAM : BL_DEL [54]= 2.17051
UG PARAM : BL_DEL [55]= 2.17051
UG PARAM : BL_DEL [56]= 2.17051
UG PARAM : BL_DEL [57]= 2.17051
UG PARAM : BL_DEL [58]= 2.17051
UG PARAM : BL_DEL [59]= 2.17051
UG PARAM : BL_DEL [60]= 2.17051
UG PARAM : BL_DEL [61]= 2.17051
UG PARAM : BL_DEL [62]= 2.17051
UG PARAM : BL_DEL [63]= 2.17051
UG PARAM : BL_DEL [64]= 2.17051
UG PARAM : BL_DEL [65]= 2.17051
UG PARAM : BL_DEL [66]= 2.17051
UG PARAM : BL_DEL [67]= 2.17051
UG PARAM : BL_DEL [68]= 2.17051
UG PARAM : BL_DEL [69]= 2.17051
UG PARAM : BL_DEL [70]= 2.17051
UG PARAM : BL_DEL [71]= 2.17051
UG PARAM : BL_DEL [72]= 2.17051
UG PARAM : BL_DEL [73]= 2.17051
UG PARAM : BL_DEL [74]= 2.17051
UG PARAM : BL_DEL [75]= 2.17051
UG PARAM : BL_DEL [76]= 2.17051
UG PARAM : BL_DEL [77]= 2.17051
UG PARAM : BL_DEL [78]= 2.17051
UG PARAM : BL_DEL [79]= 2.17051
UG PARAM : BL_DEL [80]= 2.17051
UG PARAM : BL_DEL [81]= 2.17051
UG PARAM : BL_DEL [82]= 2.17051
UG PARAM : BL_DEL [83]= 2.17051
UG PARAM : BL_DEL [84]= 2.17051
UG PARAM : BL_DEL [85]= 2.17051
UG PARAM : BL_DEL [86]= 2.17051
UG PARAM : BL_DEL [87]= 2.17051
UG PARAM : BL_DEL [88]= 2.17051
UG PARAM : BL_DEL [89]= 2.17051
UG PARAM : BL_DEL [90]= 2.17051
UG PARAM : BL_DEL [91]= 2.17051
UG PARAM : BL_DEL [92]= 2.17051
UG PARAM : BL_DEL [93]= 2.17051
UG PARAM : BL_DEL [94]= 2.17051
UG PARAM : BL_DEL [95]= 2.17051
UG PARAM : BL_DEL [96]= 2.17051
UG PARAM : BL_DEL [97]= 2.17051
UG PARAM : BL_DEL [98]= 2.17051
UG PARAM : BL_DEL [99]= 2.17051
UG PARAM : BL_DEL [117]= 0
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 51880 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid w/BL
UG3 : 2 Solid w/BL
UG3 : 3 Solid w/BL
UG3 : 4 Solid w/BL
UG3 : 5 Solid w/BL
UG3 : 6 Solid w/BL
UG3 : 7 Solid w/BL
UG3 : 8 Solid w/BL
UG3 : 9 Solid w/BL
UG3 : 10 Solid w/BL
UG3 : 11 Solid w/BL
UG3 : 12 Solid w/BL
UG3 : 13 Solid w/BL
UG3 : 14 Solid w/BL
UG3 : 15 Solid w/BL
UG3 : 16 Solid w/BL
UG3 : 17 Solid w/BL
UG3 : 18 Solid w/BL
UG3 : 19 Solid w/BL
UG3 : 20 Solid w/BL
UG3 : 21 Solid w/BL
UG3 : 22 Solid w/BL
UG3 : 23 Solid w/BL
UG3 : 24 Solid w/BL
UG3 : 25 Solid w/BL
UG3 : 26 Solid w/BL
UG3 : 27 Solid w/BL
UG3 : 28 Solid w/BL
UG3 : 29 Solid w/BL
UG3 : 30 Solid w/BL
UG3 : 31 Solid w/BL
UG3 : 32 Solid w/BL
UG3 : 33 Solid w/BL
UG3 : 34 Solid w/BL
UG3 : 35 Solid w/BL
UG3 : 36 Solid w/BL
UG3 : 37 Solid w/BL
UG3 : 38 Solid w/BL
UG3 : 39 Solid w/BL
UG3 : 40 Solid w/BL
UG3 : 41 Solid w/BL
UG3 : 42 Solid w/BL
UG3 : 43 Solid w/BL
UG3 : 44 Solid w/BL
UG3 : 45 Solid w/BL
UG3 : 46 Solid w/BL
UG3 : 47 Solid w/BL
UG3 : 48 Solid w/BL
UG3 : 49 Solid w/BL
UG3 : 50 Solid w/BL
UG3 : 51 Solid w/BL
UG3 : 52 Solid w/BL
UG3 : 53 Solid w/BL
UG3 : 54 Solid w/BL
UG3 : 55 Solid w/BL
UG3 : 56 Solid w/BL
UG3 : 57 Solid w/BL
UG3 : 58 Solid w/BL
UG3 : 59 Solid w/BL
UG3 : 60 Solid w/BL
UG3 : 61 Solid w/BL
UG3 : 62 Solid w/BL
UG3 : 63 Solid w/BL
UG3 : 64 Solid w/BL
UG3 : 65 Solid w/BL
UG3 : 66 Solid w/BL
UG3 : 67 Solid w/BL
UG3 : 68 Solid w/BL
UG3 : 69 Solid w/BL
UG3 : 70 Solid w/BL
UG3 : 71 Solid w/BL
UG3 : 72 Solid w/BL
UG3 : 73 Solid w/BL
UG3 : 74 Solid w/BL
UG3 : 75 Solid w/BL
UG3 : 76 Solid w/BL
UG3 : 77 Solid w/BL
UG3 : 78 Solid w/BL
UG3 : 79 Solid w/BL
UG3 : 80 Solid w/BL
UG3 : 81 Solid w/BL
UG3 : 82 Solid w/BL
UG3 : 83 Solid w/BL
UG3 : 84 Solid w/BL
UG3 : 85 Solid w/BL
UG3 : 86 Solid w/BL
UG3 : 87 Solid w/BL
UG3 : 88 Solid w/BL
UG3 : 89 Solid w/BL
UG3 : 90 Solid w/BL
UG3 : 91 Solid w/BL
UG3 : 92 Solid w/BL
UG3 : 93 Solid w/BL
UG3 : 94 Solid w/BL
UG3 : 95 Solid w/BL
UG3 : 96 Solid w/BL
UG3 : 97 Solid w/BL
UG3 : 98 Solid w/BL
UG3 : 99 Solid w/BL
UG3 : 100 Solid w/BL
UG3 : 101 Solid w/BL
UG3 : 102 Solid w/BL
UG3 : 103 Solid w/BL
UG3 : 104 Solid w/BL
UG3 : 105 Solid w/BL
UG3 : 106 Solid w/BL
UG3 : 107 Solid w/BL
UG3 : 108 Solid w/BL
UG3 : 109 Solid w/BL
UG3 : 110 Solid w/BL
UG3 : 111 Solid w/BL
UG3 : 112 Solid w/BL
UG3 : 113 FarField
UG3 : 114 FarField
UG3 : 115 FarField
UG3 : 116 FarField
UG3 : 117 FarField
UG3 : 118 FarField
AFLR3 : CPU Time = 0.181 seconds
AFLR3 : DONE
ANBL3 : ---------------------------------------
ANBL3 : ANBL3 LIBRARY
ANBL3 : ADVANCING-NORMAL
ANBL3 : BOUNDARY-LAYER (BL)
ANBL3 : STRUCTURED-LAYER (SL)
ANBL3 : SPECIFIED NORMAL SPACING (SNS)
ANBL3 : TETRAHEDRAL/PENTAHEDRAL GRID GENERATOR
ANBL3 : Version Number 9.34.2
ANBL3 : Version Date 03/10/23 @ 04:32PM
ANBL3 : Compile OS Darwin 22.6.0 x86_64
ANBL3 : Compile Date 11/01/23 @ 12:20PM
ANBL3 : Copyright 1994-2021, D.L. Marcum
ANBL3 : ---------------------------------------
ANBL3 BLC: BL BOUNDARY CONDITIONS CHECK
ANBL3 BLC: Nodes, Elements = 51880 0
ANBL3 : CPU Time = 0.148 seconds
ANBL3 : DONE
ANBL3 BLG: BL NODE GENERATION
ANBL3 BLG: Nodes, Layer = 0 0
ANBL3 BLG: Nodes, Layer = 101726 2
ANBL3 BLG: Nodes, Layer = 148389 3
ANBL3 BLG: Nodes, Layer = 189603 4
ANBL3 BLG: Nodes, Layer = 225990 5
ANBL3 BLG: Nodes, Layer = 257451 6
ANBL3 : CPU Time = 50.109 seconds
ANBL3 : DONE
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 51880 0
AFLR3 : CPU Time = 0.094 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 51880 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 10378 68544
AFLR3 IG : Nodes, Elements = 20756 136739
AFLR3 IG : Nodes, Elements = 31134 203061
AFLR3 IG : Nodes, Elements = 41512 265677
AFLR3 IG : Nodes, Elements = 51887 338578
AFLR3 IG : Nodes, Elements = 51887 338579
AFLR3 IG : Nodes, Elements = 51887 337490
AFLR3 IG : Nodes, Elements = 51887 340041
AFLR3 IG : Nodes, Elements = 51887 336036
AFLR3 IG : Nodes, Elements = 51887 336037
AFLR3 IG : Nodes, Elements = 51887 335998
AFLR3 IG : Nodes, Elements = 51887 337035
AFLR3 IG : Nodes, Elements = 51887 337036
AFLR3 IG : Nodes, Elements = 51887 336992
AFLR3 IG : Nodes, Elements = 51887 333785
AFLR3 IG : Nodes, Elements = 51887 333787
AFLR3 IG : Nodes, Elements = 51887 333786
AFLR3 IG : Nodes, Elements = 51887 334674
AFLR3 IG : Nodes, Elements = 51887 333824
AFLR3 IG : Nodes, Elements = 51887 333826
AFLR3 IG : Nodes, Elements = 51887 334549
AFLR3 IG : Nodes, Elements = 51887 334510
AFLR3 IG : Nodes, Elements = 51887 333396
AFLR3 IG : Nodes, Elements = 51887 333397
AFLR3 IG : Nodes, Elements = 51887 334233
AFLR3 IG : Nodes, Elements = 51887 333428
AFLR3 IG : Nodes, Elements = 51887 334134
AFLR3 IG : Nodes, Elements = 51887 334104
AFLR3 IG : Nodes, Elements = 51887 333143
AFLR3 IG : Nodes, Elements = 51887 333943
AFLR3 IG : Nodes, Elements = 51887 333202
AFLR3 IG : Nodes, Elements = 51887 333853
AFLR3 IG : Nodes, Elements = 51887 333818
AFLR3 IG : Nodes, Elements = 51887 333004
AFLR3 IG : Nodes, Elements = 51887 333005
AFLR3 IG : Nodes, Elements = 51887 333003
AFLR3 IG : Nodes, Elements = 51887 333825
AFLR3 IG : Nodes, Elements = 51887 333066
AFLR3 IG : Nodes, Elements = 51887 333730
AFLR3 IG : Nodes, Elements = 51887 333698
AFLR3 IG : Nodes, Elements = 51887 332938
AFLR3 IG : Nodes, Elements = 51887 333732
AFLR3 IG : Nodes, Elements = 51887 332963
AFLR3 IG : Nodes, Elements = 51887 333614
AFLR3 IG : Nodes, Elements = 51887 333588
AFLR3 IG : Nodes, Elements = 51887 332944
AFLR3 IG : Nodes, Elements = 51887 333692
AFLR3 IG : Nodes, Elements = 51887 332974
AFLR3 IG : Nodes, Elements = 51887 333621
AFLR3 IG : Nodes, Elements = 51887 333591
AFLR3 IG : Nodes, Elements = 51887 332907
AFLR3 IG : Nodes, Elements = 51887 332908
AFLR3 IG : Nodes, Elements = 51887 333652
AFLR3 IG : Nodes, Elements = 51887 332941
AFLR3 IG : Nodes, Elements = 51887 333551
AFLR3 IG : Nodes, Elements = 51887 333522
AFLR3 IG : Nodes, Elements = 51887 332910
AFLR3 IG : Nodes, Elements = 51887 333612
AFLR3 IG : Nodes, Elements = 51887 332938
AFLR3 IG : Nodes, Elements = 51887 333522
AFLR3 IG : Nodes, Elements = 51887 333490
AFLR3 IG : Nodes, Elements = 51887 332887
AFLR3 IG : Nodes, Elements = 51887 333601
AFLR3 IG : Nodes, Elements = 51887 332940
AFLR3 IG : Nodes, Elements = 51887 333521
AFLR3 IG : Nodes, Elements = 51887 333492
AFLR3 IG : Nodes, Elements = 51887 332917
AFLR3 IG : Nodes, Elements = 51887 333647
AFLR3 IG : Nodes, Elements = 51887 332914
AFLR3 IG : Nodes, Elements = 51887 332917
AFLR3 IG : Nodes, Elements = 51887 333205
AFLR3 IG : Nodes, Elements = 51887 333191
AFLR3 IG : Nodes, Elements = 51887 332814
AFLR3 IG : Nodes, Elements = 51887 333027
AFLR3 IG : Nodes, Elements = 51887 332825
AFLR3 IG : Nodes, Elements = 51887 333001
AFLR3 IG : Nodes, Elements = 51887 332992
AFLR3 IG : Nodes, Elements = 51887 332804
AFLR3 IG : Nodes, Elements = 51887 333020
AFLR3 IG : Nodes, Elements = 51887 332821
AFLR3 IG : Nodes, Elements = 51887 332985
AFLR3 IG : Nodes, Elements = 51887 332977
AFLR3 IG : Nodes, Elements = 51887 332795
AFLR3 IG : Nodes, Elements = 51887 332794
AFLR3 IG : Nodes, Elements = 51887 332944
AFLR3 IG : Nodes, Elements = 51887 332812
AFLR3 IG : Nodes, Elements = 51887 332916
AFLR3 IG : Nodes, Elements = 51887 332906
AFLR3 IG : Nodes, Elements = 51887 332793
AFLR3 IG : Nodes, Elements = 51887 333116
AFLR3 IG : Nodes, Elements = 51887 332834
AFLR3 IG : Nodes, Elements = 51887 332863
AFLR3 IG : Nodes, Elements = 51887 332862
AFLR3 IG : Nodes, Elements = 51887 332826
AFLR3 IG : Nodes, Elements = 51887 332827
AFLR3 IG : Nodes, Elements = 51887 332826
AFLR3 IG : Nodes, Elements = 51880 178760
AFLR3 IG : Nodes, Elements = 51880 182479
AFLR3 IG : Nodes, Elements = 51880 165613
AFLR3 IG : Nodes, Elements = 51880 162420
AFLR3 : CPU Time = 25.489 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 51880 162420
AFLR3 GGi: Nodes, Elements = 51883 162429
AFLR3 GGi: Nodes, Elements = 51883 162481
AFLR3 GGi: Nodes, Elements = 51883 162366
AFLR3 GGi: Nodes, Elements = 51883 162326
AFLR3 GGi: Nodes, Elements = 51884 162329
AFLR3 GGi: Nodes, Elements = 51884 162344
AFLR3 GGi: Nodes, Elements = 51884 162304
AFLR3 GGi: Nodes, Elements = 51884 162289
AFLR3 GGi: Nodes, Elements = 51885 162292
AFLR3 GGi: Nodes, Elements = 51885 162302
AFLR3 GGi: Nodes, Elements = 51885 162277
AFLR3 GGi: Nodes, Elements = 51885 162264
AFLR3 GG : Nodes, Elements = 64868 201337
AFLR3 GG : Nodes, Elements = 64868 247755
AFLR3 GG : Nodes, Elements = 64868 233272
AFLR3 GG : Nodes, Elements = 64868 230980
AFLR3 GG : Nodes, Elements = 76530 266127
AFLR3 GG : Nodes, Elements = 76530 317378
AFLR3 GG : Nodes, Elements = 76530 302469
AFLR3 GG : Nodes, Elements = 76530 300472
AFLR3 GG : Nodes, Elements = 88215 335680
AFLR3 GG : Nodes, Elements = 88215 386267
AFLR3 GG : Nodes, Elements = 88215 372979
AFLR3 GG : Nodes, Elements = 88215 370800
AFLR3 GG : Nodes, Elements = 99281 404126
AFLR3 GG : Nodes, Elements = 99281 451175
AFLR3 GG : Nodes, Elements = 99281 438865
AFLR3 GG : Nodes, Elements = 99281 436833
AFLR3 GG : Nodes, Elements = 109620 467987
AFLR3 GG : Nodes, Elements = 109620 511970
AFLR3 GG : Nodes, Elements = 109620 500532
AFLR3 GG : Nodes, Elements = 109620 498559
AFLR3 GG : Nodes, Elements = 119279 527641
AFLR3 GG : Nodes, Elements = 119279 568729
AFLR3 GG : Nodes, Elements = 119279 558006
AFLR3 GG : Nodes, Elements = 119279 556285
AFLR3 GG : Nodes, Elements = 128285 583402
AFLR3 GG : Nodes, Elements = 128285 621430
AFLR3 GG : Nodes, Elements = 128285 611604
AFLR3 GG : Nodes, Elements = 128285 609940
AFLR3 GG : Nodes, Elements = 136795 635558
AFLR3 GG : Nodes, Elements = 136795 671523
AFLR3 GG : Nodes, Elements = 136795 662306
AFLR3 GG : Nodes, Elements = 136795 660758
AFLR3 GG : Nodes, Elements = 144839 684966
AFLR3 GG : Nodes, Elements = 144839 719009
AFLR3 GG : Nodes, Elements = 144839 710239
AFLR3 GG : Nodes, Elements = 144839 708815
AFLR3 GG : Nodes, Elements = 152354 731449
AFLR3 GG : Nodes, Elements = 152354 763306
AFLR3 GG : Nodes, Elements = 152354 755031
AFLR3 GG : Nodes, Elements = 152354 753693
AFLR3 GG : Nodes, Elements = 159540 775329
AFLR3 GG : Nodes, Elements = 159540 805413
AFLR3 GG : Nodes, Elements = 159540 797743
AFLR3 GG : Nodes, Elements = 159540 796414
AFLR3 GG : Nodes, Elements = 166292 816752
AFLR3 GG : Nodes, Elements = 166292 845085
AFLR3 GG : Nodes, Elements = 166292 837859
AFLR3 GG : Nodes, Elements = 166292 836627
AFLR3 GG : Nodes, Elements = 172749 856076
AFLR3 GG : Nodes, Elements = 172749 883413
AFLR3 GG : Nodes, Elements = 172749 876293
AFLR3 GG : Nodes, Elements = 172749 875098
AFLR3 GG : Nodes, Elements = 178803 893330
AFLR3 GG : Nodes, Elements = 178803 919329
AFLR3 GG : Nodes, Elements = 178803 912496
AFLR3 GG : Nodes, Elements = 178803 911295
AFLR3 GG : Nodes, Elements = 184674 928983
AFLR3 GG : Nodes, Elements = 184674 953650
AFLR3 GG : Nodes, Elements = 184674 947209
AFLR3 GG : Nodes, Elements = 184674 946144
AFLR3 GG : Nodes, Elements = 190292 963081
AFLR3 GG : Nodes, Elements = 190292 986894
AFLR3 GG : Nodes, Elements = 190292 980738
AFLR3 GG : Nodes, Elements = 190292 979661
AFLR3 GG : Nodes, Elements = 195610 995659
AFLR3 GG : Nodes, Elements = 195610 1018207
AFLR3 GG : Nodes, Elements = 195610 1012366
AFLR3 GG : Nodes, Elements = 195610 1011366
AFLR3 GG : Nodes, Elements = 200778 1026923
AFLR3 GG : Nodes, Elements = 200778 1048801
AFLR3 GG : Nodes, Elements = 200778 1043170
AFLR3 GG : Nodes, Elements = 200778 1042158
AFLR3 GG : Nodes, Elements = 205724 1057052
AFLR3 GG : Nodes, Elements = 205724 1077940
AFLR3 GG : Nodes, Elements = 205724 1072575
AFLR3 GG : Nodes, Elements = 205724 1071640
AFLR3 GG : Nodes, Elements = 210460 1085897
AFLR3 GG : Nodes, Elements = 210460 1105993
AFLR3 GG : Nodes, Elements = 210460 1100756
AFLR3 GG : Nodes, Elements = 210460 1099881
AFLR3 GG : Nodes, Elements = 215076 1113770
AFLR3 GG : Nodes, Elements = 215076 1133223
AFLR3 GG : Nodes, Elements = 215076 1128306
AFLR3 GG : Nodes, Elements = 215076 1127439
AFLR3 GG : Nodes, Elements = 219470 1140663
AFLR3 GG : Nodes, Elements = 219470 1159066
AFLR3 GG : Nodes, Elements = 219470 1154300
AFLR3 GG : Nodes, Elements = 219470 1153573
AFLR3 GG : Nodes, Elements = 223623 1166077
AFLR3 GG : Nodes, Elements = 223623 1183913
AFLR3 GG : Nodes, Elements = 223623 1179257
AFLR3 GG : Nodes, Elements = 223623 1178516
AFLR3 GG : Nodes, Elements = 227646 1190615
AFLR3 GG : Nodes, Elements = 227646 1207551
AFLR3 GG : Nodes, Elements = 227646 1203228
AFLR3 GG : Nodes, Elements = 227646 1202505
AFLR3 GG : Nodes, Elements = 231428 1213873
AFLR3 GG : Nodes, Elements = 231428 1230058
AFLR3 GG : Nodes, Elements = 231428 1225852
AFLR3 GG : Nodes, Elements = 231428 1225144
AFLR3 GG : Nodes, Elements = 235036 1235995
AFLR3 GG : Nodes, Elements = 235036 1251123
AFLR3 GG : Nodes, Elements = 235036 1247254
AFLR3 GG : Nodes, Elements = 235036 1246614
AFLR3 GG : Nodes, Elements = 238439 1256846
AFLR3 GG : Nodes, Elements = 238439 1271084
AFLR3 GG : Nodes, Elements = 238439 1267528
AFLR3 GG : Nodes, Elements = 238439 1266946
AFLR3 GG : Nodes, Elements = 241701 1276753
AFLR3 GG : Nodes, Elements = 241701 1290478
AFLR3 GG : Nodes, Elements = 241701 1287001
AFLR3 GG : Nodes, Elements = 241701 1286402
AFLR3 GG : Nodes, Elements = 244689 1295377
AFLR3 GG : Nodes, Elements = 244689 1308048
AFLR3 GG : Nodes, Elements = 244689 1304776
AFLR3 GG : Nodes, Elements = 244689 1304261
AFLR3 GG : Nodes, Elements = 247531 1312804
AFLR3 GG : Nodes, Elements = 247531 1324708
AFLR3 GG : Nodes, Elements = 247531 1321687
AFLR3 GG : Nodes, Elements = 247531 1321234
AFLR3 GG : Nodes, Elements = 250186 1329212
AFLR3 GG : Nodes, Elements = 250186 1340424
AFLR3 GG : Nodes, Elements = 250186 1337507
AFLR3 GG : Nodes, Elements = 250186 1337067
AFLR3 GG : Nodes, Elements = 252620 1344374
AFLR3 GG : Nodes, Elements = 252620 1354681
AFLR3 GG : Nodes, Elements = 252620 1351968
AFLR3 GG : Nodes, Elements = 252620 1351622
AFLR3 GG : Nodes, Elements = 254882 1358422
AFLR3 GG : Nodes, Elements = 254882 1367939
AFLR3 GG : Nodes, Elements = 254882 1365500
AFLR3 GG : Nodes, Elements = 254882 1365120
AFLR3 GG : Nodes, Elements = 256922 1371248
AFLR3 GG : Nodes, Elements = 256922 1379879
AFLR3 GG : Nodes, Elements = 256922 1377655
AFLR3 GG : Nodes, Elements = 256922 1377357
AFLR3 GG : Nodes, Elements = 258831 1383091
AFLR3 GG : Nodes, Elements = 258831 1391189
AFLR3 GG : Nodes, Elements = 258831 1389056
AFLR3 GG : Nodes, Elements = 258831 1388730
AFLR3 GG : Nodes, Elements = 260604 1394054
AFLR3 GG : Nodes, Elements = 260604 1401444
AFLR3 GG : Nodes, Elements = 260604 1399574
AFLR3 GG : Nodes, Elements = 260604 1399319
AFLR3 GG : Nodes, Elements = 262204 1404122
AFLR3 GG : Nodes, Elements = 262204 1410873
AFLR3 GG : Nodes, Elements = 262204 1409130
AFLR3 GG : Nodes, Elements = 262204 1408887
AFLR3 GG : Nodes, Elements = 263671 1413291
AFLR3 GG : Nodes, Elements = 263671 1419457
AFLR3 GG : Nodes, Elements = 263671 1417918
AFLR3 GG : Nodes, Elements = 263671 1417676
AFLR3 GG : Nodes, Elements = 264968 1421568
AFLR3 GG : Nodes, Elements = 264968 1426961
AFLR3 GG : Nodes, Elements = 264968 1425546
AFLR3 GG : Nodes, Elements = 264968 1425377
AFLR3 GG : Nodes, Elements = 266104 1428785
AFLR3 GG : Nodes, Elements = 266104 1433489
AFLR3 GG : Nodes, Elements = 266104 1432293
AFLR3 GG : Nodes, Elements = 266104 1432158
AFLR3 GG : Nodes, Elements = 267033 1434947
AFLR3 GG : Nodes, Elements = 267033 1438921
AFLR3 GG : Nodes, Elements = 267033 1437884
AFLR3 GG : Nodes, Elements = 267033 1437708
AFLR3 GG : Nodes, Elements = 267780 1439955
AFLR3 GG : Nodes, Elements = 267780 1443172
AFLR3 GG : Nodes, Elements = 267780 1442287
AFLR3 GG : Nodes, Elements = 267780 1442160
AFLR3 GG : Nodes, Elements = 268395 1444005
AFLR3 GG : Nodes, Elements = 268395 1446584
AFLR3 GG : Nodes, Elements = 268395 1445896
AFLR3 GG : Nodes, Elements = 268395 1445784
AFLR3 GG : Nodes, Elements = 268871 1447215
AFLR3 GG : Nodes, Elements = 268871 1449282
AFLR3 GG : Nodes, Elements = 268871 1448717
AFLR3 GG : Nodes, Elements = 268871 1448631
AFLR3 GG : Nodes, Elements = 269256 1449788
AFLR3 GG : Nodes, Elements = 269256 1451440
AFLR3 GG : Nodes, Elements = 269256 1450973
AFLR3 GG : Nodes, Elements = 269256 1450893
AFLR3 GG : Nodes, Elements = 269582 1451872
AFLR3 GG : Nodes, Elements = 269582 1453281
AFLR3 GG : Nodes, Elements = 269582 1452907
AFLR3 GG : Nodes, Elements = 269582 1452832
AFLR3 GG : Nodes, Elements = 269868 1453691
AFLR3 GG : Nodes, Elements = 269868 1454983
AFLR3 GG : Nodes, Elements = 269868 1454590
AFLR3 GG : Nodes, Elements = 269868 1454506
AFLR3 GG : Nodes, Elements = 270071 1455115
AFLR3 GG : Nodes, Elements = 270071 1456085
AFLR3 GG : Nodes, Elements = 270071 1455778
AFLR3 GG : Nodes, Elements = 270071 1455708
AFLR3 GG : Nodes, Elements = 270245 1456230
AFLR3 GG : Nodes, Elements = 270245 1457093
AFLR3 GG : Nodes, Elements = 270245 1456817
AFLR3 GG : Nodes, Elements = 270245 1456722
AFLR3 GG : Nodes, Elements = 270404 1457199
AFLR3 GG : Nodes, Elements = 270404 1457986
AFLR3 GG : Nodes, Elements = 270404 1457735
AFLR3 GG : Nodes, Elements = 270404 1457677
AFLR3 GG : Nodes, Elements = 270519 1458022
AFLR3 GG : Nodes, Elements = 270519 1458630
AFLR3 GG : Nodes, Elements = 270519 1458408
AFLR3 GG : Nodes, Elements = 270519 1458355
AFLR3 GG : Nodes, Elements = 270601 1458601
AFLR3 GG : Nodes, Elements = 270601 1459037
AFLR3 GG : Nodes, Elements = 270601 1458881
AFLR3 GG : Nodes, Elements = 270601 1458840
AFLR3 GG : Nodes, Elements = 270648 1458981
AFLR3 GG : Nodes, Elements = 270648 1459250
AFLR3 GG : Nodes, Elements = 270648 1459141
AFLR3 GG : Nodes, Elements = 270648 1459113
AFLR3 GG : Nodes, Elements = 270675 1459194
AFLR3 GG : Nodes, Elements = 270675 1459379
AFLR3 GG : Nodes, Elements = 270675 1459286
AFLR3 GG : Nodes, Elements = 270675 1459261
AFLR3 GG : Nodes, Elements = 270700 1459336
AFLR3 GG : Nodes, Elements = 270700 1459514
AFLR3 GG : Nodes, Elements = 270700 1459445
AFLR3 GG : Nodes, Elements = 270700 1459418
AFLR3 GG : Nodes, Elements = 270732 1459514
AFLR3 GG : Nodes, Elements = 270732 1459697
AFLR3 GG : Nodes, Elements = 270732 1459606
AFLR3 GG : Nodes, Elements = 270732 1459587
AFLR3 GG : Nodes, Elements = 270746 1459629
AFLR3 GG : Nodes, Elements = 270746 1459719
AFLR3 GG : Nodes, Elements = 270746 1459670
AFLR3 GG : Nodes, Elements = 270746 1459669
AFLR3 GG : Nodes, Elements = 270751 1459684
AFLR3 GG : Nodes, Elements = 270751 1459713
AFLR3 GG : Nodes, Elements = 270751 1459698
AFLR3 GG : Nodes, Elements = 270751 1459696
AFLR3 GG : Nodes, Elements = 270817 1459894
AFLR3 GG : Nodes, Elements = 270817 1460256
AFLR3 GG : Nodes, Elements = 270817 1460103
AFLR3 GG : Nodes, Elements = 270817 1460087
AFLR3 GG : Nodes, Elements = 270830 1460126
AFLR3 GG : Nodes, Elements = 270830 1460186
AFLR3 GG : Nodes, Elements = 270830 1460165
AFLR3 GG : Nodes, Elements = 270830 1460159
AFLR3 GG : Nodes, Elements = 270835 1460174
AFLR3 GG : Nodes, Elements = 270835 1460204
AFLR3 GG : Nodes, Elements = 270835 1460189
AFLR3 GG : Nodes, Elements = 270835 1460187
AFLR3 : CPU Time = 45.068 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 270835 1460187
AFLR3 QI : Nodes, Elements = 267259 1440039
AFLR3 QI : Nodes, Elements = 266823 1437558
AFLR3 QI : Nodes, Elements = 266798 1437421
AFLR3 QI : Nodes, Elements = 266798 1451054
AFLR3 QI : Nodes, Elements = 266798 1437012
AFLR3 QI : Nodes, Elements = 266798 1435493
AFLR3 QI : Nodes, Elements = 266798 1438513
AFLR3 QI : Nodes, Elements = 266798 1434869
AFLR3 QI : Nodes, Elements = 266798 1434060
AFLR3 QI : Nodes, Elements = 266798 1436926
AFLR3 QI : Nodes, Elements = 266798 1434171
AFLR3 QI : Nodes, Elements = 266798 1434010
AFLR3 QI : Nodes, Elements = 266798 1436793
AFLR3 QI : Nodes, Elements = 266798 1434144
AFLR3 QI : Nodes, Elements = 266798 1433997
AFLR3 QI : Nodes, Elements = 266798 1436514
AFLR3 QI : Nodes, Elements = 266798 1434095
AFLR3 QI : Nodes, Elements = 266798 1433871
AFLR3 QI : Nodes, Elements = 266798 1433827
AFLR3 QI : Nodes, Elements = 266812 1433892
AFLR3 QI : Nodes, Elements = 266812 1436386
AFLR3 QI : Nodes, Elements = 266812 1434032
AFLR3 QI : Nodes, Elements = 266812 1433888
AFLR3 QI : Nodes, Elements = 266812 1436248
AFLR3 QI : Nodes, Elements = 266812 1433988
AFLR3 QI : Nodes, Elements = 266812 1433787
AFLR3 : CPU Time = 13.066 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 266812 1433787
AFLR3 QRG: Nodes, Elements = 266818 1433820
AFLR3 QRG: Nodes, Elements = 266818 1433821
AFLR3 QRG: Nodes, Elements = 266820 1433831
AFLR3 QRG: Nodes, Elements = 266822 1433844
AFLR3 QRG: Nodes, Elements = 266830 1433881
AFLR3 QRG: Nodes, Elements = 266838 1433920
AFLR3 QRG: Nodes, Elements = 266838 1433919
AFLR3 QRG: Nodes, Elements = 266839 1433925
AFLR3 QRG: Nodes, Elements = 266844 1433949
AFLR3 QRG: Nodes, Elements = 266849 1433975
AFLR3 QRG: Nodes, Elements = 266850 1433979
AFLR3 QRG: Nodes, Elements = 266856 1434010
AFLR3 QRG: Nodes, Elements = 266857 1434015
AFLR3 QRG: Nodes, Elements = 266858 1434019
AFLR3 QRG: Nodes, Elements = 266861 1434032
AFLR3 QRG: Nodes, Elements = 266872 1434088
AFLR3 : CPU Time = 0.653 seconds
AFLR3 : DONE
ANBL3 BLM: BL VOLUME GRID MERGE
ANBL3 BLM: Nodes, Elements = 266872 1434088
UG3 : OUTPUT GRID
UG3 : Grid File Name = .tmp.b8.ugrid
UG3 : Quad Surface Faces= 0
UG3 : Tria Surface Faces= 103724
UG3 : Nodes = 472463
UG3 : Total Elements = 1864759
UG3 : Hex Elements = 0
UG3 : Pent_5 Elements = 20660
UG3 : Pent_6 Elements = 390906
UG3 : Tet Elements = 1453193
ANBL3 BLM: Nodes, Elements = 472463 2667231
ANBL3 BLM: Nodes, Elements = 472463 19105
ANBL3 : CPU Time = 1.107 seconds
ANBL3 : DONE
OVERALL : CPU Time = 2.290 minutes
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1453193
UG3 : Min, Max Ang = 1.004 178.1
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 346
UG3 : No. Angle>179.9 = 0
UG3 : No. Pyramid Elems = 20660
UG3 : Min, Max Ang = 7.23 174.4
UG3 : Average Angle = 82.6
UG3 : No. Angle>160.0 = 128
UG3 : No. Angle>179.9 = 0
UG3 : No. Prism Elems = 390906
UG3 : Min, Max Ang = 6.851 174.6
UG3 : Average Angle = 80.1
UG3 : No. Angle>160.0 = 732
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 1453193
UG3 : Min Vol = 8.19e-06
UG3 : Average Vol = 4.1e+04
UG3 : Total-Tet-Vol = 5.96e+10
UG3 : No. Vol<TOL = 0
UG3 : No. Pyramid Elems = 20660
UG3 : Min Vol = 2.24e-05
UG3 : Average Vol = 0.0433
UG3 : Total-Pyramid-Vol = 894
UG3 : No. Vol<TOL = 0
UG3 : No. Prism Elems = 390906
UG3 : Min Vol = 2.9e-05
UG3 : Average Vol = 0.112
UG3 : Total-Prism-Vol = 4.38e+04
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 1453193
UG3 : Min, Max Q = 0.0876 1
UG3 : Average Q = 0.851
UG3 : No. Q< 0.1 = 3
UG3 : No. Q< 0.01 = 0
UG3 : No. Pyramid Elems = 20660
UG3 : Min, Max Q = 0.212 1
UG3 : Average Q = 0.781
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : No. Prism Elems = 390906
UG3 : Min, Max Q = 0.254 1
UG3 : Average Q = 0.909
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
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EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 29
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EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 31
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EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 33
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 35
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EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 37
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 38
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 39
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 40
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 41
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 42
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 43
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 44
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 45
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 46
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 47
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 48
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 49
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 50
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 51
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 52
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 53
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 54
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 55
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 56
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 57
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 58
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 59
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 60
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 61
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 62
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 63
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 64
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 65
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 66
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 67
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 68
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 69
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 70
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 71
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 72
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 73
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 74
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 75
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 76
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 77
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 78
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 79
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 80
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 81
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 82
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 83
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 84
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 85
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 86
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 87
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 88
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 89
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 90
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 91
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 92
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 93
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 94
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 95
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 96
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 97
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 98
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 99
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 100
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 101
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 102
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 103
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 104
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 105
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 106
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 107
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 108
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 109
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 110
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 111
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 112
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 113
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 114
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 115
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 116
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 117
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 118
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 119
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 120
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 121
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 122
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 123
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 124
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 125
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 126
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 127
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 128
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 129
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 130
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 131
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 132
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 133
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 134
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 135
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 136
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 137
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 138
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 139
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 140
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 141
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 142
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 143
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 144
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 145
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 146
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 147
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 148
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 149
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 150
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 151
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 152
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 153
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 154
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 155
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 156
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 157
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 158
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 159
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 160
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 161
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 162
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 163
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 164
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 165
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 166
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 167
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 168
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 169
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 170
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 171
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 172
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 173
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 174
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 175
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 176
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 18
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 19
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 20
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 21
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 22
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 23
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 24
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 25
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 26
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 27
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 28
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 29
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 30
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 31
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 32
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 33
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 34
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 35
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 36
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 37
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 38
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 39
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 40
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 41
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 42
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 43
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 44
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 45
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 46
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 47
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 48
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 49
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 50
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 51
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 52
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 53
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 54
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 55
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 56
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 57
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 58
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 59
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 60
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 61
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 62
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 63
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 64
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 65
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 66
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 67
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 177
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 178
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 179
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 180
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 181
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 182
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 183
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 184
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 185
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 68
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 69
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 70
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 71
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 72
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 186
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 187
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 188
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 189
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 190
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 191
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 192
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 193
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 194
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 73
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 74
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 75
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 76
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 77
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 195
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 196
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 197
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 198
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 199
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 200
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 201
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 202
EGADS : CREATING TESSELLATION FOR BODY 3 EDGE 203
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 78
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 79
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 80
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 81
EGADS : CREATING TESSELLATION FOR BODY 3 FACE 82
EGADS : CREATING TESSELLATION FOR BODY 4 EDGE 204
EGADS : CREATING TESSELLATION FOR BODY 4 EDGE 205
EGADS : CREATING TESSELLATION FOR BODY 4 EDGE 206
EGADS : CREATING TESSELLATION FOR BODY 4 EDGE 207
EGADS : CREATING TESSELLATION FOR BODY 4 EDGE 208
EGADS : CREATING TESSELLATION FOR BODY 4 EDGE 209
EGADS : CREATING TESSELLATION FOR BODY 4 EDGE 210
EGADS : CREATING TESSELLATION FOR BODY 4 EDGE 211
EGADS : CREATING TESSELLATION FOR BODY 4 EDGE 212
EGADS : CREATING TESSELLATION FOR BODY 4 FACE 83
EGADS : CREATING TESSELLATION FOR BODY 4 FACE 84
EGADS : CREATING TESSELLATION FOR BODY 4 FACE 85
EGADS : CREATING TESSELLATION FOR BODY 4 FACE 86
EGADS : CREATING TESSELLATION FOR BODY 4 FACE 87
EGADS : CREATING TESSELLATION FOR BODY 5 EDGE 213
EGADS : CREATING TESSELLATION FOR BODY 5 EDGE 214
EGADS : CREATING TESSELLATION FOR BODY 5 EDGE 215
EGADS : CREATING TESSELLATION FOR BODY 5 EDGE 216
EGADS : CREATING TESSELLATION FOR BODY 5 EDGE 217
EGADS : CREATING TESSELLATION FOR BODY 5 EDGE 218
EGADS : CREATING TESSELLATION FOR BODY 5 EDGE 219
EGADS : CREATING TESSELLATION FOR BODY 5 EDGE 220
EGADS : CREATING TESSELLATION FOR BODY 5 EDGE 221
EGADS : CREATING TESSELLATION FOR BODY 5 FACE 88
EGADS : CREATING TESSELLATION FOR BODY 5 FACE 89
EGADS : CREATING TESSELLATION FOR BODY 5 FACE 90
EGADS : CREATING TESSELLATION FOR BODY 5 FACE 91
EGADS : CREATING TESSELLATION FOR BODY 5 FACE 92
EGADS : CREATING TESSELLATION FOR BODY 6 EDGE 222
EGADS : CREATING TESSELLATION FOR BODY 6 EDGE 223
EGADS : CREATING TESSELLATION FOR BODY 6 EDGE 224
EGADS : CREATING TESSELLATION FOR BODY 6 EDGE 225
EGADS : CREATING TESSELLATION FOR BODY 6 EDGE 226
EGADS : CREATING TESSELLATION FOR BODY 6 EDGE 227
EGADS : CREATING TESSELLATION FOR BODY 6 EDGE 228
EGADS : CREATING TESSELLATION FOR BODY 6 EDGE 229
EGADS : CREATING TESSELLATION FOR BODY 6 EDGE 230
EGADS : CREATING TESSELLATION FOR BODY 6 FACE 93
EGADS : CREATING TESSELLATION FOR BODY 6 FACE 94
EGADS : CREATING TESSELLATION FOR BODY 6 FACE 95
EGADS : CREATING TESSELLATION FOR BODY 6 FACE 96
EGADS : CREATING TESSELLATION FOR BODY 6 FACE 97
EGADS : CREATING TESSELLATION FOR BODY 7 EDGE 231
EGADS : CREATING TESSELLATION FOR BODY 7 EDGE 232
EGADS : CREATING TESSELLATION FOR BODY 7 EDGE 233
EGADS : CREATING TESSELLATION FOR BODY 7 EDGE 234
EGADS : CREATING TESSELLATION FOR BODY 7 EDGE 235
EGADS : CREATING TESSELLATION FOR BODY 7 EDGE 236
EGADS : CREATING TESSELLATION FOR BODY 7 EDGE 237
EGADS : CREATING TESSELLATION FOR BODY 7 EDGE 238
EGADS : CREATING TESSELLATION FOR BODY 7 EDGE 239
EGADS : CREATING TESSELLATION FOR BODY 7 FACE 98
EGADS : CREATING TESSELLATION FOR BODY 7 FACE 99
EGADS : CREATING TESSELLATION FOR BODY 7 FACE 100
EGADS : CREATING TESSELLATION FOR BODY 7 FACE 101
EGADS : CREATING TESSELLATION FOR BODY 7 FACE 102
EGADS : CREATING TESSELLATION FOR BODY 8 EDGE 240
EGADS : CREATING TESSELLATION FOR BODY 8 EDGE 241
EGADS : CREATING TESSELLATION FOR BODY 8 EDGE 242
EGADS : CREATING TESSELLATION FOR BODY 8 EDGE 243
EGADS : CREATING TESSELLATION FOR BODY 8 EDGE 244
EGADS : CREATING TESSELLATION FOR BODY 8 EDGE 245
EGADS : CREATING TESSELLATION FOR BODY 8 EDGE 246
EGADS : CREATING TESSELLATION FOR BODY 8 EDGE 247
EGADS : CREATING TESSELLATION FOR BODY 8 EDGE 248
EGADS : CREATING TESSELLATION FOR BODY 8 FACE 103
EGADS : CREATING TESSELLATION FOR BODY 8 FACE 104
EGADS : CREATING TESSELLATION FOR BODY 8 FACE 105
EGADS : CREATING TESSELLATION FOR BODY 8 FACE 106
EGADS : CREATING TESSELLATION FOR BODY 8 FACE 107
EGADS : CREATING TESSELLATION FOR BODY 9 EDGE 249
EGADS : CREATING TESSELLATION FOR BODY 9 EDGE 250
EGADS : CREATING TESSELLATION FOR BODY 9 EDGE 251
EGADS : CREATING TESSELLATION FOR BODY 9 EDGE 252
EGADS : CREATING TESSELLATION FOR BODY 9 EDGE 253
EGADS : CREATING TESSELLATION FOR BODY 9 EDGE 254
EGADS : CREATING TESSELLATION FOR BODY 9 EDGE 255
EGADS : CREATING TESSELLATION FOR BODY 9 EDGE 256
EGADS : CREATING TESSELLATION FOR BODY 9 EDGE 257
EGADS : CREATING TESSELLATION FOR BODY 9 FACE 108
EGADS : CREATING TESSELLATION FOR BODY 9 FACE 109
EGADS : CREATING TESSELLATION FOR BODY 9 FACE 110
EGADS : CREATING TESSELLATION FOR BODY 9 FACE 111
EGADS : CREATING TESSELLATION FOR BODY 9 FACE 112
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 258
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 259
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 260
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 261
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 262
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 263
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 264
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 265
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 266
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 267
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 268
EGADS : CREATING TESSELLATION FOR BODY 10 EDGE 269
EGADS : CREATING TESSELLATION FOR BODY 10 FACE 113
EGADS : CREATING TESSELLATION FOR BODY 10 FACE 114
EGADS : CREATING TESSELLATION FOR BODY 10 FACE 115
EGADS : CREATING TESSELLATION FOR BODY 10 FACE 116
EGADS : CREATING TESSELLATION FOR BODY 10 FACE 117
EGADS : CREATING TESSELLATION FOR BODY 10 FACE 118
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 18
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 19
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 20
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 21
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 22
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 23
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 24
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 25
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 26
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 27
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 28
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 29
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 30
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 31
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 32
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 33
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 34
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 35
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 36
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 37
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 38
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 39
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 40
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 41
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 42
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 43
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 44
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 45
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 46
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 47
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 48
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 49
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 50
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 51
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 52
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 53
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 54
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 55
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 56
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 57
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 58
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 59
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 60
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 61
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 62
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 63
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 64
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 65
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 66
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 67
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 68
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 69
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 70
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 71
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 72
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 73
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 74
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 75
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 76
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 77
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 78
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 79
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 80
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 81
EGADS : CHECKING NODE MAP FOR BODY 3 FACE 82
EGADS : CHECKING NODE MAP FOR BODY 4 FACE 83
EGADS : CHECKING NODE MAP FOR BODY 4 FACE 84
EGADS : CHECKING NODE MAP FOR BODY 4 FACE 85
EGADS : CHECKING NODE MAP FOR BODY 4 FACE 86
EGADS : CHECKING NODE MAP FOR BODY 4 FACE 87
EGADS : CHECKING NODE MAP FOR BODY 5 FACE 88
EGADS : CHECKING NODE MAP FOR BODY 5 FACE 89
EGADS : CHECKING NODE MAP FOR BODY 5 FACE 90
EGADS : CHECKING NODE MAP FOR BODY 5 FACE 91
EGADS : CHECKING NODE MAP FOR BODY 5 FACE 92
EGADS : CHECKING NODE MAP FOR BODY 6 FACE 93
EGADS : CHECKING NODE MAP FOR BODY 6 FACE 94
EGADS : CHECKING NODE MAP FOR BODY 6 FACE 95
EGADS : CHECKING NODE MAP FOR BODY 6 FACE 96
EGADS : CHECKING NODE MAP FOR BODY 6 FACE 97
EGADS : CHECKING NODE MAP FOR BODY 7 FACE 98
EGADS : CHECKING NODE MAP FOR BODY 7 FACE 99
EGADS : CHECKING NODE MAP FOR BODY 7 FACE 100
EGADS : CHECKING NODE MAP FOR BODY 7 FACE 101
EGADS : CHECKING NODE MAP FOR BODY 7 FACE 102
EGADS : CHECKING NODE MAP FOR BODY 8 FACE 103
EGADS : CHECKING NODE MAP FOR BODY 8 FACE 104
EGADS : CHECKING NODE MAP FOR BODY 8 FACE 105
EGADS : CHECKING NODE MAP FOR BODY 8 FACE 106
EGADS : CHECKING NODE MAP FOR BODY 8 FACE 107
EGADS : CHECKING NODE MAP FOR BODY 9 FACE 108
EGADS : CHECKING NODE MAP FOR BODY 9 FACE 109
EGADS : CHECKING NODE MAP FOR BODY 9 FACE 110
EGADS : CHECKING NODE MAP FOR BODY 9 FACE 111
EGADS : CHECKING NODE MAP FOR BODY 9 FACE 112
EGADS : CHECKING NODE MAP FOR BODY 10 FACE 113
EGADS : CHECKING NODE MAP FOR BODY 10 FACE 114
EGADS : CHECKING NODE MAP FOR BODY 10 FACE 115
EGADS : CHECKING NODE MAP FOR BODY 10 FACE 116
EGADS : CHECKING NODE MAP FOR BODY 10 FACE 117
EGADS : CHECKING NODE MAP FOR BODY 10 FACE 118
Volume mesh:
Number of nodes = 472463
Number of elements = 1968483
Number of triangles = 103724
Number of quadrilatarals = 0
Number of tetrahedrals = 1453193
Number of pyramids = 20660
Number of prisms = 390906
Number of hexahedrals = 0
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
real 3m21.390s
user 3m20.211s
sys 0m12.402s
+ status=0
+ set +x
=================================================
data/session07/12_aflr4_aflr3_ViscousTransport.py passed (as expected)
=================================================
=================================================
aflr4_curv_factor.py test;
+ python aflr4_curv_factor.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 6
EGADS : 2 Yes 0 0 1 1 1 1 4 5
EGADS : 3 Yes 0 0 1 1 1 1 4 8
EGADS : 4 Yes 0 0 1 1 1 2 3 5
EGADS : 5 Yes 0 0 1 1 1 2 4
EGADS : 6 Yes 0 0 1 1 1 1 7 8
EGADS : 7 Yes 0 0 1 1 1 6 9 10
EGADS : 8 Yes 0 0 1 1 1 3 6 9
EGADS : 9 Yes 0 0 1 1 1 7 8 10
EGADS : 10 Yes 0 0 1 1 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.302
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 24884 49047 0
AFLR4 : Nodes, Trias,Quads= 19518 38315 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 51292 101491 0
AFLR4 : Nodes, Trias,Quads= 29743 58393 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 12434 24262 0
AFLR4 : Nodes, Trias,Quads= 9090 17574 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 42374 83719 0
AFLR4 : Nodes, Trias,Quads= 25099 49169 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 121 175 0
AFLR4 : Nodes, Trias,Quads= 101 135 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 24944 49167 0
AFLR4 : Nodes, Trias,Quads= 20103 39485 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 50472 99851 0
AFLR4 : Nodes, Trias,Quads= 29637 58181 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 11747 22888 0
AFLR4 : Nodes, Trias,Quads= 9180 17754 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 43574 86119 0
AFLR4 : Nodes, Trias,Quads= 25109 49189 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 121 175 0
AFLR4 : Nodes, Trias,Quads= 101 135 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 164487 328966 7180
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 164487 328966
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 17390 33750 0
AFLR4 : Nodes, Trias,Quads= 32860 64690 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 31290 61090 0
AFLR4 : Nodes, Trias,Quads= 45238 88986 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 13604 26291 0
AFLR4 : Nodes, Trias,Quads= 18527 36137 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 29109 56772 0
AFLR4 : Nodes, Trias,Quads= 31778 62110 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 199 298 0
AFLR4 : Nodes, Trias,Quads= 185 270 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 17365 33700 0
AFLR4 : Nodes, Trias,Quads= 32973 64916 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 31485 61480 0
AFLR4 : Nodes, Trias,Quads= 45246 89002 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 13973 27029 0
AFLR4 : Nodes, Trias,Quads= 18549 36181 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 29417 57388 0
AFLR4 : Nodes, Trias,Quads= 31852 62258 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 199 298 0
AFLR4 : Nodes, Trias,Quads= 185 270 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 252732 505456 10114
OVERALL : CPU Time = 12.711 seconds
Body 1 (of 2)
Number of nodes = 252412
Number of elements = 504820
Number of triangle elements = 504820
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 320
Number of elements = 636
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 252732
Total number of elements = 505456
Total number of triangle elements = 505456
Total number of quadrilateral elements = 0
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 6
EGADS : 2 Yes 0 0 1 1 1 1 4 5
EGADS : 3 Yes 0 0 1 1 1 1 4 8
EGADS : 4 Yes 0 0 1 1 1 2 3 5
EGADS : 5 Yes 0 0 1 1 1 2 4
EGADS : 6 Yes 0 0 1 1 1 1 7 8
EGADS : 7 Yes 0 0 1 1 1 6 9 10
EGADS : 8 Yes 0 0 1 1 1 3 6 9
EGADS : 9 Yes 0 0 1 1 1 7 8 10
EGADS : 10 Yes 0 0 1 1 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.302
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 9007 17500 0
AFLR4 : Nodes, Trias,Quads= 5492 10470 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 19257 37710 0
AFLR4 : Nodes, Trias,Quads= 6995 13186 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 10154 19797 0
AFLR4 : Nodes, Trias,Quads= 5055 9599 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 16967 33133 0
AFLR4 : Nodes, Trias,Quads= 6575 12349 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 46 53 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 8983 17452 0
AFLR4 : Nodes, Trias,Quads= 5519 10524 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 17856 34908 0
AFLR4 : Nodes, Trias,Quads= 7001 13198 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 8865 17219 0
AFLR4 : Nodes, Trias,Quads= 5045 9579 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 16322 31843 0
AFLR4 : Nodes, Trias,Quads= 6569 12337 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 46 53 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 45996 91984 5486
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 45996 91984
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 13047 25194 0
AFLR4 : Nodes, Trias,Quads= 11650 22400 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 27646 53873 0
AFLR4 : Nodes, Trias,Quads= 17621 33823 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 12513 24157 0
AFLR4 : Nodes, Trias,Quads= 11328 21787 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 27612 53806 0
AFLR4 : Nodes, Trias,Quads= 17071 32724 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 200 300 0
AFLR4 : Nodes, Trias,Quads= 186 272 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 13070 25240 0
AFLR4 : Nodes, Trias,Quads= 11571 22242 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 27812 54205 0
AFLR4 : Nodes, Trias,Quads= 17651 33883 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 12528 24187 0
AFLR4 : Nodes, Trias,Quads= 11341 21813 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 27858 54298 0
AFLR4 : Nodes, Trias,Quads= 17109 32800 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 200 300 0
AFLR4 : Nodes, Trias,Quads= 186 272 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 111330 222652 9560
OVERALL : CPU Time = 5.045 seconds
Body 1 (of 2)
Number of nodes = 111010
Number of elements = 222016
Number of triangle elements = 222016
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 320
Number of elements = 636
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 111330
Total number of elements = 222652
Total number of triangle elements = 222652
Total number of quadrilateral elements = 0
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 6
EGADS : 2 Yes 0 0 1 1 1 1 4 5
EGADS : 3 Yes 0 0 1 1 1 1 4 8
EGADS : 4 Yes 0 0 1 1 1 2 3 5
EGADS : 5 Yes 0 0 1 1 1 2 4
EGADS : 6 Yes 0 0 1 1 1 1 7 8
EGADS : 7 Yes 0 0 1 1 1 6 9 10
EGADS : 8 Yes 0 0 1 1 1 3 6 9
EGADS : 9 Yes 0 0 1 1 1 7 8 10
EGADS : 10 Yes 0 0 1 1 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.302
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 8732 16959 0
AFLR4 : Nodes, Trias,Quads= 5233 9961 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 18090 35394 0
AFLR4 : Nodes, Trias,Quads= 5568 10350 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 10182 19859 0
AFLR4 : Nodes, Trias,Quads= 4951 9397 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 16338 31891 0
AFLR4 : Nodes, Trias,Quads= 5435 10085 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 45 51 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 8705 16905 0
AFLR4 : Nodes, Trias,Quads= 5312 10119 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 17908 35030 0
AFLR4 : Nodes, Trias,Quads= 5567 10348 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 8823 17141 0
AFLR4 : Nodes, Trias,Quads= 4980 9455 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 16876 32967 0
AFLR4 : Nodes, Trias,Quads= 5357 9929 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 55 71 0
AFLR4 : Nodes, Trias,Quads= 46 53 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 40196 80384 5388
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 40196 80384
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 13069 25242 0
AFLR4 : Nodes, Trias,Quads= 9852 18808 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 26868 52324 0
AFLR4 : Nodes, Trias,Quads= 15231 29050 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 12381 23898 0
AFLR4 : Nodes, Trias,Quads= 9776 18688 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 27048 52685 0
AFLR4 : Nodes, Trias,Quads= 14966 28521 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 200 300 0
AFLR4 : Nodes, Trias,Quads= 186 272 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 12940 24984 0
AFLR4 : Nodes, Trias,Quads= 9917 18938 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 27325 53238 0
AFLR4 : Nodes, Trias,Quads= 15148 28884 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 12423 23982 0
AFLR4 : Nodes, Trias,Quads= 9812 18760 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 27246 53081 0
AFLR4 : Nodes, Trias,Quads= 15188 28965 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 200 300 0
AFLR4 : Nodes, Trias,Quads= 186 272 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 95901 191794 9514
OVERALL : CPU Time = 4.360 seconds
Body 1 (of 2)
Number of nodes = 95581
Number of elements = 191158
Number of triangle elements = 191158
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 320
Number of elements = 636
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 95901
Total number of elements = 191794
Total number of triangle elements = 191794
Total number of quadrilateral elements = 0
real 1m9.104s
user 1m3.308s
sys 0m3.835s
+ status=0
+ set +x
=================================================
solutions/session07/aflr4_curv_factor.py passed (as expected)
=================================================
=================================================
aflr4_InviscidTransport.py test;
+ python aflr4_InviscidTransport.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building pylonOml
MESSAGE:: Building nacelleOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
MESSAGE:: Building fuseOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Fuselage, index = 1
Name = Wing, index = 2
Name = Htail, index = 3
Name = Pylon, index = 4
Name = Vtail, index = 5
Name = Nacelle, index = 6
Name = Farfield, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 8
Name = Fuselage, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = Htail, index = 4
Name = Pylon, index = 5
Name = Vtail, index = 6
Name = Nacelle, index = 7
Name = Farfield, index = 8
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - Fuselage
Mesh sizing name - Htail
Mesh sizing name - Pylon
Mesh sizing name - Vtail
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 40 Faces
EGADS : Body 0 has 95 Edges
EGADS : Body 0 has 44 Loops
EGADS : Body 0 has 53 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 4 2 3 4 5 6
EGADS : 2 Yes 0 0 1 0 4 1 7 8 9 10
EGADS : 3 Yes 0 0 1 0 4 1 8 11 12 13 14
EGADS : 4 Yes 0 0 1 0 4 1 7 12
EGADS : 5 Yes 0 0 1 0 4 1 6 15
EGADS : 6 Yes 0 0 1 0 4 1 5 16 17 18
EGADS : 7 Yes 0 0 1 0 4 2 4 19
EGADS : 8 Yes 0 0 1 0 4 2 3 11 19 20 21
EGADS : 9 Yes 0 0 1 0 4 2 10 22 23 24
EGADS : 10 Yes 0 0 1 0 4 2 9 25
EGADS : 11 Yes 0 0 1 0 4 3 8 12 19
EGADS : 12 Yes 0 0 1 0 4 3 4 11 13 14 19
EGADS : 26
EGADS : 13 Yes 0 0 1 0 4 3 12 14 27
EGADS : 14 Yes 0 0 1 0 4 3 12 13 27
EGADS : 15 Yes 0 0 1 0 4 5 16 28
EGADS : 16 Yes 0 0 1 0 4 6 15 28
EGADS : 17 Yes 0 0 1 0 1 6 18 29
EGADS : 18 Yes 0 0 1 0 1 6 17 30
EGADS : 19 Yes 0 0 1 0 4 7 8 11 12 20 21
EGADS : 31
EGADS : 20 Yes 0 0 1 0 4 8 19 21 32
EGADS : 21 Yes 0 0 1 0 4 8 19 20 32
EGADS : 22 Yes 0 0 1 0 4 9 25 33
EGADS : 23 Yes 0 0 1 0 1 9 24 34
EGADS : 24 Yes 0 0 1 0 1 9 23 35
EGADS : 25 Yes 0 0 1 0 4 10 22 33
EGADS : 26 Yes 0 0 1 0 4 12 31 36
EGADS : 27 Yes 0 0 1 0 4 13 14
EGADS : 28 Yes 0 0 1 0 4 15 16
EGADS : 29 Yes 0 0 1 0 1 17 30 37
EGADS : 30 Yes 0 0 1 0 1 18 29 38
EGADS : 31 Yes 0 0 1 0 4 19 26 36
EGADS : 32 Yes 0 0 1 0 4 20 21
EGADS : 33 Yes 0 0 1 0 4 22 25
EGADS : 34 Yes 0 0 1 0 1 23 35 39
EGADS : 35 Yes 0 0 1 0 1 24 34 40
EGADS : 36 Yes 0 0 1 0 4 26 31
EGADS : 37 Yes 0 0 1 0 1 29 38
EGADS : 38 Yes 0 0 1 0 1 30 37
EGADS : 39 Yes 0 0 1 0 1 34 40
EGADS : 40 Yes 0 0 1 0 1 35 39
EGADS : 41 Yes 1 0 1 NA NA 43 44 45 46
EGADS : 42 Yes 1 0 1 NA NA 43 44 45 46
EGADS : 43 Yes 1 0 1 NA NA 41 42 45 46
EGADS : 44 Yes 1 0 1 NA NA 41 42 45 46
EGADS : 45 Yes 1 0 1 NA NA 41 42 43 44
EGADS : 46 Yes 1 0 1 NA NA 41 42 43 44
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 4 3 -2 -5 -6
EGADS : 2 -7 9 1 -8 10 11
EGADS : 3 -12 2 17 -16 -15 14 -13
EGADS : 4 -3 18 19 -20
EGADS : 5 21 22 -23 5
EGADS : 6 23 24 -21 6 25 26
EGADS : 7 -19 27 7 -28
EGADS : 8 -29 8 12 -33 -32 31 30
EGADS : 9 -34 -10 36 -35 37 38
EGADS : 10 -36 -11 34 -39
EGADS : 11 13 40 41 33
EGADS : 12 -17 20 46 45 44 -40 -14 -43 -42
EGADS : 13 47 48 -49 43 15
EGADS : 14 49 50 -47 16 42
EGADS : 15 51 53 -52 -22
EGADS : 16 52 54 -51 -24
EGADS : 17 -55 57 -25 -56
EGADS : 18 -57 58 56 -26
EGADS : 19 -46 28 29 61 60 32 -41 -44 59
EGADS : 20 -62 -61 -30 64 -63
EGADS : 21 -64 -31 -60 62 -65
EGADS : 22 -66 35 67 -68
EGADS : 23 69 70 -37 -71
EGADS : 24 71 -38 -70 -72
EGADS : 25 -67 39 66 -73
EGADS : 26 -74 -45 76 -75
EGADS : 27 -48 -50
EGADS : 28 -53 -54
EGADS : 29 77 55 78 79 -80 -81
EGADS : 30 -77 83 80 -82 -78 -58
EGADS : 31 -76 -59 74 -84
EGADS : 32 65 63
EGADS : 33 73 68
EGADS : 34 85 -69 86 87 -88 -89
EGADS : 35 -85 91 88 -90 -86 72
EGADS : 36 75 84
EGADS : 37 -79 92 81 -93
EGADS : 38 82 93 -83 -92
EGADS : 39 -87 94 89 -95
EGADS : 40 90 95 -91 -94
EGADS : 41 96 97 -98 -99
EGADS : 42 -100 103 102 -101
EGADS : 43 104 100 -105 -96
EGADS : 44 -106 98 107 -102
EGADS : 45 99 106 -103 -104
EGADS : 46 -97 105 101 -107
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1 2
EGADS : 2 3 4
EGADS : 3 5
EGADS : 4 6
EGADS : 5 7
EGADS : 6 8 9
EGADS : 7 10
EGADS : 8 11
EGADS : 9 12 13
EGADS : 10 14
EGADS : 11 15
EGADS : 12 16
EGADS : 13 17
EGADS : 14 18
EGADS : 15 19
EGADS : 16 20
EGADS : 17 21
EGADS : 18 22
EGADS : 19 23
EGADS : 20 24
EGADS : 21 25
EGADS : 22 26
EGADS : 23 27
EGADS : 24 28
EGADS : 25 29
EGADS : 26 30
EGADS : 27 31
EGADS : 28 32
EGADS : 29 33
EGADS : 30 34
EGADS : 31 35
EGADS : 32 36
EGADS : 33 37
EGADS : 34 38
EGADS : 35 39
EGADS : 36 40
EGADS : 37 41
EGADS : 38 42
EGADS : 39 43
EGADS : 40 44
EGADS : 41 45
EGADS : 42 46
EGADS : 43 47
EGADS : 44 48
EGADS : 45 49
EGADS : 46 50
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 4 3 -2
EGADS : 2 Yes -5 -6
EGADS : 3 Yes -7 9 1 -8
EGADS : 4 Yes 10 11
EGADS : 5 Yes -12 2 17 -16 -15 14 -13
EGADS : 6 Yes -3 18 19 -20
EGADS : 7 Yes 21 22 -23 5
EGADS : 8 Yes 23 24 -21 6
EGADS : 9 Yes 25 26
EGADS : 10 Yes -19 27 7 -28
EGADS : 11 Yes -29 8 12 -33 -32 31 30
EGADS : 12 Yes -34 -10 36 -35
EGADS : 13 Yes 37 38
EGADS : 14 Yes -36 -11 34 -39
EGADS : 15 Yes 13 40 41 33
EGADS : 16 Yes -17 20 46 45 44 -40 -14 -43 -42
EGADS : 17 Yes 47 48 -49 43 15
EGADS : 18 Yes 49 50 -47 16 42
EGADS : 19 Yes 51 53 -52 -22
EGADS : 20 Yes 52 54 -51 -24
EGADS : 21 Yes -55 57 -25 -56
EGADS : 22 Yes -57 58 56 -26
EGADS : 23 Yes -46 28 29 61 60 32 -41 -44 59
EGADS : 24 Yes -62 -61 -30 64 -63
EGADS : 25 Yes -64 -31 -60 62 -65
EGADS : 26 Yes -66 35 67 -68
EGADS : 27 Yes 69 70 -37 -71
EGADS : 28 Yes 71 -38 -70 -72
EGADS : 29 Yes -67 39 66 -73
EGADS : 30 Yes -74 -45 76 -75
EGADS : 31 Yes -48 -50
EGADS : 32 Yes -53 -54
EGADS : 33 Yes 77 55 78 79 -80 -81
EGADS : 34 Yes -77 83 80 -82 -78 -58
EGADS : 35 Yes -76 -59 74 -84
EGADS : 36 Yes 65 63
EGADS : 37 Yes 73 68
EGADS : 38 Yes 85 -69 86 87 -88 -89
EGADS : 39 Yes -85 91 88 -90 -86 72
EGADS : 40 Yes 75 84
EGADS : 41 Yes -79 92 81 -93
EGADS : 42 Yes 82 93 -83 -92
EGADS : 43 Yes -87 94 89 -95
EGADS : 44 Yes 90 95 -91 -94
EGADS : 45 Yes 96 97 -98 -99
EGADS : 46 Yes -100 103 102 -101
EGADS : 47 Yes 104 100 -105 -96
EGADS : 48 Yes -106 98 107 -102
EGADS : 49 Yes 99 106 -103 -104
EGADS : 50 Yes -97 105 101 -107
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 2 3 1 1 3
EGADS : 3 0 Yes 1 3 1 1 4
EGADS : 4 0 DEGEN 1 1 - 1
EGADS : 5 0 Yes 4 5 1 1 5
EGADS : 6 0 Yes 5 4 1 1 6
EGADS : 7 0 Yes 1 6 1 2 7
EGADS : 8 0 Yes 6 2 1 2 8
EGADS : 9 0 DEGEN 1 1 - 2
EGADS : 10 0 Yes 7 8 1 2 9
EGADS : 11 0 Yes 8 7 1 2 10
EGADS : 12 0 Yes 2 9 1 3 8
EGADS : 13 0 Yes 9 10 1 3 11
EGADS : 14 0 Yes 11 10 1 3 12
EGADS : 15 0 Yes 11 12 1 3 13
EGADS : 16 0 Yes 12 13 1 3 14
EGADS : 17 0 Yes 3 13 1 3 12
EGADS : 18 0 DEGEN 1 1 - 4
EGADS : 19 0 Yes 1 14 1 4 7
EGADS : 20 0 Yes 3 14 1 4 12
EGADS : 21 0 Yes 5 15 1 5 6
EGADS : 22 0 Yes 15 16 1 5 15
EGADS : 23 0 Yes 4 16 1 5 6
EGADS : 24 0 Yes 16 15 1 6 16
EGADS : 25 0 Yes 17 18 1 6 17
EGADS : 26 0 Yes 18 17 1 6 18
EGADS : 27 0 DEGEN 1 1 - 7
EGADS : 28 0 Yes 14 6 1 7 19
EGADS : 29 0 Yes 6 19 1 8 19
EGADS : 30 0 Yes 20 19 1 8 20
EGADS : 31 0 Yes 21 20 1 8 21
EGADS : 32 0 Yes 21 22 1 8 19
EGADS : 33 0 Yes 22 9 1 8 11
EGADS : 34 0 Yes 8 23 1 9 10
EGADS : 35 0 Yes 23 24 1 9 22
EGADS : 36 0 Yes 7 24 1 9 10
EGADS : 37 0 Yes 25 26 1 9 23
EGADS : 38 0 Yes 26 25 1 9 24
EGADS : 39 0 Yes 24 23 1 10 25
EGADS : 40 0 Yes 10 27 1 11 12
EGADS : 41 0 Yes 27 22 1 11 19
EGADS : 42 0 Yes 13 28 1 12 14
EGADS : 43 0 Yes 28 11 1 12 13
EGADS : 44 0 Yes 29 27 1 12 19
EGADS : 45 0 Yes 30 29 1 12 26
EGADS : 46 0 Yes 14 30 1 12 19
EGADS : 47 0 Yes 12 31 1 13 14
EGADS : 48 0 Yes 31 32 1 13 27
EGADS : 49 0 Yes 28 32 1 13 14
EGADS : 50 0 Yes 32 31 1 14 27
EGADS : 51 0 Yes 15 33 1 15 16
EGADS : 52 0 Yes 16 34 1 15 16
EGADS : 53 0 Yes 33 34 1 15 28
EGADS : 54 0 Yes 34 33 1 16 28
EGADS : 55 0 Yes 35 36 1 17 29
EGADS : 56 0 Yes 36 17 1 17 18
EGADS : 57 0 Yes 35 18 1 17 18
EGADS : 58 0 Yes 35 36 1 18 30
EGADS : 59 0 Yes 29 30 1 19 31
EGADS : 60 0 Yes 37 21 1 19 21
EGADS : 61 0 Yes 19 37 1 19 20
EGADS : 62 0 Yes 37 38 1 20 21
EGADS : 63 0 Yes 38 39 1 20 32
EGADS : 64 0 Yes 20 39 1 20 21
EGADS : 65 0 Yes 39 38 1 21 32
EGADS : 66 0 Yes 23 40 1 22 25
EGADS : 67 0 Yes 24 41 1 22 25
EGADS : 68 0 Yes 40 41 1 22 33
EGADS : 69 0 Yes 42 43 1 23 34
EGADS : 70 0 Yes 43 26 1 23 24
EGADS : 71 0 Yes 42 25 1 23 24
EGADS : 72 0 Yes 42 43 1 24 35
EGADS : 73 0 Yes 41 40 1 25 33
EGADS : 74 0 Yes 29 44 1 26 31
EGADS : 75 0 Yes 44 45 1 26 36
EGADS : 76 0 Yes 30 45 1 26 31
EGADS : 77 0 Yes 46 35 1 29 30
EGADS : 78 0 Yes 36 47 1 29 30
EGADS : 79 0 Yes 47 48 1 29 37
EGADS : 80 0 Yes 49 48 1 29 30
EGADS : 81 0 Yes 46 49 1 29 37
EGADS : 82 0 Yes 47 48 1 30 38
EGADS : 83 0 Yes 46 49 1 30 38
EGADS : 84 0 Yes 45 44 1 31 36
EGADS : 85 0 Yes 50 43 1 34 35
EGADS : 86 0 Yes 42 51 1 34 35
EGADS : 87 0 Yes 51 52 1 34 39
EGADS : 88 0 Yes 53 52 1 34 35
EGADS : 89 0 Yes 50 53 1 34 39
EGADS : 90 0 Yes 51 52 1 35 40
EGADS : 91 0 Yes 50 53 1 35 40
EGADS : 92 0 Yes 47 46 1 37 38
EGADS : 93 0 Yes 48 49 1 37 38
EGADS : 94 0 Yes 51 50 1 39 40
EGADS : 95 0 Yes 52 53 1 39 40
EGADS : 96 1 Yes 55 54 NA 41 43
EGADS : 97 1 Yes 54 56 NA 41 46
EGADS : 98 1 Yes 57 56 NA 41 44
EGADS : 99 1 Yes 55 57 NA 41 45
EGADS : 100 1 Yes 59 58 NA 42 43
EGADS : 101 1 Yes 58 60 NA 42 46
EGADS : 102 1 Yes 61 60 NA 42 44
EGADS : 103 1 Yes 59 61 NA 42 45
EGADS : 104 1 Yes 55 59 NA 43 45
EGADS : 105 1 Yes 54 58 NA 43 46
EGADS : 106 1 Yes 57 61 NA 44 45
EGADS : 107 1 Yes 56 60 NA 44 46
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 121.026192 0 0
EGADS : 3 Yes 121.026192 10 0
EGADS : 4 Yes 54.9020417 7.00084115 0
EGADS : 5 Yes 97.361045 7.90366896 0
EGADS : 6 Yes 121.026192 0 0
EGADS : 7 Yes 97.361045 0 0
EGADS : 8 Yes 54.9020417 0 0
EGADS : 9 Yes 165.026192 0 7
EGADS : 10 Yes 165.026192 0.5 8.5
EGADS : 11 Yes 156.577382 2.32417494 6.86784347
EGADS : 12 Yes 160.457816 1.16501909 6.24763245
EGADS : 13 Yes 152.092394 3.29252447 6.00142548
EGADS : 14 Yes 121.026192 0 10
EGADS : 15 Yes 97.9335611 36.1389817 0
EGADS : 16 Yes 75.3047874 36.1389817 0
EGADS : 17 Yes 72.4759225 29.3018771 0
EGADS : 18 Yes 83.5054156 29.3018771 0
EGADS : 19 Yes 152.092394 0 6.00142548
EGADS : 20 Yes 160.457816 0 6.24763245
EGADS : 21 Yes 156.577382 0 6.86784347
EGADS : 22 Yes 165.026192 0 8.5
EGADS : 23 Yes 75.3047874 0 0
EGADS : 24 Yes 97.9335611 0 0
EGADS : 25 Yes 72.4759225 0 0
EGADS : 26 Yes 83.5054156 0 0
EGADS : 27 Yes 165.026192 0 10
EGADS : 28 Yes 139.227902 5.03861756 7.07099122
EGADS : 29 Yes 159.822328 0 10
EGADS : 30 Yes 137.454662 0 10
EGADS : 31 Yes 173.282633 35.781198 13.6055284
EGADS : 32 Yes 165.02399 35.781198 13.6055284
EGADS : 33 Yes 123.552357 97.6729236 4.7180639
EGADS : 34 Yes 118.391317 97.6729236 3.99272703
EGADS : 35 Yes 79.4370049 29.3018771 0
EGADS : 36 Yes 70.524066 29.3018771 0
EGADS : 37 Yes 139.227902 0 7.07099122
EGADS : 38 Yes 165.02399 0 13.6055284
EGADS : 39 Yes 173.282633 0 13.6055284
EGADS : 40 Yes 118.391317 0 3.99272703
EGADS : 41 Yes 123.552357 0 4.7180639
EGADS : 42 Yes 70.524066 0 0
EGADS : 43 Yes 79.4370049 0 0
EGADS : 44 Yes 169.38016 0 35.487551
EGADS : 45 Yes 162.942213 0 35.487551
EGADS : 46 Yes 90.5173952 29.3018771 0
EGADS : 47 Yes 60.5173952 29.3018771 0
EGADS : 48 Yes 60.5173952 29.3018771 0
EGADS : 49 Yes 90.5173952 29.3018771 0
EGADS : 50 Yes 90.5173952 0 0
EGADS : 51 Yes 60.5173952 0 0
EGADS : 52 Yes 60.5173952 0 0
EGADS : 53 Yes 90.5173952 0 0
EGADS : 54 Yes 0 0 1962.43554
EGADS : 55 Yes 0 0 0
EGADS : 56 Yes 0 1953.45847 1962.43554
EGADS : 57 Yes 0 1953.45847 0
EGADS : 58 Yes 2040.09979 0 1962.43554
EGADS : 59 Yes 2040.09979 0 0
EGADS : 60 Yes 2040.09979 1953.45847 1962.43554
EGADS : 61 Yes 2040.09979 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 53.021
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 530.302
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : 23 CAD geometry 0 STD w/BL
AFLR4 : 24 CAD geometry 0 STD w/BL
AFLR4 : 25 CAD geometry 0 STD w/BL
AFLR4 : 26 CAD geometry 0 STD w/BL
AFLR4 : 27 CAD geometry 0 STD w/BL
AFLR4 : 28 CAD geometry 0 STD w/BL
AFLR4 : 29 CAD geometry 0 STD w/BL
AFLR4 : 30 CAD geometry 0 STD w/BL
AFLR4 : 31 CAD geometry 0 STD w/BL
AFLR4 : 32 CAD geometry 0 STD w/BL
AFLR4 : 33 CAD geometry 0 STD w/BL
AFLR4 : 34 CAD geometry 0 STD w/BL
AFLR4 : 35 CAD geometry 0 STD w/BL
AFLR4 : 36 CAD geometry 0 STD w/BL
AFLR4 : 37 CAD geometry 0 STD w/BL
AFLR4 : 38 CAD geometry 0 STD w/BL
AFLR4 : 39 CAD geometry 0 STD w/BL
AFLR4 : 40 CAD geometry 0 STD w/BL
AFLR4 : 41 CAD geometry 0 FARFIELD
AFLR4 : 42 CAD geometry 0 FARFIELD
AFLR4 : 43 CAD geometry 0 FARFIELD
AFLR4 : 44 CAD geometry 0 FARFIELD
AFLR4 : 45 CAD geometry 0 FARFIELD
AFLR4 : 46 CAD geometry 0 FARFIELD
AFLR4 : Case has 6 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 7 8 11 12 19
AFLR4 : Component 2 includes Definitions 5 6 9 10 15 16 22 25 28 33
AFLR4 : Component 3 includes Definitions 13 14 20 21 27 32
AFLR4 : Component 4 includes Definitions 26 31 36
AFLR4 : Component 5 includes Definitions 29 30 34 35 37 38 39 40
AFLR4 : Component 6 includes Definitions 17 18 23 24
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR4 : Define CAD surface definition 25
AFLR4 : Define CAD surface definition 26
AFLR4 : Define CAD surface definition 27
AFLR4 : Define CAD surface definition 28
AFLR4 : Define CAD surface definition 29
AFLR4 : Define CAD surface definition 30
AFLR4 : Define CAD surface definition 31
AFLR4 : Define CAD surface definition 32
AFLR4 : Define CAD surface definition 33
AFLR4 : Define CAD surface definition 34
AFLR4 : Define CAD surface definition 35
AFLR4 : Define CAD surface definition 36
AFLR4 : Define CAD surface definition 37
AFLR4 : Define CAD surface definition 38
AFLR4 : Define CAD surface definition 39
AFLR4 : Define CAD surface definition 40
AFLR4 : Define CAD surface definition 41
AFLR4 : Define CAD surface definition 42
AFLR4 : Define CAD surface definition 43
AFLR4 : Define CAD surface definition 44
AFLR4 : Define CAD surface definition 45
AFLR4 : Define CAD surface definition 46
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 246 377 0
AFLR4 : Nodes, Trias,Quads= 228 341 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 245 375 0
AFLR4 : Nodes, Trias,Quads= 231 347 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 193 322 0
AFLR4 : Nodes, Trias,Quads= 123 182 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 151 227 0
AFLR4 : Nodes, Trias,Quads= 168 261 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1008 1880 0
AFLR4 : Nodes, Trias,Quads= 667 1198 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1591 2995 0
AFLR4 : Nodes, Trias,Quads= 1102 2017 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 151 227 0
AFLR4 : Nodes, Trias,Quads= 169 263 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 193 322 0
AFLR4 : Nodes, Trias,Quads= 125 186 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1596 3005 0
AFLR4 : Nodes, Trias,Quads= 1074 1961 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 1006 1876 0
AFLR4 : Nodes, Trias,Quads= 664 1192 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 506 895 0
AFLR4 : Nodes, Trias,Quads= 318 519 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1283 2419 0
AFLR4 : Nodes, Trias,Quads= 743 1339 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1282 2418 0
AFLR4 : Nodes, Trias,Quads= 752 1358 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 2043 3860 0
AFLR4 : Nodes, Trias,Quads= 939 1652 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 1981 3736 0
AFLR4 : Nodes, Trias,Quads= 917 1608 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 360 636 0
AFLR4 : Nodes, Trias,Quads= 217 350 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 364 644 0
AFLR4 : Nodes, Trias,Quads= 222 360 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 554 991 0
AFLR4 : Nodes, Trias,Quads= 313 509 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 1279 2412 0
AFLR4 : Nodes, Trias,Quads= 752 1358 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 1280 2413 0
AFLR4 : Nodes, Trias,Quads= 746 1345 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 1992 3758 0
AFLR4 : Nodes, Trias,Quads= 930 1634 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 361 638 0
AFLR4 : Nodes, Trias,Quads= 220 356 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 359 634 0
AFLR4 : Nodes, Trias,Quads= 217 350 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 1997 3768 0
AFLR4 : Nodes, Trias,Quads= 933 1640 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 1185 2231 0
AFLR4 : Nodes, Trias,Quads= 777 1415 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 23 28 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 4557 8810 0
AFLR4 : Nodes, Trias,Quads= 4493 8682 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 4584 8864 0
AFLR4 : Nodes, Trias,Quads= 4397 8490 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 1154 2169 0
AFLR4 : Nodes, Trias,Quads= 790 1441 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 23 28 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 4604 8904 0
AFLR4 : Nodes, Trias,Quads= 4409 8514 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 4566 8828 0
AFLR4 : Nodes, Trias,Quads= 4389 8474 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 26 32 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 4906 9488 0
AFLR4 : Nodes, Trias,Quads= 4320 8316 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 4954 9584 0
AFLR4 : Nodes, Trias,Quads= 4337 8350 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 4906 9488 0
AFLR4 : Nodes, Trias,Quads= 4320 8316 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 4954 9584 0
AFLR4 : Nodes, Trias,Quads= 4337 8350 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 46710 93420 6222
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 46710 93420
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 279 433 0
AFLR4 : Nodes, Trias,Quads= 411 697 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 278 431 0
AFLR4 : Nodes, Trias,Quads= 418 711 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 242 410 0
AFLR4 : Nodes, Trias,Quads= 156 238 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 173 265 0
AFLR4 : Nodes, Trias,Quads= 209 337 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 1032 1928 0
AFLR4 : Nodes, Trias,Quads= 926 1716 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1629 3071 0
AFLR4 : Nodes, Trias,Quads= 1448 2709 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 172 263 0
AFLR4 : Nodes, Trias,Quads= 211 341 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 242 410 0
AFLR4 : Nodes, Trias,Quads= 158 242 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1619 3052 0
AFLR4 : Nodes, Trias,Quads= 1459 2732 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 1061 1985 0
AFLR4 : Nodes, Trias,Quads= 914 1691 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 566 1006 0
AFLR4 : Nodes, Trias,Quads= 447 768 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1270 2391 0
AFLR4 : Nodes, Trias,Quads= 995 1841 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1288 2429 0
AFLR4 : Nodes, Trias,Quads= 990 1833 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 1939 3656 0
AFLR4 : Nodes, Trias,Quads= 1621 3020 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 1963 3703 0
AFLR4 : Nodes, Trias,Quads= 1594 2965 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 356 628 0
AFLR4 : Nodes, Trias,Quads= 275 466 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 369 653 0
AFLR4 : Nodes, Trias,Quads= 290 495 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 592 1060 0
AFLR4 : Nodes, Trias,Quads= 435 746 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 1250 2354 0
AFLR4 : Nodes, Trias,Quads= 997 1848 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 1228 2308 0
AFLR4 : Nodes, Trias,Quads= 997 1846 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 2002 3781 0
AFLR4 : Nodes, Trias,Quads= 1595 2967 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 367 649 0
AFLR4 : Nodes, Trias,Quads= 286 487 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 357 630 0
AFLR4 : Nodes, Trias,Quads= 277 470 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 1993 3764 0
AFLR4 : Nodes, Trias,Quads= 1596 2970 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 1194 2247 0
AFLR4 : Nodes, Trias,Quads= 942 1743 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 30 40 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 4710 9112 0
AFLR4 : Nodes, Trias,Quads= 4567 8826 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 4722 9136 0
AFLR4 : Nodes, Trias,Quads= 4491 8674 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 1221 2301 0
AFLR4 : Nodes, Trias,Quads= 955 1769 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 30 40 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 4711 9114 0
AFLR4 : Nodes, Trias,Quads= 4490 8672 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 4729 9150 0
AFLR4 : Nodes, Trias,Quads= 4472 8636 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 26 32 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 4980 9633 0
AFLR4 : Nodes, Trias,Quads= 4414 8501 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 5016 9705 0
AFLR4 : Nodes, Trias,Quads= 4436 8545 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 4980 9633 0
AFLR4 : Nodes, Trias,Quads= 4414 8501 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 5016 9705 0
AFLR4 : Nodes, Trias,Quads= 4436 8545 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 53649 107298 6318
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 55553 111106
AFLR4 : Nodes, Trias = 56001 112002
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 822 1389 0
AFLR4 : Nodes, Trias,Quads= 1166 2077 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 895 1527 0
AFLR4 : Nodes, Trias,Quads= 1199 2135 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 500 889 0
AFLR4 : Nodes, Trias,Quads= 338 565 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 431 741 0
AFLR4 : Nodes, Trias,Quads= 531 941 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 2548 4881 0
AFLR4 : Nodes, Trias,Quads= 1626 3037 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 3802 7298 0
AFLR4 : Nodes, Trias,Quads= 3198 6090 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 503 876 0
AFLR4 : Nodes, Trias,Quads= 623 1116 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 502 892 0
AFLR4 : Nodes, Trias,Quads= 351 590 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 3816 7325 0
AFLR4 : Nodes, Trias,Quads= 3204 6101 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 2634 5054 0
AFLR4 : Nodes, Trias,Quads= 1634 3054 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 897 1624 0
AFLR4 : Nodes, Trias,Quads= 699 1228 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1666 3146 0
AFLR4 : Nodes, Trias,Quads= 1327 2468 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1654 3125 0
AFLR4 : Nodes, Trias,Quads= 1272 2361 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 2414 4594 0
AFLR4 : Nodes, Trias,Quads= 1819 3404 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2390 4545 0
AFLR4 : Nodes, Trias,Quads= 1802 3369 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 1557 2934 0
AFLR4 : Nodes, Trias,Quads= 935 1690 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 1503 2831 0
AFLR4 : Nodes, Trias,Quads= 899 1623 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 1056 1933 0
AFLR4 : Nodes, Trias,Quads= 835 1491 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 1750 3308 0
AFLR4 : Nodes, Trias,Quads= 1338 2484 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 1647 3107 0
AFLR4 : Nodes, Trias,Quads= 1344 2501 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 2393 4552 0
AFLR4 : Nodes, Trias,Quads= 1781 3328 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 1483 2791 0
AFLR4 : Nodes, Trias,Quads= 902 1629 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 1617 3051 0
AFLR4 : Nodes, Trias,Quads= 963 1743 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 2471 4709 0
AFLR4 : Nodes, Trias,Quads= 1809 3385 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 1469 2777 0
AFLR4 : Nodes, Trias,Quads= 1074 1987 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 30 39 0
AFLR4 : Nodes, Trias,Quads= 19 17 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 6620 12887 0
AFLR4 : Nodes, Trias,Quads= 4948 9543 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 7027 13701 0
AFLR4 : Nodes, Trias,Quads= 4861 9369 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 1460 2759 0
AFLR4 : Nodes, Trias,Quads= 1102 2043 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 30 39 0
AFLR4 : Nodes, Trias,Quads= 19 17 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 6822 13291 0
AFLR4 : Nodes, Trias,Quads= 4902 9451 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 7325 14295 0
AFLR4 : Nodes, Trias,Quads= 4905 9455 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 5067 9804 0
AFLR4 : Nodes, Trias,Quads= 4460 8590 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 5098 9866 0
AFLR4 : Nodes, Trias,Quads= 4493 8656 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 5066 9802 0
AFLR4 : Nodes, Trias,Quads= 4460 8590 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 5098 9866 0
AFLR4 : Nodes, Trias,Quads= 4493 8656 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 73 116 0
AFLR4 : Nodes, Trias,Quads= 68 106 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 67752 135504 8062
OVERALL : CPU Time = 7.876 seconds
Body 1 (of 2)
Number of nodes = 67432
Number of elements = 134868
Number of triangle elements = 134868
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 320
Number of elements = 636
Number of triangle elements = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 67752
Total number of elements = 135504
Total number of triangle elements = 135504
Total number of quadrilateral elements = 0
real 0m29.653s
user 0m30.935s
sys 0m4.005s
+ status=0
+ set +x
=================================================
solutions/session07/aflr4_InviscidTransport.py passed (as expected)
=================================================
=================================================
aflr4_InviscidTransport_150k.py test;
+ python aflr4_InviscidTransport_150k.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building pylonOml
MESSAGE:: Building nacelleOml
MESSAGE:: Building htailOml
MESSAGE:: Building vtailOml
MESSAGE:: Building fuseOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Fuselage, index = 1
Name = Wing, index = 2
Name = Htail, index = 3
Name = Pylon, index = 4
Name = Vtail, index = 5
Name = Nacelle, index = 6
Name = Farfield, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 8
Name = Fuselage, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = Htail, index = 4
Name = Pylon, index = 5
Name = Vtail, index = 6
Name = Nacelle, index = 7
Name = Farfield, index = 8
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - Fuselage
Mesh sizing name - Htail
Mesh sizing name - Pylon
Mesh sizing name - Vtail
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 40 Faces
EGADS : Body 0 has 95 Edges
EGADS : Body 0 has 44 Loops
EGADS : Body 0 has 53 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2 3 4 5 6
EGADS : 2 Yes 0 0 1 0 1 1 7 8 9 10
EGADS : 3 Yes 0 0 1 0 1 1 8 11 12 13 14
EGADS : 4 Yes 0 0 1 0 1 1 7 12
EGADS : 5 Yes 0 0 1 0 2 1 6 15
EGADS : 6 Yes 0 0 1 0 2 1 5 16 17 18
EGADS : 7 Yes 0 0 1 0 1 2 4 19
EGADS : 8 Yes 0 0 1 0 1 2 3 11 19 20 21
EGADS : 9 Yes 0 0 1 0 2 2 10 22 23 24
EGADS : 10 Yes 0 0 1 0 2 2 9 25
EGADS : 11 Yes 0 0 1 0 1 3 8 12 19
EGADS : 12 Yes 0 0 1 0 1 3 4 11 13 14 19
EGADS : 26
EGADS : 13 Yes 0 0 1 0 2 3 12 14 27
EGADS : 14 Yes 0 0 1 0 2 3 12 13 27
EGADS : 15 Yes 0 0 1 0 2 5 16 28
EGADS : 16 Yes 0 0 1 0 2 6 15 28
EGADS : 17 Yes 0 0 1 0 1 6 18 29
EGADS : 18 Yes 0 0 1 0 1 6 17 30
EGADS : 19 Yes 0 0 1 0 1 7 8 11 12 20 21
EGADS : 31
EGADS : 20 Yes 0 0 1 0 2 8 19 21 32
EGADS : 21 Yes 0 0 1 0 2 8 19 20 32
EGADS : 22 Yes 0 0 1 0 2 9 25 33
EGADS : 23 Yes 0 0 1 0 1 9 24 34
EGADS : 24 Yes 0 0 1 0 1 9 23 35
EGADS : 25 Yes 0 0 1 0 2 10 22 33
EGADS : 26 Yes 0 0 1 0 2 12 31 36
EGADS : 27 Yes 0 0 1 0 2 13 14
EGADS : 28 Yes 0 0 1 0 2 15 16
EGADS : 29 Yes 0 0 1 0 1 17 30 37
EGADS : 30 Yes 0 0 1 0 1 18 29 38
EGADS : 31 Yes 0 0 1 0 2 19 26 36
EGADS : 32 Yes 0 0 1 0 2 20 21
EGADS : 33 Yes 0 0 1 0 2 22 25
EGADS : 34 Yes 0 0 1 0 1 23 35 39
EGADS : 35 Yes 0 0 1 0 1 24 34 40
EGADS : 36 Yes 0 0 1 0 2 26 31
EGADS : 37 Yes 0 0 1 0 1 29 38
EGADS : 38 Yes 0 0 1 0 1 30 37
EGADS : 39 Yes 0 0 1 0 1 34 40
EGADS : 40 Yes 0 0 1 0 1 35 39
EGADS : 41 Yes 1 0 1 NA NA 43 44 45 46
EGADS : 42 Yes 1 0 1 NA NA 43 44 45 46
EGADS : 43 Yes 1 0 1 NA NA 41 42 45 46
EGADS : 44 Yes 1 0 1 NA NA 41 42 45 46
EGADS : 45 Yes 1 0 1 NA NA 41 42 43 44
EGADS : 46 Yes 1 0 1 NA NA 41 42 43 44
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 4 3 -2 -5 -6
EGADS : 2 -7 9 1 -8 10 11
EGADS : 3 -12 2 17 -16 -15 14 -13
EGADS : 4 -3 18 19 -20
EGADS : 5 21 22 -23 5
EGADS : 6 23 24 -21 6 25 26
EGADS : 7 -19 27 7 -28
EGADS : 8 -29 8 12 -33 -32 31 30
EGADS : 9 -34 -10 36 -35 37 38
EGADS : 10 -36 -11 34 -39
EGADS : 11 13 40 41 33
EGADS : 12 -17 20 46 45 44 -40 -14 -43 -42
EGADS : 13 47 48 -49 43 15
EGADS : 14 49 50 -47 16 42
EGADS : 15 51 53 -52 -22
EGADS : 16 52 54 -51 -24
EGADS : 17 -55 57 -25 -56
EGADS : 18 -57 58 56 -26
EGADS : 19 -46 28 29 61 60 32 -41 -44 59
EGADS : 20 -62 -61 -30 64 -63
EGADS : 21 -64 -31 -60 62 -65
EGADS : 22 -66 35 67 -68
EGADS : 23 69 70 -37 -71
EGADS : 24 71 -38 -70 -72
EGADS : 25 -67 39 66 -73
EGADS : 26 -74 -45 76 -75
EGADS : 27 -48 -50
EGADS : 28 -53 -54
EGADS : 29 77 55 78 79 -80 -81
EGADS : 30 -77 83 80 -82 -78 -58
EGADS : 31 -76 -59 74 -84
EGADS : 32 65 63
EGADS : 33 73 68
EGADS : 34 85 -69 86 87 -88 -89
EGADS : 35 -85 91 88 -90 -86 72
EGADS : 36 75 84
EGADS : 37 -79 92 81 -93
EGADS : 38 82 93 -83 -92
EGADS : 39 -87 94 89 -95
EGADS : 40 90 95 -91 -94
EGADS : 41 96 97 -98 -99
EGADS : 42 -100 103 102 -101
EGADS : 43 104 100 -105 -96
EGADS : 44 -106 98 107 -102
EGADS : 45 99 106 -103 -104
EGADS : 46 -97 105 101 -107
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1 2
EGADS : 2 3 4
EGADS : 3 5
EGADS : 4 6
EGADS : 5 7
EGADS : 6 8 9
EGADS : 7 10
EGADS : 8 11
EGADS : 9 12 13
EGADS : 10 14
EGADS : 11 15
EGADS : 12 16
EGADS : 13 17
EGADS : 14 18
EGADS : 15 19
EGADS : 16 20
EGADS : 17 21
EGADS : 18 22
EGADS : 19 23
EGADS : 20 24
EGADS : 21 25
EGADS : 22 26
EGADS : 23 27
EGADS : 24 28
EGADS : 25 29
EGADS : 26 30
EGADS : 27 31
EGADS : 28 32
EGADS : 29 33
EGADS : 30 34
EGADS : 31 35
EGADS : 32 36
EGADS : 33 37
EGADS : 34 38
EGADS : 35 39
EGADS : 36 40
EGADS : 37 41
EGADS : 38 42
EGADS : 39 43
EGADS : 40 44
EGADS : 41 45
EGADS : 42 46
EGADS : 43 47
EGADS : 44 48
EGADS : 45 49
EGADS : 46 50
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 4 3 -2
EGADS : 2 Yes -5 -6
EGADS : 3 Yes -7 9 1 -8
EGADS : 4 Yes 10 11
EGADS : 5 Yes -12 2 17 -16 -15 14 -13
EGADS : 6 Yes -3 18 19 -20
EGADS : 7 Yes 21 22 -23 5
EGADS : 8 Yes 23 24 -21 6
EGADS : 9 Yes 25 26
EGADS : 10 Yes -19 27 7 -28
EGADS : 11 Yes -29 8 12 -33 -32 31 30
EGADS : 12 Yes -34 -10 36 -35
EGADS : 13 Yes 37 38
EGADS : 14 Yes -36 -11 34 -39
EGADS : 15 Yes 13 40 41 33
EGADS : 16 Yes -17 20 46 45 44 -40 -14 -43 -42
EGADS : 17 Yes 47 48 -49 43 15
EGADS : 18 Yes 49 50 -47 16 42
EGADS : 19 Yes 51 53 -52 -22
EGADS : 20 Yes 52 54 -51 -24
EGADS : 21 Yes -55 57 -25 -56
EGADS : 22 Yes -57 58 56 -26
EGADS : 23 Yes -46 28 29 61 60 32 -41 -44 59
EGADS : 24 Yes -62 -61 -30 64 -63
EGADS : 25 Yes -64 -31 -60 62 -65
EGADS : 26 Yes -66 35 67 -68
EGADS : 27 Yes 69 70 -37 -71
EGADS : 28 Yes 71 -38 -70 -72
EGADS : 29 Yes -67 39 66 -73
EGADS : 30 Yes -74 -45 76 -75
EGADS : 31 Yes -48 -50
EGADS : 32 Yes -53 -54
EGADS : 33 Yes 77 55 78 79 -80 -81
EGADS : 34 Yes -77 83 80 -82 -78 -58
EGADS : 35 Yes -76 -59 74 -84
EGADS : 36 Yes 65 63
EGADS : 37 Yes 73 68
EGADS : 38 Yes 85 -69 86 87 -88 -89
EGADS : 39 Yes -85 91 88 -90 -86 72
EGADS : 40 Yes 75 84
EGADS : 41 Yes -79 92 81 -93
EGADS : 42 Yes 82 93 -83 -92
EGADS : 43 Yes -87 94 89 -95
EGADS : 44 Yes 90 95 -91 -94
EGADS : 45 Yes 96 97 -98 -99
EGADS : 46 Yes -100 103 102 -101
EGADS : 47 Yes 104 100 -105 -96
EGADS : 48 Yes -106 98 107 -102
EGADS : 49 Yes 99 106 -103 -104
EGADS : 50 Yes -97 105 101 -107
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 2
EGADS : 2 0 Yes 2 3 1 1 3
EGADS : 3 0 Yes 1 3 1 1 4
EGADS : 4 0 DEGEN 1 1 - 1
EGADS : 5 0 Yes 4 5 1 1 5
EGADS : 6 0 Yes 5 4 1 1 6
EGADS : 7 0 Yes 1 6 1 2 7
EGADS : 8 0 Yes 6 2 1 2 8
EGADS : 9 0 DEGEN 1 1 - 2
EGADS : 10 0 Yes 7 8 1 2 9
EGADS : 11 0 Yes 8 7 1 2 10
EGADS : 12 0 Yes 2 9 1 3 8
EGADS : 13 0 Yes 9 10 1 3 11
EGADS : 14 0 Yes 11 10 1 3 12
EGADS : 15 0 Yes 11 12 1 3 13
EGADS : 16 0 Yes 12 13 1 3 14
EGADS : 17 0 Yes 3 13 1 3 12
EGADS : 18 0 DEGEN 1 1 - 4
EGADS : 19 0 Yes 1 14 1 4 7
EGADS : 20 0 Yes 3 14 1 4 12
EGADS : 21 0 Yes 5 15 1 5 6
EGADS : 22 0 Yes 15 16 1 5 15
EGADS : 23 0 Yes 4 16 1 5 6
EGADS : 24 0 Yes 16 15 1 6 16
EGADS : 25 0 Yes 17 18 1 6 17
EGADS : 26 0 Yes 18 17 1 6 18
EGADS : 27 0 DEGEN 1 1 - 7
EGADS : 28 0 Yes 14 6 1 7 19
EGADS : 29 0 Yes 6 19 1 8 19
EGADS : 30 0 Yes 20 19 1 8 20
EGADS : 31 0 Yes 21 20 1 8 21
EGADS : 32 0 Yes 21 22 1 8 19
EGADS : 33 0 Yes 22 9 1 8 11
EGADS : 34 0 Yes 8 23 1 9 10
EGADS : 35 0 Yes 23 24 1 9 22
EGADS : 36 0 Yes 7 24 1 9 10
EGADS : 37 0 Yes 25 26 1 9 23
EGADS : 38 0 Yes 26 25 1 9 24
EGADS : 39 0 Yes 24 23 1 10 25
EGADS : 40 0 Yes 10 27 1 11 12
EGADS : 41 0 Yes 27 22 1 11 19
EGADS : 42 0 Yes 13 28 1 12 14
EGADS : 43 0 Yes 28 11 1 12 13
EGADS : 44 0 Yes 29 27 1 12 19
EGADS : 45 0 Yes 30 29 1 12 26
EGADS : 46 0 Yes 14 30 1 12 19
EGADS : 47 0 Yes 12 31 1 13 14
EGADS : 48 0 Yes 31 32 1 13 27
EGADS : 49 0 Yes 28 32 1 13 14
EGADS : 50 0 Yes 32 31 1 14 27
EGADS : 51 0 Yes 15 33 1 15 16
EGADS : 52 0 Yes 16 34 1 15 16
EGADS : 53 0 Yes 33 34 1 15 28
EGADS : 54 0 Yes 34 33 1 16 28
EGADS : 55 0 Yes 35 36 1 17 29
EGADS : 56 0 Yes 36 17 1 17 18
EGADS : 57 0 Yes 35 18 1 17 18
EGADS : 58 0 Yes 35 36 1 18 30
EGADS : 59 0 Yes 29 30 1 19 31
EGADS : 60 0 Yes 37 21 1 19 21
EGADS : 61 0 Yes 19 37 1 19 20
EGADS : 62 0 Yes 37 38 1 20 21
EGADS : 63 0 Yes 38 39 1 20 32
EGADS : 64 0 Yes 20 39 1 20 21
EGADS : 65 0 Yes 39 38 1 21 32
EGADS : 66 0 Yes 23 40 1 22 25
EGADS : 67 0 Yes 24 41 1 22 25
EGADS : 68 0 Yes 40 41 1 22 33
EGADS : 69 0 Yes 42 43 1 23 34
EGADS : 70 0 Yes 43 26 1 23 24
EGADS : 71 0 Yes 42 25 1 23 24
EGADS : 72 0 Yes 42 43 1 24 35
EGADS : 73 0 Yes 41 40 1 25 33
EGADS : 74 0 Yes 29 44 1 26 31
EGADS : 75 0 Yes 44 45 1 26 36
EGADS : 76 0 Yes 30 45 1 26 31
EGADS : 77 0 Yes 46 35 1 29 30
EGADS : 78 0 Yes 36 47 1 29 30
EGADS : 79 0 Yes 47 48 1 29 37
EGADS : 80 0 Yes 49 48 1 29 30
EGADS : 81 0 Yes 46 49 1 29 37
EGADS : 82 0 Yes 47 48 1 30 38
EGADS : 83 0 Yes 46 49 1 30 38
EGADS : 84 0 Yes 45 44 1 31 36
EGADS : 85 0 Yes 50 43 1 34 35
EGADS : 86 0 Yes 42 51 1 34 35
EGADS : 87 0 Yes 51 52 1 34 39
EGADS : 88 0 Yes 53 52 1 34 35
EGADS : 89 0 Yes 50 53 1 34 39
EGADS : 90 0 Yes 51 52 1 35 40
EGADS : 91 0 Yes 50 53 1 35 40
EGADS : 92 0 Yes 47 46 1 37 38
EGADS : 93 0 Yes 48 49 1 37 38
EGADS : 94 0 Yes 51 50 1 39 40
EGADS : 95 0 Yes 52 53 1 39 40
EGADS : 96 1 Yes 55 54 NA 41 43
EGADS : 97 1 Yes 54 56 NA 41 46
EGADS : 98 1 Yes 57 56 NA 41 44
EGADS : 99 1 Yes 55 57 NA 41 45
EGADS : 100 1 Yes 59 58 NA 42 43
EGADS : 101 1 Yes 58 60 NA 42 46
EGADS : 102 1 Yes 61 60 NA 42 44
EGADS : 103 1 Yes 59 61 NA 42 45
EGADS : 104 1 Yes 55 59 NA 43 45
EGADS : 105 1 Yes 54 58 NA 43 46
EGADS : 106 1 Yes 57 61 NA 44 45
EGADS : 107 1 Yes 56 60 NA 44 46
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0
EGADS : 2 Yes 121.026192 0 0
EGADS : 3 Yes 121.026192 10 0
EGADS : 4 Yes 54.9020417 7.00084115 0
EGADS : 5 Yes 97.361045 7.90366896 0
EGADS : 6 Yes 121.026192 0 0
EGADS : 7 Yes 97.361045 0 0
EGADS : 8 Yes 54.9020417 0 0
EGADS : 9 Yes 165.026192 0 7
EGADS : 10 Yes 165.026192 0.5 8.5
EGADS : 11 Yes 156.577382 2.32417494 6.86784347
EGADS : 12 Yes 160.457816 1.16501909 6.24763245
EGADS : 13 Yes 152.092394 3.29252447 6.00142548
EGADS : 14 Yes 121.026192 0 10
EGADS : 15 Yes 97.9335611 36.1389817 0
EGADS : 16 Yes 75.3047874 36.1389817 0
EGADS : 17 Yes 72.4759225 29.3018771 0
EGADS : 18 Yes 83.5054156 29.3018771 0
EGADS : 19 Yes 152.092394 0 6.00142548
EGADS : 20 Yes 160.457816 0 6.24763245
EGADS : 21 Yes 156.577382 0 6.86784347
EGADS : 22 Yes 165.026192 0 8.5
EGADS : 23 Yes 75.3047874 0 0
EGADS : 24 Yes 97.9335611 0 0
EGADS : 25 Yes 72.4759225 0 0
EGADS : 26 Yes 83.5054156 0 0
EGADS : 27 Yes 165.026192 0 10
EGADS : 28 Yes 139.227902 5.03861756 7.07099122
EGADS : 29 Yes 159.822328 0 10
EGADS : 30 Yes 137.454662 0 10
EGADS : 31 Yes 173.282633 35.781198 13.6055284
EGADS : 32 Yes 165.02399 35.781198 13.6055284
EGADS : 33 Yes 123.552357 97.6729236 4.7180639
EGADS : 34 Yes 118.391317 97.6729236 3.99272703
EGADS : 35 Yes 79.4370049 29.3018771 0
EGADS : 36 Yes 70.524066 29.3018771 0
EGADS : 37 Yes 139.227902 0 7.07099122
EGADS : 38 Yes 165.02399 0 13.6055284
EGADS : 39 Yes 173.282633 0 13.6055284
EGADS : 40 Yes 118.391317 0 3.99272703
EGADS : 41 Yes 123.552357 0 4.7180639
EGADS : 42 Yes 70.524066 0 0
EGADS : 43 Yes 79.4370049 0 0
EGADS : 44 Yes 169.38016 0 35.487551
EGADS : 45 Yes 162.942213 0 35.487551
EGADS : 46 Yes 90.5173952 29.3018771 0
EGADS : 47 Yes 60.5173952 29.3018771 0
EGADS : 48 Yes 60.5173952 29.3018771 0
EGADS : 49 Yes 90.5173952 29.3018771 0
EGADS : 50 Yes 90.5173952 0 0
EGADS : 51 Yes 60.5173952 0 0
EGADS : 52 Yes 60.5173952 0 0
EGADS : 53 Yes 90.5173952 0 0
EGADS : 54 Yes 0 0 1962.43554
EGADS : 55 Yes 0 0 0
EGADS : 56 Yes 0 1953.45847 1962.43554
EGADS : 57 Yes 0 1953.45847 0
EGADS : 58 Yes 2040.09979 0 1962.43554
EGADS : 59 Yes 2040.09979 0 0
EGADS : 60 Yes 2040.09979 1953.45847 1962.43554
EGADS : 61 Yes 2040.09979 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 53.021
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 1060.6
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 2
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : 23 CAD geometry 0 STD w/BL
AFLR4 : 24 CAD geometry 0 STD w/BL
AFLR4 : 25 CAD geometry 0 STD w/BL
AFLR4 : 26 CAD geometry 0 STD w/BL
AFLR4 : 27 CAD geometry 0 STD w/BL
AFLR4 : 28 CAD geometry 0 STD w/BL
AFLR4 : 29 CAD geometry 0 STD w/BL
AFLR4 : 30 CAD geometry 0 STD w/BL
AFLR4 : 31 CAD geometry 0 STD w/BL
AFLR4 : 32 CAD geometry 0 STD w/BL
AFLR4 : 33 CAD geometry 0 STD w/BL
AFLR4 : 34 CAD geometry 0 STD w/BL
AFLR4 : 35 CAD geometry 0 STD w/BL
AFLR4 : 36 CAD geometry 0 STD w/BL
AFLR4 : 37 CAD geometry 0 STD w/BL
AFLR4 : 38 CAD geometry 0 STD w/BL
AFLR4 : 39 CAD geometry 0 STD w/BL
AFLR4 : 40 CAD geometry 0 STD w/BL
AFLR4 : 41 CAD geometry 0 FARFIELD
AFLR4 : 42 CAD geometry 0 FARFIELD
AFLR4 : 43 CAD geometry 0 FARFIELD
AFLR4 : 44 CAD geometry 0 FARFIELD
AFLR4 : 45 CAD geometry 0 FARFIELD
AFLR4 : 46 CAD geometry 0 FARFIELD
AFLR4 : Case has 6 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 7 8 11 12 19
AFLR4 : Component 2 includes Definitions 5 6 9 10 15 16 22 25 28 33
AFLR4 : Component 3 includes Definitions 13 14 20 21 27 32
AFLR4 : Component 4 includes Definitions 26 31 36
AFLR4 : Component 5 includes Definitions 29 30 34 35 37 38 39 40
AFLR4 : Component 6 includes Definitions 17 18 23 24
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Define CAD surface definition 23
AFLR4 : Define CAD surface definition 24
AFLR4 : Define CAD surface definition 25
AFLR4 : Define CAD surface definition 26
AFLR4 : Define CAD surface definition 27
AFLR4 : Define CAD surface definition 28
AFLR4 : Define CAD surface definition 29
AFLR4 : Define CAD surface definition 30
AFLR4 : Define CAD surface definition 31
AFLR4 : Define CAD surface definition 32
AFLR4 : Define CAD surface definition 33
AFLR4 : Define CAD surface definition 34
AFLR4 : Define CAD surface definition 35
AFLR4 : Define CAD surface definition 36
AFLR4 : Define CAD surface definition 37
AFLR4 : Define CAD surface definition 38
AFLR4 : Define CAD surface definition 39
AFLR4 : Define CAD surface definition 40
AFLR4 : Define CAD surface definition 41
AFLR4 : Define CAD surface definition 42
AFLR4 : Define CAD surface definition 43
AFLR4 : Define CAD surface definition 44
AFLR4 : Define CAD surface definition 45
AFLR4 : Define CAD surface definition 46
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 327 522 0
AFLR4 : Nodes, Trias,Quads= 305 478 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 329 526 0
AFLR4 : Nodes, Trias,Quads= 303 474 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 207 346 0
AFLR4 : Nodes, Trias,Quads= 137 206 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 192 299 0
AFLR4 : Nodes, Trias,Quads= 210 335 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 720 1326 0
AFLR4 : Nodes, Trias,Quads= 529 944 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 997 1847 0
AFLR4 : Nodes, Trias,Quads= 752 1357 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 192 299 0
AFLR4 : Nodes, Trias,Quads= 209 333 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 206 344 0
AFLR4 : Nodes, Trias,Quads= 136 204 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 997 1847 0
AFLR4 : Nodes, Trias,Quads= 746 1345 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 714 1314 0
AFLR4 : Nodes, Trias,Quads= 521 928 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 34 46 0
AFLR4 : Nodes, Trias,Quads= 32 42 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 731 1320 0
AFLR4 : Nodes, Trias,Quads= 492 842 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1370 2586 0
AFLR4 : Nodes, Trias,Quads= 805 1456 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1357 2560 0
AFLR4 : Nodes, Trias,Quads= 802 1450 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 1943 3668 0
AFLR4 : Nodes, Trias,Quads= 877 1536 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 1868 3519 0
AFLR4 : Nodes, Trias,Quads= 849 1481 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 150 248 0
AFLR4 : Nodes, Trias,Quads= 96 140 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 158 264 0
AFLR4 : Nodes, Trias,Quads= 98 144 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 850 1558 0
AFLR4 : Nodes, Trias,Quads= 456 770 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 1363 2572 0
AFLR4 : Nodes, Trias,Quads= 809 1464 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 1368 2582 0
AFLR4 : Nodes, Trias,Quads= 808 1462 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 1874 3531 0
AFLR4 : Nodes, Trias,Quads= 851 1485 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 157 262 0
AFLR4 : Nodes, Trias,Quads= 98 144 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 152 252 0
AFLR4 : Nodes, Trias,Quads= 95 138 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 1917 3616 0
AFLR4 : Nodes, Trias,Quads= 875 1532 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 1258 2369 0
AFLR4 : Nodes, Trias,Quads= 856 1565 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 23 28 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 1026 1934 0
AFLR4 : Nodes, Trias,Quads= 996 1874 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 1024 1930 0
AFLR4 : Nodes, Trias,Quads= 1031 1944 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 1283 2419 0
AFLR4 : Nodes, Trias,Quads= 848 1549 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 32 40 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 23 28 0
AFLR4 : Nodes, Trias,Quads= 16 14 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 1022 1926 0
AFLR4 : Nodes, Trias,Quads= 1023 1928 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 1026 1934 0
AFLR4 : Nodes, Trias,Quads= 1023 1928 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 26 32 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 549 997 0
AFLR4 : Nodes, Trias,Quads= 464 827 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 539 977 0
AFLR4 : Nodes, Trias,Quads= 461 821 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 549 997 0
AFLR4 : Nodes, Trias,Quads= 464 827 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 539 977 0
AFLR4 : Nodes, Trias,Quads= 461 821 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 17483 34966 4366
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 17483 34966
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 341 543 0
AFLR4 : Nodes, Trias,Quads= 530 921 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 335 531 0
AFLR4 : Nodes, Trias,Quads= 523 907 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 275 472 0
AFLR4 : Nodes, Trias,Quads= 184 290 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 222 354 0
AFLR4 : Nodes, Trias,Quads= 237 384 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 782 1447 0
AFLR4 : Nodes, Trias,Quads= 663 1209 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1016 1884 0
AFLR4 : Nodes, Trias,Quads= 903 1658 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 221 352 0
AFLR4 : Nodes, Trias,Quads= 238 386 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 260 442 0
AFLR4 : Nodes, Trias,Quads= 179 280 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1017 1886 0
AFLR4 : Nodes, Trias,Quads= 895 1642 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 784 1451 0
AFLR4 : Nodes, Trias,Quads= 654 1191 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 34 46 0
AFLR4 : Nodes, Trias,Quads= 32 42 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 797 1447 0
AFLR4 : Nodes, Trias,Quads= 657 1167 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1388 2619 0
AFLR4 : Nodes, Trias,Quads= 1053 1949 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1387 2619 0
AFLR4 : Nodes, Trias,Quads= 1033 1911 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 1865 3515 0
AFLR4 : Nodes, Trias,Quads= 1494 2773 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 1851 3487 0
AFLR4 : Nodes, Trias,Quads= 1475 2735 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 151 250 0
AFLR4 : Nodes, Trias,Quads= 104 156 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 153 254 0
AFLR4 : Nodes, Trias,Quads= 106 160 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 864 1581 0
AFLR4 : Nodes, Trias,Quads= 654 1161 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 1408 2661 0
AFLR4 : Nodes, Trias,Quads= 1029 1903 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 1379 2601 0
AFLR4 : Nodes, Trias,Quads= 1055 1953 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 1863 3512 0
AFLR4 : Nodes, Trias,Quads= 1504 2794 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 152 252 0
AFLR4 : Nodes, Trias,Quads= 107 162 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 148 244 0
AFLR4 : Nodes, Trias,Quads= 107 162 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 1874 3534 0
AFLR4 : Nodes, Trias,Quads= 1468 2722 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 1251 2354 0
AFLR4 : Nodes, Trias,Quads= 1009 1870 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 30 40 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 1050 1977 0
AFLR4 : Nodes, Trias,Quads= 1007 1891 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 1063 2003 0
AFLR4 : Nodes, Trias,Quads= 1050 1977 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 1283 2418 0
AFLR4 : Nodes, Trias,Quads= 993 1838 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 30 40 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 1068 2013 0
AFLR4 : Nodes, Trias,Quads= 1038 1953 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 1051 1979 0
AFLR4 : Nodes, Trias,Quads= 1060 1997 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 26 32 0
AFLR4 : Nodes, Trias,Quads= 18 16 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 614 1122 0
AFLR4 : Nodes, Trias,Quads= 538 970 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 613 1120 0
AFLR4 : Nodes, Trias,Quads= 536 966 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 614 1122 0
AFLR4 : Nodes, Trias,Quads= 538 970 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 613 1120 0
AFLR4 : Nodes, Trias,Quads= 536 966 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 23106 46212 4470
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 24906 49812
AFLR4 : Nodes, Trias = 25207 50414
AFLR4 : Nodes, Trias = 25245 50490
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 842 1427 0
AFLR4 : Nodes, Trias,Quads= 1286 2315 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 824 1394 0
AFLR4 : Nodes, Trias,Quads= 1230 2206 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 546 976 0
AFLR4 : Nodes, Trias,Quads= 382 648 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 478 832 0
AFLR4 : Nodes, Trias,Quads= 548 972 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 2072 3948 0
AFLR4 : Nodes, Trias,Quads= 1403 2610 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 2244 4252 0
AFLR4 : Nodes, Trias,Quads= 2187 4138 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 508 888 0
AFLR4 : Nodes, Trias,Quads= 579 1030 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 553 990 0
AFLR4 : Nodes, Trias,Quads= 378 640 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 2230 4228 0
AFLR4 : Nodes, Trias,Quads= 2157 4082 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 1967 3745 0
AFLR4 : Nodes, Trias,Quads= 1349 2509 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 34 46 0
AFLR4 : Nodes, Trias,Quads= 32 42 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 1260 2312 0
AFLR4 : Nodes, Trias,Quads= 1211 2214 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 1804 3408 0
AFLR4 : Nodes, Trias,Quads= 1444 2688 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 1966 3721 0
AFLR4 : Nodes, Trias,Quads= 1473 2735 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 2243 4262 0
AFLR4 : Nodes, Trias,Quads= 1711 3198 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2224 4225 0
AFLR4 : Nodes, Trias,Quads= 1670 3117 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 867 1604 0
AFLR4 : Nodes, Trias,Quads= 540 950 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 781 1440 0
AFLR4 : Nodes, Trias,Quads= 488 854 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 1502 2798 0
AFLR4 : Nodes, Trias,Quads= 1196 2186 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 1929 3652 0
AFLR4 : Nodes, Trias,Quads= 1448 2690 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 1717 3238 0
AFLR4 : Nodes, Trias,Quads= 1404 2612 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 2242 4262 0
AFLR4 : Nodes, Trias,Quads= 1671 3120 0
AFLR4 : Generate optimal mesh on surface definition 23
AFLR2 : Nodes, Trias,Quads= 740 1361 0
AFLR4 : Nodes, Trias,Quads= 455 791 0
AFLR4 : Generate optimal mesh on surface definition 24
AFLR2 : Nodes, Trias,Quads= 829 1531 0
AFLR4 : Nodes, Trias,Quads= 516 905 0
AFLR4 : Generate optimal mesh on surface definition 25
AFLR2 : Nodes, Trias,Quads= 2260 4297 0
AFLR4 : Nodes, Trias,Quads= 1664 3105 0
AFLR4 : Generate optimal mesh on surface definition 26
AFLR2 : Nodes, Trias,Quads= 1507 2846 0
AFLR4 : Nodes, Trias,Quads= 1151 2134 0
AFLR4 : Generate optimal mesh on surface definition 27
AFLR2 : Nodes, Trias,Quads= 35 45 0
AFLR4 : Nodes, Trias,Quads= 23 21 0
AFLR4 : Generate optimal mesh on surface definition 28
AFLR2 : Nodes, Trias,Quads= 30 39 0
AFLR4 : Nodes, Trias,Quads= 19 17 0
AFLR4 : Generate optimal mesh on surface definition 29
AFLR2 : Nodes, Trias,Quads= 1742 3319 0
AFLR4 : Nodes, Trias,Quads= 1421 2677 0
AFLR4 : Generate optimal mesh on surface definition 30
AFLR2 : Nodes, Trias,Quads= 1706 3250 0
AFLR4 : Nodes, Trias,Quads= 1419 2676 0
AFLR4 : Generate optimal mesh on surface definition 31
AFLR2 : Nodes, Trias,Quads= 1521 2874 0
AFLR4 : Nodes, Trias,Quads= 1145 2122 0
AFLR4 : Generate optimal mesh on surface definition 32
AFLR2 : Nodes, Trias,Quads= 33 42 0
AFLR4 : Nodes, Trias,Quads= 22 20 0
AFLR4 : Generate optimal mesh on surface definition 33
AFLR2 : Nodes, Trias,Quads= 30 39 0
AFLR4 : Nodes, Trias,Quads= 19 17 0
AFLR4 : Generate optimal mesh on surface definition 34
AFLR2 : Nodes, Trias,Quads= 1700 3238 0
AFLR4 : Nodes, Trias,Quads= 1405 2648 0
AFLR4 : Generate optimal mesh on surface definition 35
AFLR2 : Nodes, Trias,Quads= 1792 3419 0
AFLR4 : Nodes, Trias,Quads= 1444 2723 0
AFLR4 : Generate optimal mesh on surface definition 36
AFLR2 : Nodes, Trias,Quads= 30 38 0
AFLR4 : Nodes, Trias,Quads= 20 18 0
AFLR4 : Generate optimal mesh on surface definition 37
AFLR2 : Nodes, Trias,Quads= 617 1127 0
AFLR4 : Nodes, Trias,Quads= 563 1019 0
AFLR4 : Generate optimal mesh on surface definition 38
AFLR2 : Nodes, Trias,Quads= 618 1129 0
AFLR4 : Nodes, Trias,Quads= 558 1009 0
AFLR4 : Generate optimal mesh on surface definition 39
AFLR2 : Nodes, Trias,Quads= 617 1127 0
AFLR4 : Nodes, Trias,Quads= 563 1019 0
AFLR4 : Generate optimal mesh on surface definition 40
AFLR2 : Nodes, Trias,Quads= 618 1129 0
AFLR4 : Nodes, Trias,Quads= 559 1011 0
AFLR4 : Generate optimal mesh on surface definition 41
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 42
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 43
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 44
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 45
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
AFLR4 : Generate optimal mesh on surface definition 46
AFLR2 : Nodes, Trias,Quads= 20 26 0
AFLR4 : Nodes, Trias,Quads= 16 18 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 35798 71596 6018
OVERALL : CPU Time = 4.487 seconds
Body 1 (of 2)
Number of nodes = 35742
Number of elements = 71488
Number of triangle elements = 71488
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 56
Number of elements = 108
Number of triangle elements = 108
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 35798
Total number of elements = 71596
Total number of triangle elements = 71596
Total number of quadrilateral elements = 0
--> Toal Elements 71596
real 0m26.201s
user 0m27.113s
sys 0m4.550s
+ status=0
+ set +x
=================================================
solutions/session07/aflr4_InviscidTransport_150k.py passed (as expected)
=================================================
=================================================
2_su2_InviscidWing.py test;
+ python 2_su2_InviscidWing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 6
EGADS : 2 Yes 0 0 1 1 1 1 4 5
EGADS : 3 Yes 0 0 1 1 1 1 4 8
EGADS : 4 Yes 0 0 1 1 1 2 3 5
EGADS : 5 Yes 0 0 1 1 1 2 4
EGADS : 6 Yes 0 0 1 1 1 1 7 8
EGADS : 7 Yes 0 0 1 1 1 6 9 10
EGADS : 8 Yes 0 0 1 1 1 3 6 9
EGADS : 9 Yes 0 0 1 1 1 7 8 10
EGADS : 10 Yes 0 0 1 1 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 2651.51
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 5
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1107 2082 0
AFLR4 : Nodes, Trias,Quads= 685 1238 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1473 2759 0
AFLR4 : Nodes, Trias,Quads= 721 1255 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1116 2100 0
AFLR4 : Nodes, Trias,Quads= 671 1210 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1458 2729 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1108 2084 0
AFLR4 : Nodes, Trias,Quads= 683 1234 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 1488 2789 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1112 2092 0
AFLR4 : Nodes, Trias,Quads= 653 1174 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1456 2725 0
AFLR4 : Nodes, Trias,Quads= 708 1229 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 4933 9858 1312
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 4933 9858
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 12796 24695 0
AFLR4 : Nodes, Trias,Quads= 7764 14631 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 29245 57075 0
AFLR4 : Nodes, Trias,Quads= 12448 23481 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 12136 23411 0
AFLR4 : Nodes, Trias,Quads= 7447 14033 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 29424 57435 0
AFLR4 : Nodes, Trias,Quads= 12399 23385 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 196 293 0
AFLR4 : Nodes, Trias,Quads= 188 277 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 12819 24741 0
AFLR4 : Nodes, Trias,Quads= 7725 14553 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 29449 57483 0
AFLR4 : Nodes, Trias,Quads= 12413 23411 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 12144 23427 0
AFLR4 : Nodes, Trias,Quads= 7471 14081 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 29445 57477 0
AFLR4 : Nodes, Trias,Quads= 12478 23543 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 196 293 0
AFLR4 : Nodes, Trias,Quads= 188 277 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 75858 151708 9398
OVERALL : CPU Time = 3.002 seconds
Body 1 (of 2)
Number of nodes = 75838
Number of elements = 151672
Number of triangle elements = 151672
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75858
Total number of elements = 151708
Total number of triangle elements = 151708
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 6
EGADS : 2 Yes 0 0 1 1 1 1 4 5
EGADS : 3 Yes 0 0 1 1 1 1 4 8
EGADS : 4 Yes 0 0 1 1 1 2 3 5
EGADS : 5 Yes 0 0 1 1 1 2 4
EGADS : 6 Yes 0 0 1 1 1 1 7 8
EGADS : 7 Yes 0 0 1 1 1 6 9 10
EGADS : 8 Yes 0 0 1 1 1 3 6 9
EGADS : 9 Yes 0 0 1 1 1 7 8 10
EGADS : 10 Yes 0 0 1 1 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 13.1976
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 428.309
AFLR4 : Abs Min Surf Spacing = 0.032994
AFLR4 : Min Surf Spacing = 0.065988
AFLR4 : Max Surf Spacing = 1.31976
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 151708
AFLR43 : Nodes = 75858
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 75858 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 FarField
UG3 : 12 FarField
UG3 : 13 FarField
UG3 : 14 FarField
UG3 : 15 FarField
UG3 : 16 FarField
AFLR3 : CPU Time = 0.250 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 75858 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 15174 110930
AFLR3 IG : Nodes, Elements = 30348 239512
AFLR3 IG : Nodes, Elements = 45522 364376
AFLR3 IG : Nodes, Elements = 60696 488708
AFLR3 IG : Nodes, Elements = 75865 649511
AFLR3 IG : Nodes, Elements = 75865 648308
AFLR3 IG : Nodes, Elements = 75865 648424
AFLR3 IG : Nodes, Elements = 75865 647472
AFLR3 IG : Nodes, Elements = 75858 416319
AFLR3 IG : Nodes, Elements = 75858 417620
AFLR3 IG : Nodes, Elements = 75858 262267
AFLR3 IG : Nodes, Elements = 75858 238929
AFLR3 : CPU Time = 9.489 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 75858 238929
AFLR3 GG : Nodes, Elements = 97121 303288
AFLR3 GG : Nodes, Elements = 97121 384995
AFLR3 GG : Nodes, Elements = 97121 351355
AFLR3 GG : Nodes, Elements = 114881 407778
AFLR3 GG : Nodes, Elements = 114881 484750
AFLR3 GG : Nodes, Elements = 114881 454637
AFLR3 GG : Nodes, Elements = 138960 529123
AFLR3 GG : Nodes, Elements = 138960 631021
AFLR3 GG : Nodes, Elements = 138960 592337
AFLR3 GG : Nodes, Elements = 164714 671223
AFLR3 GG : Nodes, Elements = 164714 782517
AFLR3 GG : Nodes, Elements = 164714 744165
AFLR3 GG : Nodes, Elements = 193389 831240
AFLR3 GG : Nodes, Elements = 193389 952591
AFLR3 GG : Nodes, Elements = 193389 915788
AFLR3 GG : Nodes, Elements = 223793 1007653
AFLR3 GG : Nodes, Elements = 223793 1131220
AFLR3 GG : Nodes, Elements = 223793 1095610
AFLR3 GG : Nodes, Elements = 254697 1188716
AFLR3 GG : Nodes, Elements = 254697 1312627
AFLR3 GG : Nodes, Elements = 254697 1278678
AFLR3 GG : Nodes, Elements = 285123 1370225
AFLR3 GG : Nodes, Elements = 285123 1492164
AFLR3 GG : Nodes, Elements = 285123 1459185
AFLR3 GG : Nodes, Elements = 314749 1548281
AFLR3 GG : Nodes, Elements = 314749 1666496
AFLR3 GG : Nodes, Elements = 314749 1635328
AFLR3 GG : Nodes, Elements = 343185 1720784
AFLR3 GG : Nodes, Elements = 343185 1834449
AFLR3 GG : Nodes, Elements = 343185 1804754
AFLR3 GG : Nodes, Elements = 370197 1885926
AFLR3 GG : Nodes, Elements = 370197 1992358
AFLR3 GG : Nodes, Elements = 370197 1965216
AFLR3 GG : Nodes, Elements = 395625 2041613
AFLR3 GG : Nodes, Elements = 395625 2142093
AFLR3 GG : Nodes, Elements = 395625 2116556
AFLR3 GG : Nodes, Elements = 419704 2188894
AFLR3 GG : Nodes, Elements = 419704 2283914
AFLR3 GG : Nodes, Elements = 419704 2259708
AFLR3 GG : Nodes, Elements = 442391 2327833
AFLR3 GG : Nodes, Elements = 442391 2417661
AFLR3 GG : Nodes, Elements = 442391 2394642
AFLR3 GG : Nodes, Elements = 463683 2458572
AFLR3 GG : Nodes, Elements = 463683 2543123
AFLR3 GG : Nodes, Elements = 463683 2521112
AFLR3 GG : Nodes, Elements = 483827 2581588
AFLR3 GG : Nodes, Elements = 483827 2661051
AFLR3 GG : Nodes, Elements = 483827 2640939
AFLR3 GG : Nodes, Elements = 502669 2697501
AFLR3 GG : Nodes, Elements = 502669 2770894
AFLR3 GG : Nodes, Elements = 502669 2752651
AFLR3 GG : Nodes, Elements = 520300 2805580
AFLR3 GG : Nodes, Elements = 520300 2874408
AFLR3 GG : Nodes, Elements = 520300 2857298
AFLR3 GG : Nodes, Elements = 536675 2906461
AFLR3 GG : Nodes, Elements = 536675 2970904
AFLR3 GG : Nodes, Elements = 536675 2954392
AFLR3 GG : Nodes, Elements = 551844 2999934
AFLR3 GG : Nodes, Elements = 551844 3060132
AFLR3 GG : Nodes, Elements = 551844 3044500
AFLR3 GG : Nodes, Elements = 565681 3086032
AFLR3 GG : Nodes, Elements = 565681 3140377
AFLR3 GG : Nodes, Elements = 565681 3126467
AFLR3 GG : Nodes, Elements = 578520 3165000
AFLR3 GG : Nodes, Elements = 578520 3215601
AFLR3 GG : Nodes, Elements = 578520 3202688
AFLR3 GG : Nodes, Elements = 590236 3237862
AFLR3 GG : Nodes, Elements = 590236 3283447
AFLR3 GG : Nodes, Elements = 590236 3272024
AFLR3 GG : Nodes, Elements = 600891 3304007
AFLR3 GG : Nodes, Elements = 600891 3345640
AFLR3 GG : Nodes, Elements = 600891 3335099
AFLR3 GG : Nodes, Elements = 610653 3364398
AFLR3 GG : Nodes, Elements = 610653 3402538
AFLR3 GG : Nodes, Elements = 610653 3392929
AFLR3 GG : Nodes, Elements = 619681 3420022
AFLR3 GG : Nodes, Elements = 619681 3455219
AFLR3 GG : Nodes, Elements = 619681 3446093
AFLR3 GG : Nodes, Elements = 628219 3471726
AFLR3 GG : Nodes, Elements = 628219 3505699
AFLR3 GG : Nodes, Elements = 628219 3496844
AFLR3 GG : Nodes, Elements = 636038 3520308
AFLR3 GG : Nodes, Elements = 636038 3551135
AFLR3 GG : Nodes, Elements = 636038 3543045
AFLR3 GG : Nodes, Elements = 643376 3565069
AFLR3 GG : Nodes, Elements = 643376 3593962
AFLR3 GG : Nodes, Elements = 643376 3586413
AFLR3 GG : Nodes, Elements = 650191 3606868
AFLR3 GG : Nodes, Elements = 650191 3633632
AFLR3 GG : Nodes, Elements = 650191 3626847
AFLR3 GG : Nodes, Elements = 656508 3645807
AFLR3 GG : Nodes, Elements = 656508 3670861
AFLR3 GG : Nodes, Elements = 656508 3664202
AFLR3 GG : Nodes, Elements = 662433 3681982
AFLR3 GG : Nodes, Elements = 662433 3705355
AFLR3 GG : Nodes, Elements = 662433 3699226
AFLR3 GG : Nodes, Elements = 667990 3715904
AFLR3 GG : Nodes, Elements = 667990 3737646
AFLR3 GG : Nodes, Elements = 667990 3731986
AFLR3 GG : Nodes, Elements = 673254 3747784
AFLR3 GG : Nodes, Elements = 673254 3768503
AFLR3 GG : Nodes, Elements = 673254 3763031
AFLR3 GG : Nodes, Elements = 678157 3777746
AFLR3 GG : Nodes, Elements = 678157 3796918
AFLR3 GG : Nodes, Elements = 678157 3791911
AFLR3 GG : Nodes, Elements = 682710 3805572
AFLR3 GG : Nodes, Elements = 682710 3823091
AFLR3 GG : Nodes, Elements = 682710 3818679
AFLR3 GG : Nodes, Elements = 686953 3831414
AFLR3 GG : Nodes, Elements = 686953 3848097
AFLR3 GG : Nodes, Elements = 686953 3843660
AFLR3 GG : Nodes, Elements = 690854 3855370
AFLR3 GG : Nodes, Elements = 690854 3870670
AFLR3 GG : Nodes, Elements = 690854 3866655
AFLR3 GG : Nodes, Elements = 694460 3877474
AFLR3 GG : Nodes, Elements = 694460 3891624
AFLR3 GG : Nodes, Elements = 694460 3887901
AFLR3 GG : Nodes, Elements = 697850 3898077
AFLR3 GG : Nodes, Elements = 697850 3911030
AFLR3 GG : Nodes, Elements = 697850 3907854
AFLR3 GG : Nodes, Elements = 700996 3917295
AFLR3 GG : Nodes, Elements = 700996 3929596
AFLR3 GG : Nodes, Elements = 700996 3926327
AFLR3 GG : Nodes, Elements = 703836 3934850
AFLR3 GG : Nodes, Elements = 703836 3945999
AFLR3 GG : Nodes, Elements = 703836 3942976
AFLR3 GG : Nodes, Elements = 706440 3950791
AFLR3 GG : Nodes, Elements = 706440 3961150
AFLR3 GG : Nodes, Elements = 706440 3958314
AFLR3 GG : Nodes, Elements = 708730 3965187
AFLR3 GG : Nodes, Elements = 708730 3974144
AFLR3 GG : Nodes, Elements = 708730 3971783
AFLR3 GG : Nodes, Elements = 710708 3977720
AFLR3 GG : Nodes, Elements = 710708 3985328
AFLR3 GG : Nodes, Elements = 710708 3983276
AFLR3 GG : Nodes, Elements = 712424 3988426
AFLR3 GG : Nodes, Elements = 712424 3995075
AFLR3 GG : Nodes, Elements = 712424 3993284
AFLR3 GG : Nodes, Elements = 713833 3997513
AFLR3 GG : Nodes, Elements = 713833 4003187
AFLR3 GG : Nodes, Elements = 713833 4001605
AFLR3 GG : Nodes, Elements = 715022 4005173
AFLR3 GG : Nodes, Elements = 715022 4009923
AFLR3 GG : Nodes, Elements = 715022 4008585
AFLR3 GG : Nodes, Elements = 715991 4011493
AFLR3 GG : Nodes, Elements = 715991 4015396
AFLR3 GG : Nodes, Elements = 715991 4014283
AFLR3 GG : Nodes, Elements = 716774 4016634
AFLR3 GG : Nodes, Elements = 716774 4019712
AFLR3 GG : Nodes, Elements = 716774 4018875
AFLR3 GG : Nodes, Elements = 717387 4020715
AFLR3 GG : Nodes, Elements = 717387 4023245
AFLR3 GG : Nodes, Elements = 717387 4022493
AFLR3 GG : Nodes, Elements = 717893 4024011
AFLR3 GG : Nodes, Elements = 717893 4025943
AFLR3 GG : Nodes, Elements = 717893 4025436
AFLR3 GG : Nodes, Elements = 718259 4026534
AFLR3 GG : Nodes, Elements = 718259 4027955
AFLR3 GG : Nodes, Elements = 718259 4027575
AFLR3 GG : Nodes, Elements = 718519 4028355
AFLR3 GG : Nodes, Elements = 718519 4029402
AFLR3 GG : Nodes, Elements = 718519 4029087
AFLR3 GG : Nodes, Elements = 718704 4029642
AFLR3 GG : Nodes, Elements = 718704 4030385
AFLR3 GG : Nodes, Elements = 718704 4030160
AFLR3 GG : Nodes, Elements = 718834 4030550
AFLR3 GG : Nodes, Elements = 718834 4031082
AFLR3 GG : Nodes, Elements = 718834 4030929
AFLR3 GG : Nodes, Elements = 718902 4031133
AFLR3 GG : Nodes, Elements = 718902 4031395
AFLR3 GG : Nodes, Elements = 718902 4031313
AFLR3 GG : Nodes, Elements = 718948 4031451
AFLR3 GG : Nodes, Elements = 718948 4031642
AFLR3 GG : Nodes, Elements = 718948 4031580
AFLR3 GG : Nodes, Elements = 718969 4031643
AFLR3 GG : Nodes, Elements = 718969 4031735
AFLR3 GG : Nodes, Elements = 718969 4031696
AFLR3 GG : Nodes, Elements = 718984 4031741
AFLR3 GG : Nodes, Elements = 718984 4031806
AFLR3 GG : Nodes, Elements = 718984 4031777
AFLR3 GG : Nodes, Elements = 718993 4031804
AFLR3 GG : Nodes, Elements = 718993 4031837
AFLR3 GG : Nodes, Elements = 718993 4031826
AFLR3 GG : Nodes, Elements = 718998 4031841
AFLR3 GG : Nodes, Elements = 718998 4031865
AFLR3 GG : Nodes, Elements = 718998 4031858
AFLR3 GG : Nodes, Elements = 718999 4031861
AFLR3 GG : Nodes, Elements = 718999 4031864
AFLR3 GG : Nodes, Elements = 718999 4031863
AFLR3 GG : Nodes, Elements = 719001 4031869
AFLR3 GG : Nodes, Elements = 719001 4031880
AFLR3 GG : Nodes, Elements = 719001 4031877
AFLR3 GG : Nodes, Elements = 719182 4032420
AFLR3 GG : Nodes, Elements = 719182 4033198
AFLR3 GG : Nodes, Elements = 719182 4032854
AFLR3 GG : Nodes, Elements = 719277 4033139
AFLR3 GG : Nodes, Elements = 719277 4033530
AFLR3 GG : Nodes, Elements = 719277 4033396
AFLR3 GG : Nodes, Elements = 719330 4033555
AFLR3 GG : Nodes, Elements = 719330 4033763
AFLR3 GG : Nodes, Elements = 719330 4033690
AFLR3 GG : Nodes, Elements = 719355 4033765
AFLR3 GG : Nodes, Elements = 719355 4033857
AFLR3 GG : Nodes, Elements = 719355 4033821
AFLR3 GG : Nodes, Elements = 719369 4033863
AFLR3 GG : Nodes, Elements = 719369 4033917
AFLR3 GG : Nodes, Elements = 719369 4033898
AFLR3 GG : Nodes, Elements = 719383 4033940
AFLR3 GG : Nodes, Elements = 719383 4033992
AFLR3 GG : Nodes, Elements = 719383 4033979
AFLR3 GG : Nodes, Elements = 719395 4034015
AFLR3 GG : Nodes, Elements = 719395 4034054
AFLR3 GG : Nodes, Elements = 719395 4034046
AFLR3 GG : Nodes, Elements = 719407 4034082
AFLR3 GG : Nodes, Elements = 719407 4034126
AFLR3 GG : Nodes, Elements = 719407 4034113
AFLR3 GG : Nodes, Elements = 719420 4034152
AFLR3 GG : Nodes, Elements = 719420 4034200
AFLR3 GG : Nodes, Elements = 719420 4034189
AFLR3 GG : Nodes, Elements = 719433 4034228
AFLR3 GG : Nodes, Elements = 719433 4034279
AFLR3 GG : Nodes, Elements = 719433 4034259
AFLR3 GG : Nodes, Elements = 719444 4034292
AFLR3 GG : Nodes, Elements = 719444 4034335
AFLR3 GG : Nodes, Elements = 719444 4034325
AFLR3 GG : Nodes, Elements = 719456 4034361
AFLR3 GG : Nodes, Elements = 719456 4034413
AFLR3 GG : Nodes, Elements = 719456 4034391
AFLR3 GG : Nodes, Elements = 719466 4034421
AFLR3 GG : Nodes, Elements = 719466 4034464
AFLR3 GG : Nodes, Elements = 719466 4034450
AFLR3 GG : Nodes, Elements = 719473 4034471
AFLR3 GG : Nodes, Elements = 719473 4034501
AFLR3 GG : Nodes, Elements = 719473 4034489
AFLR3 GG : Nodes, Elements = 719480 4034510
AFLR3 GG : Nodes, Elements = 719480 4034538
AFLR3 GG : Nodes, Elements = 719480 4034527
AFLR3 GG : Nodes, Elements = 719485 4034542
AFLR3 GG : Nodes, Elements = 719485 4034561
AFLR3 GG : Nodes, Elements = 719485 4034557
AFLR3 GG : Nodes, Elements = 719487 4034563
AFLR3 GG : Nodes, Elements = 719487 4034569
AFLR3 GG : Nodes, Elements = 719487 4034565
AFLR3 : CPU Time = 3.566 minutes
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 719487 4034565
AFLR3 QI : Nodes, Elements = 713385 4000426
AFLR3 QI : Nodes, Elements = 711508 3989918
AFLR3 QI : Nodes, Elements = 710920 3986583
AFLR3 QI : Nodes, Elements = 710776 3985748
AFLR3 QI : Nodes, Elements = 710748 3985588
AFLR3 QI : Nodes, Elements = 710743 3985561
AFLR3 QI : Nodes, Elements = 710743 4003656
AFLR3 QI : Nodes, Elements = 710743 3982935
AFLR3 QI : Nodes, Elements = 710743 3974745
AFLR3 QI : Nodes, Elements = 710743 3989028
AFLR3 QI : Nodes, Elements = 710743 3974612
AFLR3 QI : Nodes, Elements = 710743 3974054
AFLR3 QI : Nodes, Elements = 710743 3987417
AFLR3 QI : Nodes, Elements = 710743 3974401
AFLR3 QI : Nodes, Elements = 710743 3974017
AFLR3 QI : Nodes, Elements = 710743 3979294
AFLR3 QI : Nodes, Elements = 710743 3973431
AFLR3 QI : Nodes, Elements = 710743 3973015
AFLR3 QI : Nodes, Elements = 710743 3976140
AFLR3 QI : Nodes, Elements = 710743 3972740
AFLR3 QI : Nodes, Elements = 710743 3972458
AFLR3 QI : Nodes, Elements = 710745 3972468
AFLR3 QI : Nodes, Elements = 710745 3975502
AFLR3 QI : Nodes, Elements = 710745 3972483
AFLR3 QI : Nodes, Elements = 710745 3972442
AFLR3 QI : Nodes, Elements = 710745 3974767
AFLR3 QI : Nodes, Elements = 710745 3972343
AFLR3 QI : Nodes, Elements = 710745 3972116
AFLR3 QI : Nodes, Elements = 710745 3972468
AFLR3 : CPU Time = 59.981 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 710745 3972468
AFLR3 QRG: Nodes, Elements = 710738 3972415
AFLR3 QRG: Nodes, Elements = 710737 3972412
AFLR3 QRG: Nodes, Elements = 710736 3972407
AFLR3 QRG: Nodes, Elements = 710735 3972404
AFLR3 : CPU Time = 1.637 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 3972404
UG3 : Min, Max Ang = 5.965 164.8
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 15
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 3972404
UG3 : Min Vol = 2.05e-06
UG3 : Average Vol = 1.5e+04
UG3 : Total-Tet-Vol = 5.96e+10
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 3972404
UG3 : Min, Max Q = 0.0339 1
UG3 : Average Q = 0.886
UG3 : No. Q< 0.1 = 131
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 4.835 minutes
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 3972404
UG3 : Min, Max Ang = 5.965 164.8
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 15
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 3972404
UG3 : Min Vol = 2.05e-06
UG3 : Average Vol = 1.5e+04
UG3 : Total-Tet-Vol = 5.96e+10
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 3972404
UG3 : Min, Max Q = 0.185 1
UG3 : Average Q = 0.849
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
Number of nodes = 710735
Number of elements = 4124112
Number of triangles = 151708
Number of quadrilatarals = 0
Number of tetrahedrals = 3972404
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.
Surface(s) plotted in the output file: BC_1.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| PARAVIEW| 250|
| SURFACE_PARAVIEW| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_inviscidWing.dat.
Surface file name: surface_flow_inviscidWing.
Volume file name: flow_inviscidWing.
Restart file name: restart_flow_inviscidWing.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
710735 grid points.
3972404 volume elements.
2 surface markers.
151672 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
3972404 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.96352e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 122.726. Mean K: 4.02923. Standard deviation K: 11.9588.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 41.2956| 87.7171|
| CV Face Area Aspect Ratio| 1.01507| 3558.28|
| CV Sub-Volume Ratio| 1.00331| 26134.6|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 710735| 1/1.00| 10|
| 1| 116837| 1/6.08| 8.21704|
| 2| 17954| 1/6.51| 6.60187|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 97.6729 m.
Wetted area = 8795.17 m^2.
Area projection in the x-plane = 681.447 m^2, y-plane = 449.382 m^2, z-plane = 4224.13 m^2.
Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m.
Min. coordinate in the x-direction = 49.9621 m, y-direction = -97.6729 m, z-direction = -8.47903 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 221265| 1| m^2/s^2| 221265|
| Velocity-X| 170.123| 1| m/s| 170.123|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 2.9695| 1| m/s| 2.9695|
| Velocity Magnitude| 170.149| 1| m/s| 170.149|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.7822e+01| 0.412038| 2.691946| 2.165035| 5.894884| -0.418144|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.4169e+01| 3.113112| 5.540727| 5.357351| 8.581389| -0.195270|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.1964e+01| 4.878789| 7.415716| 7.123386| 10.367147| 33.442093|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.0492e+01| 6.719770| 9.117839| 9.138945| 12.141986| 82.633563|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.9978e+01| 6.428549| 8.846011| 8.684212| 11.812950| 2.047813|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 2.9323e+01| 6.529556| 9.108075| 9.053230| 11.985107| -187.204252|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 2.8918e+01| 6.551368| 9.076621| 8.775585| 11.970950| 8.293945|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 2.8792e+01| 10.333504| 13.145661| 12.761047| 16.115295| 2.521525|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 2.8604e+01| 10.333474| 13.145657| 12.761157| 16.115295| -177.944708|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 2.8353e+01| 8.917656| 11.735777| 11.457880| 14.726305| -89.948696|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 8.91766| < -8| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_inviscidWing.dat |
Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|CSV file |surface_flow_inviscidWing.csv |
Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|Paraview |flow_inviscidWing.vtu |
Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|Paraview surface |surface_flow_inviscidWing.vtu |
Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
+-----------------------------------------------------------------------+
Warning: there are 1401 non-physical points in the solution.
Warning: 492 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
==> Total Forces and Moments
--> Cl = 56.960356 Cd = -0.633254
--> Cmx = -1.702452 Cmy = -10.524391 Cmz = 0.029811
--> Cx = -1.627253 Cy = 0.798211 Cz = 56.940628
real 13m38.480s
user 13m3.281s
sys 0m22.281s
+ status=0
+ set +x
=================================================
data/session08/2_su2_InviscidWing.py passed (as expected)
=================================================
=================================================
1_astros_ModalCantilever.py test;
+ python 1_astros_ModalCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Running mASTROS pre-analysis...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
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 - EigenAnalysis
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....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
==> Running mASTROS post-analysis...
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
--> Eigen-frequencies:
1 : 0.00145606
2 : 0.0014575
3 : 0.00332859
4 : 0.00333096
5 : 0.00445176
6 : 0.00445507
7 : 0.00894917
8 : 0.0089521
9 : 0.0110353
10: 0.0110413
real 1m35.086s
user 1m17.963s
sys 0m30.506s
+ status=0
+ set +x
=================================================
data/session09/1_astros_ModalCantilever.py passed (as expected)
=================================================
=================================================
2_astros_ModalSupport.py test;
+ python 2_astros_ModalSupport.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Running mASTROS pre-analysis...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Name = ribSupport, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, 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 = 831
Number of elements = 962
Number of triangle elements = 0
Number of quadrilateral elements = 962
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 = 832
Total number of elements = 962
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 = 1
Name = ribRootPoint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = leftPointLoad, index = 1
Name = ritePointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = ribRoot, 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 = 6
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Name = ribSupport, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 831
Number of elements = 962
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 962
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 = 832
Combined Number of elements = 963
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 962
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 6
Property name - leftWingSkin
Property name - ribSupport
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribRootPoint
No "constraintType" specified for Constraint tuple ribRootPoint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple ribRootPoint, going to use constraint name
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribRootPoint
No "groupName" specified for Support tuple ribRootPoint, going to use support name
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - ribRoot
No "groupName" specified for Connection tuple ribRoot!
Looking for automatic connections from the use of capsConnectLink for ribRoot
9 automatic connections were made for capsConnect ribRoot (node id 832)
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 - EigenAnalysis
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 connection cards - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing support cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
==> Running mASTROS post-analysis...
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
--> Eigen-frequencies:
1 : 2.14626e-08
2 : 0.00142073
3 : 0.00174522
4 : 0.00323727
5 : 0.00324323
6 : 0.00433058
7 : 0.00512596
8 : 0.00873541
9 : 0.010065
10: 0.010703
real 5m35.391s
user 4m24.241s
sys 1m31.400s
+ status=0
+ set +x
=================================================
data/session09/2_astros_ModalSupport.py passed (as expected)
=================================================
=================================================
3_astros_StaticCantilever.py test;
+ python 3_astros_StaticCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Running mASTROS pre-analysis...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftPointLoad
No "groupName" specified for Load tuple leftPointLoad, going to use load name
Load name - ritePointLoad
No "groupName" specified for Load tuple ritePointLoad, going to use load name
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
Writing coordinate system cards
==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
==> Running mASTROS post-analysis...
--> Maximum displacements:
--> Tmax 238433.3403112283
--> T1max 16861.9
--> T2max 16414.9
--> T3max 237286.0
real 0m37.437s
user 0m42.285s
sys 0m8.236s
+ status=0
+ set +x
=================================================
data/session09/3_astros_StaticCantilever.py passed (as expected)
=================================================
=================================================
4_astros_Composite.py test;
+ python 4_astros_Composite.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
==> Running mASTROS pre-analysis...
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftPointLoad
No "groupName" specified for Load tuple leftPointLoad, going to use load name
Load name - ritePointLoad
No "groupName" specified for Load tuple ritePointLoad, going to use load name
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
Writing coordinate system cards
==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
==> Running mASTROS post-analysis...
--> Maximum displacements:
--> Tmax 52594.60117638786
--> T1max 4359.68
--> T2max 3216.5
--> T3max 52322.2
real 0m34.758s
user 0m41.116s
sys 0m7.756s
+ status=0
+ set +x
=================================================
data/session09/4_astros_Composite.py passed (as expected)
=================================================
[macys-VM:53141] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/3663265792/sm_segment.macys-VM.502.da590000.0 could be created.
=================================================
6_tacs_StaticCantilever.py test;
+ python 6_tacs_StaticCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[macys-VM:53150] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/4015390720/sm_segment.macys-VM.502.ef560000.0 could be created.
==> Loading geometry from file "../ESP/transport.csm"...
==> Running TACS pre-analysis...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftWingSkin
No "groupName" specified for Load tuple leftWingSkin, going to use load name
Load name - riteWingSkin
No "groupName" specified for Load tuple riteWingSkin, going to use load name
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
[0] Creating TACSAssembler with numOwnedNodes = 425 numElements = 482
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 2.84, nnz(ILU) = 11729
==> Running TACS...
==> Running TACS post-analysis...
Tacs Analysis Outputs...
functional mass = 511406.709389084
functional ks_vmfailure = 0.019135051727266705
real 0m35.007s
user 0m40.707s
sys 0m7.794s
+ status=0
+ set +x
=================================================
data/session09/6_tacs_StaticCantilever.py passed (as expected)
=================================================
=================================================
7_tacs_sizing.py test;
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
+ python 7_tacs_sizing.py
[macys-VM:53178] shmem: mmap: an error occurred while determining whether or not /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T//ompi.macys-VM.502/jf.0/293797888/sm_segment.macys-VM.502.11830000.0 could be created.
==> Loading geometry from file "../ESP/transport.csm"...
==> Starting optimization...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 3852
Number of elements = 4061
Number of triangle elements = 0
Number of quadrilateral elements = 4061
----------------------------
Total number of nodes = 3852
Total number of elements = 4061
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 3852
Number of elements = 4061
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 4061
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftWingSkin
No "groupName" specified for Load tuple leftWingSkin, going to use load name
Load name - riteWingSkin
No "groupName" specified for Load tuple riteWingSkin, going to use load name
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 3
Design_Variable name - ribThk
Design_Variable name - skinThk
Design_Variable name - sparThk
Design_Variable_Relation name - relLeftSkin
Design_Variable_Relation name - relRib
Design_Variable_Relation name - relRiteSkin
Design_Variable_Relation name - relSpar
Number of design variable relations - 4
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
Writing design variable cards
Writing design variable relation cards
[0] Creating TACSAssembler with numOwnedNodes = 3852 numElements = 4061
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session09/7_tacs_sizing.py:144: DeprecationWarning: Conversion of an array with ndim > 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.)
xarray[ithick] = float(inputs[thick_dv])
--> ribThk [0.05]
--> skinThk [0.003]
--> sparThk [0.1]
--> mass [351348.85843741]
--> ks_vmfailure [0.18465374]
--> mass [351348.85843741]
--> ks_vmfailure [0.18465374]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00701607]]
--> ks_vmfailure skinThk [[-0.7773577]]
--> ks_vmfailure sparThk [[-0.00419852]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.001]
--> skinThk [0.00739074]
--> sparThk [0.001]
--> mass [164778.0669354]
--> ks_vmfailure [0.18458271]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.2719378]]
--> ks_vmfailure skinThk [[-0.30939955]]
--> ks_vmfailure sparThk [[-0.20978603]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.001]
--> skinThk [0.001]
--> sparThk [0.02273644]
--> mass [129232.41480384]
--> ks_vmfailure [0.20239501]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.001]
--> skinThk [0.00647627]
--> sparThk [0.00411034]
--> mass [159691.72861108]
--> ks_vmfailure [0.18468723]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.28428468]]
--> ks_vmfailure skinThk [[-0.36623705]]
--> ks_vmfailure sparThk [[-0.04561164]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.01797054]
--> skinThk [0.001]
--> sparThk [0.0012247]
--> mass [135761.31328029]
--> ks_vmfailure [0.20097432]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00336292]
--> skinThk [0.00571377]
--> sparThk [0.00370855]
--> mass [156359.73946962]
--> ks_vmfailure [0.18476613]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.04724024]]
--> ks_vmfailure skinThk [[-0.42968566]]
--> ks_vmfailure sparThk [[-0.05558717]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00375419]
--> skinThk [0.0118629]
--> sparThk [0.00560564]
--> mass [221348.46863653]
--> ks_vmfailure [0.18335024]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00340205]
--> skinThk [0.00632869]
--> sparThk [0.00389826]
--> mass [162858.61238631]
--> ks_vmfailure [0.18451389]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.0033671]
--> skinThk [0.00577947]
--> sparThk [0.00372882]
--> mass [157054.09480563]
--> ks_vmfailure [0.18473688]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.04660765]]
--> ks_vmfailure skinThk [[-0.4208561]]
--> ks_vmfailure sparThk [[-0.05458696]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.001]
--> skinThk [0.0114244]
--> sparThk [0.01236646]
--> mass [220187.17353899]
--> ks_vmfailure [0.18349008]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.22376311]]
--> ks_vmfailure skinThk [[-0.11542908]]
--> ks_vmfailure sparThk [[-0.00924892]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00726772]
--> skinThk [0.01192034]
--> sparThk [0.01564752]
--> mass [242329.88959071]
--> ks_vmfailure [0.18318718]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00374643]
--> skinThk [0.01164171]
--> sparThk [0.01380417]
--> mass [229889.80331156]
--> ks_vmfailure [0.18327675]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.0024241]
--> skinThk [0.01153708]
--> sparThk [0.01311196]
--> mass [225218.27426134]
--> ks_vmfailure [0.18333401]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.04342338]]
--> ks_vmfailure skinThk [[-0.10932276]]
--> ks_vmfailure sparThk [[-0.00862543]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00273423]
--> skinThk [0.02300858]
--> sparThk [0.02081621]
--> mass [351071.64511817]
--> ks_vmfailure [0.18265072]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00246133]
--> skinThk [0.01291395]
--> sparThk [0.01403666]
--> mass [240323.8805217]
--> ks_vmfailure [0.18319035]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.04030186]]
--> ks_vmfailure skinThk [[-0.08766021]]
--> ks_vmfailure sparThk [[-0.00725047]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00615236]
--> skinThk [0.02577931]
--> sparThk [0.00214913]
--> mass [361343.3111648]
--> ks_vmfailure [0.18263733]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00640621]]
--> ks_vmfailure skinThk [[-0.02501964]]
--> ks_vmfailure sparThk [[-0.04131406]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00713229]
--> skinThk [0.02677304]
--> sparThk [0.01682192]
--> mass [392609.26145734]
--> ks_vmfailure [0.18251681]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00663018]
--> skinThk [0.02626385]
--> sparThk [0.00930356]
--> mass [376588.5352551]
--> ks_vmfailure [0.18255199]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00641281]
--> skinThk [0.02604342]
--> sparThk [0.00604884]
--> mass [369653.12752473]
--> ks_vmfailure [0.18257185]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00605011]]
--> ks_vmfailure skinThk [[-0.02434576]]
--> ks_vmfailure sparThk [[-0.00555075]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00973724]
--> skinThk [0.04835413]
--> sparThk [0.00759182]
--> mass [602336.95393367]
--> ks_vmfailure [0.18225672]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00752073]
--> skinThk [0.03347884]
--> sparThk [0.00656306]
--> mass [447198.89241696]
--> ks_vmfailure [0.18242234]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00423675]]
--> ks_vmfailure skinThk [[-0.01486495]]
--> ks_vmfailure sparThk [[-0.00451758]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.0124042]
--> skinThk [0.0584906]
--> sparThk [0.01317179]
--> mass [716837.81941702]
--> ks_vmfailure [0.18217977]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00154607]]
--> ks_vmfailure skinThk [[-0.00498161]]
--> ks_vmfailure sparThk [[-0.00115578]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.01929412]
--> skinThk [0.0907852]
--> sparThk [0.02029644]
--> mass [1064336.64937422]
--> ks_vmfailure [0.18206339]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00064649]]
--> ks_vmfailure skinThk [[-0.00208487]]
--> ks_vmfailure sparThk [[-0.00048512]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.02545589]
--> skinThk [0.11766677]
--> sparThk [0.02722878]
--> mass [1355781.80313859]
--> ks_vmfailure [0.18201458]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.0003768]]
--> ks_vmfailure skinThk [[-0.00124124]]
--> ks_vmfailure sparThk [[-0.00027327]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.02816254]
--> skinThk [0.12784859]
--> sparThk [0.03061479]
--> mass [1467935.22745818]
--> ks_vmfailure [0.1820012]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00031099]]
--> ks_vmfailure skinThk [[-0.00105064]]
--> ks_vmfailure sparThk [[-0.00021914]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.02874646]
--> skinThk [0.12860075]
--> sparThk [0.03166037]
--> mass [1478053.31814195]
--> ks_vmfailure [0.18200001]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00030043]]
--> ks_vmfailure skinThk [[-0.00103744]]
--> ks_vmfailure sparThk [[-0.00020726]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.02995586]
--> skinThk [0.12773281]
--> sparThk [0.03432126]
--> mass [1475323.34496521]
--> ks_vmfailure [0.18200005]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00028252]]
--> ks_vmfailure skinThk [[-0.00104812]]
--> ks_vmfailure sparThk [[-0.00018401]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03300208]
--> skinThk [0.12582911]
--> sparThk [0.04074914]
--> mass [1470920.51864181]
--> ks_vmfailure [0.18200021]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00024502]]
--> ks_vmfailure skinThk [[-0.00107038]]
--> ks_vmfailure sparThk [[-0.00014848]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03417055]
--> skinThk [0.12543858]
--> sparThk [0.04303483]
--> mass [1472403.16573053]
--> ks_vmfailure [0.18200002]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00023279]]
--> ks_vmfailure skinThk [[-0.00107335]]
--> ks_vmfailure sparThk [[-0.00014019]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03466542]
--> skinThk [0.12523006]
--> sparThk [0.04393549]
--> mass [1472509.96085976]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022797]]
--> ks_vmfailure skinThk [[-0.00107536]]
--> ks_vmfailure sparThk [[-0.00013746]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03477347]
--> skinThk [0.12519387]
--> sparThk [0.0440588]
--> mass [1472530.51058047]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022693]]
--> ks_vmfailure skinThk [[-0.00107573]]
--> ks_vmfailure sparThk [[-0.00013712]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03499382]
--> skinThk [0.12513458]
--> sparThk [0.04415985]
--> mass [1472520.45921217]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022479]]
--> ks_vmfailure skinThk [[-0.00107642]]
--> ks_vmfailure sparThk [[-0.00013689]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03528599]
--> skinThk [0.12508834]
--> sparThk [0.04404565]
--> mass [1472505.6089541]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022196]]
--> ks_vmfailure skinThk [[-0.00107708]]
--> ks_vmfailure sparThk [[-0.00013735]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03554749]
--> skinThk [0.12509498]
--> sparThk [0.04357431]
--> mass [1472488.97649504]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.0002194]]
--> ks_vmfailure skinThk [[-0.0010773]]
--> ks_vmfailure sparThk [[-0.00013892]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03557543]
--> skinThk [0.12515335]
--> sparThk [0.04308255]
--> mass [1472485.55740288]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00021902]]
--> ks_vmfailure skinThk [[-0.00107687]]
--> ks_vmfailure sparThk [[-0.00014054]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03549811]
--> skinThk [0.12518986]
--> sparThk [0.04292621]
--> mass [1472487.79718265]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.0002197]]
--> ks_vmfailure skinThk [[-0.00107651]]
--> ks_vmfailure sparThk [[-0.00014103]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03546495]
--> skinThk [0.12519741]
--> sparThk [0.04292079]
--> mass [1472488.35761213]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022001]]
--> ks_vmfailure skinThk [[-0.00107642]]
--> ks_vmfailure sparThk [[-0.00014104]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03546229]
--> skinThk [0.12519748]
--> sparThk [0.04292444]
--> mass [1472488.40726924]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022004]]
--> ks_vmfailure skinThk [[-0.00107641]]
--> ks_vmfailure sparThk [[-0.00014103]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03546228]
--> skinThk [0.12519745]
--> sparThk [0.0429247]
--> mass [1472488.40797224]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812601]]
--> mass skinThk [[10032748.65480208]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022004]]
--> ks_vmfailure skinThk [[-0.00107641]]
--> ks_vmfailure sparThk [[-0.00014103]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03546228]
--> skinThk [0.12519745]
--> sparThk [0.0429247]
--> mass [1472488.40757359]
--> ks_vmfailure [0.182]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03546228]
--> skinThk [0.12519745]
--> sparThk [0.0429247]
--> mass [1472488.40784458]
--> ks_vmfailure [0.182]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03546228]
--> skinThk [0.12519745]
--> sparThk [0.0429247]
--> mass [1472488.40795767]
--> ks_vmfailure [0.182]
Optimization terminated successfully (Exit mode 0)
Current function value: 4.2071097370219075
Iterations: 29
Function evaluations: 42
Gradient evaluations: 29
Optimization Complete
-----------------------------------
==> Optimized value:
--> ribThk [0.03546228]
--> skinThk [0.12519745]
--> sparThk [0.0429247]
real 2m20.696s
user 2m26.881s
sys 0m9.217s
+ status=0
+ set +x
=================================================
data/session09/7_tacs_sizing.py passed (as expected)
=================================================
=================================================
2_aeroelastic_Iterative_SU2_Astros.py test;
+ python 2_aeroelastic_Iterative_SU2_Astros.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
==> Running SU2 pre-analysis...
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0.5 1 2 3 6
EGADS : 2 Yes 0 0 1 0.5 1 1 4 5
EGADS : 3 Yes 0 0 1 0.5 1 1 4 8
EGADS : 4 Yes 0 0 1 0.5 1 2 3 5
EGADS : 5 Yes 0 0 1 0.5 1 2 4
EGADS : 6 Yes 0 0 1 0.5 1 1 7 8
EGADS : 7 Yes 0 0 1 0.5 1 6 9 10
EGADS : 8 Yes 0 0 1 0.5 1 3 6 9
EGADS : 9 Yes 0 0 1 0.5 1 7 8 10
EGADS : 10 Yes 0 0 1 0.5 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 11135.8
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 16
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 242 426 0
AFLR4 : Nodes, Trias,Quads= 203 348 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 301 529 0
AFLR4 : Nodes, Trias,Quads= 178 283 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 233 409 0
AFLR4 : Nodes, Trias,Quads= 189 321 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 292 511 0
AFLR4 : Nodes, Trias,Quads= 174 275 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 9 10 0
AFLR4 : Nodes, Trias,Quads= 6 4 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 241 424 0
AFLR4 : Nodes, Trias,Quads= 202 346 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 302 531 0
AFLR4 : Nodes, Trias,Quads= 177 281 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 235 413 0
AFLR4 : Nodes, Trias,Quads= 189 321 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 293 513 0
AFLR4 : Nodes, Trias,Quads= 173 273 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 9 10 0
AFLR4 : Nodes, Trias,Quads= 6 4 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1238 2468 542
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1238 2468
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1695 3170 0
AFLR4 : Nodes, Trias,Quads= 1371 2522 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 3139 5972 0
AFLR4 : Nodes, Trias,Quads= 1805 3304 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1597 2983 0
AFLR4 : Nodes, Trias,Quads= 1311 2411 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 3114 5923 0
AFLR4 : Nodes, Trias,Quads= 1786 3267 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 36 46 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1691 3162 0
AFLR4 : Nodes, Trias,Quads= 1376 2532 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 3162 6018 0
AFLR4 : Nodes, Trias,Quads= 1802 3298 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1600 2989 0
AFLR4 : Nodes, Trias,Quads= 1326 2441 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 3109 5913 0
AFLR4 : Nodes, Trias,Quads= 1784 3263 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 36 46 0
AFLR4 : Nodes, Trias,Quads= 24 22 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 11563 23118 2164
OVERALL : CPU Time = 0.363 seconds
Body 1 (of 2)
Number of nodes = 11543
Number of elements = 23082
Number of triangle elements = 23082
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 11563
Total number of elements = 23118
Total number of triangle elements = 23118
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0.5 1 2 3 6
EGADS : 2 Yes 0 0 1 0.5 1 1 4 5
EGADS : 3 Yes 0 0 1 0.5 1 1 4 8
EGADS : 4 Yes 0 0 1 0.5 1 2 3 5
EGADS : 5 Yes 0 0 1 0.5 1 2 4
EGADS : 6 Yes 0 0 1 0.5 1 1 7 8
EGADS : 7 Yes 0 0 1 0.5 1 6 9 10
EGADS : 8 Yes 0 0 1 0.5 1 3 6 9
EGADS : 9 Yes 0 0 1 0.5 1 7 8 10
EGADS : 10 Yes 0 0 1 0.5 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 13.1976
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 428.309
AFLR4 : Abs Min Surf Spacing = 0.032994
AFLR4 : Min Surf Spacing = 0.065988
AFLR4 : Max Surf Spacing = 1.31976
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 23118
AFLR43 : Nodes = 11563
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 11563 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 FarField
UG3 : 12 FarField
UG3 : 13 FarField
UG3 : 14 FarField
UG3 : 15 FarField
UG3 : 16 FarField
AFLR3 : CPU Time = 0.036 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 11563 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 2314 16716
AFLR3 IG : Nodes, Elements = 4628 33740
AFLR3 IG : Nodes, Elements = 6942 53623
AFLR3 IG : Nodes, Elements = 9256 74438
AFLR3 IG : Nodes, Elements = 11570 95707
AFLR3 IG : Nodes, Elements = 11570 95483
AFLR3 IG : Nodes, Elements = 11563 61784
AFLR3 IG : Nodes, Elements = 11563 61867
AFLR3 IG : Nodes, Elements = 11563 39409
AFLR3 IG : Nodes, Elements = 11563 34878
AFLR3 : CPU Time = 0.828 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 11563 34878
AFLR3 GG : Nodes, Elements = 16496 49957
AFLR3 GG : Nodes, Elements = 16496 70754
AFLR3 GG : Nodes, Elements = 16496 65441
AFLR3 GG : Nodes, Elements = 20474 77967
AFLR3 GG : Nodes, Elements = 20474 92760
AFLR3 GG : Nodes, Elements = 20474 87583
AFLR3 GG : Nodes, Elements = 24849 101329
AFLR3 GG : Nodes, Elements = 24849 118564
AFLR3 GG : Nodes, Elements = 24849 113057
AFLR3 GG : Nodes, Elements = 29511 127335
AFLR3 GG : Nodes, Elements = 29511 145756
AFLR3 GG : Nodes, Elements = 29511 140522
AFLR3 GG : Nodes, Elements = 34372 155355
AFLR3 GG : Nodes, Elements = 34372 174698
AFLR3 GG : Nodes, Elements = 34372 169453
AFLR3 GG : Nodes, Elements = 39230 184208
AFLR3 GG : Nodes, Elements = 39230 203201
AFLR3 GG : Nodes, Elements = 39230 198077
AFLR3 GG : Nodes, Elements = 44067 212787
AFLR3 GG : Nodes, Elements = 44067 231574
AFLR3 GG : Nodes, Elements = 44067 226725
AFLR3 GG : Nodes, Elements = 48793 241074
AFLR3 GG : Nodes, Elements = 48793 259704
AFLR3 GG : Nodes, Elements = 48793 254826
AFLR3 GG : Nodes, Elements = 53425 268867
AFLR3 GG : Nodes, Elements = 53425 286996
AFLR3 GG : Nodes, Elements = 53425 282350
AFLR3 GG : Nodes, Elements = 57940 296060
AFLR3 GG : Nodes, Elements = 57940 313822
AFLR3 GG : Nodes, Elements = 57940 309079
AFLR3 GG : Nodes, Elements = 62354 322460
AFLR3 GG : Nodes, Elements = 62354 339840
AFLR3 GG : Nodes, Elements = 62354 335275
AFLR3 GG : Nodes, Elements = 66713 348501
AFLR3 GG : Nodes, Elements = 66713 365339
AFLR3 GG : Nodes, Elements = 66713 361041
AFLR3 GG : Nodes, Elements = 70982 373968
AFLR3 GG : Nodes, Elements = 70982 390795
AFLR3 GG : Nodes, Elements = 70982 386488
AFLR3 GG : Nodes, Elements = 75066 398863
AFLR3 GG : Nodes, Elements = 75066 414944
AFLR3 GG : Nodes, Elements = 75066 410652
AFLR3 GG : Nodes, Elements = 79089 422849
AFLR3 GG : Nodes, Elements = 79089 438593
AFLR3 GG : Nodes, Elements = 79089 434590
AFLR3 GG : Nodes, Elements = 82990 446388
AFLR3 GG : Nodes, Elements = 82990 461737
AFLR3 GG : Nodes, Elements = 82990 457790
AFLR3 GG : Nodes, Elements = 86679 468952
AFLR3 GG : Nodes, Elements = 86679 483418
AFLR3 GG : Nodes, Elements = 86679 479677
AFLR3 GG : Nodes, Elements = 90286 490569
AFLR3 GG : Nodes, Elements = 90286 504620
AFLR3 GG : Nodes, Elements = 90286 501105
AFLR3 GG : Nodes, Elements = 93781 511664
AFLR3 GG : Nodes, Elements = 93781 525309
AFLR3 GG : Nodes, Elements = 93781 521819
AFLR3 GG : Nodes, Elements = 97084 531790
AFLR3 GG : Nodes, Elements = 97084 544813
AFLR3 GG : Nodes, Elements = 97084 541433
AFLR3 GG : Nodes, Elements = 100278 551068
AFLR3 GG : Nodes, Elements = 100278 563612
AFLR3 GG : Nodes, Elements = 100278 560342
AFLR3 GG : Nodes, Elements = 103376 569686
AFLR3 GG : Nodes, Elements = 103376 581814
AFLR3 GG : Nodes, Elements = 103376 578764
AFLR3 GG : Nodes, Elements = 106363 587778
AFLR3 GG : Nodes, Elements = 106363 599392
AFLR3 GG : Nodes, Elements = 106363 596512
AFLR3 GG : Nodes, Elements = 109168 604963
AFLR3 GG : Nodes, Elements = 109168 615928
AFLR3 GG : Nodes, Elements = 109168 613178
AFLR3 GG : Nodes, Elements = 111839 621232
AFLR3 GG : Nodes, Elements = 111839 631817
AFLR3 GG : Nodes, Elements = 111839 629118
AFLR3 GG : Nodes, Elements = 114346 636681
AFLR3 GG : Nodes, Elements = 114346 646453
AFLR3 GG : Nodes, Elements = 114346 644024
AFLR3 GG : Nodes, Elements = 116718 651184
AFLR3 GG : Nodes, Elements = 116718 660339
AFLR3 GG : Nodes, Elements = 116718 658008
AFLR3 GG : Nodes, Elements = 119006 664904
AFLR3 GG : Nodes, Elements = 119006 674034
AFLR3 GG : Nodes, Elements = 119006 671709
AFLR3 GG : Nodes, Elements = 121097 678015
AFLR3 GG : Nodes, Elements = 121097 686107
AFLR3 GG : Nodes, Elements = 121097 684043
AFLR3 GG : Nodes, Elements = 123032 689878
AFLR3 GG : Nodes, Elements = 123032 697499
AFLR3 GG : Nodes, Elements = 123032 695602
AFLR3 GG : Nodes, Elements = 124821 701006
AFLR3 GG : Nodes, Elements = 124821 707974
AFLR3 GG : Nodes, Elements = 124821 706183
AFLR3 GG : Nodes, Elements = 126503 711252
AFLR3 GG : Nodes, Elements = 126503 717957
AFLR3 GG : Nodes, Elements = 126503 716225
AFLR3 GG : Nodes, Elements = 128091 721014
AFLR3 GG : Nodes, Elements = 128091 727222
AFLR3 GG : Nodes, Elements = 128091 725653
AFLR3 GG : Nodes, Elements = 129503 729914
AFLR3 GG : Nodes, Elements = 129503 735418
AFLR3 GG : Nodes, Elements = 129503 734022
AFLR3 GG : Nodes, Elements = 130827 738013
AFLR3 GG : Nodes, Elements = 130827 743263
AFLR3 GG : Nodes, Elements = 130827 741872
AFLR3 GG : Nodes, Elements = 132013 745441
AFLR3 GG : Nodes, Elements = 132013 750146
AFLR3 GG : Nodes, Elements = 132013 748949
AFLR3 GG : Nodes, Elements = 133097 752213
AFLR3 GG : Nodes, Elements = 133097 756440
AFLR3 GG : Nodes, Elements = 133097 755409
AFLR3 GG : Nodes, Elements = 134096 758410
AFLR3 GG : Nodes, Elements = 134096 762353
AFLR3 GG : Nodes, Elements = 134096 761358
AFLR3 GG : Nodes, Elements = 135016 764123
AFLR3 GG : Nodes, Elements = 135016 767759
AFLR3 GG : Nodes, Elements = 135016 766857
AFLR3 GG : Nodes, Elements = 135836 769326
AFLR3 GG : Nodes, Elements = 135836 772483
AFLR3 GG : Nodes, Elements = 135836 771678
AFLR3 GG : Nodes, Elements = 136555 773841
AFLR3 GG : Nodes, Elements = 136555 776675
AFLR3 GG : Nodes, Elements = 136555 775958
AFLR3 GG : Nodes, Elements = 137193 777874
AFLR3 GG : Nodes, Elements = 137193 780391
AFLR3 GG : Nodes, Elements = 137193 779778
AFLR3 GG : Nodes, Elements = 137745 781434
AFLR3 GG : Nodes, Elements = 137745 783542
AFLR3 GG : Nodes, Elements = 137745 783014
AFLR3 GG : Nodes, Elements = 138168 784283
AFLR3 GG : Nodes, Elements = 138168 786000
AFLR3 GG : Nodes, Elements = 138168 785511
AFLR3 GG : Nodes, Elements = 138509 786534
AFLR3 GG : Nodes, Elements = 138509 787906
AFLR3 GG : Nodes, Elements = 138509 787512
AFLR3 GG : Nodes, Elements = 138768 788291
AFLR3 GG : Nodes, Elements = 138768 789371
AFLR3 GG : Nodes, Elements = 138768 789056
AFLR3 GG : Nodes, Elements = 138948 789596
AFLR3 GG : Nodes, Elements = 138948 790332
AFLR3 GG : Nodes, Elements = 138948 790114
AFLR3 GG : Nodes, Elements = 139074 790493
AFLR3 GG : Nodes, Elements = 139074 791015
AFLR3 GG : Nodes, Elements = 139074 790850
AFLR3 GG : Nodes, Elements = 139160 791108
AFLR3 GG : Nodes, Elements = 139160 791448
AFLR3 GG : Nodes, Elements = 139160 791345
AFLR3 GG : Nodes, Elements = 139211 791498
AFLR3 GG : Nodes, Elements = 139211 791701
AFLR3 GG : Nodes, Elements = 139211 791640
AFLR3 GG : Nodes, Elements = 139242 791733
AFLR3 GG : Nodes, Elements = 139242 791861
AFLR3 GG : Nodes, Elements = 139242 791819
AFLR3 GG : Nodes, Elements = 139249 791840
AFLR3 GG : Nodes, Elements = 139249 791873
AFLR3 GG : Nodes, Elements = 139249 791858
AFLR3 GG : Nodes, Elements = 139252 791867
AFLR3 GG : Nodes, Elements = 139252 791877
AFLR3 GG : Nodes, Elements = 139252 791873
AFLR3 GG : Nodes, Elements = 139253 791876
AFLR3 GG : Nodes, Elements = 139253 791883
AFLR3 GG : Nodes, Elements = 139253 791878
AFLR3 GG : Nodes, Elements = 139260 791899
AFLR3 GG : Nodes, Elements = 139260 791926
AFLR3 GG : Nodes, Elements = 139260 791914
AFLR3 GG : Nodes, Elements = 139262 791920
AFLR3 GG : Nodes, Elements = 139262 791928
AFLR3 GG : Nodes, Elements = 139262 791923
AFLR3 GG : Nodes, Elements = 139263 791926
AFLR3 GG : Nodes, Elements = 139263 791930
AFLR3 GG : Nodes, Elements = 139263 791927
AFLR3 : CPU Time = 16.631 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 139263 791927
AFLR3 QI : Nodes, Elements = 138470 787420
AFLR3 QI : Nodes, Elements = 138371 786852
AFLR3 QI : Nodes, Elements = 138355 786758
AFLR3 QI : Nodes, Elements = 138353 786746
AFLR3 QI : Nodes, Elements = 138353 790318
AFLR3 QI : Nodes, Elements = 138353 786519
AFLR3 QI : Nodes, Elements = 138353 784972
AFLR3 QI : Nodes, Elements = 138353 785336
AFLR3 QI : Nodes, Elements = 138353 784715
AFLR3 QI : Nodes, Elements = 138353 784549
AFLR3 : CPU Time = 2.805 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 784549
UG3 : Min, Max Ang = 3.352 156.2
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 784549
UG3 : Min Vol = 0.00102
UG3 : Average Vol = 7.6e+04
UG3 : Total-Tet-Vol = 5.96e+10
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 784549
UG3 : Min, Max Q = 0.0447 1
UG3 : Average Q = 0.9
UG3 : No. Q< 0.1 = 34
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 20.675 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 784549
UG3 : Min, Max Ang = 3.352 156.2
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 784549
UG3 : Min Vol = 0.00102
UG3 : Average Vol = 7.6e+04
UG3 : Total-Tet-Vol = 5.96e+10
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 784549
UG3 : Min, Max Q = 0.206 1
UG3 : Average Q = 0.858
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
Number of nodes = 138353
Number of elements = 807667
Number of triangles = 23118
Number of quadrilatarals = 0
Number of tetrahedrals = 784549
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
==> Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.
Surface(s) plotted in the output file: BC_1.
Surface(s) affected by the design variables: BC_1.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat.
Surface file name: surface_flow_aeroelasticIterative.
Volume file name: flow_aeroelasticIterative.
Restart file name: restart_flow_aeroelasticIterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
138353 grid points.
784549 volume elements.
2 surface markers.
23082 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
784549 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.96352e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 29.8369. Mean K: 1.54048. Standard deviation K: 3.02418.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 53.2849| 87.2163|
| CV Face Area Aspect Ratio| 1.05837| 624.248|
| CV Sub-Volume Ratio| 1.03302| 9859.67|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 138353| 1/1.00| 10|
| 1| 22635| 1/6.11| 8.20393|
| 2| 3435| 1/6.59| 6.5639|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 97.6729 m.
Wetted area = 8661.74 m^2.
Area projection in the x-plane = 677.811 m^2, y-plane = 441.377 m^2, z-plane = 4150.71 m^2.
Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m.
Min. coordinate in the x-direction = 50 m, y-direction = -97.6729 m, z-direction = -8.47948 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 6.3736e+00| 0.748156| 2.907167| 2.644419| 6.217262| -0.776081|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.9463e+00| 2.193422| 4.562457| 4.459169| 7.653331| -0.476445|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.7283e+00| 3.220298| 5.616950| 5.416508| 8.692127| 1.468288|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.6391e+00| 4.326237| 6.696479| 6.559465| 9.797905| -16.210089|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.5928e+00| 5.449284| 7.811591| 7.705956| 10.920940| -8.274538|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 5.44928| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticIterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|CSV file |surface_flow_aeroelasticIterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary |flow_aeroelasticIterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticIterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
==> Running SU2 post-analysis...
==> Running ASTROS pre-analysis...
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
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 = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
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
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 11543
CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure'
Rank 0: src = 2.608592e+12, tgt = 2.608592e+12, diff = 1.062328e+03
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 11543
CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure'
Rank 0: src = 2.590668e+12, tgt = 2.590668e+12, diff = 9.744878e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 11543
CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure'
Rank 0: src = 8.484994e+08, tgt = 8.485003e+08, diff = 9.237144e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 11543
CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure'
Rank 0: src = 8.699308e+08, tgt = 8.699317e+08, diff = 8.929823e+02
Extracting external pressure loads from data transfer....
TransferName = upperWing
Number of Elements = 98 (total = 98)
Extracting external pressure loads from data transfer....
TransferName = lowerWing
Number of Elements = 98 (total = 196)
Extracting external pressure loads from data transfer....
TransferName = leftTip
Number of Elements = 17 (total = 213)
Extracting external pressure loads from data transfer....
TransferName = riteTip
Number of Elements = 17 (total = 230)
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
Writing coordinate system cards
==> Running mASTROS......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
==> Running ASTROS post-analysis...
==> Running SU2 pre-analysis...
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
==> Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
138353 grid points.
784549 volume elements.
2 surface markers.
23082 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
784549 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 5.96352e+10.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
WARNING: Convexity is not checked for 3D elements (issue #1171).
Completed in 90.932321 seconds on 1 core.
----------------------- Write deformed grid files -----------------------
|SU2 mesh |../aflr3/aflr3_CAPS.su2 |
|CSV file |surface_deformed.csv |
|Tecplot binary |volume_deformed.szplt |
|Tecplot binary surface |surface_deformed.szplt |
Adding any FFD information to the SU2 file.
------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.
------------------------- Exit Success (SU2_DEF) ------------------------
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.1 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2024, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.
Surface(s) plotted in the output file: BC_1.
Surface(s) affected by the design variables: BC_1.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat.
Surface file name: surface_flow_aeroelasticIterative.
Volume file name: flow_aeroelasticIterative.
Restart file name: restart_flow_aeroelasticIterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
138353 grid points.
784549 volume elements.
2 surface markers.
23082 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
784549 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 161258 TETRAHEDRON volume elements.
There has been a re-orientation of 6205 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.96714e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 50.446. Mean K: 1.91664. Standard deviation K: 2.5278.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.20947| 85.7885|
| CV Face Area Aspect Ratio| 1.07738| 5213.62|
| CV Sub-Volume Ratio| 1.05919| 3.08401e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 138353| 1/1.00| 10|
| 1| 22610| 1/6.12| 8.20091|
| 2| 3433| 1/6.59| 6.56263|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 112.067 m.
Wetted area = 687669 m^2.
Area projection in the x-plane = 192396 m^2, y-plane = 170768 m^2, z-plane = 62406.8 m^2.
Max. coordinate in the x-direction = 176.384 m, y-direction = 112.067 m, z-direction = 225.336 m.
Min. coordinate in the x-direction = 43.9729 m, y-direction = -116.9 m, z-direction = -695.222 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 5.5746e+00| 4.679017| 7.655201| 7.476894| 10.148122| -0.028447|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 6.8386e+00| 4.935745| 7.624566| 7.419008| 10.339948| 0.000774|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 7.2443e+00| 5.516931| 7.941695| 7.846123| 10.991518| 0.005062|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 8.1423e+00| 6.288641| 8.672463| 8.604690| 11.749243| 0.020913|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 8.6891e+00| 6.376675| 8.830266| 8.721765| 11.869846| 0.031217|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 6.37668| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticIterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|CSV file |surface_flow_aeroelasticIterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary |flow_aeroelasticIterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticIterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 9965 non-physical points in the solution.
Warning: 3124 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
==> Running SU2 post-analysis...
==> Running ASTROS pre-analysis...
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 11543
CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure'
Rank 0: src = 1.582269e+12, tgt = 1.582269e+12, diff = 6.849866e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 11543
CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure'
Rank 0: src = 1.353977e+12, tgt = 1.353977e+12, diff = 1.758545e+00
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 11543
CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure'
Rank 0: src = 3.008368e+08, tgt = 3.008449e+08, diff = 8.122931e+03
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 11543
CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure'
Rank 0: src = 2.657267e+08, tgt = 2.657268e+08, diff = 1.194048e+02
Extracting external pressure loads from data transfer....
TransferName = upperWing
Number of Elements = 98 (total = 98)
Extracting external pressure loads from data transfer....
TransferName = lowerWing
Number of Elements = 98 (total = 196)
Extracting external pressure loads from data transfer....
TransferName = leftTip
Number of Elements = 17 (total = 213)
Extracting external pressure loads from data transfer....
TransferName = riteTip
Number of Elements = 17 (total = 230)
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
Writing coordinate system cards
==> Running mASTROS......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
==> Running ASTROS post-analysis...
real 5m50.184s
user 5m5.247s
sys 0m35.629s
+ status=0
+ set +x
=================================================
data/session10/2_aeroelastic_Iterative_SU2_Astros.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
session08 cart3d
session08 fun3d
session09 nastran
session11 fun3d+astros
=================================================
All tests pass!
=================================================
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt
+ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ find /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
data/Plugs/plugs0a.csm
data/Plugs/plugs0b.csm
data/Plugs/plugs0c.csm
data/Plugs/plugs0d.csm
total 50872
-rw-r--r-- 1 jenkins staff 1.2M Jul 26 12:16 ASTRO.D01
-rw-r--r-- 1 jenkins staff 277K Jul 26 12:16 ASTRO.IDX
-rwxr-xr-x 1 jenkins staff 129K Jul 26 12:17 ESPxddm
-rwxr-xr-x 1 jenkins staff 210K Jul 26 12:17 Slugs
-rwxr-xr-x 1 jenkins staff 85K Jul 26 12:17 TestFit
-rwxr-xr-x 1 jenkins staff 1.8M Jul 26 12:16 avl
-rwxr-xr-x 1 jenkins staff 34K Jul 26 12:17 cart3dTest
-rwxr-xr-x 1 jenkins staff 34K Jul 26 12:17 egads2cart
-rwxr-xr-x 1 jenkins staff 70K Jul 26 12:17 egads2cgt
-rwxr-xr-x 1 jenkins staff 416K Jul 26 12:17 friction
-rwxr-xr-x 1 jenkins staff 8.9M Jul 26 12:16 mastros.exe
-rwxr-xr-x 1 jenkins staff 2.2M Jul 26 12:16 mses
-rwxr-xr-x 1 jenkins staff 2.5M Jul 26 12:16 mset
-rwxr-xr-x 1 jenkins staff 34K Jul 26 12:17 phaseUtil
-rw-r--r-- 1 jenkins staff 1.6K Jul 28 00:53 pod.egads
-rw-r--r-- 1 jenkins staff 0B Jul 28 00:53 port7681.jrnl
-rwxr-xr-x 1 jenkins staff 1.2M Jul 26 12:16 pplot
-rwxr-xr-x 1 jenkins staff 1.2M Jul 26 12:16 pxplot
-rwxr-xr-x 1 jenkins staff 68K Jul 26 12:17 sensCSM
-rwxr-xr-x 1 jenkins staff 206K Jul 26 12:17 serveCSM
-rwxr-xr-x 1 jenkins staff 174K Jul 26 12:17 serveESP
-rwxr-xr-x 1 jenkins staff 51K Jul 26 12:17 vCurvature
-rwxr-xr-x 1 jenkins staff 35K Jul 26 12:17 vGeom
-rwxr-xr-x 1 jenkins staff 52K Jul 26 12:17 vTess
-rwxr-xr-x 1 jenkins staff 2.0M Jul 26 12:17 vTesstatic
-rw-r--r-- 1 jenkins staff 196K Jul 28 00:53 wingMultiModel.bdf
-rwxr-xr-x 1 jenkins staff 1.8M Jul 26 12:16 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/verify_7.8.1/plugs0a.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 5.416e-07, rmsbest= 6.132e-04, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 2, unclass= 0
Starting pass 3 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m19.657s
user 0m13.462s
sys 0m2.321s
++ set +x
data/Plugs/plugs0a passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/verify_7.8.1/plugs0b.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 3.039e-07, rmsbest= 4.036e-02, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 2.814e-07, rmsbest= 1.924e-03, reclass= 1033, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 4.494e-07, rmsbest= 5.920e-04, reclass= 473, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 17, unclass= 0
Starting pass 5 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m13.154s
user 0m15.398s
sys 0m0.334s
++ set +x
data/Plugs/plugs0b passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/verify_7.8.1/plugs0c.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m32.024s
user 0m46.122s
sys 0m0.759s
++ set +x
data/Plugs/plugs0c passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/verify_7.8.1/plugs0d.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m32.412s
user 0m46.668s
sys 0m0.761s
++ set +x
data/Plugs/plugs0d passed (as expected)
--------------------------------------------------------------------------------------------------
[Execution node] check if [macys_VM] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [macys_VM] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_bPreBuilt/ESPVersion=126,buildnode=macys_VM #77'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS