Started by upstream project "ESP_bPreBuilt" build number 69
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 '2024-04-28T12:59:25.118 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 2481
Checking out a fresh workspace because /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 '2024-04-28T12:59:25.118 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 858
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [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/jenkins13527214763841815410.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_PreBuilt.sh
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.6
++ OCCTREF=7.6
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.34.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ 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
++ [[ '' == \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
++ [[ 7.6 != '' ]]
++ [[ '' != '' ]]
++ [[ macys_VM == *\r\e\y\n\o\l\d\s* ]]
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
+++ [[ -r /usr/local/etc/profile.d/bash_completion.sh ]]
+++ . /usr/local/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
+++ export PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d '/Users/jenkins/util/ESP/OpenCASCADE-.?'
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_11.5.14
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
++ export PATH=/Users/jenkins/workspace/ESP_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-v8.0.0/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-v8.0.0/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-v8.0.0/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-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/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-v8.0.0/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-v8.0.0/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/ESPbeta-macos-x86_64.tgz
--2024-04-28 12:59:38-- https://acdl.mit.edu/ESP/archive/ESPbeta-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: 517018302 (493M) [application/x-gzip]
Saving to: ‘ESPbeta-macos-x86_64.tgz’
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13100K .......... .......... .......... .......... .......... 2% 4.16M 70s
13150K .......... .......... .......... .......... .......... 2% 5.43M 70s
13200K .......... .......... .......... .......... .......... 2% 4.67M 71s
13250K .......... .......... .......... .......... .......... 2% 4.58M 71s
13300K .......... .......... .......... .......... .......... 2% 3.71M 71s
13350K .......... .......... .......... .......... .......... 2% 3.19M 71s
13400K .......... .......... .......... .......... .......... 2% 4.70M 71s
13450K .......... .......... .......... .......... .......... 2% 2.64M 72s
13500K .......... .......... .......... .......... .......... 2% 4.65M 72s
13550K .......... .......... .......... .......... .......... 2% 4.12M 72s
13600K .......... .......... .......... .......... .......... 2% 4.56M 72s
13650K .......... .......... .......... .......... .......... 2% 11.3M 72s
13700K .......... .......... .......... .......... .......... 2% 11.7M 72s
13750K .......... .......... .......... .......... .......... 2% 8.86M 72s
13800K .......... .......... .......... .......... .......... 2% 28.8M 72s
13850K .......... .......... .......... .......... .......... 2% 9.22M 72s
13900K .......... .......... .......... .......... .......... 2% 9.60M 71s
13950K .......... .......... .......... .......... .......... 2% 8.63M 71s
14000K .......... .......... .......... .......... .......... 2% 7.28M 71s
14050K .......... .......... .......... .......... .......... 2% 9.10M 71s
14100K .......... .......... .......... .......... .......... 2% 9.15M 71s
14150K .......... .......... .......... .......... .......... 2% 9.13M 71s
14200K .......... .......... .......... .......... .......... 2% 4.18M 71s
14250K .......... .......... .......... .......... .......... 2% 3.74M 71s
14300K .......... .......... .......... .......... .......... 2% 6.18M 71s
14350K .......... .......... .......... .......... .......... 2% 6.02M 72s
14400K .......... .......... .......... .......... .......... 2% 6.17M 72s
14450K .......... .......... .......... .......... .......... 2% 4.51M 72s
14500K .......... .......... .......... .......... .......... 2% 8.41M 72s
14550K .......... .......... .......... .......... .......... 2% 12.6M 71s
14600K .......... .......... .......... .......... .......... 2% 10.1M 71s
14650K .......... .......... .......... .......... .......... 2% 9.11M 71s
14700K .......... .......... .......... .......... .......... 2% 5.74M 71s
14750K .......... .......... .......... .......... .......... 2% 7.39M 71s
14800K .......... .......... .......... .......... .......... 2% 7.32M 71s
14850K .......... .......... .......... .......... .......... 2% 4.73M 71s
14900K .......... .......... .......... .......... .......... 2% 7.17M 71s
14950K .......... .......... .......... .......... .......... 2% 3.68M 72s
15000K .......... .......... .......... .......... .......... 2% 5.26M 72s
15050K .......... .......... .......... .......... .......... 2% 4.23M 72s
15100K .......... .......... .......... .......... .......... 3% 3.76M 72s
15150K .......... .......... .......... .......... .......... 3% 4.66M 72s
15200K .......... .......... .......... .......... .......... 3% 3.79M 72s
15250K .......... .......... .......... .......... .......... 3% 5.29M 72s
15300K .......... .......... .......... .......... .......... 3% 6.25M 72s
15350K .......... .......... .......... .......... .......... 3% 3.07M 72s
15400K .......... .......... .......... .......... .......... 3% 7.35M 72s
15450K .......... .......... .......... .......... .......... 3% 6.43M 72s
15500K .......... .......... .......... .......... .......... 3% 6.14M 72s
15550K .......... .......... .......... .......... .......... 3% 5.47M 72s
15600K .......... .......... .......... .......... .......... 3% 3.19M 73s
15650K .......... .......... .......... .......... .......... 3% 4.65M 73s
15700K .......... .......... .......... .......... .......... 3% 5.34M 73s
15750K .......... .......... .......... .......... .......... 3% 11.8M 73s
15800K .......... .......... .......... .......... .......... 3% 12.1M 73s
15850K .......... .......... .......... .......... .......... 3% 7.27M 73s
15900K .......... .......... .......... .......... .......... 3% 12.2M 73s
15950K .......... .......... .......... .......... .......... 3% 7.04M 72s
16000K .......... .......... .......... .......... .......... 3% 12.1M 72s
16050K .......... .......... .......... .......... .......... 3% 7.44M 72s
16100K .......... .......... .......... .......... .......... 3% 5.22M 72s
16150K .......... .......... .......... .......... .......... 3% 7.23M 72s
16200K .......... .......... .......... .......... .......... 3% 7.03M 72s
16250K .......... .......... .......... .......... .......... 3% 6.33M 72s
16300K .......... .......... .......... .......... .......... 3% 9.03M 72s
16350K .......... .......... .......... .......... .......... 3% 11.6M 72s
16400K .......... .......... .......... .......... .......... 3% 18.0M 72s
16450K .......... .......... .......... .......... .......... 3% 9.12M 72s
16500K .......... .......... .......... .......... .......... 3% 11.5M 72s
16550K .......... .......... .......... .......... .......... 3% 11.6M 72s
16600K .......... .......... .......... .......... .......... 3% 6.17M 72s
16650K .......... .......... .......... .......... .......... 3% 5.30M 72s
16700K .......... .......... .......... .......... .......... 3% 9.30M 72s
16750K .......... .......... .......... .......... .......... 3% 7.47M 72s
16800K .......... .......... .......... .......... .......... 3% 7.31M 72s
16850K .......... .......... .......... .......... .......... 3% 6.33M 72s
16900K .......... .......... .......... .......... .......... 3% 7.32M 72s
16950K .......... .......... .......... .......... .......... 3% 6.26M 72s
17000K .......... .......... .......... .......... .......... 3% 4.27M 72s
17050K .......... .......... .......... .......... .......... 3% 6.44M 72s
17100K .......... .......... .......... .......... .......... 3% 5.36M 72s
17150K .......... .......... .......... .......... .......... 3% 4.71M 72s
17200K .......... .......... .......... .......... .......... 3% 6.85M 72s
17250K .......... .......... .......... .......... .......... 3% 12.0M 72s
17300K .......... .......... .......... .......... .......... 3% 11.7M 72s
17350K .......... .......... .......... .......... .......... 3% 11.3M 72s
17400K .......... .......... .......... .......... .......... 3% 11.4M 72s
17450K .......... .......... .......... .......... .......... 3% 11.8M 71s
17500K .......... .......... .......... .......... .......... 3% 11.0M 71s
17550K .......... .......... .......... .......... .......... 3% 11.6M 71s
17600K .......... .......... .......... .......... .......... 3% 8.16M 71s
17650K .......... .......... .......... .......... .......... 3% 16.3M 71s
17700K .......... .......... .......... .......... .......... 3% 15.1M 71s
17750K .......... .......... .......... .......... .......... 3% 18.5M 71s
17800K .......... .......... .......... .......... .......... 3% 9.12M 71s
17850K .......... .......... .......... .......... .......... 3% 180M 71s
17900K .......... .......... .......... .......... .......... 3% 6.45M 71s
17950K .......... .......... .......... .......... .......... 3% 12.3M 70s
18000K .......... .......... .......... .......... .......... 3% 11.8M 70s
18050K .......... .......... .......... .......... .......... 3% 5.30M 70s
18100K .......... .......... .......... .......... .......... 3% 6.21M 70s
18150K .......... .......... .......... .......... .......... 3% 6.13M 70s
18200K .......... .......... .......... .......... .......... 3% 6.22M 70s
18250K .......... .......... .......... .......... .......... 3% 7.43M 70s
18300K .......... .......... .......... .......... .......... 3% 8.59M 70s
18350K .......... .......... .......... .......... .......... 3% 17.8M 70s
18400K .......... .......... .......... .......... .......... 3% 9.22M 70s
18450K .......... .......... .......... .......... .......... 3% 11.3M 70s
18500K .......... .......... .......... .......... .......... 3% 12.5M 70s
18550K .......... .......... .......... .......... .......... 3% 4.10M 70s
18600K .......... .......... .......... .......... .......... 3% 4.65M 70s
18650K .......... .......... .......... .......... .......... 3% 7.25M 70s
18700K .......... .......... .......... .......... .......... 3% 3.86M 70s
18750K .......... .......... .......... .......... .......... 3% 4.17M 70s
18800K .......... .......... .......... .......... .......... 3% 4.13M 71s
18850K .......... .......... .......... .......... .......... 3% 4.80M 71s
18900K .......... .......... .......... .......... .......... 3% 4.21M 71s
18950K .......... .......... .......... .......... .......... 3% 6.53M 71s
19000K .......... .......... .......... .......... .......... 3% 16.8M 71s
19050K .......... .......... .......... .......... .......... 3% 15.4M 70s
19100K .......... .......... .......... .......... .......... 3% 7.50M 70s
19150K .......... .......... .......... .......... .......... 3% 12.3M 70s
19200K .......... .......... .......... .......... .......... 3% 8.69M 70s
19250K .......... .......... .......... .......... .......... 3% 17.3M 70s
19300K .......... .......... .......... .......... .......... 3% 16.9M 70s
19350K .......... .......... .......... .......... .......... 3% 15.0M 70s
19400K .......... .......... .......... .......... .......... 3% 29.1M 70s
19450K .......... .......... .......... .......... .......... 3% 14.8M 70s
19500K .......... .......... .......... .......... .......... 3% 20.1M 70s
19550K .......... .......... .......... .......... .......... 3% 18.1M 69s
19600K .......... .......... .......... .......... .......... 3% 5.63M 70s
19650K .......... .......... .......... .......... .......... 3% 6.64M 70s
19700K .......... .......... .......... .......... .......... 3% 8.79M 69s
19750K .......... .......... .......... .......... .......... 3% 6.47M 69s
19800K .......... .......... .......... .......... .......... 3% 6.49M 69s
19850K .......... .......... .......... .......... .......... 3% 4.69M 70s
19900K .......... .......... .......... .......... .......... 3% 4.82M 70s
19950K .......... .......... .......... .......... .......... 3% 4.20M 70s
20000K .......... .......... .......... .......... .......... 3% 6.13M 70s
20050K .......... .......... .......... .......... .......... 3% 4.12M 70s
20100K .......... .......... .......... .......... .......... 3% 3.88M 70s
20150K .......... .......... .......... .......... .......... 4% 5.35M 70s
20200K .......... .......... .......... .......... .......... 4% 3.21M 70s
20250K .......... .......... .......... .......... .......... 4% 6.52M 70s
20300K .......... .......... .......... .......... .......... 4% 5.35M 70s
20350K .......... .......... .......... .......... .......... 4% 5.38M 70s
20400K .......... .......... .......... .......... .......... 4% 6.24M 70s
20450K .......... .......... .......... .......... .......... 4% 5.22M 70s
20500K .......... .......... .......... .......... .......... 4% 6.33M 70s
20550K .......... .......... .......... .......... .......... 4% 3.12M 70s
20600K .......... .......... .......... .......... .......... 4% 3.79M 71s
20650K .......... .......... .......... .......... .......... 4% 4.66M 71s
20700K .......... .......... .......... .......... .......... 4% 4.29M 71s
20750K .......... .......... .......... .......... .......... 4% 3.34M 71s
20800K .......... .......... .......... .......... .......... 4% 3.72M 71s
20850K .......... .......... .......... .......... .......... 4% 2.81M 71s
20900K .......... .......... .......... .......... .......... 4% 2.29M 72s
20950K .......... .......... .......... .......... .......... 4% 3.74M 72s
21000K .......... .......... .......... .......... .......... 4% 4.09M 72s
21050K .......... .......... .......... .......... .......... 4% 7.44M 72s
21100K .......... .......... .......... .......... .......... 4% 6.18M 72s
21150K .......... .......... .......... .......... .......... 4% 7.33M 72s
21200K .......... .......... .......... .......... .......... 4% 7.35M 72s
21250K .......... .......... .......... .......... .......... 4% 6.96M 72s
21300K .......... .......... .......... .......... .......... 4% 5.30M 72s
21350K .......... .......... .......... .......... .......... 4% 4.61M 72s
21400K .......... .......... .......... .......... .......... 4% 3.82M 72s
21450K .......... .......... .......... .......... .......... 4% 3.49M 72s
21500K .......... .......... .......... .......... .......... 4% 6.20M 72s
21550K .......... .......... .......... .......... .......... 4% 4.72M 72s
21600K .......... .......... .......... .......... .......... 4% 3.40M 72s
21650K .......... .......... .......... .......... .......... 4% 4.74M 72s
21700K .......... .......... .......... .......... .......... 4% 3.71M 72s
21750K .......... .......... .......... .......... .......... 4% 4.64M 73s
21800K .......... .......... .......... .......... .......... 4% 3.71M 73s
21850K .......... .......... .......... .......... .......... 4% 3.68M 73s
21900K .......... .......... .......... .......... .......... 4% 4.19M 73s
21950K .......... .......... .......... .......... .......... 4% 2.82M 73s
22000K .......... .......... .......... .......... .......... 4% 3.71M 73s
22050K .......... .......... .......... .......... .......... 4% 4.64M 73s
22100K .......... .......... .......... .......... .......... 4% 3.69M 73s
22150K .......... .......... .......... .......... .......... 4% 6.09M 73s
22200K .......... .......... .......... .......... .......... 4% 8.86M 73s
22250K .......... .......... .......... .......... .......... 4% 12.3M 73s
22300K .......... .......... .......... .......... .......... 4% 11.8M 73s
22350K .......... .......... .......... .......... .......... 4% 6.36M 73s
22400K .......... .......... .......... .......... .......... 4% 16.7M 73s
22450K .......... .......... .......... .......... .......... 4% 10.0M 73s
22500K .......... .......... .......... .......... .......... 4% 12.1M 73s
22550K .......... .......... .......... .......... .......... 4% 9.35M 73s
22600K .......... .......... .......... .......... .......... 4% 8.38M 73s
22650K .......... .......... .......... .......... .......... 4% 12.6M 73s
22700K .......... .......... .......... .......... .......... 4% 9.60M 73s
22750K .......... .......... .......... .......... .......... 4% 11.1M 73s
22800K .......... .......... .......... .......... .......... 4% 9.57M 72s
22850K .......... .......... .......... .......... .......... 4% 17.2M 72s
22900K .......... .......... .......... .......... .......... 4% 9.67M 72s
22950K .......... .......... .......... .......... .......... 4% 9.27M 72s
23000K .......... .......... .......... .......... .......... 4% 9.43M 72s
23050K .......... .......... .......... .......... .......... 4% 7.36M 72s
23100K .......... .......... .......... .......... .......... 4% 6.09M 72s
23150K .......... .......... .......... .......... .......... 4% 6.51M 72s
23200K .......... .......... .......... .......... .......... 4% 5.28M 72s
23250K .......... .......... .......... .......... .......... 4% 4.61M 72s
23300K .......... .......... .......... .......... .......... 4% 3.77M 72s
23350K .......... .......... .......... .......... .......... 4% 3.20M 73s
23400K .......... .......... .......... .......... .......... 4% 3.72M 73s
23450K .......... .......... .......... .......... .......... 4% 8.67M 73s
23500K .......... .......... .......... .......... .......... 4% 33.5M 72s
23550K .......... .......... .......... .......... .......... 4% 8.68M 72s
23600K .......... .......... .......... .......... .......... 4% 7.48M 72s
23650K .......... .......... .......... .......... .......... 4% 7.22M 72s
23700K .......... .......... .......... .......... .......... 4% 6.08M 72s
23750K .......... .......... .......... .......... .......... 4% 11.5M 72s
23800K .......... .......... .......... .......... .......... 4% 7.15M 72s
23850K .......... .......... .......... .......... .......... 4% 5.70M 72s
23900K .......... .......... .......... .......... .......... 4% 11.7M 72s
23950K .......... .......... .......... .......... .......... 4% 6.22M 72s
24000K .......... .......... .......... .......... .......... 4% 9.04M 72s
24050K .......... .......... .......... .......... .......... 4% 7.21M 72s
24100K .......... .......... .......... .......... .......... 4% 6.05M 72s
24150K .......... .......... .......... .......... .......... 4% 7.60M 72s
24200K .......... .......... .......... .......... .......... 4% 6.13M 72s
24250K .......... .......... .......... .......... .......... 4% 7.53M 72s
24300K .......... .......... .......... .......... .......... 4% 4.66M 72s
24350K .......... .......... .......... .......... .......... 4% 4.89M 72s
24400K .......... .......... .......... .......... .......... 4% 9.00M 72s
24450K .......... .......... .......... .......... .......... 4% 4.29M 72s
24500K .......... .......... .......... .......... .......... 4% 3.38M 72s
24550K .......... .......... .......... .......... .......... 4% 3.67M 72s
24600K .......... .......... .......... .......... .......... 4% 4.15M 72s
24650K .......... .......... .......... .......... .......... 4% 2.16M 73s
24700K .......... .......... .......... .......... .......... 4% 2.88M 73s
24750K .......... .......... .......... .......... .......... 4% 6.05M 73s
24800K .......... .......... .......... .......... .......... 4% 18.0M 73s
24850K .......... .......... .......... .......... .......... 4% 8.86M 73s
24900K .......... .......... .......... .......... .......... 4% 12.0M 73s
24950K .......... .......... .......... .......... .......... 4% 4.65M 73s
25000K .......... .......... .......... .......... .......... 4% 7.77M 73s
25050K .......... .......... .......... .......... .......... 4% 4.61M 73s
25100K .......... .......... .......... .......... .......... 4% 7.51M 73s
25150K .......... .......... .......... .......... .......... 4% 6.15M 73s
25200K .......... .......... .......... .......... .......... 5% 3.10M 73s
25250K .......... .......... .......... .......... .......... 5% 4.64M 73s
25300K .......... .......... .......... .......... .......... 5% 5.28M 73s
25350K .......... .......... .......... .......... .......... 5% 5.31M 73s
25400K .......... .......... .......... .......... .......... 5% 5.33M 73s
25450K .......... .......... .......... .......... .......... 5% 8.87M 73s
25500K .......... .......... .......... .......... .......... 5% 4.69M 73s
25550K .......... .......... .......... .......... .......... 5% 3.76M 73s
25600K .......... .......... .......... .......... .......... 5% 3.69M 73s
25650K .......... .......... .......... .......... .......... 5% 6.29M 73s
25700K .......... .......... .......... .......... .......... 5% 3.80M 73s
25750K .......... .......... .......... .......... .......... 5% 7.54M 73s
25800K .......... .......... .......... .......... .......... 5% 4.10M 73s
25850K .......... .......... .......... .......... .......... 5% 4.11M 73s
25900K .......... .......... .......... .......... .......... 5% 4.73M 73s
25950K .......... .......... .......... .......... .......... 5% 6.16M 73s
26000K .......... .......... .......... .......... .......... 5% 4.01M 74s
26050K .......... .......... .......... .......... .......... 5% 5.28M 74s
26100K .......... .......... .......... .......... .......... 5% 4.15M 74s
26150K .......... .......... .......... .......... .......... 5% 5.35M 74s
26200K .......... .......... .......... .......... .......... 5% 3.78M 74s
26250K .......... .......... .......... .......... .......... 5% 9.31M 74s
26300K .......... .......... .......... .......... .......... 5% 11.7M 74s
26350K .......... .......... .......... .......... .......... 5% 11.0M 74s
26400K .......... .......... .......... .......... .......... 5% 9.21M 73s
26450K .......... .......... .......... .......... .......... 5% 8.53M 73s
26500K .......... .......... .......... .......... .......... 5% 9.20M 73s
26550K .......... .......... .......... .......... .......... 5% 6.47M 73s
26600K .......... .......... .......... .......... .......... 5% 3.76M 73s
26650K .......... .......... .......... .......... .......... 5% 7.41M 73s
26700K .......... .......... .......... .......... .......... 5% 6.18M 73s
26750K .......... .......... .......... .......... .......... 5% 7.04M 73s
26800K .......... .......... .......... .......... .......... 5% 4.68M 73s
26850K .......... .......... .......... .......... .......... 5% 4.21M 74s
26900K .......... .......... .......... .......... .......... 5% 7.45M 73s
26950K .......... .......... .......... .......... .......... 5% 4.58M 74s
27000K .......... .......... .......... .......... .......... 5% 11.8M 73s
27050K .......... .......... .......... .......... .......... 5% 28.0M 73s
27100K .......... .......... .......... .......... .......... 5% 12.1M 73s
27150K .......... .......... .......... .......... .......... 5% 7.22M 73s
27200K .......... .......... .......... .......... .......... 5% 8.67M 73s
27250K .......... .......... .......... .......... .......... 5% 5.40M 73s
27300K .......... .......... .......... .......... .......... 5% 9.10M 73s
27350K .......... .......... .......... .......... .......... 5% 5.24M 73s
27400K .......... .......... .......... .......... .......... 5% 9.15M 73s
27450K .......... .......... .......... .......... .......... 5% 7.06M 73s
27500K .......... .......... .......... .......... .......... 5% 7.11M 73s
27550K .......... .......... .......... .......... .......... 5% 6.15M 73s
27600K .......... .......... .......... .......... .......... 5% 6.27M 73s
27650K .......... .......... .......... .......... .......... 5% 7.75M 73s
27700K .......... .......... .......... .......... .......... 5% 5.92M 73s
27750K .......... .......... .......... .......... .......... 5% 11.8M 73s
27800K .......... .......... .......... .......... .......... 5% 6.18M 73s
27850K .......... .......... .......... .......... .......... 5% 6.12M 73s
27900K .......... .......... .......... .......... .......... 5% 9.02M 73s
27950K .......... .......... .......... .......... .......... 5% 7.26M 73s
28000K .......... .......... .......... .......... .......... 5% 5.46M 73s
28050K .......... .......... .......... .......... .......... 5% 5.58M 73s
28100K .......... .......... .......... .......... .......... 5% 4.66M 73s
28150K .......... .......... .......... .......... .......... 5% 4.23M 73s
28200K .......... .......... .......... .......... .......... 5% 4.63M 73s
28250K .......... .......... .......... .......... .......... 5% 3.76M 73s
28300K .......... .......... .......... .......... .......... 5% 4.12M 73s
28350K .......... .......... .......... .......... .......... 5% 4.14M 73s
28400K .......... .......... .......... .......... .......... 5% 9.15M 73s
28450K .......... .......... .......... .......... .......... 5% 7.17M 73s
28500K .......... .......... .......... .......... .......... 5% 9.15M 73s
28550K .......... .......... .......... .......... .......... 5% 8.77M 73s
28600K .......... .......... .......... .......... .......... 5% 8.87M 73s
28650K .......... .......... .......... .......... .......... 5% 9.79M 73s
28700K .......... .......... .......... .......... .......... 5% 5.20M 73s
28750K .......... .......... .......... .......... .......... 5% 6.24M 73s
28800K .......... .......... .......... .......... .......... 5% 11.0M 73s
28850K .......... .......... .......... .......... .......... 5% 8.66M 73s
28900K .......... .......... .......... .......... .......... 5% 17.1M 73s
28950K .......... .......... .......... .......... .......... 5% 7.49M 73s
29000K .......... .......... .......... .......... .......... 5% 6.17M 73s
29050K .......... .......... .......... .......... .......... 5% 12.3M 73s
29100K .......... .......... .......... .......... .......... 5% 9.14M 73s
29150K .......... .......... .......... .......... .......... 5% 7.32M 73s
29200K .......... .......... .......... .......... .......... 5% 9.25M 73s
29250K .......... .......... .......... .......... .......... 5% 6.85M 73s
29300K .......... .......... .......... .......... .......... 5% 5.40M 73s
29350K .......... .......... .......... .......... .......... 5% 4.60M 73s
29400K .......... .......... .......... .......... .......... 5% 8.73M 73s
29450K .......... .......... .......... .......... .......... 5% 10.9M 73s
29500K .......... .......... .......... .......... .......... 5% 24.6M 72s
29550K .......... .......... .......... .......... .......... 5% 18.1M 72s
29600K .......... .......... .......... .......... .......... 5% 11.0M 72s
29650K .......... .......... .......... .......... .......... 5% 26.9M 72s
29700K .......... .......... .......... .......... .......... 5% 11.2M 72s
29750K .......... .......... .......... .......... .......... 5% 15.1M 72s
29800K .......... .......... .......... .......... .......... 5% 9.45M 72s
29850K .......... .......... .......... .......... .......... 5% 7.47M 72s
29900K .......... .......... .......... .......... .......... 5% 5.43M 72s
29950K .......... .......... .......... .......... .......... 5% 8.60M 72s
30000K .......... .......... .......... .......... .......... 5% 8.82M 72s
30050K .......... .......... .......... .......... .......... 5% 12.1M 72s
30100K .......... .......... .......... .......... .......... 5% 6.17M 72s
30150K .......... .......... .......... .......... .......... 5% 11.5M 72s
30200K .......... .......... .......... .......... .......... 5% 11.4M 72s
30250K .......... .......... .......... .......... .......... 6% 11.4M 72s
30300K .......... .......... .......... .......... .......... 6% 11.9M 72s
30350K .......... .......... .......... .......... .......... 6% 9.30M 72s
30400K .......... .......... .......... .......... .......... 6% 9.03M 72s
30450K .......... .......... .......... .......... .......... 6% 11.0M 72s
30500K .......... .......... .......... .......... .......... 6% 11.8M 71s
30550K .......... .......... .......... .......... .......... 6% 11.8M 71s
30600K .......... .......... .......... .......... .......... 6% 7.15M 71s
30650K .......... .......... .......... .......... .......... 6% 7.34M 71s
30700K .......... .......... .......... .......... .......... 6% 13.9M 71s
30750K .......... .......... .......... .......... .......... 6% 9.09M 71s
30800K .......... .......... .......... .......... .......... 6% 7.06M 71s
30850K .......... .......... .......... .......... .......... 6% 2.85M 71s
30900K .......... .......... .......... .......... .......... 6% 5.05M 71s
30950K .......... .......... .......... .......... .......... 6% 4.54M 71s
31000K .......... .......... .......... .......... .......... 6% 3.90M 72s
31050K .......... .......... .......... .......... .......... 6% 4.69M 72s
31100K .......... .......... .......... .......... .......... 6% 6.10M 72s
31150K .......... .......... .......... .......... .......... 6% 6.13M 72s
31200K .......... .......... .......... .......... .......... 6% 4.72M 72s
31250K .......... .......... .......... .......... .......... 6% 4.74M 72s
31300K .......... .......... .......... .......... .......... 6% 3.75M 72s
31350K .......... .......... .......... .......... .......... 6% 6.67M 72s
31400K .......... .......... .......... .......... .......... 6% 12.5M 72s
31450K .......... .......... .......... .......... .......... 6% 9.14M 72s
31500K .......... .......... .......... .......... .......... 6% 12.4M 72s
31550K .......... .......... .......... .......... .......... 6% 8.41M 71s
31600K .......... .......... .......... .......... .......... 6% 7.44M 71s
31650K .......... .......... .......... .......... .......... 6% 8.83M 71s
31700K .......... .......... .......... .......... .......... 6% 7.54M 71s
31750K .......... .......... .......... .......... .......... 6% 8.97M 71s
31800K .......... .......... .......... .......... .......... 6% 17.7M 71s
31850K .......... .......... .......... .......... .......... 6% 6.27M 71s
31900K .......... .......... .......... .......... .......... 6% 12.4M 71s
31950K .......... .......... .......... .......... .......... 6% 8.35M 71s
32000K .......... .......... .......... .......... .......... 6% 16.8M 71s
32050K .......... .......... .......... .......... .......... 6% 6.26M 71s
32100K .......... .......... .......... .......... .......... 6% 6.10M 71s
32150K .......... .......... .......... .......... .......... 6% 4.82M 71s
32200K .......... .......... .......... .......... .......... 6% 3.70M 71s
32250K .......... .......... .......... .......... .......... 6% 6.07M 71s
32300K .......... .......... .......... .......... .......... 6% 6.28M 71s
32350K .......... .......... .......... .......... .......... 6% 4.65M 71s
32400K .......... .......... .......... .......... .......... 6% 4.71M 71s
32450K .......... .......... .......... .......... .......... 6% 5.29M 71s
32500K .......... .......... .......... .......... .......... 6% 19.2M 71s
32550K .......... .......... .......... .......... .......... 6% 12.0M 71s
32600K .......... .......... .......... .......... .......... 6% 15.5M 71s
32650K .......... .......... .......... .......... .......... 6% 9.14M 71s
32700K .......... .......... .......... .......... .......... 6% 12.7M 71s
32750K .......... .......... .......... .......... .......... 6% 18.1M 71s
32800K .......... .......... .......... .......... .......... 6% 12.4M 71s
32850K .......... .......... .......... .......... .......... 6% 6.38M 71s
32900K .......... .......... .......... .......... .......... 6% 9.20M 71s
32950K .......... .......... .......... .......... .......... 6% 7.41M 71s
33000K .......... .......... .......... .......... .......... 6% 11.4M 71s
33050K .......... .......... .......... .......... .......... 6% 12.1M 71s
33100K .......... .......... .......... .......... .......... 6% 5.58M 71s
33150K .......... .......... .......... .......... .......... 6% 12.1M 71s
33200K .......... .......... .......... .......... .......... 6% 6.11M 71s
33250K .......... .......... .......... .......... .......... 6% 9.65M 71s
33300K .......... .......... .......... .......... .......... 6% 5.18M 71s
33350K .......... .......... .......... .......... .......... 6% 3.39M 71s
33400K .......... .......... .......... .......... .......... 6% 6.14M 71s
33450K .......... .......... .......... .......... .......... 6% 4.70M 71s
33500K .......... .......... .......... .......... .......... 6% 5.47M 71s
33550K .......... .......... .......... .......... .......... 6% 5.29M 71s
33600K .......... .......... .......... .......... .......... 6% 3.84M 71s
33650K .......... .......... .......... .......... .......... 6% 17.4M 71s
33700K .......... .......... .......... .......... .......... 6% 6.27M 71s
33750K .......... .......... .......... .......... .......... 6% 6.11M 71s
33800K .......... .......... .......... .......... .......... 6% 6.29M 71s
33850K .......... .......... .......... .......... .......... 6% 7.49M 71s
33900K .......... .......... .......... .......... .......... 6% 6.92M 71s
33950K .......... .......... .......... .......... .......... 6% 8.90M 71s
34000K .......... .......... .......... .......... .......... 6% 6.12M 71s
34050K .......... .......... .......... .......... .......... 6% 9.38M 71s
34100K .......... .......... .......... .......... .......... 6% 9.12M 71s
34150K .......... .......... .......... .......... .......... 6% 7.44M 71s
34200K .......... .......... .......... .......... .......... 6% 5.38M 71s
34250K .......... .......... .......... .......... .......... 6% 5.34M 71s
34300K .......... .......... .......... .......... .......... 6% 4.57M 71s
34350K .......... .......... .......... .......... .......... 6% 4.16M 71s
34400K .......... .......... .......... .......... .......... 6% 5.38M 71s
34450K .......... .......... .......... .......... .......... 6% 5.34M 71s
34500K .......... .......... .......... .......... .......... 6% 6.13M 71s
34550K .......... .......... .......... .......... .......... 6% 7.56M 71s
34600K .......... .......... .......... .......... .......... 6% 4.79M 71s
34650K .......... .......... .......... .......... .......... 6% 4.12M 71s
34700K .......... .......... .......... .......... .......... 6% 3.46M 71s
34750K .......... .......... .......... .......... .......... 6% 6.24M 71s
34800K .......... .......... .......... .......... .......... 6% 5.39M 71s
34850K .......... .......... .......... .......... .......... 6% 3.21M 71s
34900K .......... .......... .......... .......... .......... 6% 6.93M 71s
34950K .......... .......... .......... .......... .......... 6% 9.43M 71s
35000K .......... .......... .......... .......... .......... 6% 5.97M 71s
35050K .......... .......... .......... .......... .......... 6% 4.49M 71s
35100K .......... .......... .......... .......... .......... 6% 4.14M 71s
35150K .......... .......... .......... .......... .......... 6% 3.75M 71s
35200K .......... .......... .......... .......... .......... 6% 4.70M 71s
35250K .......... .......... .......... .......... .......... 6% 4.68M 71s
35300K .......... .......... .......... .......... .......... 7% 5.41M 71s
35350K .......... .......... .......... .......... .......... 7% 8.03M 71s
35400K .......... .......... .......... .......... .......... 7% 18.1M 71s
35450K .......... .......... .......... .......... .......... 7% 21.6M 71s
35500K .......... .......... .......... .......... .......... 7% 12.1M 71s
35550K .......... .......... .......... .......... .......... 7% 20.8M 71s
35600K .......... .......... .......... .......... .......... 7% 15.1M 71s
35650K .......... .......... .......... .......... .......... 7% 9.42M 71s
35700K .......... .......... .......... .......... .......... 7% 11.5M 71s
35750K .......... .......... .......... .......... .......... 7% 23.5M 71s
35800K .......... .......... .......... .......... .......... 7% 7.64M 71s
35850K .......... .......... .......... .......... .......... 7% 8.84M 71s
35900K .......... .......... .......... .......... .......... 7% 6.07M 71s
35950K .......... .......... .......... .......... .......... 7% 2.86M 71s
36000K .......... .......... .......... .......... .......... 7% 3.78M 71s
36050K .......... .......... .......... .......... .......... 7% 2.89M 71s
36100K .......... .......... .......... .......... .......... 7% 1.96M 71s
36150K .......... .......... .......... .......... .......... 7% 1.41M 71s
36200K .......... .......... .......... .......... .......... 7% 4.17M 71s
36250K .......... .......... .......... .......... .......... 7% 4.12M 71s
36300K .......... .......... .......... .......... .......... 7% 3.38M 72s
36350K .......... .......... .......... .......... .......... 7% 2.48M 72s
36400K .......... .......... .......... .......... .......... 7% 6.20M 72s
36450K .......... .......... .......... .......... .......... 7% 6.18M 72s
36500K .......... .......... .......... .......... .......... 7% 7.22M 72s
36550K .......... .......... .......... .......... .......... 7% 8.93M 72s
36600K .......... .......... .......... .......... .......... 7% 5.35M 72s
36650K .......... .......... .......... .......... .......... 7% 5.43M 72s
36700K .......... .......... .......... .......... .......... 7% 4.13M 72s
36750K .......... .......... .......... .......... .......... 7% 5.28M 72s
36800K .......... .......... .......... .......... .......... 7% 3.65M 72s
36850K .......... .......... .......... .......... .......... 7% 5.89M 72s
36900K .......... .......... .......... .......... .......... 7% 12.2M 72s
36950K .......... .......... .......... .......... .......... 7% 8.50M 72s
37000K .......... .......... .......... .......... .......... 7% 17.6M 72s
37050K .......... .......... .......... .......... .......... 7% 8.75M 72s
37100K .......... .......... .......... .......... .......... 7% 5.26M 72s
37150K .......... .......... .......... .......... .......... 7% 5.34M 72s
37200K .......... .......... .......... .......... .......... 7% 4.15M 72s
37250K .......... .......... .......... .......... .......... 7% 2.32M 72s
37300K .......... .......... .......... .......... .......... 7% 5.18M 72s
37350K .......... .......... .......... .......... .......... 7% 2.47M 72s
37400K .......... .......... .......... .......... .......... 7% 3.10M 72s
37450K .......... .......... .......... .......... .......... 7% 5.27M 72s
37500K .......... .......... .......... .......... .......... 7% 16.6M 72s
37550K .......... .......... .......... .......... .......... 7% 12.3M 72s
37600K .......... .......... .......... .......... .......... 7% 7.48M 72s
37650K .......... .......... .......... .......... .......... 7% 7.38M 72s
37700K .......... .......... .......... .......... .......... 7% 11.8M 72s
37750K .......... .......... .......... .......... .......... 7% 7.34M 72s
37800K .......... .......... .......... .......... .......... 7% 6.33M 72s
37850K .......... .......... .......... .......... .......... 7% 5.76M 72s
37900K .......... .......... .......... .......... .......... 7% 9.15M 72s
37950K .......... .......... .......... .......... .......... 7% 6.18M 72s
38000K .......... .......... .......... .......... .......... 7% 8.79M 72s
38050K .......... .......... .......... .......... .......... 7% 31.1M 72s
38100K .......... .......... .......... .......... .......... 7% 11.7M 72s
38150K .......... .......... .......... .......... .......... 7% 18.3M 72s
38200K .......... .......... .......... .......... .......... 7% 9.64M 72s
38250K .......... .......... .......... .......... .......... 7% 17.6M 71s
38300K .......... .......... .......... .......... .......... 7% 11.1M 71s
38350K .......... .......... .......... .......... .......... 7% 7.46M 71s
38400K .......... .......... .......... .......... .......... 7% 7.59M 71s
38450K .......... .......... .......... .......... .......... 7% 7.32M 71s
38500K .......... .......... .......... .......... .......... 7% 9.22M 71s
38550K .......... .......... .......... .......... .......... 7% 8.82M 71s
38600K .......... .......... .......... .......... .......... 7% 6.17M 71s
38650K .......... .......... .......... .......... .......... 7% 7.01M 71s
38700K .......... .......... .......... .......... .......... 7% 9.26M 71s
38750K .......... .......... .......... .......... .......... 7% 6.19M 71s
38800K .......... .......... .......... .......... .......... 7% 18.4M 71s
38850K .......... .......... .......... .......... .......... 7% 5.49M 71s
38900K .......... .......... .......... .......... .......... 7% 6.18M 71s
38950K .......... .......... .......... .......... .......... 7% 6.26M 71s
39000K .......... .......... .......... .......... .......... 7% 4.76M 71s
39050K .......... .......... .......... .......... .......... 7% 3.23M 71s
39100K .......... .......... .......... .......... .......... 7% 4.13M 71s
39150K .......... .......... .......... .......... .......... 7% 9.10M 71s
39200K .......... .......... .......... .......... .......... 7% 6.23M 71s
39250K .......... .......... .......... .......... .......... 7% 4.67M 71s
39300K .......... .......... .......... .......... .......... 7% 5.23M 71s
39350K .......... .......... .......... .......... .......... 7% 3.49M 71s
39400K .......... .......... .......... .......... .......... 7% 6.17M 71s
39450K .......... .......... .......... .......... .......... 7% 8.81M 71s
39500K .......... .......... .......... .......... .......... 7% 12.8M 71s
39550K .......... .......... .......... .......... .......... 7% 12.1M 71s
39600K .......... .......... .......... .......... .......... 7% 11.0M 71s
39650K .......... .......... .......... .......... .......... 7% 16.1M 71s
39700K .......... .......... .......... .......... .......... 7% 6.59M 71s
39750K .......... .......... .......... .......... .......... 7% 9.08M 71s
39800K .......... .......... .......... .......... .......... 7% 16.0M 71s
39850K .......... .......... .......... .......... .......... 7% 11.5M 71s
39900K .......... .......... .......... .......... .......... 7% 9.27M 71s
39950K .......... .......... .......... .......... .......... 7% 9.17M 71s
40000K .......... .......... .......... .......... .......... 7% 12.0M 71s
40050K .......... .......... .......... .......... .......... 7% 12.0M 71s
40100K .......... .......... .......... .......... .......... 7% 8.97M 71s
40150K .......... .......... .......... .......... .......... 7% 6.08M 71s
40200K .......... .......... .......... .......... .......... 7% 6.28M 71s
40250K .......... .......... .......... .......... .......... 7% 11.5M 71s
40300K .......... .......... .......... .......... .......... 7% 9.15M 71s
40350K .......... .......... .......... .......... .......... 8% 7.55M 71s
40400K .......... .......... .......... .......... .......... 8% 3.79M 71s
40450K .......... .......... .......... .......... .......... 8% 4.10M 71s
40500K .......... .......... .......... .......... .......... 8% 4.58M 71s
40550K .......... .......... .......... .......... .......... 8% 5.24M 71s
40600K .......... .......... .......... .......... .......... 8% 6.08M 71s
40650K .......... .......... .......... .......... .......... 8% 6.22M 71s
40700K .......... .......... .......... .......... .......... 8% 3.85M 71s
40750K .......... .......... .......... .......... .......... 8% 4.59M 71s
40800K .......... .......... .......... .......... .......... 8% 4.66M 71s
40850K .......... .......... .......... .......... .......... 8% 4.73M 71s
40900K .......... .......... .......... .......... .......... 8% 9.19M 71s
40950K .......... .......... .......... .......... .......... 8% 12.1M 71s
41000K .......... .......... .......... .......... .......... 8% 15.8M 71s
41050K .......... .......... .......... .......... .......... 8% 12.8M 71s
41100K .......... .......... .......... .......... .......... 8% 16.3M 71s
41150K .......... .......... .......... .......... .......... 8% 9.05M 71s
41200K .......... .......... .......... .......... .......... 8% 7.10M 71s
41250K .......... .......... .......... .......... .......... 8% 6.35M 71s
41300K .......... .......... .......... .......... .......... 8% 7.22M 71s
41350K .......... .......... .......... .......... .......... 8% 6.29M 71s
41400K .......... .......... .......... .......... .......... 8% 6.20M 71s
41450K .......... .......... .......... .......... .......... 8% 4.25M 71s
41500K .......... .......... .......... .......... .......... 8% 3.41M 71s
41550K .......... .......... .......... .......... .......... 8% 2.48M 71s
41600K .......... .......... .......... .......... .......... 8% 1.69M 71s
41650K .......... .......... .......... .......... .......... 8% 2.31M 71s
41700K .......... .......... .......... .......... .......... 8% 1.78M 71s
41750K .......... .......... .......... .......... .......... 8% 5.09M 71s
41800K .......... .......... .......... .......... .......... 8% 11.4M 71s
41850K .......... .......... .......... .......... .......... 8% 9.06M 71s
41900K .......... .......... .......... .......... .......... 8% 8.82M 71s
41950K .......... .......... .......... .......... .......... 8% 6.17M 71s
42000K .......... .......... .......... .......... .......... 8% 7.37M 71s
42050K .......... .......... .......... .......... .......... 8% 7.48M 71s
42100K .......... .......... .......... .......... .......... 8% 5.30M 71s
42150K .......... .......... .......... .......... .......... 8% 7.11M 71s
42200K .......... .......... .......... .......... .......... 8% 6.25M 71s
42250K .......... .......... .......... .......... .......... 8% 4.65M 71s
42300K .......... .......... .......... .......... .......... 8% 5.48M 71s
42350K .......... .......... .......... .......... .......... 8% 9.04M 71s
42400K .......... .......... .......... .......... .......... 8% 11.7M 71s
42450K .......... .......... .......... .......... .......... 8% 5.21M 71s
42500K .......... .......... .......... .......... .......... 8% 9.19M 71s
42550K .......... .......... .......... .......... .......... 8% 11.4M 71s
42600K .......... .......... .......... .......... .......... 8% 11.6M 71s
42650K .......... .......... .......... .......... .......... 8% 7.06M 71s
42700K .......... .......... .......... .......... .......... 8% 7.54M 71s
42750K .......... .......... .......... .......... .......... 8% 7.24M 71s
42800K .......... .......... .......... .......... .......... 8% 9.33M 71s
42850K .......... .......... .......... .......... .......... 8% 6.11M 71s
42900K .......... .......... .......... .......... .......... 8% 7.37M 71s
42950K .......... .......... .......... .......... .......... 8% 4.08M 71s
43000K .......... .......... .......... .......... .......... 8% 6.37M 71s
43050K .......... .......... .......... .......... .......... 8% 9.11M 71s
43100K .......... .......... .......... .......... .......... 8% 11.4M 71s
43150K .......... .......... .......... .......... .......... 8% 29.4M 71s
43200K .......... .......... .......... .......... .......... 8% 11.0M 71s
43250K .......... .......... .......... .......... .......... 8% 6.10M 71s
43300K .......... .......... .......... .......... .......... 8% 6.34M 71s
43350K .......... .......... .......... .......... .......... 8% 6.16M 71s
43400K .......... .......... .......... .......... .......... 8% 5.25M 71s
43450K .......... .......... .......... .......... .......... 8% 6.06M 71s
43500K .......... .......... .......... .......... .......... 8% 4.18M 71s
43550K .......... .......... .......... .......... .......... 8% 4.66M 71s
43600K .......... .......... .......... .......... .......... 8% 4.09M 71s
43650K .......... .......... .......... .......... .......... 8% 3.43M 71s
43700K .......... .......... .......... .......... .......... 8% 5.42M 71s
43750K .......... .......... .......... .......... .......... 8% 5.35M 71s
43800K .......... .......... .......... .......... .......... 8% 4.19M 71s
43850K .......... .......... .......... .......... .......... 8% 3.79M 71s
43900K .......... .......... .......... .......... .......... 8% 7.12M 71s
43950K .......... .......... .......... .......... .......... 8% 9.32M 71s
44000K .......... .......... .......... .......... .......... 8% 7.47M 71s
44050K .......... .......... .......... .......... .......... 8% 4.76M 71s
44100K .......... .......... .......... .......... .......... 8% 5.32M 71s
44150K .......... .......... .......... .......... .......... 8% 6.12M 71s
44200K .......... .......... .......... .......... .......... 8% 4.17M 71s
44250K .......... .......... .......... .......... .......... 8% 7.23M 71s
44300K .......... .......... .......... .......... .......... 8% 6.19M 71s
44350K .......... .......... .......... .......... .......... 8% 4.13M 71s
44400K .......... .......... .......... .......... .......... 8% 3.22M 71s
44450K .......... .......... .......... .......... .......... 8% 3.38M 71s
44500K .......... .......... .......... .......... .......... 8% 6.14M 71s
44550K .......... .......... .......... .......... .......... 8% 4.76M 71s
44600K .......... .......... .......... .......... .......... 8% 4.72M 71s
44650K .......... .......... .......... .......... .......... 8% 5.28M 71s
44700K .......... .......... .......... .......... .......... 8% 7.27M 71s
44750K .......... .......... .......... .......... .......... 8% 11.8M 71s
44800K .......... .......... .......... .......... .......... 8% 7.51M 71s
44850K .......... .......... .......... .......... .......... 8% 7.37M 71s
44900K .......... .......... .......... .......... .......... 8% 7.52M 71s
44950K .......... .......... .......... .......... .......... 8% 7.52M 71s
45000K .......... .......... .......... .......... .......... 8% 7.66M 71s
45050K .......... .......... .......... .......... .......... 8% 12.1M 71s
45100K .......... .......... .......... .......... .......... 8% 11.5M 71s
45150K .......... .......... .......... .......... .......... 8% 18.1M 71s
45200K .......... .......... .......... .......... .......... 8% 12.6M 71s
45250K .......... .......... .......... .......... .......... 8% 12.6M 71s
45300K .......... .......... .......... .......... .......... 8% 18.6M 71s
45350K .......... .......... .......... .......... .......... 8% 9.03M 71s
45400K .......... .......... .......... .......... .......... 9% 11.8M 71s
45450K .......... .......... .......... .......... .......... 9% 9.17M 71s
45500K .......... .......... .......... .......... .......... 9% 9.40M 71s
45550K .......... .......... .......... .......... .......... 9% 9.69M 71s
45600K .......... .......... .......... .......... .......... 9% 7.48M 71s
45650K .......... .......... .......... .......... .......... 9% 7.24M 71s
45700K .......... .......... .......... .......... .......... 9% 4.10M 71s
45750K .......... .......... .......... .......... .......... 9% 4.24M 71s
45800K .......... .......... .......... .......... .......... 9% 5.16M 71s
45850K .......... .......... .......... .......... .......... 9% 4.27M 71s
45900K .......... .......... .......... .......... .......... 9% 7.41M 71s
45950K .......... .......... .......... .......... .......... 9% 11.5M 71s
46000K .......... .......... .......... .......... .......... 9% 7.04M 71s
46050K .......... .......... .......... .......... .......... 9% 12.3M 71s
46100K .......... .......... .......... .......... .......... 9% 7.31M 70s
46150K .......... .......... .......... .......... .......... 9% 11.6M 70s
46200K .......... .......... .......... .......... .......... 9% 7.44M 70s
46250K .......... .......... .......... .......... .......... 9% 9.65M 70s
46300K .......... .......... .......... .......... .......... 9% 11.6M 70s
46350K .......... .......... .......... .......... .......... 9% 5.34M 70s
46400K .......... .......... .......... .......... .......... 9% 7.46M 70s
46450K .......... .......... .......... .......... .......... 9% 7.03M 70s
46500K .......... .......... .......... .......... .......... 9% 5.27M 70s
46550K .......... .......... .......... .......... .......... 9% 6.27M 70s
46600K .......... .......... .......... .......... .......... 9% 3.38M 70s
46650K .......... .......... .......... .......... .......... 9% 3.84M 70s
46700K .......... .......... .......... .......... .......... 9% 4.65M 70s
46750K .......... .......... .......... .......... .......... 9% 6.21M 70s
46800K .......... .......... .......... .......... .......... 9% 7.45M 70s
46850K .......... .......... .......... .......... .......... 9% 24.4M 70s
46900K .......... .......... .......... .......... .......... 9% 11.5M 70s
46950K .......... .......... .......... .......... .......... 9% 17.3M 70s
47000K .......... .......... .......... .......... .......... 9% 9.47M 70s
47050K .......... .......... .......... .......... .......... 9% 7.38M 70s
47100K .......... .......... .......... .......... .......... 9% 6.02M 70s
47150K .......... .......... .......... .......... .......... 9% 7.36M 70s
47200K .......... .......... .......... .......... .......... 9% 5.46M 70s
47250K .......... .......... .......... .......... .......... 9% 5.21M 70s
47300K .......... .......... .......... .......... .......... 9% 6.25M 70s
47350K .......... .......... .......... .......... .......... 9% 4.69M 70s
47400K .......... .......... .......... .......... .......... 9% 16.1M 70s
47450K .......... .......... .......... .......... .......... 9% 7.77M 70s
47500K .......... .......... .......... .......... .......... 9% 11.5M 70s
47550K .......... .......... .......... .......... .......... 9% 11.8M 70s
47600K .......... .......... .......... .......... .......... 9% 9.26M 70s
47650K .......... .......... .......... .......... .......... 9% 8.70M 70s
47700K .......... .......... .......... .......... .......... 9% 6.04M 70s
47750K .......... .......... .......... .......... .......... 9% 6.42M 70s
47800K .......... .......... .......... .......... .......... 9% 7.70M 70s
47850K .......... .......... .......... .......... .......... 9% 7.31M 70s
47900K .......... .......... .......... .......... .......... 9% 9.28M 70s
47950K .......... .......... .......... .......... .......... 9% 6.30M 70s
48000K .......... .......... .......... .......... .......... 9% 5.38M 70s
48050K .......... .......... .......... .......... .......... 9% 4.77M 70s
48100K .......... .......... .......... .......... .......... 9% 4.70M 70s
48150K .......... .......... .......... .......... .......... 9% 5.33M 70s
48200K .......... .......... .......... .......... .......... 9% 6.30M 70s
48250K .......... .......... .......... .......... .......... 9% 3.75M 70s
48300K .......... .......... .......... .......... .......... 9% 5.28M 70s
48350K .......... .......... .......... .......... .......... 9% 3.39M 70s
48400K .......... .......... .......... .......... .......... 9% 3.43M 70s
48450K .......... .......... .......... .......... .......... 9% 3.33M 70s
48500K .......... .......... .......... .......... .......... 9% 7.43M 70s
48550K .......... .......... .......... .......... .......... 9% 6.07M 70s
48600K .......... .......... .......... .......... .......... 9% 6.19M 70s
48650K .......... .......... .......... .......... .......... 9% 6.10M 70s
48700K .......... .......... .......... .......... .......... 9% 3.45M 70s
48750K .......... .......... .......... .......... .......... 9% 12.2M 70s
48800K .......... .......... .......... .......... .......... 9% 11.1M 70s
48850K .......... .......... .......... .......... .......... 9% 6.18M 70s
48900K .......... .......... .......... .......... .......... 9% 7.56M 70s
48950K .......... .......... .......... .......... .......... 9% 7.43M 70s
49000K .......... .......... .......... .......... .......... 9% 11.0M 70s
49050K .......... .......... .......... .......... .......... 9% 9.10M 70s
49100K .......... .......... .......... .......... .......... 9% 8.61M 70s
49150K .......... .......... .......... .......... .......... 9% 9.30M 70s
49200K .......... .......... .......... .......... .......... 9% 11.9M 70s
49250K .......... .......... .......... .......... .......... 9% 27.4M 70s
49300K .......... .......... .......... .......... .......... 9% 9.21M 70s
49350K .......... .......... .......... .......... .......... 9% 18.4M 70s
49400K .......... .......... .......... .......... .......... 9% 17.5M 70s
49450K .......... .......... .......... .......... .......... 9% 17.0M 70s
49500K .......... .......... .......... .......... .......... 9% 12.2M 70s
49550K .......... .......... .......... .......... .......... 9% 13.2M 70s
49600K .......... .......... .......... .......... .......... 9% 11.6M 70s
49650K .......... .......... .......... .......... .......... 9% 29.0M 69s
49700K .......... .......... .......... .......... .......... 9% 10.8M 69s
49750K .......... .......... .......... .......... .......... 9% 18.5M 69s
49800K .......... .......... .......... .......... .......... 9% 9.74M 69s
49850K .......... .......... .......... .......... .......... 9% 112M 69s
49900K .......... .......... .......... .......... .......... 9% 7.69M 69s
49950K .......... .......... .......... .......... .......... 9% 15.6M 69s
50000K .......... .......... .......... .......... .......... 9% 12.1M 69s
50050K .......... .......... .......... .......... .......... 9% 11.3M 69s
50100K .......... .......... .......... .......... .......... 9% 10.4M 69s
50150K .......... .......... .......... .......... .......... 9% 9.41M 69s
50200K .......... .......... .......... .......... .......... 9% 8.61M 69s
50250K .......... .......... .......... .......... .......... 9% 12.2M 69s
50300K .......... .......... .......... .......... .......... 9% 9.32M 69s
50350K .......... .......... .......... .......... .......... 9% 23.7M 69s
50400K .......... .......... .......... .......... .......... 9% 13.1M 69s
50450K .......... .......... .......... .......... .......... 10% 12.4M 69s
50500K .......... .......... .......... .......... .......... 10% 9.30M 69s
50550K .......... .......... .......... .......... .......... 10% 9.46M 69s
50600K .......... .......... .......... .......... .......... 10% 7.29M 69s
50650K .......... .......... .......... .......... .......... 10% 5.22M 69s
50700K .......... .......... .......... .......... .......... 10% 6.21M 69s
50750K .......... .......... .......... .......... .......... 10% 8.79M 69s
50800K .......... .......... .......... .......... .......... 10% 7.55M 69s
50850K .......... .......... .......... .......... .......... 10% 4.19M 69s
50900K .......... .......... .......... .......... .......... 10% 4.31M 69s
50950K .......... .......... .......... .......... .......... 10% 6.16M 69s
51000K .......... .......... .......... .......... .......... 10% 6.21M 69s
51050K .......... .......... .......... .......... .......... 10% 8.49M 69s
51100K .......... .......... .......... .......... .......... 10% 12.0M 69s
51150K .......... .......... .......... .......... .......... 10% 9.07M 69s
51200K .......... .......... .......... .......... .......... 10% 9.41M 69s
51250K .......... .......... .......... .......... .......... 10% 7.36M 69s
51300K .......... .......... .......... .......... .......... 10% 8.85M 69s
51350K .......... .......... .......... .......... .......... 10% 4.74M 69s
51400K .......... .......... .......... .......... .......... 10% 7.27M 69s
51450K .......... .......... .......... .......... .......... 10% 4.68M 69s
51500K .......... .......... .......... .......... .......... 10% 7.52M 69s
51550K .......... .......... .......... .......... .......... 10% 5.29M 69s
51600K .......... .......... .......... .......... .......... 10% 6.15M 69s
51650K .......... .......... .......... .......... .......... 10% 5.13M 69s
51700K .......... .......... .......... .......... .......... 10% 15.1M 69s
51750K .......... .......... .......... .......... .......... 10% 17.3M 69s
51800K .......... .......... .......... .......... .......... 10% 12.7M 68s
51850K .......... .......... .......... .......... .......... 10% 9.31M 68s
51900K .......... .......... .......... .......... .......... 10% 6.25M 68s
51950K .......... .......... .......... .......... .......... 10% 6.25M 68s
52000K .......... .......... .......... .......... .......... 10% 9.75M 68s
52050K .......... .......... .......... .......... .......... 10% 8.86M 68s
52100K .......... .......... .......... .......... .......... 10% 9.09M 68s
52150K .......... .......... .......... .......... .......... 10% 5.36M 68s
52200K .......... .......... .......... .......... .......... 10% 4.67M 68s
52250K .......... .......... .......... .......... .......... 10% 7.48M 68s
52300K .......... .......... .......... .......... .......... 10% 5.30M 68s
52350K .......... .......... .......... .......... .......... 10% 2.86M 68s
52400K .......... .......... .......... .......... .......... 10% 5.23M 68s
52450K .......... .......... .......... .......... .......... 10% 4.15M 69s
52500K .......... .......... .......... .......... .......... 10% 3.10M 69s
52550K .......... .......... .......... .......... .......... 10% 4.70M 69s
52600K .......... .......... .......... .......... .......... 10% 3.72M 69s
52650K .......... .......... .......... .......... .......... 10% 3.10M 69s
52700K .......... .......... .......... .......... .......... 10% 4.55M 69s
52750K .......... .......... .......... .......... .......... 10% 8.71M 69s
52800K .......... .......... .......... .......... .......... 10% 9.04M 69s
52850K .......... .......... .......... .......... .......... 10% 5.20M 69s
52900K .......... .......... .......... .......... .......... 10% 7.41M 69s
52950K .......... .......... .......... .......... .......... 10% 6.11M 69s
53000K .......... .......... .......... .......... .......... 10% 6.27M 69s
53050K .......... .......... .......... .......... .......... 10% 6.19M 69s
53100K .......... .......... .......... .......... .......... 10% 4.78M 69s
53150K .......... .......... .......... .......... .......... 10% 3.09M 69s
53200K .......... .......... .......... .......... .......... 10% 3.09M 69s
53250K .......... .......... .......... .......... .......... 10% 7.29M 69s
53300K .......... .......... .......... .......... .......... 10% 7.49M 69s
53350K .......... .......... .......... .......... .......... 10% 5.24M 69s
53400K .......... .......... .......... .......... .......... 10% 5.34M 69s
53450K .......... .......... .......... .......... .......... 10% 3.76M 69s
53500K .......... .......... .......... .......... .......... 10% 5.41M 69s
53550K .......... .......... .......... .......... .......... 10% 3.49M 69s
53600K .......... .......... .......... .......... .......... 10% 3.82M 69s
53650K .......... .......... .......... .......... .......... 10% 3.11M 69s
53700K .......... .......... .......... .......... .......... 10% 11.5M 69s
53750K .......... .......... .......... .......... .......... 10% 11.8M 69s
53800K .......... .......... .......... .......... .......... 10% 8.79M 69s
53850K .......... .......... .......... .......... .......... 10% 12.0M 69s
53900K .......... .......... .......... .......... .......... 10% 11.9M 69s
53950K .......... .......... .......... .......... .......... 10% 7.18M 69s
54000K .......... .......... .......... .......... .......... 10% 11.6M 69s
54050K .......... .......... .......... .......... .......... 10% 11.8M 69s
54100K .......... .......... .......... .......... .......... 10% 9.03M 69s
54150K .......... .......... .......... .......... .......... 10% 7.24M 69s
54200K .......... .......... .......... .......... .......... 10% 6.57M 69s
54250K .......... .......... .......... .......... .......... 10% 7.25M 69s
54300K .......... .......... .......... .......... .......... 10% 4.62M 69s
54350K .......... .......... .......... .......... .......... 10% 2.95M 69s
54400K .......... .......... .......... .......... .......... 10% 7.39M 69s
54450K .......... .......... .......... .......... .......... 10% 6.21M 69s
54500K .......... .......... .......... .......... .......... 10% 7.42M 69s
54550K .......... .......... .......... .......... .......... 10% 6.04M 69s
54600K .......... .......... .......... .......... .......... 10% 4.16M 69s
54650K .......... .......... .......... .......... .......... 10% 7.49M 69s
54700K .......... .......... .......... .......... .......... 10% 9.13M 69s
54750K .......... .......... .......... .......... .......... 10% 7.45M 69s
54800K .......... .......... .......... .......... .......... 10% 5.41M 69s
54850K .......... .......... .......... .......... .......... 10% 7.29M 69s
54900K .......... .......... .......... .......... .......... 10% 4.68M 69s
54950K .......... .......... .......... .......... .......... 10% 4.14M 69s
55000K .......... .......... .......... .......... .......... 10% 5.33M 69s
55050K .......... .......... .......... .......... .......... 10% 4.15M 69s
55100K .......... .......... .......... .......... .......... 10% 3.19M 69s
55150K .......... .......... .......... .......... .......... 10% 4.10M 69s
55200K .......... .......... .......... .......... .......... 10% 3.72M 69s
55250K .......... .......... .......... .......... .......... 10% 8.49M 69s
55300K .......... .......... .......... .......... .......... 10% 16.5M 69s
55350K .......... .......... .......... .......... .......... 10% 11.8M 69s
55400K .......... .......... .......... .......... .......... 10% 9.79M 69s
55450K .......... .......... .......... .......... .......... 10% 18.9M 69s
55500K .......... .......... .......... .......... .......... 11% 9.86M 69s
55550K .......... .......... .......... .......... .......... 11% 9.18M 69s
55600K .......... .......... .......... .......... .......... 11% 12.1M 69s
55650K .......... .......... .......... .......... .......... 11% 15.9M 68s
55700K .......... .......... .......... .......... .......... 11% 11.5M 68s
55750K .......... .......... .......... .......... .......... 11% 11.8M 68s
55800K .......... .......... .......... .......... .......... 11% 8.96M 68s
55850K .......... .......... .......... .......... .......... 11% 7.38M 68s
55900K .......... .......... .......... .......... .......... 11% 6.28M 68s
55950K .......... .......... .......... .......... .......... 11% 6.11M 68s
56000K .......... .......... .......... .......... .......... 11% 6.10M 68s
56050K .......... .......... .......... .......... .......... 11% 6.11M 68s
56100K .......... .......... .......... .......... .......... 11% 8.41M 68s
56150K .......... .......... .......... .......... .......... 11% 16.7M 68s
56200K .......... .......... .......... .......... .......... 11% 16.1M 68s
56250K .......... .......... .......... .......... .......... 11% 16.2M 68s
56300K .......... .......... .......... .......... .......... 11% 13.4M 68s
56350K .......... .......... .......... .......... .......... 11% 8.53M 68s
56400K .......... .......... .......... .......... .......... 11% 5.30M 68s
56450K .......... .......... .......... .......... .......... 11% 7.22M 68s
56500K .......... .......... .......... .......... .......... 11% 5.50M 68s
56550K .......... .......... .......... .......... .......... 11% 7.38M 68s
56600K .......... .......... .......... .......... .......... 11% 5.27M 68s
56650K .......... .......... .......... .......... .......... 11% 12.4M 68s
56700K .......... .......... .......... .......... .......... 11% 9.07M 68s
56750K .......... .......... .......... .......... .......... 11% 11.6M 68s
56800K .......... .......... .......... .......... .......... 11% 11.8M 68s
56850K .......... .......... .......... .......... .......... 11% 7.41M 68s
56900K .......... .......... .......... .......... .......... 11% 12.0M 68s
56950K .......... .......... .......... .......... .......... 11% 5.54M 68s
57000K .......... .......... .......... .......... .......... 11% 8.79M 68s
57050K .......... .......... .......... .......... .......... 11% 5.25M 68s
57100K .......... .......... .......... .......... .......... 11% 5.29M 68s
57150K .......... .......... .......... .......... .......... 11% 5.24M 68s
57200K .......... .......... .......... .......... .......... 11% 3.31M 68s
57250K .......... .......... .......... .......... .......... 11% 6.37M 68s
57300K .......... .......... .......... .......... .......... 11% 9.36M 68s
57350K .......... .......... .......... .......... .......... 11% 7.40M 68s
57400K .......... .......... .......... .......... .......... 11% 4.48M 68s
57450K .......... .......... .......... .......... .......... 11% 3.72M 68s
57500K .......... .......... .......... .......... .......... 11% 5.35M 68s
57550K .......... .......... .......... .......... .......... 11% 5.27M 68s
57600K .......... .......... .......... .......... .......... 11% 4.20M 68s
57650K .......... .......... .......... .......... .......... 11% 3.78M 68s
57700K .......... .......... .......... .......... .......... 11% 3.70M 68s
57750K .......... .......... .......... .......... .......... 11% 4.67M 68s
57800K .......... .......... .......... .......... .......... 11% 4.63M 68s
57850K .......... .......... .......... .......... .......... 11% 5.89M 68s
57900K .......... .......... .......... .......... .......... 11% 9.10M 68s
57950K .......... .......... .......... .......... .......... 11% 9.23M 68s
58000K .......... .......... .......... .......... .......... 11% 7.44M 68s
58050K .......... .......... .......... .......... .......... 11% 4.59M 68s
58100K .......... .......... .......... .......... .......... 11% 4.65M 68s
58150K .......... .......... .......... .......... .......... 11% 7.47M 68s
58200K .......... .......... .......... .......... .......... 11% 6.17M 68s
58250K .......... .......... .......... .......... .......... 11% 9.24M 68s
58300K .......... .......... .......... .......... .......... 11% 6.35M 68s
58350K .......... .......... .......... .......... .......... 11% 5.34M 68s
58400K .......... .......... .......... .......... .......... 11% 11.1M 68s
58450K .......... .......... .......... .......... .......... 11% 4.77M 68s
58500K .......... .......... .......... .......... .......... 11% 5.31M 68s
58550K .......... .......... .......... .......... .......... 11% 7.31M 68s
58600K .......... .......... .......... .......... .......... 11% 4.13M 68s
58650K .......... .......... .......... .......... .......... 11% 6.25M 68s
58700K .......... .......... .......... .......... .......... 11% 4.14M 68s
58750K .......... .......... .......... .......... .......... 11% 5.34M 68s
58800K .......... .......... .......... .......... .......... 11% 9.22M 68s
58850K .......... .......... .......... .......... .......... 11% 8.96M 68s
58900K .......... .......... .......... .......... .......... 11% 9.16M 68s
58950K .......... .......... .......... .......... .......... 11% 7.47M 68s
59000K .......... .......... .......... .......... .......... 11% 6.25M 68s
59050K .......... .......... .......... .......... .......... 11% 7.52M 68s
59100K .......... .......... .......... .......... .......... 11% 5.31M 68s
59150K .......... .......... .......... .......... .......... 11% 4.61M 68s
59200K .......... .......... .......... .......... .......... 11% 3.49M 68s
59250K .......... .......... .......... .......... .......... 11% 4.78M 68s
59300K .......... .......... .......... .......... .......... 11% 4.57M 68s
59350K .......... .......... .......... .......... .......... 11% 4.15M 68s
59400K .......... .......... .......... .......... .......... 11% 3.36M 68s
59450K .......... .......... .......... .......... .......... 11% 3.05M 68s
59500K .......... .......... .......... .......... .......... 11% 4.16M 68s
59550K .......... .......... .......... .......... .......... 11% 5.54M 68s
59600K .......... .......... .......... .......... .......... 11% 8.89M 68s
59650K .......... .......... .......... .......... .......... 11% 9.11M 68s
59700K .......... .......... .......... .......... .......... 11% 9.14M 68s
59750K .......... .......... .......... .......... .......... 11% 12.5M 68s
59800K .......... .......... .......... .......... .......... 11% 16.8M 68s
59850K .......... .......... .......... .......... .......... 11% 9.43M 68s
59900K .......... .......... .......... .......... .......... 11% 9.06M 68s
59950K .......... .......... .......... .......... .......... 11% 7.66M 68s
60000K .......... .......... .......... .......... .......... 11% 11.5M 68s
60050K .......... .......... .......... .......... .......... 11% 7.49M 68s
60100K .......... .......... .......... .......... .......... 11% 8.99M 68s
60150K .......... .......... .......... .......... .......... 11% 6.17M 68s
60200K .......... .......... .......... .......... .......... 11% 4.64M 68s
60250K .......... .......... .......... .......... .......... 11% 6.18M 68s
60300K .......... .......... .......... .......... .......... 11% 6.14M 68s
60350K .......... .......... .......... .......... .......... 11% 4.66M 68s
60400K .......... .......... .......... .......... .......... 11% 4.66M 68s
60450K .......... .......... .......... .......... .......... 11% 4.15M 68s
60500K .......... .......... .......... .......... .......... 11% 2.91M 68s
60550K .......... .......... .......... .......... .......... 12% 4.68M 68s
60600K .......... .......... .......... .......... .......... 12% 2.87M 68s
60650K .......... .......... .......... .......... .......... 12% 3.10M 68s
60700K .......... .......... .......... .......... .......... 12% 2.84M 68s
60750K .......... .......... .......... .......... .......... 12% 3.74M 68s
60800K .......... .......... .......... .......... .......... 12% 16.3M 68s
60850K .......... .......... .......... .......... .......... 12% 11.2M 68s
60900K .......... .......... .......... .......... .......... 12% 18.4M 68s
60950K .......... .......... .......... .......... .......... 12% 8.67M 68s
61000K .......... .......... .......... .......... .......... 12% 9.79M 68s
61050K .......... .......... .......... .......... .......... 12% 12.1M 68s
61100K .......... .......... .......... .......... .......... 12% 6.18M 68s
61150K .......... .......... .......... .......... .......... 12% 6.05M 68s
61200K .......... .......... .......... .......... .......... 12% 5.77M 68s
61250K .......... .......... .......... .......... .......... 12% 7.28M 68s
61300K .......... .......... .......... .......... .......... 12% 4.76M 68s
61350K .......... .......... .......... .......... .......... 12% 3.45M 68s
61400K .......... .......... .......... .......... .......... 12% 3.75M 68s
61450K .......... .......... .......... .......... .......... 12% 4.78M 68s
61500K .......... .......... .......... .......... .......... 12% 9.18M 68s
61550K .......... .......... .......... .......... .......... 12% 16.4M 68s
61600K .......... .......... .......... .......... .......... 12% 11.3M 68s
61650K .......... .......... .......... .......... .......... 12% 12.2M 68s
61700K .......... .......... .......... .......... .......... 12% 6.07M 68s
61750K .......... .......... .......... .......... .......... 12% 12.4M 68s
61800K .......... .......... .......... .......... .......... 12% 5.21M 68s
61850K .......... .......... .......... .......... .......... 12% 8.94M 68s
61900K .......... .......... .......... .......... .......... 12% 7.44M 68s
61950K .......... .......... .......... .......... .......... 12% 5.97M 68s
62000K .......... .......... .......... .......... .......... 12% 7.23M 68s
62050K .......... .......... .......... .......... .......... 12% 7.45M 68s
62100K .......... .......... .......... .......... .......... 12% 7.00M 68s
62150K .......... .......... .......... .......... .......... 12% 7.20M 68s
62200K .......... .......... .......... .......... .......... 12% 6.21M 68s
62250K .......... .......... .......... .......... .......... 12% 23.6M 68s
62300K .......... .......... .......... .......... .......... 12% 6.29M 68s
62350K .......... .......... .......... .......... .......... 12% 140M 68s
62400K .......... .......... .......... .......... .......... 12% 9.55M 68s
62450K .......... .......... .......... .......... .......... 12% 10.5M 68s
62500K .......... .......... .......... .......... .......... 12% 16.9M 68s
62550K .......... .......... .......... .......... .......... 12% 17.2M 68s
62600K .......... .......... .......... .......... .......... 12% 8.69M 68s
62650K .......... .......... .......... .......... .......... 12% 16.8M 67s
62700K .......... .......... .......... .......... .......... 12% 6.00M 67s
62750K .......... .......... .......... .......... .......... 12% 5.50M 67s
62800K .......... .......... .......... .......... .......... 12% 6.23M 67s
62850K .......... .......... .......... .......... .......... 12% 5.28M 67s
62900K .......... .......... .......... .......... .......... 12% 9.13M 67s
62950K .......... .......... .......... .......... .......... 12% 5.31M 67s
63000K .......... .......... .......... .......... .......... 12% 2.89M 68s
63050K .......... .......... .......... .......... .......... 12% 4.10M 68s
63100K .......... .......... .......... .......... .......... 12% 3.69M 68s
63150K .......... .......... .......... .......... .......... 12% 4.57M 68s
63200K .......... .......... .......... .......... .......... 12% 16.6M 68s
63250K .......... .......... .......... .......... .......... 12% 11.7M 67s
63300K .......... .......... .......... .......... .......... 12% 17.8M 67s
63350K .......... .......... .......... .......... .......... 12% 9.43M 67s
63400K .......... .......... .......... .......... .......... 12% 15.1M 67s
63450K .......... .......... .......... .......... .......... 12% 12.2M 67s
63500K .......... .......... .......... .......... .......... 12% 8.92M 67s
63550K .......... .......... .......... .......... .......... 12% 9.75M 67s
63600K .......... .......... .......... .......... .......... 12% 11.1M 67s
63650K .......... .......... .......... .......... .......... 12% 7.13M 67s
63700K .......... .......... .......... .......... .......... 12% 5.33M 67s
63750K .......... .......... .......... .......... .......... 12% 6.10M 67s
63800K .......... .......... .......... .......... .......... 12% 6.05M 67s
63850K .......... .......... .......... .......... .......... 12% 9.28M 67s
63900K .......... .......... .......... .......... .......... 12% 7.21M 67s
63950K .......... .......... .......... .......... .......... 12% 35.1M 67s
64000K .......... .......... .......... .......... .......... 12% 9.03M 67s
64050K .......... .......... .......... .......... .......... 12% 7.38M 67s
64100K .......... .......... .......... .......... .......... 12% 9.30M 67s
64150K .......... .......... .......... .......... .......... 12% 9.03M 67s
64200K .......... .......... .......... .......... .......... 12% 6.08M 67s
64250K .......... .......... .......... .......... .......... 12% 5.26M 67s
64300K .......... .......... .......... .......... .......... 12% 11.9M 67s
64350K .......... .......... .......... .......... .......... 12% 7.44M 67s
64400K .......... .......... .......... .......... .......... 12% 9.02M 67s
64450K .......... .......... .......... .......... .......... 12% 7.16M 67s
64500K .......... .......... .......... .......... .......... 12% 4.17M 67s
64550K .......... .......... .......... .......... .......... 12% 4.04M 67s
64600K .......... .......... .......... .......... .......... 12% 5.23M 67s
64650K .......... .......... .......... .......... .......... 12% 7.49M 67s
64700K .......... .......... .......... .......... .......... 12% 9.05M 67s
64750K .......... .......... .......... .......... .......... 12% 9.78M 67s
64800K .......... .......... .......... .......... .......... 12% 18.8M 67s
64850K .......... .......... .......... .......... .......... 12% 9.21M 67s
64900K .......... .......... .......... .......... .......... 12% 9.12M 67s
64950K .......... .......... .......... .......... .......... 12% 8.95M 67s
65000K .......... .......... .......... .......... .......... 12% 12.4M 67s
65050K .......... .......... .......... .......... .......... 12% 11.7M 67s
65100K .......... .......... .......... .......... .......... 12% 6.20M 67s
65150K .......... .......... .......... .......... .......... 12% 9.05M 67s
65200K .......... .......... .......... .......... .......... 12% 7.39M 67s
65250K .......... .......... .......... .......... .......... 12% 8.62M 67s
65300K .......... .......... .......... .......... .......... 12% 7.74M 67s
65350K .......... .......... .......... .......... .......... 12% 4.52M 67s
65400K .......... .......... .......... .......... .......... 12% 4.42M 67s
65450K .......... .......... .......... .......... .......... 12% 5.20M 67s
65500K .......... .......... .......... .......... .......... 12% 8.96M 67s
65550K .......... .......... .......... .......... .......... 12% 15.6M 67s
65600K .......... .......... .......... .......... .......... 13% 9.37M 67s
65650K .......... .......... .......... .......... .......... 13% 17.9M 67s
65700K .......... .......... .......... .......... .......... 13% 9.32M 67s
65750K .......... .......... .......... .......... .......... 13% 17.6M 67s
65800K .......... .......... .......... .......... .......... 13% 12.6M 67s
65850K .......... .......... .......... .......... .......... 13% 6.36M 67s
65900K .......... .......... .......... .......... .......... 13% 9.43M 67s
65950K .......... .......... .......... .......... .......... 13% 6.17M 67s
66000K .......... .......... .......... .......... .......... 13% 9.30M 66s
66050K .......... .......... .......... .......... .......... 13% 9.08M 66s
66100K .......... .......... .......... .......... .......... 13% 7.39M 66s
66150K .......... .......... .......... .......... .......... 13% 12.2M 66s
66200K .......... .......... .......... .......... .......... 13% 8.87M 66s
66250K .......... .......... .......... .......... .......... 13% 9.17M 66s
66300K .......... .......... .......... .......... .......... 13% 9.39M 66s
66350K .......... .......... .......... .......... .......... 13% 8.82M 66s
66400K .......... .......... .......... .......... .......... 13% 4.16M 66s
66450K .......... .......... .......... .......... .......... 13% 5.21M 66s
66500K .......... .......... .......... .......... .......... 13% 7.52M 66s
66550K .......... .......... .......... .......... .......... 13% 7.44M 66s
66600K .......... .......... .......... .......... .......... 13% 3.16M 66s
66650K .......... .......... .......... .......... .......... 13% 3.42M 66s
66700K .......... .......... .......... .......... .......... 13% 3.09M 66s
66750K .......... .......... .......... .......... .......... 13% 2.45M 67s
66800K .......... .......... .......... .......... .......... 13% 2.18M 67s
66850K .......... .......... .......... .......... .......... 13% 5.93M 67s
66900K .......... .......... .......... .......... .......... 13% 18.0M 67s
66950K .......... .......... .......... .......... .......... 13% 17.2M 67s
67000K .......... .......... .......... .......... .......... 13% 12.2M 67s
67050K .......... .......... .......... .......... .......... 13% 8.93M 66s
67100K .......... .......... .......... .......... .......... 13% 9.11M 66s
67150K .......... .......... .......... .......... .......... 13% 9.30M 66s
67200K .......... .......... .......... .......... .......... 13% 9.27M 66s
67250K .......... .......... .......... .......... .......... 13% 7.11M 66s
67300K .......... .......... .......... .......... .......... 13% 5.34M 66s
67350K .......... .......... .......... .......... .......... 13% 5.09M 66s
67400K .......... .......... .......... .......... .......... 13% 9.04M 66s
67450K .......... .......... .......... .......... .......... 13% 7.43M 66s
67500K .......... .......... .......... .......... .......... 13% 5.08M 66s
67550K .......... .......... .......... .......... .......... 13% 5.36M 66s
67600K .......... .......... .......... .......... .......... 13% 3.74M 66s
67650K .......... .......... .......... .......... .......... 13% 2.64M 66s
67700K .......... .......... .......... .......... .......... 13% 1.43M 67s
67750K .......... .......... .......... .......... .......... 13% 2.06M 67s
67800K .......... .......... .......... .......... .......... 13% 5.20M 67s
67850K .......... .......... .......... .......... .......... 13% 11.1M 67s
67900K .......... .......... .......... .......... .......... 13% 11.4M 67s
67950K .......... .......... .......... .......... .......... 13% 12.1M 67s
68000K .......... .......... .......... .......... .......... 13% 9.36M 67s
68050K .......... .......... .......... .......... .......... 13% 7.63M 67s
68100K .......... .......... .......... .......... .......... 13% 5.38M 67s
68150K .......... .......... .......... .......... .......... 13% 7.62M 67s
68200K .......... .......... .......... .......... .......... 13% 5.22M 67s
68250K .......... .......... .......... .......... .......... 13% 5.32M 67s
68300K .......... .......... .......... .......... .......... 13% 17.5M 67s
68350K .......... .......... .......... .......... .......... 13% 11.1M 67s
68400K .......... .......... .......... .......... .......... 13% 11.9M 67s
68450K .......... .......... .......... .......... .......... 13% 8.39M 66s
68500K .......... .......... .......... .......... .......... 13% 7.37M 66s
68550K .......... .......... .......... .......... .......... 13% 6.22M 66s
68600K .......... .......... .......... .......... .......... 13% 4.67M 66s
68650K .......... .......... .......... .......... .......... 13% 5.35M 66s
68700K .......... .......... .......... .......... .......... 13% 5.46M 66s
68750K .......... .......... .......... .......... .......... 13% 7.35M 66s
68800K .......... .......... .......... .......... .......... 13% 11.6M 66s
68850K .......... .......... .......... .......... .......... 13% 9.63M 66s
68900K .......... .......... .......... .......... .......... 13% 9.06M 66s
68950K .......... .......... .......... .......... .......... 13% 11.7M 66s
69000K .......... .......... .......... .......... .......... 13% 7.55M 66s
69050K .......... .......... .......... .......... .......... 13% 6.47M 66s
69100K .......... .......... .......... .......... .......... 13% 5.10M 66s
69150K .......... .......... .......... .......... .......... 13% 7.27M 66s
69200K .......... .......... .......... .......... .......... 13% 2.83M 66s
69250K .......... .......... .......... .......... .......... 13% 4.65M 66s
69300K .......... .......... .......... .......... .......... 13% 4.14M 66s
69350K .......... .......... .......... .......... .......... 13% 3.39M 66s
69400K .......... .......... .......... .......... .......... 13% 5.38M 66s
69450K .......... .......... .......... .......... .......... 13% 4.05M 66s
69500K .......... .......... .......... .......... .......... 13% 2.91M 67s
69550K .......... .......... .......... .......... .......... 13% 3.70M 67s
69600K .......... .......... .......... .......... .......... 13% 2.88M 67s
69650K .......... .......... .......... .......... .......... 13% 5.21M 67s
69700K .......... .......... .......... .......... .......... 13% 3.58M 67s
69750K .......... .......... .......... .......... .......... 13% 7.40M 67s
69800K .......... .......... .......... .......... .......... 13% 6.18M 67s
69850K .......... .......... .......... .......... .......... 13% 12.1M 67s
69900K .......... .......... .......... .......... .......... 13% 11.9M 67s
69950K .......... .......... .......... .......... .......... 13% 7.19M 67s
70000K .......... .......... .......... .......... .......... 13% 7.52M 67s
70050K .......... .......... .......... .......... .......... 13% 6.17M 67s
70100K .......... .......... .......... .......... .......... 13% 3.80M 67s
70150K .......... .......... .......... .......... .......... 13% 4.63M 67s
70200K .......... .......... .......... .......... .......... 13% 2.75M 67s
70250K .......... .......... .......... .......... .......... 13% 4.58M 67s
70300K .......... .......... .......... .......... .......... 13% 6.09M 67s
70350K .......... .......... .......... .......... .......... 13% 4.64M 67s
70400K .......... .......... .......... .......... .......... 13% 7.39M 67s
70450K .......... .......... .......... .......... .......... 13% 6.18M 67s
70500K .......... .......... .......... .......... .......... 13% 4.62M 67s
70550K .......... .......... .......... .......... .......... 13% 3.71M 67s
70600K .......... .......... .......... .......... .......... 13% 3.11M 67s
70650K .......... .......... .......... .......... .......... 14% 3.11M 67s
70700K .......... .......... .......... .......... .......... 14% 4.69M 67s
70750K .......... .......... .......... .......... .......... 14% 6.23M 67s
70800K .......... .......... .......... .......... .......... 14% 4.66M 67s
70850K .......... .......... .......... .......... .......... 14% 2.91M 67s
70900K .......... .......... .......... .......... .......... 14% 3.69M 67s
70950K .......... .......... .......... .......... .......... 14% 5.22M 67s
71000K .......... .......... .......... .......... .......... 14% 9.21M 67s
71050K .......... .......... .......... .......... .......... 14% 7.55M 67s
71100K .......... .......... .......... .......... .......... 14% 6.09M 67s
71150K .......... .......... .......... .......... .......... 14% 5.55M 67s
71200K .......... .......... .......... .......... .......... 14% 7.36M 67s
71250K .......... .......... .......... .......... .......... 14% 4.75M 67s
71300K .......... .......... .......... .......... .......... 14% 5.31M 67s
71350K .......... .......... .......... .......... .......... 14% 6.10M 67s
71400K .......... .......... .......... .......... .......... 14% 4.20M 67s
71450K .......... .......... .......... .......... .......... 14% 3.17M 67s
71500K .......... .......... .......... .......... .......... 14% 6.20M 67s
71550K .......... .......... .......... .......... .......... 14% 4.62M 67s
71600K .......... .......... .......... .......... .......... 14% 4.61M 67s
71650K .......... .......... .......... .......... .......... 14% 7.51M 67s
71700K .......... .......... .......... .......... .......... 14% 4.64M 67s
71750K .......... .......... .......... .......... .......... 14% 3.75M 67s
71800K .......... .......... .......... .......... .......... 14% 3.81M 67s
71850K .......... .......... .......... .......... .......... 14% 3.46M 67s
71900K .......... .......... .......... .......... .......... 14% 8.85M 67s
71950K .......... .......... .......... .......... .......... 14% 11.5M 67s
72000K .......... .......... .......... .......... .......... 14% 9.53M 67s
72050K .......... .......... .......... .......... .......... 14% 17.6M 67s
72100K .......... .......... .......... .......... .......... 14% 8.72M 67s
72150K .......... .......... .......... .......... .......... 14% 9.26M 67s
72200K .......... .......... .......... .......... .......... 14% 9.06M 67s
72250K .......... .......... .......... .......... .......... 14% 8.84M 67s
72300K .......... .......... .......... .......... .......... 14% 12.0M 67s
72350K .......... .......... .......... .......... .......... 14% 11.9M 67s
72400K .......... .......... .......... .......... .......... 14% 9.85M 67s
72450K .......... .......... .......... .......... .......... 14% 9.18M 67s
72500K .......... .......... .......... .......... .......... 14% 8.59M 67s
72550K .......... .......... .......... .......... .......... 14% 9.27M 67s
72600K .......... .......... .......... .......... .......... 14% 6.30M 67s
72650K .......... .......... .......... .......... .......... 14% 4.07M 67s
72700K .......... .......... .......... .......... .......... 14% 5.30M 67s
72750K .......... .......... .......... .......... .......... 14% 4.17M 67s
72800K .......... .......... .......... .......... .......... 14% 4.17M 67s
72850K .......... .......... .......... .......... .......... 14% 4.65M 67s
72900K .......... .......... .......... .......... .......... 14% 3.20M 67s
72950K .......... .......... .......... .......... .......... 14% 1.92M 67s
73000K .......... .......... .......... .......... .......... 14% 4.62M 67s
73050K .......... .......... .......... .......... .......... 14% 6.13M 67s
73100K .......... .......... .......... .......... .......... 14% 12.4M 67s
73150K .......... .......... .......... .......... .......... 14% 9.12M 67s
73200K .......... .......... .......... .......... .......... 14% 8.65M 67s
73250K .......... .......... .......... .......... .......... 14% 7.31M 67s
73300K .......... .......... .......... .......... .......... 14% 7.22M 67s
73350K .......... .......... .......... .......... .......... 14% 5.27M 67s
73400K .......... .......... .......... .......... .......... 14% 3.78M 67s
73450K .......... .......... .......... .......... .......... 14% 3.09M 67s
73500K .......... .......... .......... .......... .......... 14% 3.36M 67s
73550K .......... .......... .......... .......... .......... 14% 3.36M 67s
73600K .......... .......... .......... .......... .......... 14% 2.63M 67s
73650K .......... .......... .......... .......... .......... 14% 10.8M 67s
73700K .......... .......... .......... .......... .......... 14% 9.56M 67s
73750K .......... .......... .......... .......... .......... 14% 12.0M 67s
73800K .......... .......... .......... .......... .......... 14% 16.9M 67s
73850K .......... .......... .......... .......... .......... 14% 8.96M 67s
73900K .......... .......... .......... .......... .......... 14% 17.7M 67s
73950K .......... .......... .......... .......... .......... 14% 6.97M 67s
74000K .......... .......... .......... .......... .......... 14% 9.27M 67s
74050K .......... .......... .......... .......... .......... 14% 4.22M 67s
74100K .......... .......... .......... .......... .......... 14% 4.17M 67s
74150K .......... .......... .......... .......... .......... 14% 7.43M 67s
74200K .......... .......... .......... .......... .......... 14% 3.68M 67s
74250K .......... .......... .......... .......... .......... 14% 1.98M 67s
74300K .......... .......... .......... .......... .......... 14% 1.76M 67s
74350K .......... .......... .......... .......... .......... 14% 1.70M 67s
74400K .......... .......... .......... .......... .......... 14% 1.54M 67s
74450K .......... .......... .......... .......... .......... 14% 3.41M 67s
74500K .......... .......... .......... .......... .......... 14% 2.34M 67s
74550K .......... .......... .......... .......... .......... 14% 2.06M 67s
74600K .......... .......... .......... .......... .......... 14% 1.08M 67s
74650K .......... .......... .......... .......... .......... 14% 2.06M 68s
74700K .......... .......... .......... .......... .......... 14% 2.47M 68s
74750K .......... .......... .......... .......... .......... 14% 11.0M 68s
74800K .......... .......... .......... .......... .......... 14% 25.2M 68s
74850K .......... .......... .......... .......... .......... 14% 25.3M 68s
74900K .......... .......... .......... .......... .......... 14% 11.7M 67s
74950K .......... .......... .......... .......... .......... 14% 31.0M 67s
75000K .......... .......... .......... .......... .......... 14% 16.1M 67s
75050K .......... .......... .......... .......... .......... 14% 14.9M 67s
75100K .......... .......... .......... .......... .......... 14% 16.4M 67s
75150K .......... .......... .......... .......... .......... 14% 26.7M 67s
75200K .......... .......... .......... .......... .......... 14% 11.5M 67s
75250K .......... .......... .......... .......... .......... 14% 17.6M 67s
75300K .......... .......... .......... .......... .......... 14% 10.4M 67s
75350K .......... .......... .......... .......... .......... 14% 11.0M 67s
75400K .......... .......... .......... .......... .......... 14% 17.5M 67s
75450K .......... .......... .......... .......... .......... 14% 10.8M 67s
75500K .......... .......... .......... .......... .......... 14% 17.9M 67s
75550K .......... .......... .......... .......... .......... 14% 9.47M 67s
75600K .......... .......... .......... .......... .......... 14% 10.3M 67s
75650K .......... .......... .......... .......... .......... 14% 9.65M 67s
75700K .......... .......... .......... .......... .......... 15% 6.14M 67s
75750K .......... .......... .......... .......... .......... 15% 4.86M 67s
75800K .......... .......... .......... .......... .......... 15% 5.23M 67s
75850K .......... .......... .......... .......... .......... 15% 3.74M 67s
75900K .......... .......... .......... .......... .......... 15% 5.29M 67s
75950K .......... .......... .......... .......... .......... 15% 2.86M 67s
76000K .......... .......... .......... .......... .......... 15% 4.67M 67s
76050K .......... .......... .......... .......... .......... 15% 4.26M 67s
76100K .......... .......... .......... .......... .......... 15% 2.72M 67s
76150K .......... .......... .......... .......... .......... 15% 4.61M 67s
76200K .......... .......... .......... .......... .......... 15% 4.16M 67s
76250K .......... .......... .......... .......... .......... 15% 4.15M 67s
76300K .......... .......... .......... .......... .......... 15% 6.06M 67s
76350K .......... .......... .......... .......... .......... 15% 8.52M 67s
76400K .......... .......... .......... .......... .......... 15% 12.6M 67s
76450K .......... .......... .......... .......... .......... 15% 7.24M 67s
76500K .......... .......... .......... .......... .......... 15% 6.40M 67s
76550K .......... .......... .......... .......... .......... 15% 9.41M 67s
76600K .......... .......... .......... .......... .......... 15% 7.12M 67s
76650K .......... .......... .......... .......... .......... 15% 7.70M 67s
76700K .......... .......... .......... .......... .......... 15% 4.22M 67s
76750K .......... .......... .......... .......... .......... 15% 7.34M 67s
76800K .......... .......... .......... .......... .......... 15% 8.90M 67s
76850K .......... .......... .......... .......... .......... 15% 4.63M 67s
76900K .......... .......... .......... .......... .......... 15% 9.11M 67s
76950K .......... .......... .......... .......... .......... 15% 7.24M 67s
77000K .......... .......... .......... .......... .......... 15% 6.34M 67s
77050K .......... .......... .......... .......... .......... 15% 7.25M 67s
77100K .......... .......... .......... .......... .......... 15% 8.89M 67s
77150K .......... .......... .......... .......... .......... 15% 9.02M 67s
77200K .......... .......... .......... .......... .......... 15% 6.20M 67s
77250K .......... .......... .......... .......... .......... 15% 5.40M 67s
77300K .......... .......... .......... .......... .......... 15% 6.19M 67s
77350K .......... .......... .......... .......... .......... 15% 2.66M 67s
77400K .......... .......... .......... .......... .......... 15% 4.16M 67s
77450K .......... .......... .......... .......... .......... 15% 6.18M 67s
77500K .......... .......... .......... .......... .......... 15% 4.64M 67s
77550K .......... .......... .......... .......... .......... 15% 6.19M 67s
77600K .......... .......... .......... .......... .......... 15% 3.42M 67s
77650K .......... .......... .......... .......... .......... 15% 4.64M 67s
77700K .......... .......... .......... .......... .......... 15% 3.74M 67s
77750K .......... .......... .......... .......... .......... 15% 7.37M 67s
77800K .......... .......... .......... .......... .......... 15% 4.72M 67s
77850K .......... .......... .......... .......... .......... 15% 2.88M 67s
77900K .......... .......... .......... .......... .......... 15% 2.84M 67s
77950K .......... .......... .......... .......... .......... 15% 2.08M 67s
78000K .......... .......... .......... .......... .......... 15% 2.45M 67s
78050K .......... .......... .......... .......... .......... 15% 4.16M 67s
78100K .......... .......... .......... .......... .......... 15% 3.70M 67s
78150K .......... .......... .......... .......... .......... 15% 4.14M 67s
78200K .......... .......... .......... .......... .......... 15% 1.84M 67s
78250K .......... .......... .......... .......... .......... 15% 2.43M 67s
78300K .......... .......... .......... .......... .......... 15% 3.39M 67s
78350K .......... .......... .......... .......... .......... 15% 8.92M 67s
78400K .......... .......... .......... .......... .......... 15% 16.5M 67s
78450K .......... .......... .......... .......... .......... 15% 11.6M 67s
78500K .......... .......... .......... .......... .......... 15% 17.2M 67s
78550K .......... .......... .......... .......... .......... 15% 8.92M 67s
78600K .......... .......... .......... .......... .......... 15% 7.69M 67s
78650K .......... .......... .......... .......... .......... 15% 5.27M 67s
78700K .......... .......... .......... .......... .......... 15% 6.18M 67s
78750K .......... .......... .......... .......... .......... 15% 7.10M 67s
78800K .......... .......... .......... .......... .......... 15% 6.22M 67s
78850K .......... .......... .......... .......... .......... 15% 5.22M 67s
78900K .......... .......... .......... .......... .......... 15% 4.11M 67s
78950K .......... .......... .......... .......... .......... 15% 2.92M 67s
79000K .......... .......... .......... .......... .......... 15% 3.44M 67s
79050K .......... .......... .......... .......... .......... 15% 4.14M 67s
79100K .......... .......... .......... .......... .......... 15% 3.73M 67s
79150K .......... .......... .......... .......... .......... 15% 11.8M 67s
79200K .......... .......... .......... .......... .......... 15% 8.41M 67s
79250K .......... .......... .......... .......... .......... 15% 9.46M 67s
79300K .......... .......... .......... .......... .......... 15% 7.58M 67s
79350K .......... .......... .......... .......... .......... 15% 7.27M 67s
79400K .......... .......... .......... .......... .......... 15% 7.57M 67s
79450K .......... .......... .......... .......... .......... 15% 8.62M 67s
79500K .......... .......... .......... .......... .......... 15% 9.03M 67s
79550K .......... .......... .......... .......... .......... 15% 9.39M 67s
79600K .......... .......... .......... .......... .......... 15% 5.25M 67s
79650K .......... .......... .......... .......... .......... 15% 11.3M 67s
79700K .......... .......... .......... .......... .......... 15% 11.2M 67s
79750K .......... .......... .......... .......... .......... 15% 19.8M 67s
79800K .......... .......... .......... .......... .......... 15% 14.7M 67s
79850K .......... .......... .......... .......... .......... 15% 11.8M 67s
79900K .......... .......... .......... .......... .......... 15% 11.3M 67s
79950K .......... .......... .......... .......... .......... 15% 11.6M 67s
80000K .......... .......... .......... .......... .......... 15% 11.9M 67s
80050K .......... .......... .......... .......... .......... 15% 24.2M 67s
80100K .......... .......... .......... .......... .......... 15% 7.33M 67s
80150K .......... .......... .......... .......... .......... 15% 17.3M 67s
80200K .......... .......... .......... .......... .......... 15% 9.68M 67s
80250K .......... .......... .......... .......... .......... 15% 122M 67s
80300K .......... .......... .......... .......... .......... 15% 9.76M 67s
80350K .......... .......... .......... .......... .......... 15% 12.0M 67s
80400K .......... .......... .......... .......... .......... 15% 34.1M 67s
80450K .......... .......... .......... .......... .......... 15% 11.4M 67s
80500K .......... .......... .......... .......... .......... 15% 15.7M 67s
80550K .......... .......... .......... .......... .......... 15% 6.38M 67s
80600K .......... .......... .......... .......... .......... 15% 5.47M 67s
80650K .......... .......... .......... .......... .......... 15% 5.07M 67s
80700K .......... .......... .......... .......... .......... 15% 5.23M 67s
80750K .......... .......... .......... .......... .......... 16% 2.90M 67s
80800K .......... .......... .......... .......... .......... 16% 3.71M 67s
80850K .......... .......... .......... .......... .......... 16% 4.14M 67s
80900K .......... .......... .......... .......... .......... 16% 4.15M 67s
80950K .......... .......... .......... .......... .......... 16% 4.07M 67s
81000K .......... .......... .......... .......... .......... 16% 6.31M 67s
81050K .......... .......... .......... .......... .......... 16% 9.51M 67s
81100K .......... .......... .......... .......... .......... 16% 8.68M 67s
81150K .......... .......... .......... .......... .......... 16% 7.38M 67s
81200K .......... .......... .......... .......... .......... 16% 6.10M 67s
81250K .......... .......... .......... .......... .......... 16% 4.58M 67s
81300K .......... .......... .......... .......... .......... 16% 5.33M 67s
81350K .......... .......... .......... .......... .......... 16% 3.66M 67s
81400K .......... .......... .......... .......... .......... 16% 5.30M 67s
81450K .......... .......... .......... .......... .......... 16% 5.13M 67s
81500K .......... .......... .......... .......... .......... 16% 6.19M 67s
81550K .......... .......... .......... .......... .......... 16% 4.65M 67s
81600K .......... .......... .......... .......... .......... 16% 4.14M 67s
81650K .......... .......... .......... .......... .......... 16% 5.32M 67s
81700K .......... .......... .......... .......... .......... 16% 4.69M 67s
81750K .......... .......... .......... .......... .......... 16% 8.25M 67s
81800K .......... .......... .......... .......... .......... 16% 8.90M 67s
81850K .......... .......... .......... .......... .......... 16% 7.05M 67s
81900K .......... .......... .......... .......... .......... 16% 6.22M 67s
81950K .......... .......... .......... .......... .......... 16% 4.52M 67s
82000K .......... .......... .......... .......... .......... 16% 6.22M 67s
82050K .......... .......... .......... .......... .......... 16% 7.28M 67s
82100K .......... .......... .......... .......... .......... 16% 4.58M 67s
82150K .......... .......... .......... .......... .......... 16% 10.7M 67s
82200K .......... .......... .......... .......... .......... 16% 9.21M 67s
82250K .......... .......... .......... .......... .......... 16% 13.8M 67s
82300K .......... .......... .......... .......... .......... 16% 17.7M 67s
82350K .......... .......... .......... .......... .......... 16% 9.36M 67s
82400K .......... .......... .......... .......... .......... 16% 9.35M 67s
82450K .......... .......... .......... .......... .......... 16% 6.06M 67s
82500K .......... .......... .......... .......... .......... 16% 11.7M 66s
82550K .......... .......... .......... .......... .......... 16% 11.3M 66s
82600K .......... .......... .......... .......... .......... 16% 7.53M 66s
82650K .......... .......... .......... .......... .......... 16% 11.9M 66s
82700K .......... .......... .......... .......... .......... 16% 7.33M 66s
82750K .......... .......... .......... .......... .......... 16% 8.90M 66s
82800K .......... .......... .......... .......... .......... 16% 7.45M 66s
82850K .......... .......... .......... .......... .......... 16% 7.35M 66s
82900K .......... .......... .......... .......... .......... 16% 8.87M 66s
82950K .......... .......... .......... .......... .......... 16% 5.25M 66s
83000K .......... .......... .......... .......... .......... 16% 5.27M 66s
83050K .......... .......... .......... .......... .......... 16% 4.69M 66s
83100K .......... .......... .......... .......... .......... 16% 3.78M 66s
83150K .......... .......... .......... .......... .......... 16% 8.57M 66s
83200K .......... .......... .......... .......... .......... 16% 5.59M 66s
83250K .......... .......... .......... .......... .......... 16% 9.16M 66s
83300K .......... .......... .......... .......... .......... 16% 7.35M 66s
83350K .......... .......... .......... .......... .......... 16% 3.47M 66s
83400K .......... .......... .......... .......... .......... 16% 4.11M 66s
83450K .......... .......... .......... .......... .......... 16% 3.41M 66s
83500K .......... .......... .......... .......... .......... 16% 5.27M 66s
83550K .......... .......... .......... .......... .......... 16% 6.22M 66s
83600K .......... .......... .......... .......... .......... 16% 3.40M 66s
83650K .......... .......... .......... .......... .......... 16% 2.10M 66s
83700K .......... .......... .......... .......... .......... 16% 3.61M 66s
83750K .......... .......... .......... .......... .......... 16% 3.42M 66s
83800K .......... .......... .......... .......... .......... 16% 4.69M 66s
83850K .......... .......... .......... .......... .......... 16% 2.31M 67s
83900K .......... .......... .......... .......... .......... 16% 2.32M 67s
83950K .......... .......... .......... .......... .......... 16% 1.76M 67s
84000K .......... .......... .......... .......... .......... 16% 2.07M 67s
84050K .......... .......... .......... .......... .......... 16% 3.06M 67s
84100K .......... .......... .......... .......... .......... 16% 14.4M 67s
84150K .......... .......... .......... .......... .......... 16% 12.3M 67s
84200K .......... .......... .......... .......... .......... 16% 16.3M 67s
84250K .......... .......... .......... .......... .......... 16% 15.8M 67s
84300K .......... .......... .......... .......... .......... 16% 12.3M 67s
84350K .......... .......... .......... .......... .......... 16% 12.3M 67s
84400K .......... .......... .......... .......... .......... 16% 7.15M 67s
84450K .......... .......... .......... .......... .......... 16% 6.58M 67s
84500K .......... .......... .......... .......... .......... 16% 7.59M 67s
84550K .......... .......... .......... .......... .......... 16% 9.25M 67s
84600K .......... .......... .......... .......... .......... 16% 11.2M 67s
84650K .......... .......... .......... .......... .......... 16% 14.8M 67s
84700K .......... .......... .......... .......... .......... 16% 12.0M 66s
84750K .......... .......... .......... .......... .......... 16% 40.7M 66s
84800K .......... .......... .......... .......... .......... 16% 17.8M 66s
84850K .......... .......... .......... .......... .......... 16% 9.27M 66s
84900K .......... .......... .......... .......... .......... 16% 27.1M 66s
84950K .......... .......... .......... .......... .......... 16% 9.78M 66s
85000K .......... .......... .......... .......... .......... 16% 11.4M 66s
85050K .......... .......... .......... .......... .......... 16% 28.4M 66s
85100K .......... .......... .......... .......... .......... 16% 11.6M 66s
85150K .......... .......... .......... .......... .......... 16% 18.0M 66s
85200K .......... .......... .......... .......... .......... 16% 6.32M 66s
85250K .......... .......... .......... .......... .......... 16% 17.8M 66s
85300K .......... .......... .......... .......... .......... 16% 6.35M 66s
85350K .......... .......... .......... .......... .......... 16% 9.31M 66s
85400K .......... .......... .......... .......... .......... 16% 8.87M 66s
85450K .......... .......... .......... .......... .......... 16% 5.25M 66s
85500K .......... .......... .......... .......... .......... 16% 8.61M 66s
85550K .......... .......... .......... .......... .......... 16% 7.16M 66s
85600K .......... .......... .......... .......... .......... 16% 5.26M 66s
85650K .......... .......... .......... .......... .......... 16% 16.4M 66s
85700K .......... .......... .......... .......... .......... 16% 24.2M 66s
85750K .......... .......... .......... .......... .......... 16% 9.80M 66s
85800K .......... .......... .......... .......... .......... 17% 9.17M 66s
85850K .......... .......... .......... .......... .......... 17% 17.7M 66s
85900K .......... .......... .......... .......... .......... 17% 12.3M 66s
85950K .......... .......... .......... .......... .......... 17% 5.98M 66s
86000K .......... .......... .......... .......... .......... 17% 7.37M 66s
86050K .......... .......... .......... .......... .......... 17% 8.98M 66s
86100K .......... .......... .......... .......... .......... 17% 9.24M 66s
86150K .......... .......... .......... .......... .......... 17% 5.29M 66s
86200K .......... .......... .......... .......... .......... 17% 7.21M 66s
86250K .......... .......... .......... .......... .......... 17% 6.48M 66s
86300K .......... .......... .......... .......... .......... 17% 6.00M 66s
86350K .......... .......... .......... .......... .......... 17% 5.35M 66s
86400K .......... .......... .......... .......... .......... 17% 3.43M 66s
86450K .......... .......... .......... .......... .......... 17% 3.74M 66s
86500K .......... .......... .......... .......... .......... 17% 4.67M 66s
86550K .......... .......... .......... .......... .......... 17% 5.44M 66s
86600K .......... .......... .......... .......... .......... 17% 5.25M 66s
86650K .......... .......... .......... .......... .......... 17% 9.00M 66s
86700K .......... .......... .......... .......... .......... 17% 6.06M 66s
86750K .......... .......... .......... .......... .......... 17% 7.74M 66s
86800K .......... .......... .......... .......... .......... 17% 10.9M 66s
86850K .......... .......... .......... .......... .......... 17% 8.95M 66s
86900K .......... .......... .......... .......... .......... 17% 11.3M 66s
86950K .......... .......... .......... .......... .......... 17% 7.19M 66s
87000K .......... .......... .......... .......... .......... 17% 7.34M 66s
87050K .......... .......... .......... .......... .......... 17% 7.69M 66s
87100K .......... .......... .......... .......... .......... 17% 4.07M 66s
87150K .......... .......... .......... .......... .......... 17% 4.95M 66s
87200K .......... .......... .......... .......... .......... 17% 3.09M 66s
87250K .......... .......... .......... .......... .......... 17% 4.60M 66s
87300K .......... .......... .......... .......... .......... 17% 5.18M 66s
87350K .......... .......... .......... .......... .......... 17% 5.18M 66s
87400K .......... .......... .......... .......... .......... 17% 7.24M 66s
87450K .......... .......... .......... .......... .......... 17% 7.48M 66s
87500K .......... .......... .......... .......... .......... 17% 10.4M 66s
87550K .......... .......... .......... .......... .......... 17% 17.9M 66s
87600K .......... .......... .......... .......... .......... 17% 16.1M 66s
87650K .......... .......... .......... .......... .......... 17% 11.1M 66s
87700K .......... .......... .......... .......... .......... 17% 31.4M 66s
87750K .......... .......... .......... .......... .......... 17% 12.3M 66s
87800K .......... .......... .......... .......... .......... 17% 12.2M 66s
87850K .......... .......... .......... .......... .......... 17% 17.3M 65s
87900K .......... .......... .......... .......... .......... 17% 14.2M 65s
87950K .......... .......... .......... .......... .......... 17% 16.7M 65s
88000K .......... .......... .......... .......... .......... 17% 26.3M 65s
88050K .......... .......... .......... .......... .......... 17% 9.44M 65s
88100K .......... .......... .......... .......... .......... 17% 17.5M 65s
88150K .......... .......... .......... .......... .......... 17% 18.3M 65s
88200K .......... .......... .......... .......... .......... 17% 10.9M 65s
88250K .......... .......... .......... .......... .......... 17% 12.5M 65s
88300K .......... .......... .......... .......... .......... 17% 12.5M 65s
88350K .......... .......... .......... .......... .......... 17% 6.31M 65s
88400K .......... .......... .......... .......... .......... 17% 7.53M 65s
88450K .......... .......... .......... .......... .......... 17% 7.09M 65s
88500K .......... .......... .......... .......... .......... 17% 11.3M 65s
88550K .......... .......... .......... .......... .......... 17% 4.70M 65s
88600K .......... .......... .......... .......... .......... 17% 6.25M 65s
88650K .......... .......... .......... .......... .......... 17% 3.33M 65s
88700K .......... .......... .......... .......... .......... 17% 3.09M 65s
88750K .......... .......... .......... .......... .......... 17% 6.17M 65s
88800K .......... .......... .......... .......... .......... 17% 7.01M 65s
88850K .......... .......... .......... .......... .......... 17% 5.39M 65s
88900K .......... .......... .......... .......... .......... 17% 7.29M 65s
88950K .......... .......... .......... .......... .......... 17% 7.32M 65s
89000K .......... .......... .......... .......... .......... 17% 6.08M 65s
89050K .......... .......... .......... .......... .......... 17% 3.72M 65s
89100K .......... .......... .......... .......... .......... 17% 3.81M 65s
89150K .......... .......... .......... .......... .......... 17% 4.18M 65s
89200K .......... .......... .......... .......... .......... 17% 4.61M 65s
89250K .......... .......... .......... .......... .......... 17% 5.30M 65s
89300K .......... .......... .......... .......... .......... 17% 3.16M 65s
89350K .......... .......... .......... .......... .......... 17% 4.14M 65s
89400K .......... .......... .......... .......... .......... 17% 4.14M 65s
89450K .......... .......... .......... .......... .......... 17% 4.15M 65s
89500K .......... .......... .......... .......... .......... 17% 4.13M 65s
89550K .......... .......... .......... .......... .......... 17% 6.16M 65s
89600K .......... .......... .......... .......... .......... 17% 4.09M 65s
89650K .......... .......... .......... .......... .......... 17% 6.23M 65s
89700K .......... .......... .......... .......... .......... 17% 2.72M 65s
89750K .......... .......... .......... .......... .......... 17% 4.67M 65s
89800K .......... .......... .......... .......... .......... 17% 3.73M 65s
89850K .......... .......... .......... .......... .......... 17% 7.95M 65s
89900K .......... .......... .......... .......... .......... 17% 9.38M 65s
89950K .......... .......... .......... .......... .......... 17% 8.10M 65s
90000K .......... .......... .......... .......... .......... 17% 7.59M 65s
90050K .......... .......... .......... .......... .......... 17% 7.20M 65s
90100K .......... .......... .......... .......... .......... 17% 6.18M 65s
90150K .......... .......... .......... .......... .......... 17% 3.78M 65s
90200K .......... .......... .......... .......... .......... 17% 2.41M 65s
90250K .......... .......... .......... .......... .......... 17% 1.69M 65s
90300K .......... .......... .......... .......... .......... 17% 2.19M 65s
90350K .......... .......... .......... .......... .......... 17% 1.86M 66s
90400K .......... .......... .......... .......... .......... 17% 7.14M 66s
90450K .......... .......... .......... .......... .......... 17% 24.0M 65s
90500K .......... .......... .......... .......... .......... 17% 15.6M 65s
90550K .......... .......... .......... .......... .......... 17% 18.1M 65s
90600K .......... .......... .......... .......... .......... 17% 24.8M 65s
90650K .......... .......... .......... .......... .......... 17% 17.8M 65s
90700K .......... .......... .......... .......... .......... 17% 12.4M 65s
90750K .......... .......... .......... .......... .......... 17% 17.0M 65s
90800K .......... .......... .......... .......... .......... 17% 14.4M 65s
90850K .......... .......... .......... .......... .......... 18% 12.0M 65s
90900K .......... .......... .......... .......... .......... 18% 12.3M 65s
90950K .......... .......... .......... .......... .......... 18% 9.19M 65s
91000K .......... .......... .......... .......... .......... 18% 9.09M 65s
91050K .......... .......... .......... .......... .......... 18% 4.49M 65s
91100K .......... .......... .......... .......... .......... 18% 5.40M 65s
91150K .......... .......... .......... .......... .......... 18% 9.36M 65s
91200K .......... .......... .......... .......... .......... 18% 7.29M 65s
91250K .......... .......... .......... .......... .......... 18% 9.04M 65s
91300K .......... .......... .......... .......... .......... 18% 7.53M 65s
91350K .......... .......... .......... .......... .......... 18% 3.39M 65s
91400K .......... .......... .......... .......... .......... 18% 4.61M 65s
91450K .......... .......... .......... .......... .......... 18% 3.42M 65s
91500K .......... .......... .......... .......... .......... 18% 4.16M 65s
91550K .......... .......... .......... .......... .......... 18% 3.37M 65s
91600K .......... .......... .......... .......... .......... 18% 2.66M 65s
91650K .......... .......... .......... .......... .......... 18% 4.13M 65s
91700K .......... .......... .......... .......... .......... 18% 7.41M 65s
91750K .......... .......... .......... .......... .......... 18% 16.2M 65s
91800K .......... .......... .......... .......... .......... 18% 15.3M 65s
91850K .......... .......... .......... .......... .......... 18% 7.01M 65s
91900K .......... .......... .......... .......... .......... 18% 9.40M 65s
91950K .......... .......... .......... .......... .......... 18% 5.98M 65s
92000K .......... .......... .......... .......... .......... 18% 9.21M 65s
92050K .......... .......... .......... .......... .......... 18% 9.31M 65s
92100K .......... .......... .......... .......... .......... 18% 4.59M 65s
92150K .......... .......... .......... .......... .......... 18% 3.73M 65s
92200K .......... .......... .......... .......... .......... 18% 3.67M 65s
92250K .......... .......... .......... .......... .......... 18% 6.15M 65s
92300K .......... .......... .......... .......... .......... 18% 7.44M 65s
92350K .......... .......... .......... .......... .......... 18% 6.03M 65s
92400K .......... .......... .......... .......... .......... 18% 5.16M 65s
92450K .......... .......... .......... .......... .......... 18% 3.72M 65s
92500K .......... .......... .......... .......... .......... 18% 5.26M 65s
92550K .......... .......... .......... .......... .......... 18% 7.23M 65s
92600K .......... .......... .......... .......... .......... 18% 5.27M 65s
92650K .......... .......... .......... .......... .......... 18% 3.09M 65s
92700K .......... .......... .......... .......... .......... 18% 4.53M 65s
92750K .......... .......... .......... .......... .......... 18% 5.31M 65s
92800K .......... .......... .......... .......... .......... 18% 3.72M 65s
92850K .......... .......... .......... .......... .......... 18% 2.53M 65s
92900K .......... .......... .......... .......... .......... 18% 3.35M 65s
92950K .......... .......... .......... .......... .......... 18% 9.31M 65s
93000K .......... .......... .......... .......... .......... 18% 7.02M 65s
93050K .......... .......... .......... .......... .......... 18% 7.26M 65s
93100K .......... .......... .......... .......... .......... 18% 6.04M 65s
93150K .......... .......... .......... .......... .......... 18% 3.41M 65s
93200K .......... .......... .......... .......... .......... 18% 3.76M 65s
93250K .......... .......... .......... .......... .......... 18% 2.87M 65s
93300K .......... .......... .......... .......... .......... 18% 2.19M 65s
93350K .......... .......... .......... .......... .......... 18% 4.09M 65s
93400K .......... .......... .......... .......... .......... 18% 4.94M 65s
93450K .......... .......... .......... .......... .......... 18% 7.07M 65s
93500K .......... .......... .......... .......... .......... 18% 9.22M 65s
93550K .......... .......... .......... .......... .......... 18% 7.44M 65s
93600K .......... .......... .......... .......... .......... 18% 6.12M 65s
93650K .......... .......... .......... .......... .......... 18% 7.44M 65s
93700K .......... .......... .......... .......... .......... 18% 6.06M 65s
93750K .......... .......... .......... .......... .......... 18% 5.35M 65s
93800K .......... .......... .......... .......... .......... 18% 6.00M 65s
93850K .......... .......... .......... .......... .......... 18% 3.70M 65s
93900K .......... .......... .......... .......... .......... 18% 3.41M 65s
93950K .......... .......... .......... .......... .......... 18% 4.12M 65s
94000K .......... .......... .......... .......... .......... 18% 7.32M 65s
94050K .......... .......... .......... .......... .......... 18% 9.44M 65s
94100K .......... .......... .......... .......... .......... 18% 16.8M 65s
94150K .......... .......... .......... .......... .......... 18% 13.6M 65s
94200K .......... .......... .......... .......... .......... 18% 14.2M 65s
94250K .......... .......... .......... .......... .......... 18% 18.4M 65s
94300K .......... .......... .......... .......... .......... 18% 7.18M 65s
94350K .......... .......... .......... .......... .......... 18% 9.78M 65s
94400K .......... .......... .......... .......... .......... 18% 8.96M 65s
94450K .......... .......... .......... .......... .......... 18% 4.56M 65s
94500K .......... .......... .......... .......... .......... 18% 12.1M 65s
94550K .......... .......... .......... .......... .......... 18% 11.8M 65s
94600K .......... .......... .......... .......... .......... 18% 8.88M 65s
94650K .......... .......... .......... .......... .......... 18% 8.78M 65s
94700K .......... .......... .......... .......... .......... 18% 6.20M 65s
94750K .......... .......... .......... .......... .......... 18% 5.23M 65s
94800K .......... .......... .......... .......... .......... 18% 6.38M 65s
94850K .......... .......... .......... .......... .......... 18% 5.38M 65s
94900K .......... .......... .......... .......... .......... 18% 5.25M 65s
94950K .......... .......... .......... .......... .......... 18% 14.3M 65s
95000K .......... .......... .......... .......... .......... 18% 12.5M 65s
95050K .......... .......... .......... .......... .......... 18% 12.0M 65s
95100K .......... .......... .......... .......... .......... 18% 16.9M 65s
95150K .......... .......... .......... .......... .......... 18% 9.48M 65s
95200K .......... .......... .......... .......... .......... 18% 6.26M 65s
95250K .......... .......... .......... .......... .......... 18% 6.18M 65s
95300K .......... .......... .......... .......... .......... 18% 7.27M 65s
95350K .......... .......... .......... .......... .......... 18% 4.11M 65s
95400K .......... .......... .......... .......... .......... 18% 4.30M 65s
95450K .......... .......... .......... .......... .......... 18% 3.82M 65s
95500K .......... .......... .......... .......... .......... 18% 5.38M 65s
95550K .......... .......... .......... .......... .......... 18% 7.22M 65s
95600K .......... .......... .......... .......... .......... 18% 9.14M 65s
95650K .......... .......... .......... .......... .......... 18% 9.23M 65s
95700K .......... .......... .......... .......... .......... 18% 9.21M 65s
95750K .......... .......... .......... .......... .......... 18% 6.17M 65s
95800K .......... .......... .......... .......... .......... 18% 6.21M 65s
95850K .......... .......... .......... .......... .......... 18% 7.21M 65s
95900K .......... .......... .......... .......... .......... 19% 17.2M 65s
95950K .......... .......... .......... .......... .......... 19% 4.03M 65s
96000K .......... .......... .......... .......... .......... 19% 4.62M 65s
96050K .......... .......... .......... .......... .......... 19% 4.18M 65s
96100K .......... .......... .......... .......... .......... 19% 3.35M 65s
96150K .......... .......... .......... .......... .......... 19% 4.69M 65s
96200K .......... .......... .......... .......... .......... 19% 5.37M 65s
96250K .......... .......... .......... .......... .......... 19% 6.14M 65s
96300K .......... .......... .......... .......... .......... 19% 5.33M 65s
96350K .......... .......... .......... .......... .......... 19% 4.70M 65s
96400K .......... .......... .......... .......... .......... 19% 7.20M 65s
96450K .......... .......... .......... .......... .......... 19% 4.21M 65s
96500K .......... .......... .......... .......... .......... 19% 9.18M 65s
96550K .......... .......... .......... .......... .......... 19% 9.26M 65s
96600K .......... .......... .......... .......... .......... 19% 6.19M 65s
96650K .......... .......... .......... .......... .......... 19% 12.5M 65s
96700K .......... .......... .......... .......... .......... 19% 7.52M 65s
96750K .......... .......... .......... .......... .......... 19% 9.19M 65s
96800K .......... .......... .......... .......... .......... 19% 8.87M 65s
96850K .......... .......... .......... .......... .......... 19% 7.45M 65s
96900K .......... .......... .......... .......... .......... 19% 9.33M 65s
96950K .......... .......... .......... .......... .......... 19% 5.32M 65s
97000K .......... .......... .......... .......... .......... 19% 4.62M 65s
97050K .......... .......... .......... .......... .......... 19% 7.44M 65s
97100K .......... .......... .......... .......... .......... 19% 8.56M 65s
97150K .......... .......... .......... .......... .......... 19% 24.3M 65s
97200K .......... .......... .......... .......... .......... 19% 25.1M 64s
97250K .......... .......... .......... .......... .......... 19% 12.8M 64s
97300K .......... .......... .......... .......... .......... 19% 10.9M 64s
97350K .......... .......... .......... .......... .......... 19% 35.9M 64s
97400K .......... .......... .......... .......... .......... 19% 11.7M 64s
97450K .......... .......... .......... .......... .......... 19% 12.0M 64s
97500K .......... .......... .......... .......... .......... 19% 7.53M 64s
97550K .......... .......... .......... .......... .......... 19% 9.36M 64s
97600K .......... .......... .......... .......... .......... 19% 11.7M 64s
97650K .......... .......... .......... .......... .......... 19% 7.03M 64s
97700K .......... .......... .......... .......... .......... 19% 6.25M 64s
97750K .......... .......... .......... .......... .......... 19% 6.14M 64s
97800K .......... .......... .......... .......... .......... 19% 9.18M 64s
97850K .......... .......... .......... .......... .......... 19% 6.13M 64s
97900K .......... .......... .......... .......... .......... 19% 4.61M 64s
97950K .......... .......... .......... .......... .......... 19% 6.28M 64s
98000K .......... .......... .......... .......... .......... 19% 5.28M 64s
98050K .......... .......... .......... .......... .......... 19% 7.44M 64s
98100K .......... .......... .......... .......... .......... 19% 5.23M 64s
98150K .......... .......... .......... .......... .......... 19% 8.51M 64s
98200K .......... .......... .......... .......... .......... 19% 7.41M 64s
98250K .......... .......... .......... .......... .......... 19% 6.06M 64s
98300K .......... .......... .......... .......... .......... 19% 7.05M 64s
98350K .......... .......... .......... .......... .......... 19% 7.33M 64s
98400K .......... .......... .......... .......... .......... 19% 7.43M 64s
98450K .......... .......... .......... .......... .......... 19% 5.31M 64s
98500K .......... .......... .......... .......... .......... 19% 3.71M 64s
98550K .......... .......... .......... .......... .......... 19% 3.35M 64s
98600K .......... .......... .......... .......... .......... 19% 3.40M 64s
98650K .......... .......... .......... .......... .......... 19% 4.66M 64s
98700K .......... .......... .......... .......... .......... 19% 3.67M 64s
98750K .......... .......... .......... .......... .......... 19% 3.38M 64s
98800K .......... .......... .......... .......... .......... 19% 4.74M 64s
98850K .......... .......... .......... .......... .......... 19% 9.05M 64s
98900K .......... .......... .......... .......... .......... 19% 6.27M 64s
98950K .......... .......... .......... .......... .......... 19% 11.6M 64s
99000K .......... .......... .......... .......... .......... 19% 8.97M 64s
99050K .......... .......... .......... .......... .......... 19% 5.37M 64s
99100K .......... .......... .......... .......... .......... 19% 4.65M 64s
99150K .......... .......... .......... .......... .......... 19% 4.74M 64s
99200K .......... .......... .......... .......... .......... 19% 3.39M 64s
99250K .......... .......... .......... .......... .......... 19% 7.07M 64s
99300K .......... .......... .......... .......... .......... 19% 9.43M 64s
99350K .......... .......... .......... .......... .......... 19% 8.76M 64s
99400K .......... .......... .......... .......... .......... 19% 9.39M 64s
99450K .......... .......... .......... .......... .......... 19% 9.09M 64s
99500K .......... .......... .......... .......... .......... 19% 7.39M 64s
99550K .......... .......... .......... .......... .......... 19% 6.37M 64s
99600K .......... .......... .......... .......... .......... 19% 4.22M 64s
99650K .......... .......... .......... .......... .......... 19% 6.26M 64s
99700K .......... .......... .......... .......... .......... 19% 3.41M 64s
99750K .......... .......... .......... .......... .......... 19% 3.73M 64s
99800K .......... .......... .......... .......... .......... 19% 7.35M 64s
99850K .......... .......... .......... .......... .......... 19% 3.73M 64s
99900K .......... .......... .......... .......... .......... 19% 4.53M 64s
99950K .......... .......... .......... .......... .......... 19% 10.3M 64s
100000K .......... .......... .......... .......... .......... 19% 12.1M 64s
100050K .......... .......... .......... .......... .......... 19% 7.37M 64s
100100K .......... .......... .......... .......... .......... 19% 7.14M 64s
100150K .......... .......... .......... .......... .......... 19% 9.06M 64s
100200K .......... .......... .......... .......... .......... 19% 7.34M 64s
100250K .......... .......... .......... .......... .......... 19% 5.34M 64s
100300K .......... .......... .......... .......... .......... 19% 4.68M 64s
100350K .......... .......... .......... .......... .......... 19% 5.26M 64s
100400K .......... .......... .......... .......... .......... 19% 4.70M 64s
100450K .......... .......... .......... .......... .......... 19% 3.72M 64s
100500K .......... .......... .......... .......... .......... 19% 3.45M 64s
100550K .......... .......... .......... .......... .......... 19% 4.64M 64s
100600K .......... .......... .......... .......... .......... 19% 3.37M 64s
100650K .......... .......... .......... .......... .......... 19% 7.32M 64s
100700K .......... .......... .......... .......... .......... 19% 15.6M 64s
100750K .......... .......... .......... .......... .......... 19% 8.72M 64s
100800K .......... .......... .......... .......... .......... 19% 16.5M 64s
100850K .......... .......... .......... .......... .......... 19% 10.7M 64s
100900K .......... .......... .......... .......... .......... 19% 17.4M 64s
100950K .......... .......... .......... .......... .......... 20% 17.8M 64s
101000K .......... .......... .......... .......... .......... 20% 11.7M 64s
101050K .......... .......... .......... .......... .......... 20% 12.4M 64s
101100K .......... .......... .......... .......... .......... 20% 10.7M 64s
101150K .......... .......... .......... .......... .......... 20% 8.91M 64s
101200K .......... .......... .......... .......... .......... 20% 6.11M 64s
101250K .......... .......... .......... .......... .......... 20% 5.99M 64s
101300K .......... .......... .......... .......... .......... 20% 9.63M 64s
101350K .......... .......... .......... .......... .......... 20% 3.80M 64s
101400K .......... .......... .......... .......... .......... 20% 8.93M 64s
101450K .......... .......... .......... .......... .......... 20% 6.22M 64s
101500K .......... .......... .......... .......... .......... 20% 7.39M 64s
101550K .......... .......... .......... .......... .......... 20% 6.18M 64s
101600K .......... .......... .......... .......... .......... 20% 6.19M 64s
101650K .......... .......... .......... .......... .......... 20% 5.34M 64s
101700K .......... .......... .......... .......... .......... 20% 6.07M 64s
101750K .......... .......... .......... .......... .......... 20% 5.99M 64s
101800K .......... .......... .......... .......... .......... 20% 7.31M 64s
101850K .......... .......... .......... .......... .......... 20% 4.72M 64s
101900K .......... .......... .......... .......... .......... 20% 6.39M 64s
101950K .......... .......... .......... .......... .......... 20% 5.02M 64s
102000K .......... .......... .......... .......... .......... 20% 9.12M 64s
102050K .......... .......... .......... .......... .......... 20% 8.53M 64s
102100K .......... .......... .......... .......... .......... 20% 4.59M 64s
102150K .......... .......... .......... .......... .......... 20% 7.34M 64s
102200K .......... .......... .......... .......... .......... 20% 5.20M 64s
102250K .......... .......... .......... .......... .......... 20% 4.62M 64s
102300K .......... .......... .......... .......... .......... 20% 5.45M 64s
102350K .......... .......... .......... .......... .......... 20% 2.93M 64s
102400K .......... .......... .......... .......... .......... 20% 3.72M 64s
102450K .......... .......... .......... .......... .......... 20% 3.19M 64s
102500K .......... .......... .......... .......... .......... 20% 3.45M 64s
102550K .......... .......... .......... .......... .......... 20% 4.12M 64s
102600K .......... .......... .......... .......... .......... 20% 2.88M 64s
102650K .......... .......... .......... .......... .......... 20% 2.67M 64s
102700K .......... .......... .......... .......... .......... 20% 1.85M 64s
102750K .......... .......... .......... .......... .......... 20% 7.23M 64s
102800K .......... .......... .......... .......... .......... 20% 11.0M 64s
102850K .......... .......... .......... .......... .......... 20% 11.3M 64s
102900K .......... .......... .......... .......... .......... 20% 14.9M 64s
102950K .......... .......... .......... .......... .......... 20% 11.9M 64s
103000K .......... .......... .......... .......... .......... 20% 27.1M 64s
103050K .......... .......... .......... .......... .......... 20% 12.3M 64s
103100K .......... .......... .......... .......... .......... 20% 16.9M 64s
103150K .......... .......... .......... .......... .......... 20% 9.04M 64s
103200K .......... .......... .......... .......... .......... 20% 8.68M 64s
103250K .......... .......... .......... .......... .......... 20% 4.72M 64s
103300K .......... .......... .......... .......... .......... 20% 8.82M 64s
103350K .......... .......... .......... .......... .......... 20% 7.34M 64s
103400K .......... .......... .......... .......... .......... 20% 11.8M 64s
103450K .......... .......... .......... .......... .......... 20% 6.20M 64s
103500K .......... .......... .......... .......... .......... 20% 5.22M 64s
103550K .......... .......... .......... .......... .......... 20% 9.48M 64s
103600K .......... .......... .......... .......... .......... 20% 9.46M 64s
103650K .......... .......... .......... .......... .......... 20% 6.19M 64s
103700K .......... .......... .......... .......... .......... 20% 8.79M 64s
103750K .......... .......... .......... .......... .......... 20% 7.42M 63s
103800K .......... .......... .......... .......... .......... 20% 7.49M 63s
103850K .......... .......... .......... .......... .......... 20% 6.07M 63s
103900K .......... .......... .......... .......... .......... 20% 4.12M 63s
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104000K .......... .......... .......... .......... .......... 20% 4.68M 63s
104050K .......... .......... .......... .......... .......... 20% 2.22M 64s
104100K .......... .......... .......... .......... .......... 20% 2.32M 64s
104150K .......... .......... .......... .......... .......... 20% 8.28M 64s
104200K .......... .......... .......... .......... .......... 20% 12.1M 64s
104250K .......... .......... .......... .......... .......... 20% 12.7M 64s
104300K .......... .......... .......... .......... .......... 20% 9.01M 63s
104350K .......... .......... .......... .......... .......... 20% 6.10M 63s
104400K .......... .......... .......... .......... .......... 20% 5.38M 63s
104450K .......... .......... .......... .......... .......... 20% 6.12M 63s
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104650K .......... .......... .......... .......... .......... 20% 6.25M 63s
104700K .......... .......... .......... .......... .......... 20% 4.59M 63s
104750K .......... .......... .......... .......... .......... 20% 7.39M 63s
104800K .......... .......... .......... .......... .......... 20% 6.11M 63s
104850K .......... .......... .......... .......... .......... 20% 6.10M 63s
104900K .......... .......... .......... .......... .......... 20% 6.27M 63s
104950K .......... .......... .......... .......... .......... 20% 5.17M 63s
105000K .......... .......... .......... .......... .......... 20% 3.06M 63s
105050K .......... .......... .......... .......... .......... 20% 7.44M 63s
105100K .......... .......... .......... .......... .......... 20% 6.10M 63s
105150K .......... .......... .......... .......... .......... 20% 6.19M 63s
105200K .......... .......... .......... .......... .......... 20% 2.89M 63s
105250K .......... .......... .......... .......... .......... 20% 2.66M 63s
105300K .......... .......... .......... .......... .......... 20% 3.12M 64s
105350K .......... .......... .......... .......... .......... 20% 2.86M 64s
105400K .......... .......... .......... .......... .......... 20% 3.72M 64s
105450K .......... .......... .......... .......... .......... 20% 5.30M 64s
105500K .......... .......... .......... .......... .......... 20% 6.25M 64s
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105700K .......... .......... .......... .......... .......... 20% 1.49M 64s
105750K .......... .......... .......... .......... .......... 20% 2.32M 64s
105800K .......... .......... .......... .......... .......... 20% 2.49M 64s
105850K .......... .......... .......... .......... .......... 20% 7.27M 64s
105900K .......... .......... .......... .......... .......... 20% 7.38M 64s
105950K .......... .......... .......... .......... .......... 20% 9.00M 64s
106000K .......... .......... .......... .......... .......... 21% 11.9M 64s
106050K .......... .......... .......... .......... .......... 21% 8.95M 64s
106100K .......... .......... .......... .......... .......... 21% 9.22M 64s
106150K .......... .......... .......... .......... .......... 21% 9.24M 64s
106200K .......... .......... .......... .......... .......... 21% 5.26M 64s
106250K .......... .......... .......... .......... .......... 21% 6.19M 64s
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106500K .......... .......... .......... .......... .......... 21% 3.75M 64s
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106650K .......... .......... .......... .......... .......... 21% 6.00M 64s
106700K .......... .......... .......... .......... .......... 21% 8.82M 64s
106750K .......... .......... .......... .......... .......... 21% 16.6M 64s
106800K .......... .......... .......... .......... .......... 21% 11.5M 64s
106850K .......... .......... .......... .......... .......... 21% 12.0M 64s
106900K .......... .......... .......... .......... .......... 21% 9.20M 64s
106950K .......... .......... .......... .......... .......... 21% 7.18M 64s
107000K .......... .......... .......... .......... .......... 21% 7.63M 64s
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107100K .......... .......... .......... .......... .......... 21% 6.40M 64s
107150K .......... .......... .......... .......... .......... 21% 5.26M 64s
107200K .......... .......... .......... .......... .......... 21% 7.10M 64s
107250K .......... .......... .......... .......... .......... 21% 25.3M 64s
107300K .......... .......... .......... .......... .......... 21% 11.4M 63s
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107400K .......... .......... .......... .......... .......... 21% 12.5M 63s
107450K .......... .......... .......... .......... .......... 21% 7.34M 63s
107500K .......... .......... .......... .......... .......... 21% 4.20M 63s
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107650K .......... .......... .......... .......... .......... 21% 7.22M 63s
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107850K .......... .......... .......... .......... .......... 21% 3.73M 63s
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108000K .......... .......... .......... .......... .......... 21% 6.16M 63s
108050K .......... .......... .......... .......... .......... 21% 5.28M 63s
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108150K .......... .......... .......... .......... .......... 21% 13.9M 63s
108200K .......... .......... .......... .......... .......... 21% 6.57M 63s
108250K .......... .......... .......... .......... .......... 21% 9.22M 63s
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108650K .......... .......... .......... .......... .......... 21% 11.9M 63s
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108900K .......... .......... .......... .......... .......... 21% 6.53M 63s
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109000K .......... .......... .......... .......... .......... 21% 4.23M 63s
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109100K .......... .......... .......... .......... .......... 21% 3.38M 63s
109150K .......... .......... .......... .......... .......... 21% 2.64M 63s
109200K .......... .......... .......... .......... .......... 21% 2.79M 63s
109250K .......... .......... .......... .......... .......... 21% 11.9M 63s
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109900K .......... .......... .......... .......... .......... 21% 6.12M 63s
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110000K .......... .......... .......... .......... .......... 21% 5.20M 63s
110050K .......... .......... .......... .......... .......... 21% 4.10M 63s
110100K .......... .......... .......... .......... .......... 21% 4.10M 63s
110150K .......... .......... .......... .......... .......... 21% 6.06M 63s
110200K .......... .......... .......... .......... .......... 21% 5.23M 63s
110250K .......... .......... .......... .......... .......... 21% 6.96M 63s
110300K .......... .......... .......... .......... .......... 21% 4.08M 63s
110350K .......... .......... .......... .......... .......... 21% 7.15M 63s
110400K .......... .......... .......... .......... .......... 21% 9.38M 63s
110450K .......... .......... .......... .......... .......... 21% 6.02M 63s
110500K .......... .......... .......... .......... .......... 21% 7.21M 63s
110550K .......... .......... .......... .......... .......... 21% 5.16M 63s
110600K .......... .......... .......... .......... .......... 21% 4.04M 63s
110650K .......... .......... .......... .......... .......... 21% 4.64M 63s
110700K .......... .......... .......... .......... .......... 21% 5.31M 63s
110750K .......... .......... .......... .......... .......... 21% 7.48M 63s
110800K .......... .......... .......... .......... .......... 21% 6.33M 63s
110850K .......... .......... .......... .......... .......... 21% 4.25M 63s
110900K .......... .......... .......... .......... .......... 21% 4.50M 63s
110950K .......... .......... .......... .......... .......... 21% 4.67M 63s
111000K .......... .......... .......... .......... .......... 21% 6.20M 63s
111050K .......... .......... .......... .......... .......... 22% 3.49M 63s
111100K .......... .......... .......... .......... .......... 22% 3.71M 63s
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111200K .......... .......... .......... .......... .......... 22% 5.81M 63s
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111350K .......... .......... .......... .......... .......... 22% 10.8M 63s
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111450K .......... .......... .......... .......... .......... 22% 9.36M 63s
111500K .......... .......... .......... .......... .......... 22% 8.96M 63s
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111600K .......... .......... .......... .......... .......... 22% 17.6M 63s
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111700K .......... .......... .......... .......... .......... 22% 6.23M 63s
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111800K .......... .......... .......... .......... .......... 22% 3.76M 63s
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111900K .......... .......... .......... .......... .......... 22% 5.35M 63s
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112000K .......... .......... .......... .......... .......... 22% 5.29M 63s
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112100K .......... .......... .......... .......... .......... 22% 5.33M 63s
112150K .......... .......... .......... .......... .......... 22% 6.05M 63s
112200K .......... .......... .......... .......... .......... 22% 3.12M 63s
112250K .......... .......... .......... .......... .......... 22% 4.63M 63s
112300K .......... .......... .......... .......... .......... 22% 3.73M 63s
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112400K .......... .......... .......... .......... .......... 22% 4.56M 63s
112450K .......... .......... .......... .......... .......... 22% 5.25M 63s
112500K .......... .......... .......... .......... .......... 22% 5.37M 63s
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112600K .......... .......... .......... .......... .......... 22% 2.68M 63s
112650K .......... .......... .......... .......... .......... 22% 3.09M 63s
112700K .......... .......... .......... .......... .......... 22% 2.67M 63s
112750K .......... .......... .......... .......... .......... 22% 3.67M 63s
112800K .......... .......... .......... .......... .......... 22% 12.2M 63s
112850K .......... .......... .......... .......... .......... 22% 12.9M 63s
112900K .......... .......... .......... .......... .......... 22% 12.8M 63s
112950K .......... .......... .......... .......... .......... 22% 11.5M 63s
113000K .......... .......... .......... .......... .......... 22% 9.26M 63s
113050K .......... .......... .......... .......... .......... 22% 7.38M 63s
113100K .......... .......... .......... .......... .......... 22% 6.21M 63s
113150K .......... .......... .......... .......... .......... 22% 5.61M 63s
113200K .......... .......... .......... .......... .......... 22% 5.24M 63s
113250K .......... .......... .......... .......... .......... 22% 6.50M 63s
113300K .......... .......... .......... .......... .......... 22% 7.18M 63s
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113400K .......... .......... .......... .......... .......... 22% 18.2M 63s
113450K .......... .......... .......... .......... .......... 22% 9.79M 63s
113500K .......... .......... .......... .......... .......... 22% 12.3M 63s
113550K .......... .......... .......... .......... .......... 22% 11.0M 63s
113600K .......... .......... .......... .......... .......... 22% 11.6M 63s
113650K .......... .......... .......... .......... .......... 22% 9.11M 63s
113700K .......... .......... .......... .......... .......... 22% 10.2M 63s
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113800K .......... .......... .......... .......... .......... 22% 8.62M 63s
113850K .......... .......... .......... .......... .......... 22% 165M 63s
113900K .......... .......... .......... .......... .......... 22% 11.7M 63s
113950K .......... .......... .......... .......... .......... 22% 9.16M 63s
114000K .......... .......... .......... .......... .......... 22% 38.0M 63s
114050K .......... .......... .......... .......... .......... 22% 8.23M 63s
114100K .......... .......... .......... .......... .......... 22% 11.9M 63s
114150K .......... .......... .......... .......... .......... 22% 7.22M 63s
114200K .......... .......... .......... .......... .......... 22% 5.36M 63s
114250K .......... .......... .......... .......... .......... 22% 4.72M 63s
114300K .......... .......... .......... .......... .......... 22% 8.90M 63s
114350K .......... .......... .......... .......... .......... 22% 7.34M 63s
114400K .......... .......... .......... .......... .......... 22% 7.39M 63s
114450K .......... .......... .......... .......... .......... 22% 7.88M 63s
114500K .......... .......... .......... .......... .......... 22% 17.5M 63s
114550K .......... .......... .......... .......... .......... 22% 13.8M 62s
114600K .......... .......... .......... .......... .......... 22% 8.99M 62s
114650K .......... .......... .......... .......... .......... 22% 6.25M 62s
114700K .......... .......... .......... .......... .......... 22% 7.32M 62s
114750K .......... .......... .......... .......... .......... 22% 4.64M 62s
114800K .......... .......... .......... .......... .......... 22% 6.21M 62s
114850K .......... .......... .......... .......... .......... 22% 4.60M 62s
114900K .......... .......... .......... .......... .......... 22% 5.29M 62s
114950K .......... .......... .......... .......... .......... 22% 3.42M 62s
115000K .......... .......... .......... .......... .......... 22% 6.24M 62s
115050K .......... .......... .......... .......... .......... 22% 7.50M 62s
115100K .......... .......... .......... .......... .......... 22% 11.2M 62s
115150K .......... .......... .......... .......... .......... 22% 9.28M 62s
115200K .......... .......... .......... .......... .......... 22% 7.25M 62s
115250K .......... .......... .......... .......... .......... 22% 6.26M 62s
115300K .......... .......... .......... .......... .......... 22% 7.38M 62s
115350K .......... .......... .......... .......... .......... 22% 4.67M 62s
115400K .......... .......... .......... .......... .......... 22% 7.65M 62s
115450K .......... .......... .......... .......... .......... 22% 7.40M 62s
115500K .......... .......... .......... .......... .......... 22% 7.30M 62s
115550K .......... .......... .......... .......... .......... 22% 9.13M 62s
115600K .......... .......... .......... .......... .......... 22% 5.34M 62s
115650K .......... .......... .......... .......... .......... 22% 5.88M 62s
115700K .......... .......... .......... .......... .......... 22% 3.72M 62s
115750K .......... .......... .......... .......... .......... 22% 4.34M 62s
115800K .......... .......... .......... .......... .......... 22% 6.19M 62s
115850K .......... .......... .......... .......... .......... 22% 4.97M 62s
115900K .......... .......... .......... .......... .......... 22% 16.5M 62s
115950K .......... .......... .......... .......... .......... 22% 10.6M 62s
116000K .......... .......... .......... .......... .......... 22% 11.4M 62s
116050K .......... .......... .......... .......... .......... 22% 9.09M 62s
116100K .......... .......... .......... .......... .......... 23% 7.43M 62s
116150K .......... .......... .......... .......... .......... 23% 6.49M 62s
116200K .......... .......... .......... .......... .......... 23% 5.24M 62s
116250K .......... .......... .......... .......... .......... 23% 8.86M 62s
116300K .......... .......... .......... .......... .......... 23% 8.67M 62s
116350K .......... .......... .......... .......... .......... 23% 4.65M 62s
116400K .......... .......... .......... .......... .......... 23% 4.11M 62s
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116500K .......... .......... .......... .......... .......... 23% 6.19M 62s
116550K .......... .......... .......... .......... .......... 23% 6.23M 62s
116600K .......... .......... .......... .......... .......... 23% 5.40M 62s
116650K .......... .......... .......... .......... .......... 23% 7.02M 62s
116700K .......... .......... .......... .......... .......... 23% 9.56M 62s
116750K .......... .......... .......... .......... .......... 23% 10.4M 62s
116800K .......... .......... .......... .......... .......... 23% 17.1M 62s
116850K .......... .......... .......... .......... .......... 23% 7.00M 62s
116900K .......... .......... .......... .......... .......... 23% 8.56M 62s
116950K .......... .......... .......... .......... .......... 23% 9.32M 62s
117000K .......... .......... .......... .......... .......... 23% 9.67M 62s
117050K .......... .......... .......... .......... .......... 23% 6.38M 62s
117100K .......... .......... .......... .......... .......... 23% 7.23M 62s
117150K .......... .......... .......... .......... .......... 23% 7.59M 62s
117200K .......... .......... .......... .......... .......... 23% 9.13M 62s
117250K .......... .......... .......... .......... .......... 23% 9.29M 62s
117300K .......... .......... .......... .......... .......... 23% 9.04M 62s
117350K .......... .......... .......... .......... .......... 23% 6.31M 62s
117400K .......... .......... .......... .......... .......... 23% 6.07M 62s
117450K .......... .......... .......... .......... .......... 23% 4.16M 62s
117500K .......... .......... .......... .......... .......... 23% 6.19M 62s
117550K .......... .......... .......... .......... .......... 23% 6.13M 62s
117600K .......... .......... .......... .......... .......... 23% 3.86M 62s
117650K .......... .......... .......... .......... .......... 23% 6.25M 62s
117700K .......... .......... .......... .......... .......... 23% 8.88M 62s
117750K .......... .......... .......... .......... .......... 23% 12.0M 62s
117800K .......... .......... .......... .......... .......... 23% 8.45M 62s
117850K .......... .......... .......... .......... .......... 23% 11.3M 62s
117900K .......... .......... .......... .......... .......... 23% 7.07M 62s
117950K .......... .......... .......... .......... .......... 23% 11.4M 62s
118000K .......... .......... .......... .......... .......... 23% 6.14M 62s
118050K .......... .......... .......... .......... .......... 23% 6.44M 62s
118100K .......... .......... .......... .......... .......... 23% 4.74M 62s
118150K .......... .......... .......... .......... .......... 23% 8.99M 62s
118200K .......... .......... .......... .......... .......... 23% 7.17M 62s
118250K .......... .......... .......... .......... .......... 23% 5.62M 62s
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118350K .......... .......... .......... .......... .......... 23% 3.38M 62s
118400K .......... .......... .......... .......... .......... 23% 4.17M 62s
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118550K .......... .......... .......... .......... .......... 23% 9.07M 62s
118600K .......... .......... .......... .......... .......... 23% 6.09M 62s
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118700K .......... .......... .......... .......... .......... 23% 4.67M 62s
118750K .......... .......... .......... .......... .......... 23% 2.18M 62s
118800K .......... .......... .......... .......... .......... 23% 5.28M 62s
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118900K .......... .......... .......... .......... .......... 23% 6.05M 62s
118950K .......... .......... .......... .......... .......... 23% 5.30M 62s
119000K .......... .......... .......... .......... .......... 23% 4.12M 62s
119050K .......... .......... .......... .......... .......... 23% 3.65M 62s
119100K .......... .......... .......... .......... .......... 23% 2.86M 62s
119150K .......... .......... .......... .......... .......... 23% 2.19M 62s
119200K .......... .......... .......... .......... .......... 23% 3.03M 62s
119250K .......... .......... .......... .......... .......... 23% 12.4M 62s
119300K .......... .......... .......... .......... .......... 23% 6.10M 62s
119350K .......... .......... .......... .......... .......... 23% 7.31M 62s
119400K .......... .......... .......... .......... .......... 23% 6.21M 62s
119450K .......... .......... .......... .......... .......... 23% 6.11M 62s
119500K .......... .......... .......... .......... .......... 23% 7.37M 62s
119550K .......... .......... .......... .......... .......... 23% 11.6M 62s
119600K .......... .......... .......... .......... .......... 23% 12.0M 62s
119650K .......... .......... .......... .......... .......... 23% 9.13M 62s
119700K .......... .......... .......... .......... .......... 23% 8.86M 62s
119750K .......... .......... .......... .......... .......... 23% 3.90M 62s
119800K .......... .......... .......... .......... .......... 23% 5.30M 62s
119850K .......... .......... .......... .......... .......... 23% 3.70M 62s
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119950K .......... .......... .......... .......... .......... 23% 4.66M 62s
120000K .......... .......... .......... .......... .......... 23% 4.75M 62s
120050K .......... .......... .......... .......... .......... 23% 9.16M 62s
120100K .......... .......... .......... .......... .......... 23% 9.01M 62s
120150K .......... .......... .......... .......... .......... 23% 11.9M 62s
120200K .......... .......... .......... .......... .......... 23% 8.46M 62s
120250K .......... .......... .......... .......... .......... 23% 11.9M 62s
120300K .......... .......... .......... .......... .......... 23% 15.6M 62s
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120400K .......... .......... .......... .......... .......... 23% 8.36M 62s
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120600K .......... .......... .......... .......... .......... 23% 4.12M 62s
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120700K .......... .......... .......... .......... .......... 23% 9.19M 61s
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120800K .......... .......... .......... .......... .......... 23% 12.9M 61s
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120900K .......... .......... .......... .......... .......... 23% 11.7M 61s
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121000K .......... .......... .......... .......... .......... 23% 9.25M 61s
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121100K .......... .......... .......... .......... .......... 23% 3.75M 61s
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121500K .......... .......... .......... .......... .......... 24% 6.17M 61s
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121600K .......... .......... .......... .......... .......... 24% 2.90M 61s
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121700K .......... .......... .......... .......... .......... 24% 1.97M 61s
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121800K .......... .......... .......... .......... .......... 24% 11.6M 61s
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122000K .......... .......... .......... .......... .......... 24% 17.8M 61s
122050K .......... .......... .......... .......... .......... 24% 11.9M 61s
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122150K .......... .......... .......... .......... .......... 24% 7.41M 61s
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122250K .......... .......... .......... .......... .......... 24% 7.16M 61s
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123000K .......... .......... .......... .......... .......... 24% 6.23M 61s
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123100K .......... .......... .......... .......... .......... 24% 4.23M 61s
123150K .......... .......... .......... .......... .......... 24% 5.99M 61s
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123250K .......... .......... .......... .......... .......... 24% 6.07M 61s
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123400K .......... .......... .......... .......... .......... 24% 6.27M 61s
123450K .......... .......... .......... .......... .......... 24% 5.30M 61s
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123550K .......... .......... .......... .......... .......... 24% 7.29M 61s
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123800K .......... .......... .......... .......... .......... 24% 14.0M 61s
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123900K .......... .......... .......... .......... .......... 24% 7.41M 61s
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124000K .......... .......... .......... .......... .......... 24% 5.33M 61s
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124100K .......... .......... .......... .......... .......... 24% 10.6M 61s
124150K .......... .......... .......... .......... .......... 24% 13.8M 61s
124200K .......... .......... .......... .......... .......... 24% 11.8M 61s
124250K .......... .......... .......... .......... .......... 24% 11.0M 61s
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124400K .......... .......... .......... .......... .......... 24% 8.59M 61s
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124700K .......... .......... .......... .......... .......... 24% 6.03M 61s
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125000K .......... .......... .......... .......... .......... 24% 5.28M 61s
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125100K .......... .......... .......... .......... .......... 24% 15.1M 61s
125150K .......... .......... .......... .......... .......... 24% 9.51M 61s
125200K .......... .......... .......... .......... .......... 24% 8.88M 61s
125250K .......... .......... .......... .......... .......... 24% 8.63M 61s
125300K .......... .......... .......... .......... .......... 24% 13.0M 61s
125350K .......... .......... .......... .......... .......... 24% 9.16M 61s
125400K .......... .......... .......... .......... .......... 24% 7.47M 61s
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125500K .......... .......... .......... .......... .......... 24% 3.88M 61s
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125700K .......... .......... .......... .......... .......... 24% 11.6M 61s
125750K .......... .......... .......... .......... .......... 24% 24.7M 61s
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125850K .......... .......... .......... .......... .......... 24% 11.7M 61s
125900K .......... .......... .......... .......... .......... 24% 79.9M 61s
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126000K .......... .......... .......... .......... .......... 24% 18.1M 61s
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126100K .......... .......... .......... .......... .......... 24% 15.9M 61s
126150K .......... .......... .......... .......... .......... 24% 6.04M 61s
126200K .......... .......... .......... .......... .......... 25% 7.71M 61s
126250K .......... .......... .......... .......... .......... 25% 8.74M 61s
126300K .......... .......... .......... .......... .......... 25% 7.67M 61s
126350K .......... .......... .......... .......... .......... 25% 6.09M 61s
126400K .......... .......... .......... .......... .......... 25% 9.19M 61s
126450K .......... .......... .......... .......... .......... 25% 7.32M 61s
126500K .......... .......... .......... .......... .......... 25% 7.48M 61s
126550K .......... .......... .......... .......... .......... 25% 5.89M 61s
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126700K .......... .......... .......... .......... .......... 25% 5.42M 61s
126750K .......... .......... .......... .......... .......... 25% 6.22M 61s
126800K .......... .......... .......... .......... .......... 25% 4.86M 61s
126850K .......... .......... .......... .......... .......... 25% 2.65M 61s
126900K .......... .......... .......... .......... .......... 25% 4.13M 61s
126950K .......... .......... .......... .......... .......... 25% 2.20M 61s
127000K .......... .......... .......... .......... .......... 25% 2.18M 61s
127050K .......... .......... .......... .......... .......... 25% 3.08M 61s
127100K .......... .......... .......... .......... .......... 25% 9.35M 61s
127150K .......... .......... .......... .......... .......... 25% 9.13M 61s
127200K .......... .......... .......... .......... .......... 25% 5.30M 61s
127250K .......... .......... .......... .......... .......... 25% 4.62M 61s
127300K .......... .......... .......... .......... .......... 25% 4.65M 61s
127350K .......... .......... .......... .......... .......... 25% 2.50M 61s
127400K .......... .......... .......... .......... .......... 25% 2.33M 61s
127450K .......... .......... .......... .......... .......... 25% 2.85M 61s
127500K .......... .......... .......... .......... .......... 25% 7.43M 61s
127550K .......... .......... .......... .......... .......... 25% 5.27M 61s
127600K .......... .......... .......... .......... .......... 25% 5.31M 61s
127650K .......... .......... .......... .......... .......... 25% 4.66M 61s
127700K .......... .......... .......... .......... .......... 25% 4.12M 61s
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127800K .......... .......... .......... .......... .......... 25% 3.74M 61s
127850K .......... .......... .......... .......... .......... 25% 3.41M 61s
127900K .......... .......... .......... .......... .......... 25% 6.07M 61s
127950K .......... .......... .......... .......... .......... 25% 4.20M 61s
128000K .......... .......... .......... .......... .......... 25% 14.2M 61s
128050K .......... .......... .......... .......... .......... 25% 11.4M 61s
128100K .......... .......... .......... .......... .......... 25% 7.20M 61s
128150K .......... .......... .......... .......... .......... 25% 16.5M 61s
128200K .......... .......... .......... .......... .......... 25% 7.52M 61s
128250K .......... .......... .......... .......... .......... 25% 7.27M 61s
128300K .......... .......... .......... .......... .......... 25% 8.54M 61s
128350K .......... .......... .......... .......... .......... 25% 5.29M 61s
128400K .......... .......... .......... .......... .......... 25% 7.33M 61s
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129000K .......... .......... .......... .......... .......... 25% 4.61M 61s
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129100K .......... .......... .......... .......... .......... 25% 1.78M 61s
129150K .......... .......... .......... .......... .......... 25% 1.74M 61s
129200K .......... .......... .......... .......... .......... 25% 1.20M 61s
129250K .......... .......... .......... .......... .......... 25% 1.94M 61s
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130000K .......... .......... .......... .......... .......... 25% 11.7M 61s
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131000K .......... .......... .......... .......... .......... 25% 16.8M 61s
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131600K .......... .......... .......... .......... .......... 26% 8.99M 60s
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132150K .......... .......... .......... .......... .......... 26% 4.60M 60s
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132250K .......... .......... .......... .......... .......... 26% 11.0M 60s
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133000K .......... .......... .......... .......... .......... 26% 6.55M 60s
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133100K .......... .......... .......... .......... .......... 26% 5.23M 60s
133150K .......... .......... .......... .......... .......... 26% 5.44M 60s
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134250K .......... .......... .......... .......... .......... 26% 4.34M 61s
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135250K .......... .......... .......... .......... .......... 26% 11.9M 60s
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137250K .......... .......... .......... .......... .......... 27% 9.13M 60s
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142300K .......... .......... .......... .......... .......... 28% 19.6M 59s
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155100K .......... .......... .......... .......... .......... 30% 17.1M 57s
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155250K .......... .......... .......... .......... .......... 30% 6.24M 57s
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156250K .......... .......... .......... .......... .......... 30% 4.60M 57s
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156450K .......... .......... .......... .......... .......... 30% 4.08M 57s
156500K .......... .......... .......... .......... .......... 31% 5.30M 57s
156550K .......... .......... .......... .......... .......... 31% 6.37M 57s
156600K .......... .......... .......... .......... .......... 31% 4.24M 57s
156650K .......... .......... .......... .......... .......... 31% 4.82M 57s
156700K .......... .......... .......... .......... .......... 31% 3.73M 57s
156750K .......... .......... .......... .......... .......... 31% 7.10M 57s
156800K .......... .......... .......... .......... .......... 31% 7.19M 57s
156850K .......... .......... .......... .......... .......... 31% 7.31M 57s
156900K .......... .......... .......... .......... .......... 31% 9.17M 57s
156950K .......... .......... .......... .......... .......... 31% 7.11M 57s
157000K .......... .......... .......... .......... .......... 31% 6.12M 57s
157050K .......... .......... .......... .......... .......... 31% 11.8M 57s
157100K .......... .......... .......... .......... .......... 31% 7.40M 57s
157150K .......... .......... .......... .......... .......... 31% 17.1M 56s
157200K .......... .......... .......... .......... .......... 31% 7.09M 56s
157250K .......... .......... .......... .......... .......... 31% 11.4M 56s
157300K .......... .......... .......... .......... .......... 31% 8.97M 56s
157350K .......... .......... .......... .......... .......... 31% 8.76M 56s
157400K .......... .......... .......... .......... .......... 31% 7.87M 56s
157450K .......... .......... .......... .......... .......... 31% 8.03M 56s
157500K .......... .......... .......... .......... .......... 31% 21.3M 56s
157550K .......... .......... .......... .......... .......... 31% 17.7M 56s
157600K .......... .......... .......... .......... .......... 31% 10.4M 56s
157650K .......... .......... .......... .......... .......... 31% 13.2M 56s
157700K .......... .......... .......... .......... .......... 31% 10.5M 56s
157750K .......... .......... .......... .......... .......... 31% 9.64M 56s
157800K .......... .......... .......... .......... .......... 31% 7.33M 56s
157850K .......... .......... .......... .......... .......... 31% 7.17M 56s
157900K .......... .......... .......... .......... .......... 31% 4.26M 56s
157950K .......... .......... .......... .......... .......... 31% 8.61M 56s
158000K .......... .......... .......... .......... .......... 31% 6.12M 56s
158050K .......... .......... .......... .......... .......... 31% 9.21M 56s
158100K .......... .......... .......... .......... .......... 31% 7.33M 56s
158150K .......... .......... .......... .......... .......... 31% 4.66M 56s
158200K .......... .......... .......... .......... .......... 31% 4.19M 56s
158250K .......... .......... .......... .......... .......... 31% 6.35M 56s
158300K .......... .......... .......... .......... .......... 31% 5.27M 56s
158350K .......... .......... .......... .......... .......... 31% 6.92M 56s
158400K .......... .......... .......... .......... .......... 31% 12.0M 56s
158450K .......... .......... .......... .......... .......... 31% 18.3M 56s
158500K .......... .......... .......... .......... .......... 31% 23.2M 56s
158550K .......... .......... .......... .......... .......... 31% 25.5M 56s
158600K .......... .......... .......... .......... .......... 31% 13.5M 56s
158650K .......... .......... .......... .......... .......... 31% 31.2M 56s
158700K .......... .......... .......... .......... .......... 31% 16.2M 56s
158750K .......... .......... .......... .......... .......... 31% 13.0M 56s
158800K .......... .......... .......... .......... .......... 31% 9.32M 56s
158850K .......... .......... .......... .......... .......... 31% 11.9M 56s
158900K .......... .......... .......... .......... .......... 31% 9.82M 56s
158950K .......... .......... .......... .......... .......... 31% 8.94M 56s
159000K .......... .......... .......... .......... .......... 31% 17.3M 56s
159050K .......... .......... .......... .......... .......... 31% 8.87M 56s
159100K .......... .......... .......... .......... .......... 31% 6.33M 56s
159150K .......... .......... .......... .......... .......... 31% 12.1M 56s
159200K .......... .......... .......... .......... .......... 31% 7.16M 56s
159250K .......... .......... .......... .......... .......... 31% 6.89M 56s
159300K .......... .......... .......... .......... .......... 31% 8.64M 56s
159350K .......... .......... .......... .......... .......... 31% 7.53M 56s
159400K .......... .......... .......... .......... .......... 31% 7.49M 56s
159450K .......... .......... .......... .......... .......... 31% 7.62M 56s
159500K .......... .......... .......... .......... .......... 31% 11.8M 56s
159550K .......... .......... .......... .......... .......... 31% 7.28M 56s
159600K .......... .......... .......... .......... .......... 31% 3.73M 56s
159650K .......... .......... .......... .......... .......... 31% 3.75M 56s
159700K .......... .......... .......... .......... .......... 31% 3.38M 56s
159750K .......... .......... .......... .......... .......... 31% 3.11M 56s
159800K .......... .......... .......... .......... .......... 31% 3.41M 56s
159850K .......... .......... .......... .......... .......... 31% 4.08M 56s
159900K .......... .......... .......... .......... .......... 31% 12.8M 56s
159950K .......... .......... .......... .......... .......... 31% 9.20M 56s
160000K .......... .......... .......... .......... .......... 31% 32.6M 56s
160050K .......... .......... .......... .......... .......... 31% 12.2M 56s
160100K .......... .......... .......... .......... .......... 31% 7.30M 56s
160150K .......... .......... .......... .......... .......... 31% 4.37M 56s
160200K .......... .......... .......... .......... .......... 31% 7.35M 56s
160250K .......... .......... .......... .......... .......... 31% 5.22M 56s
160300K .......... .......... .......... .......... .......... 31% 5.78M 56s
160350K .......... .......... .......... .......... .......... 31% 6.16M 56s
160400K .......... .......... .......... .......... .......... 31% 11.6M 56s
160450K .......... .......... .......... .......... .......... 31% 7.38M 56s
160500K .......... .......... .......... .......... .......... 31% 8.97M 56s
160550K .......... .......... .......... .......... .......... 31% 9.37M 56s
160600K .......... .......... .......... .......... .......... 31% 7.42M 56s
160650K .......... .......... .......... .......... .......... 31% 6.24M 56s
160700K .......... .......... .......... .......... .......... 31% 4.76M 56s
160750K .......... .......... .......... .......... .......... 31% 4.59M 56s
160800K .......... .......... .......... .......... .......... 31% 7.33M 56s
160850K .......... .......... .......... .......... .......... 31% 5.25M 56s
160900K .......... .......... .......... .......... .......... 31% 4.64M 56s
160950K .......... .......... .......... .......... .......... 31% 3.44M 56s
161000K .......... .......... .......... .......... .......... 31% 3.76M 56s
161050K .......... .......... .......... .......... .......... 31% 4.64M 56s
161100K .......... .......... .......... .......... .......... 31% 3.76M 56s
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161200K .......... .......... .......... .......... .......... 31% 4.63M 56s
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161300K .......... .......... .......... .......... .......... 31% 3.84M 56s
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161400K .......... .......... .......... .......... .......... 31% 3.75M 56s
161450K .......... .......... .......... .......... .......... 31% 4.13M 56s
161500K .......... .......... .......... .......... .......... 31% 7.18M 56s
161550K .......... .......... .......... .......... .......... 32% 16.3M 56s
161600K .......... .......... .......... .......... .......... 32% 9.37M 56s
161650K .......... .......... .......... .......... .......... 32% 12.1M 56s
161700K .......... .......... .......... .......... .......... 32% 7.35M 56s
161750K .......... .......... .......... .......... .......... 32% 16.8M 56s
161800K .......... .......... .......... .......... .......... 32% 17.6M 56s
161850K .......... .......... .......... .......... .......... 32% 11.3M 56s
161900K .......... .......... .......... .......... .......... 32% 12.6M 55s
161950K .......... .......... .......... .......... .......... 32% 9.61M 55s
162000K .......... .......... .......... .......... .......... 32% 17.7M 55s
162050K .......... .......... .......... .......... .......... 32% 15.2M 55s
162100K .......... .......... .......... .......... .......... 32% 18.3M 55s
162150K .......... .......... .......... .......... .......... 32% 12.0M 55s
162200K .......... .......... .......... .......... .......... 32% 31.0M 55s
162250K .......... .......... .......... .......... .......... 32% 15.1M 55s
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162350K .......... .......... .......... .......... .......... 32% 12.6M 55s
162400K .......... .......... .......... .......... .......... 32% 24.1M 55s
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162500K .......... .......... .......... .......... .......... 32% 16.2M 55s
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162700K .......... .......... .......... .......... .......... 32% 9.11M 55s
162750K .......... .......... .......... .......... .......... 32% 18.1M 55s
162800K .......... .......... .......... .......... .......... 32% 162M 55s
162850K .......... .......... .......... .......... .......... 32% 11.7M 55s
162900K .......... .......... .......... .......... .......... 32% 186M 55s
162950K .......... .......... .......... .......... .......... 32% 22.7M 55s
163000K .......... .......... .......... .......... .......... 32% 14.7M 55s
163050K .......... .......... .......... .......... .......... 32% 34.1M 55s
163100K .......... .......... .......... .......... .......... 32% 26.8M 55s
163150K .......... .......... .......... .......... .......... 32% 19.0M 55s
163200K .......... .......... .......... .......... .......... 32% 17.6M 55s
163250K .......... .......... .......... .......... .......... 32% 24.3M 55s
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163500K .......... .......... .......... .......... .......... 32% 17.7M 55s
163550K .......... .......... .......... .......... .......... 32% 18.9M 55s
163600K .......... .......... .......... .......... .......... 32% 9.11M 55s
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163700K .......... .......... .......... .......... .......... 32% 6.29M 55s
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163800K .......... .......... .......... .......... .......... 32% 18.1M 55s
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163900K .......... .......... .......... .......... .......... 32% 9.38M 55s
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164000K .......... .......... .......... .......... .......... 32% 16.9M 55s
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164100K .......... .......... .......... .......... .......... 32% 9.19M 55s
164150K .......... .......... .......... .......... .......... 32% 15.9M 55s
164200K .......... .......... .......... .......... .......... 32% 8.69M 55s
164250K .......... .......... .......... .......... .......... 32% 11.9M 55s
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164400K .......... .......... .......... .......... .......... 32% 17.8M 55s
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164650K .......... .......... .......... .......... .......... 32% 26.6M 55s
164700K .......... .......... .......... .......... .......... 32% 11.9M 55s
164750K .......... .......... .......... .......... .......... 32% 31.2M 54s
164800K .......... .......... .......... .......... .......... 32% 13.5M 54s
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164900K .......... .......... .......... .......... .......... 32% 15.8M 54s
164950K .......... .......... .......... .......... .......... 32% 17.7M 54s
165000K .......... .......... .......... .......... .......... 32% 18.5M 54s
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165100K .......... .......... .......... .......... .......... 32% 9.12M 54s
165150K .......... .......... .......... .......... .......... 32% 18.4M 54s
165200K .......... .......... .......... .......... .......... 32% 8.63M 54s
165250K .......... .......... .......... .......... .......... 32% 32.7M 54s
165300K .......... .......... .......... .......... .......... 32% 45.6M 54s
165350K .......... .......... .......... .......... .......... 32% 11.6M 54s
165400K .......... .......... .......... .......... .......... 32% 17.9M 54s
165450K .......... .......... .......... .......... .......... 32% 12.1M 54s
165500K .......... .......... .......... .......... .......... 32% 13.9M 54s
165550K .......... .......... .......... .......... .......... 32% 18.7M 54s
165600K .......... .......... .......... .......... .......... 32% 15.2M 54s
165650K .......... .......... .......... .......... .......... 32% 9.69M 54s
165700K .......... .......... .......... .......... .......... 32% 9.72M 54s
165750K .......... .......... .......... .......... .......... 32% 12.5M 54s
165800K .......... .......... .......... .......... .......... 32% 8.50M 54s
165850K .......... .......... .......... .......... .......... 32% 8.87M 54s
165900K .......... .......... .......... .......... .......... 32% 6.54M 54s
165950K .......... .......... .......... .......... .......... 32% 5.31M 54s
166000K .......... .......... .......... .......... .......... 32% 9.18M 54s
166050K .......... .......... .......... .......... .......... 32% 6.71M 54s
166100K .......... .......... .......... .......... .......... 32% 12.7M 54s
166150K .......... .......... .......... .......... .......... 32% 29.3M 54s
166200K .......... .......... .......... .......... .......... 32% 11.3M 54s
166250K .......... .......... .......... .......... .......... 32% 11.7M 54s
166300K .......... .......... .......... .......... .......... 32% 24.3M 54s
166350K .......... .......... .......... .......... .......... 32% 11.7M 54s
166400K .......... .......... .......... .......... .......... 32% 12.6M 54s
166450K .......... .......... .......... .......... .......... 32% 8.66M 54s
166500K .......... .......... .......... .......... .......... 32% 8.62M 54s
166550K .......... .......... .......... .......... .......... 32% 12.1M 54s
166600K .......... .......... .......... .......... .......... 33% 12.0M 54s
166650K .......... .......... .......... .......... .......... 33% 7.54M 54s
166700K .......... .......... .......... .......... .......... 33% 10.6M 54s
166750K .......... .......... .......... .......... .......... 33% 6.21M 54s
166800K .......... .......... .......... .......... .......... 33% 7.23M 54s
166850K .......... .......... .......... .......... .......... 33% 4.07M 54s
166900K .......... .......... .......... .......... .......... 33% 5.97M 54s
166950K .......... .......... .......... .......... .......... 33% 3.46M 54s
167000K .......... .......... .......... .......... .......... 33% 6.13M 54s
167050K .......... .......... .......... .......... .......... 33% 4.73M 54s
167100K .......... .......... .......... .......... .......... 33% 2.86M 54s
167150K .......... .......... .......... .......... .......... 33% 3.11M 54s
167200K .......... .......... .......... .......... .......... 33% 3.74M 54s
167250K .......... .......... .......... .......... .......... 33% 4.13M 54s
167300K .......... .......... .......... .......... .......... 33% 8.97M 54s
167350K .......... .......... .......... .......... .......... 33% 11.9M 54s
167400K .......... .......... .......... .......... .......... 33% 7.67M 54s
167450K .......... .......... .......... .......... .......... 33% 6.01M 54s
167500K .......... .......... .......... .......... .......... 33% 7.71M 54s
167550K .......... .......... .......... .......... .......... 33% 9.27M 54s
167600K .......... .......... .......... .......... .......... 33% 5.34M 54s
167650K .......... .......... .......... .......... .......... 33% 9.12M 54s
167700K .......... .......... .......... .......... .......... 33% 8.99M 54s
167750K .......... .......... .......... .......... .......... 33% 7.28M 54s
167800K .......... .......... .......... .......... .......... 33% 17.2M 54s
167850K .......... .......... .......... .......... .......... 33% 6.27M 54s
167900K .......... .......... .......... .......... .......... 33% 37.5M 54s
167950K .......... .......... .......... .......... .......... 33% 7.27M 54s
168000K .......... .......... .......... .......... .......... 33% 16.8M 54s
168050K .......... .......... .......... .......... .......... 33% 11.6M 54s
168100K .......... .......... .......... .......... .......... 33% 6.35M 54s
168150K .......... .......... .......... .......... .......... 33% 9.23M 54s
168200K .......... .......... .......... .......... .......... 33% 6.34M 54s
168250K .......... .......... .......... .......... .......... 33% 11.9M 54s
168300K .......... .......... .......... .......... .......... 33% 8.14M 54s
168350K .......... .......... .......... .......... .......... 33% 21.7M 54s
168400K .......... .......... .......... .......... .......... 33% 16.2M 54s
168450K .......... .......... .......... .......... .......... 33% 18.4M 54s
168500K .......... .......... .......... .......... .......... 33% 23.5M 54s
168550K .......... .......... .......... .......... .......... 33% 26.8M 54s
168600K .......... .......... .......... .......... .......... 33% 21.1M 53s
168650K .......... .......... .......... .......... .......... 33% 14.8M 53s
168700K .......... .......... .......... .......... .......... 33% 18.2M 53s
168750K .......... .......... .......... .......... .......... 33% 7.70M 53s
168800K .......... .......... .......... .......... .......... 33% 161M 53s
168850K .......... .......... .......... .......... .......... 33% 7.63M 53s
168900K .......... .......... .......... .......... .......... 33% 7.55M 53s
168950K .......... .......... .......... .......... .......... 33% 6.07M 53s
169000K .......... .......... .......... .......... .......... 33% 12.2M 53s
169050K .......... .......... .......... .......... .......... 33% 9.06M 53s
169100K .......... .......... .......... .......... .......... 33% 7.25M 53s
169150K .......... .......... .......... .......... .......... 33% 20.0M 53s
169200K .......... .......... .......... .......... .......... 33% 12.3M 53s
169250K .......... .......... .......... .......... .......... 33% 11.6M 53s
169300K .......... .......... .......... .......... .......... 33% 11.8M 53s
169350K .......... .......... .......... .......... .......... 33% 11.1M 53s
169400K .......... .......... .......... .......... .......... 33% 16.4M 53s
169450K .......... .......... .......... .......... .......... 33% 9.30M 53s
169500K .......... .......... .......... .......... .......... 33% 12.3M 53s
169550K .......... .......... .......... .......... .......... 33% 16.3M 53s
169600K .......... .......... .......... .......... .......... 33% 17.3M 53s
169650K .......... .......... .......... .......... .......... 33% 15.4M 53s
169700K .......... .......... .......... .......... .......... 33% 20.1M 53s
169750K .......... .......... .......... .......... .......... 33% 27.1M 53s
169800K .......... .......... .......... .......... .......... 33% 19.4M 53s
169850K .......... .......... .......... .......... .......... 33% 18.4M 53s
169900K .......... .......... .......... .......... .......... 33% 10.9M 53s
169950K .......... .......... .......... .......... .......... 33% 13.6M 53s
170000K .......... .......... .......... .......... .......... 33% 11.6M 53s
170050K .......... .......... .......... .......... .......... 33% 9.07M 53s
170100K .......... .......... .......... .......... .......... 33% 5.50M 53s
170150K .......... .......... .......... .......... .......... 33% 6.15M 53s
170200K .......... .......... .......... .......... .......... 33% 7.53M 53s
170250K .......... .......... .......... .......... .......... 33% 6.06M 53s
170300K .......... .......... .......... .......... .......... 33% 3.44M 53s
170350K .......... .......... .......... .......... .......... 33% 3.68M 53s
170400K .......... .......... .......... .......... .......... 33% 2.00M 53s
170450K .......... .......... .......... .......... .......... 33% 5.18M 53s
170500K .......... .......... .......... .......... .......... 33% 7.10M 53s
170550K .......... .......... .......... .......... .......... 33% 15.9M 53s
170600K .......... .......... .......... .......... .......... 33% 9.17M 53s
170650K .......... .......... .......... .......... .......... 33% 11.6M 53s
170700K .......... .......... .......... .......... .......... 33% 7.16M 53s
170750K .......... .......... .......... .......... .......... 33% 6.48M 53s
170800K .......... .......... .......... .......... .......... 33% 11.5M 53s
170850K .......... .......... .......... .......... .......... 33% 7.62M 53s
170900K .......... .......... .......... .......... .......... 33% 7.35M 53s
170950K .......... .......... .......... .......... .......... 33% 8.80M 53s
171000K .......... .......... .......... .......... .......... 33% 15.4M 53s
171050K .......... .......... .......... .......... .......... 33% 17.6M 53s
171100K .......... .......... .......... .......... .......... 33% 11.7M 53s
171150K .......... .......... .......... .......... .......... 33% 9.77M 53s
171200K .......... .......... .......... .......... .......... 33% 7.44M 53s
171250K .......... .......... .......... .......... .......... 33% 11.8M 53s
171300K .......... .......... .......... .......... .......... 33% 11.8M 53s
171350K .......... .......... .......... .......... .......... 33% 9.32M 53s
171400K .......... .......... .......... .......... .......... 33% 33.3M 53s
171450K .......... .......... .......... .......... .......... 33% 6.09M 53s
171500K .......... .......... .......... .......... .......... 33% 18.0M 53s
171550K .......... .......... .......... .......... .......... 33% 10.8M 53s
171600K .......... .......... .......... .......... .......... 33% 22.5M 53s
171650K .......... .......... .......... .......... .......... 34% 12.3M 53s
171700K .......... .......... .......... .......... .......... 34% 11.0M 53s
171750K .......... .......... .......... .......... .......... 34% 17.5M 53s
171800K .......... .......... .......... .......... .......... 34% 13.7M 53s
171850K .......... .......... .......... .......... .......... 34% 11.5M 53s
171900K .......... .......... .......... .......... .......... 34% 9.47M 53s
171950K .......... .......... .......... .......... .......... 34% 11.8M 53s
172000K .......... .......... .......... .......... .......... 34% 18.3M 53s
172050K .......... .......... .......... .......... .......... 34% 13.3M 53s
172100K .......... .......... .......... .......... .......... 34% 17.1M 53s
172150K .......... .......... .......... .......... .......... 34% 29.7M 53s
172200K .......... .......... .......... .......... .......... 34% 11.4M 53s
172250K .......... .......... .......... .......... .......... 34% 13.1M 52s
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172350K .......... .......... .......... .......... .......... 34% 7.19M 52s
172400K .......... .......... .......... .......... .......... 34% 17.1M 52s
172450K .......... .......... .......... .......... .......... 34% 8.09M 52s
172500K .......... .......... .......... .......... .......... 34% 17.5M 52s
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172600K .......... .......... .......... .......... .......... 34% 10.7M 52s
172650K .......... .......... .......... .......... .......... 34% 11.6M 52s
172700K .......... .......... .......... .......... .......... 34% 17.5M 52s
172750K .......... .......... .......... .......... .......... 34% 19.5M 52s
172800K .......... .......... .......... .......... .......... 34% 18.2M 52s
172850K .......... .......... .......... .......... .......... 34% 20.8M 52s
172900K .......... .......... .......... .......... .......... 34% 18.5M 52s
172950K .......... .......... .......... .......... .......... 34% 12.5M 52s
173000K .......... .......... .......... .......... .......... 34% 20.1M 52s
173050K .......... .......... .......... .......... .......... 34% 16.0M 52s
173100K .......... .......... .......... .......... .......... 34% 18.7M 52s
173150K .......... .......... .......... .......... .......... 34% 17.0M 52s
173200K .......... .......... .......... .......... .......... 34% 18.7M 52s
173250K .......... .......... .......... .......... .......... 34% 19.1M 52s
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173500K .......... .......... .......... .......... .......... 34% 11.3M 52s
173550K .......... .......... .......... .......... .......... 34% 18.5M 52s
173600K .......... .......... .......... .......... .......... 34% 12.3M 52s
173650K .......... .......... .......... .......... .......... 34% 11.8M 52s
173700K .......... .......... .......... .......... .......... 34% 15.0M 52s
173750K .......... .......... .......... .......... .......... 34% 9.31M 52s
173800K .......... .......... .......... .......... .......... 34% 16.8M 52s
173850K .......... .......... .......... .......... .......... 34% 13.8M 52s
173900K .......... .......... .......... .......... .......... 34% 12.5M 52s
173950K .......... .......... .......... .......... .......... 34% 11.2M 52s
174000K .......... .......... .......... .......... .......... 34% 5.88M 52s
174050K .......... .......... .......... .......... .......... 34% 9.76M 52s
174100K .......... .......... .......... .......... .......... 34% 4.72M 52s
174150K .......... .......... .......... .......... .......... 34% 5.39M 52s
174200K .......... .......... .......... .......... .......... 34% 2.49M 52s
174250K .......... .......... .......... .......... .......... 34% 2.43M 52s
174300K .......... .......... .......... .......... .......... 34% 3.40M 52s
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174400K .......... .......... .......... .......... .......... 34% 7.20M 52s
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174500K .......... .......... .......... .......... .......... 34% 9.22M 52s
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174750K .......... .......... .......... .......... .......... 34% 6.02M 52s
174800K .......... .......... .......... .......... .......... 34% 7.19M 52s
174850K .......... .......... .......... .......... .......... 34% 5.23M 52s
174900K .......... .......... .......... .......... .......... 34% 10.7M 52s
174950K .......... .......... .......... .......... .......... 34% 23.6M 52s
175000K .......... .......... .......... .......... .......... 34% 13.6M 52s
175050K .......... .......... .......... .......... .......... 34% 27.2M 52s
175100K .......... .......... .......... .......... .......... 34% 12.1M 52s
175150K .......... .......... .......... .......... .......... 34% 16.4M 52s
175200K .......... .......... .......... .......... .......... 34% 9.41M 52s
175250K .......... .......... .......... .......... .......... 34% 17.7M 52s
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175350K .......... .......... .......... .......... .......... 34% 10.0M 52s
175400K .......... .......... .......... .......... .......... 34% 12.0M 52s
175450K .......... .......... .......... .......... .......... 34% 17.3M 52s
175500K .......... .......... .......... .......... .......... 34% 11.2M 52s
175550K .......... .......... .......... .......... .......... 34% 30.8M 52s
175600K .......... .......... .......... .......... .......... 34% 11.7M 52s
175650K .......... .......... .......... .......... .......... 34% 27.3M 52s
175700K .......... .......... .......... .......... .......... 34% 11.5M 52s
175750K .......... .......... .......... .......... .......... 34% 21.6M 52s
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175850K .......... .......... .......... .......... .......... 34% 13.6M 52s
175900K .......... .......... .......... .......... .......... 34% 19.4M 52s
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176000K .......... .......... .......... .......... .......... 34% 10.8M 51s
176050K .......... .......... .......... .......... .......... 34% 93.7M 51s
176100K .......... .......... .......... .......... .......... 34% 14.2M 51s
176150K .......... .......... .......... .......... .......... 34% 18.0M 51s
176200K .......... .......... .......... .......... .......... 34% 11.3M 51s
176250K .......... .......... .......... .......... .......... 34% 8.76M 51s
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176350K .......... .......... .......... .......... .......... 34% 17.7M 51s
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176450K .......... .......... .......... .......... .......... 34% 8.76M 51s
176500K .......... .......... .......... .......... .......... 34% 6.22M 51s
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176650K .......... .......... .......... .......... .......... 34% 5.37M 51s
176700K .......... .......... .......... .......... .......... 35% 9.67M 51s
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176850K .......... .......... .......... .......... .......... 35% 9.34M 51s
176900K .......... .......... .......... .......... .......... 35% 12.0M 51s
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177000K .......... .......... .......... .......... .......... 35% 9.48M 51s
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177100K .......... .......... .......... .......... .......... 35% 9.73M 51s
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177200K .......... .......... .......... .......... .......... 35% 17.6M 51s
177250K .......... .......... .......... .......... .......... 35% 9.15M 51s
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177500K .......... .......... .......... .......... .......... 35% 9.05M 51s
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177700K .......... .......... .......... .......... .......... 35% 11.9M 51s
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177850K .......... .......... .......... .......... .......... 35% 12.3M 51s
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178000K .......... .......... .......... .......... .......... 35% 11.6M 51s
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178100K .......... .......... .......... .......... .......... 35% 9.10M 51s
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178200K .......... .......... .......... .......... .......... 35% 7.14M 51s
178250K .......... .......... .......... .......... .......... 35% 6.15M 51s
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179000K .......... .......... .......... .......... .......... 35% 15.9M 51s
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179100K .......... .......... .......... .......... .......... 35% 17.7M 51s
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179250K .......... .......... .......... .......... .......... 35% 12.3M 51s
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180000K .......... .......... .......... .......... .......... 35% 9.68M 50s
180050K .......... .......... .......... .......... .......... 35% 11.1M 50s
180100K .......... .......... .......... .......... .......... 35% 18.0M 50s
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181000K .......... .......... .......... .......... .......... 35% 15.1M 50s
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181500K .......... .......... .......... .......... .......... 35% 16.0M 50s
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181900K .......... .......... .......... .......... .......... 36% 6.34M 50s
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182150K .......... .......... .......... .......... .......... 36% 8.70M 50s
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182250K .......... .......... .......... .......... .......... 36% 7.39M 50s
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183000K .......... .......... .......... .......... .......... 36% 4.15M 50s
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183150K .......... .......... .......... .......... .......... 36% 28.9M 50s
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183250K .......... .......... .......... .......... .......... 36% 32.4M 50s
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183950K .......... .......... .......... .......... .......... 36% 6.14M 49s
184000K .......... .......... .......... .......... .......... 36% 17.6M 49s
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184100K .......... .......... .......... .......... .......... 36% 8.27M 49s
184150K .......... .......... .......... .......... .......... 36% 9.69M 49s
184200K .......... .......... .......... .......... .......... 36% 6.45M 49s
184250K .......... .......... .......... .......... .......... 36% 12.3M 49s
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184750K .......... .......... .......... .......... .......... 36% 6.38M 49s
184800K .......... .......... .......... .......... .......... 36% 9.20M 49s
184850K .......... .......... .......... .......... .......... 36% 6.96M 49s
184900K .......... .......... .......... .......... .......... 36% 17.3M 49s
184950K .......... .......... .......... .......... .......... 36% 8.79M 49s
185000K .......... .......... .......... .......... .......... 36% 11.6M 49s
185050K .......... .......... .......... .......... .......... 36% 8.90M 49s
185100K .......... .......... .......... .......... .......... 36% 11.0M 49s
185150K .......... .......... .......... .......... .......... 36% 6.21M 49s
185200K .......... .......... .......... .......... .......... 36% 4.73M 49s
185250K .......... .......... .......... .......... .......... 36% 9.03M 49s
185300K .......... .......... .......... .......... .......... 36% 7.36M 49s
185350K .......... .......... .......... .......... .......... 36% 6.27M 49s
185400K .......... .......... .......... .......... .......... 36% 6.19M 49s
185450K .......... .......... .......... .......... .......... 36% 4.34M 49s
185500K .......... .......... .......... .......... .......... 36% 3.75M 49s
185550K .......... .......... .......... .......... .......... 36% 3.75M 49s
185600K .......... .......... .......... .......... .......... 36% 3.74M 49s
185650K .......... .......... .......... .......... .......... 36% 4.14M 49s
185700K .......... .......... .......... .......... .......... 36% 7.03M 49s
185750K .......... .......... .......... .......... .......... 36% 11.2M 49s
185800K .......... .......... .......... .......... .......... 36% 17.2M 49s
185850K .......... .......... .......... .......... .......... 36% 12.0M 49s
185900K .......... .......... .......... .......... .......... 36% 7.29M 49s
185950K .......... .......... .......... .......... .......... 36% 7.18M 49s
186000K .......... .......... .......... .......... .......... 36% 6.51M 49s
186050K .......... .......... .......... .......... .......... 36% 6.16M 49s
186100K .......... .......... .......... .......... .......... 36% 7.31M 49s
186150K .......... .......... .......... .......... .......... 36% 12.0M 49s
186200K .......... .......... .......... .......... .......... 36% 9.24M 49s
186250K .......... .......... .......... .......... .......... 36% 12.4M 49s
186300K .......... .......... .......... .......... .......... 36% 12.3M 49s
186350K .......... .......... .......... .......... .......... 36% 25.4M 49s
186400K .......... .......... .......... .......... .......... 36% 92.5M 49s
186450K .......... .......... .......... .......... .......... 36% 22.0M 49s
186500K .......... .......... .......... .......... .......... 36% 20.4M 49s
186550K .......... .......... .......... .......... .......... 36% 24.9M 49s
186600K .......... .......... .......... .......... .......... 36% 25.6M 49s
186650K .......... .......... .......... .......... .......... 36% 38.0M 49s
186700K .......... .......... .......... .......... .......... 36% 18.7M 49s
186750K .......... .......... .......... .......... .......... 36% 17.0M 49s
186800K .......... .......... .......... .......... .......... 37% 7.57M 49s
186850K .......... .......... .......... .......... .......... 37% 13.2M 49s
186900K .......... .......... .......... .......... .......... 37% 9.16M 49s
186950K .......... .......... .......... .......... .......... 37% 9.50M 49s
187000K .......... .......... .......... .......... .......... 37% 10.9M 49s
187050K .......... .......... .......... .......... .......... 37% 9.20M 49s
187100K .......... .......... .......... .......... .......... 37% 12.4M 49s
187150K .......... .......... .......... .......... .......... 37% 11.6M 49s
187200K .......... .......... .......... .......... .......... 37% 11.2M 49s
187250K .......... .......... .......... .......... .......... 37% 10.6M 49s
187300K .......... .......... .......... .......... .......... 37% 12.9M 49s
187350K .......... .......... .......... .......... .......... 37% 9.03M 49s
187400K .......... .......... .......... .......... .......... 37% 9.21M 49s
187450K .......... .......... .......... .......... .......... 37% 9.43M 49s
187500K .......... .......... .......... .......... .......... 37% 12.1M 49s
187550K .......... .......... .......... .......... .......... 37% 6.42M 49s
187600K .......... .......... .......... .......... .......... 37% 6.80M 49s
187650K .......... .......... .......... .......... .......... 37% 7.30M 49s
187700K .......... .......... .......... .......... .......... 37% 7.34M 49s
187750K .......... .......... .......... .......... .......... 37% 9.14M 49s
187800K .......... .......... .......... .......... .......... 37% 15.3M 49s
187850K .......... .......... .......... .......... .......... 37% 17.2M 49s
187900K .......... .......... .......... .......... .......... 37% 17.5M 49s
187950K .......... .......... .......... .......... .......... 37% 15.1M 49s
188000K .......... .......... .......... .......... .......... 37% 8.92M 49s
188050K .......... .......... .......... .......... .......... 37% 19.8M 49s
188100K .......... .......... .......... .......... .......... 37% 7.04M 49s
188150K .......... .......... .......... .......... .......... 37% 11.3M 49s
188200K .......... .......... .......... .......... .......... 37% 11.7M 49s
188250K .......... .......... .......... .......... .......... 37% 17.3M 49s
188300K .......... .......... .......... .......... .......... 37% 12.0M 49s
188350K .......... .......... .......... .......... .......... 37% 10.7M 48s
188400K .......... .......... .......... .......... .......... 37% 7.23M 48s
188450K .......... .......... .......... .......... .......... 37% 8.99M 48s
188500K .......... .......... .......... .......... .......... 37% 13.1M 48s
188550K .......... .......... .......... .......... .......... 37% 9.55M 48s
188600K .......... .......... .......... .......... .......... 37% 11.5M 48s
188650K .......... .......... .......... .......... .......... 37% 11.6M 48s
188700K .......... .......... .......... .......... .......... 37% 9.28M 48s
188750K .......... .......... .......... .......... .......... 37% 11.2M 48s
188800K .......... .......... .......... .......... .......... 37% 5.27M 48s
188850K .......... .......... .......... .......... .......... 37% 5.27M 48s
188900K .......... .......... .......... .......... .......... 37% 7.63M 48s
188950K .......... .......... .......... .......... .......... 37% 5.43M 48s
189000K .......... .......... .......... .......... .......... 37% 9.41M 48s
189050K .......... .......... .......... .......... .......... 37% 6.30M 48s
189100K .......... .......... .......... .......... .......... 37% 4.64M 48s
189150K .......... .......... .......... .......... .......... 37% 7.30M 48s
189200K .......... .......... .......... .......... .......... 37% 11.5M 48s
189250K .......... .......... .......... .......... .......... 37% 12.3M 48s
189300K .......... .......... .......... .......... .......... 37% 11.6M 48s
189350K .......... .......... .......... .......... .......... 37% 11.7M 48s
189400K .......... .......... .......... .......... .......... 37% 7.63M 48s
189450K .......... .......... .......... .......... .......... 37% 9.19M 48s
189500K .......... .......... .......... .......... .......... 37% 11.5M 48s
189550K .......... .......... .......... .......... .......... 37% 9.45M 48s
189600K .......... .......... .......... .......... .......... 37% 7.10M 48s
189650K .......... .......... .......... .......... .......... 37% 11.2M 48s
189700K .......... .......... .......... .......... .......... 37% 11.3M 48s
189750K .......... .......... .......... .......... .......... 37% 12.6M 48s
189800K .......... .......... .......... .......... .......... 37% 12.0M 48s
189850K .......... .......... .......... .......... .......... 37% 7.38M 48s
189900K .......... .......... .......... .......... .......... 37% 11.5M 48s
189950K .......... .......... .......... .......... .......... 37% 10.6M 48s
190000K .......... .......... .......... .......... .......... 37% 13.1M 48s
190050K .......... .......... .......... .......... .......... 37% 9.32M 48s
190100K .......... .......... .......... .......... .......... 37% 9.29M 48s
190150K .......... .......... .......... .......... .......... 37% 15.0M 48s
190200K .......... .......... .......... .......... .......... 37% 14.1M 48s
190250K .......... .......... .......... .......... .......... 37% 16.3M 48s
190300K .......... .......... .......... .......... .......... 37% 10.2M 48s
190350K .......... .......... .......... .......... .......... 37% 10.9M 48s
190400K .......... .......... .......... .......... .......... 37% 21.9M 48s
190450K .......... .......... .......... .......... .......... 37% 15.0M 48s
190500K .......... .......... .......... .......... .......... 37% 12.3M 48s
190550K .......... .......... .......... .......... .......... 37% 12.1M 48s
190600K .......... .......... .......... .......... .......... 37% 11.6M 48s
190650K .......... .......... .......... .......... .......... 37% 147M 48s
190700K .......... .......... .......... .......... .......... 37% 33.8M 48s
190750K .......... .......... .......... .......... .......... 37% 8.72M 48s
190800K .......... .......... .......... .......... .......... 37% 145M 48s
190850K .......... .......... .......... .......... .......... 37% 9.54M 48s
190900K .......... .......... .......... .......... .......... 37% 40.8M 48s
190950K .......... .......... .......... .......... .......... 37% 10.8M 48s
191000K .......... .......... .......... .......... .......... 37% 12.0M 48s
191050K .......... .......... .......... .......... .......... 37% 12.8M 48s
191100K .......... .......... .......... .......... .......... 37% 12.2M 48s
191150K .......... .......... .......... .......... .......... 37% 15.7M 48s
191200K .......... .......... .......... .......... .......... 37% 17.1M 48s
191250K .......... .......... .......... .......... .......... 37% 11.8M 48s
191300K .......... .......... .......... .......... .......... 37% 9.70M 48s
191350K .......... .......... .......... .......... .......... 37% 14.8M 48s
191400K .......... .......... .......... .......... .......... 37% 8.38M 48s
191450K .......... .......... .......... .......... .......... 37% 9.63M 48s
191500K .......... .......... .......... .......... .......... 37% 18.4M 48s
191550K .......... .......... .......... .......... .......... 37% 15.8M 48s
191600K .......... .......... .......... .......... .......... 37% 11.5M 48s
191650K .......... .......... .......... .......... .......... 37% 16.9M 48s
191700K .......... .......... .......... .......... .......... 37% 11.8M 48s
191750K .......... .......... .......... .......... .......... 37% 15.0M 48s
191800K .......... .......... .......... .......... .......... 37% 11.1M 48s
191850K .......... .......... .......... .......... .......... 38% 15.8M 48s
191900K .......... .......... .......... .......... .......... 38% 18.0M 48s
191950K .......... .......... .......... .......... .......... 38% 11.4M 48s
192000K .......... .......... .......... .......... .......... 38% 12.3M 48s
192050K .......... .......... .......... .......... .......... 38% 13.0M 48s
192100K .......... .......... .......... .......... .......... 38% 16.5M 48s
192150K .......... .......... .......... .......... .......... 38% 9.03M 48s
192200K .......... .......... .......... .......... .......... 38% 9.87M 48s
192250K .......... .......... .......... .......... .......... 38% 11.8M 47s
192300K .......... .......... .......... .......... .......... 38% 12.0M 47s
192350K .......... .......... .......... .......... .......... 38% 15.3M 47s
192400K .......... .......... .......... .......... .......... 38% 11.9M 47s
192450K .......... .......... .......... .......... .......... 38% 15.0M 47s
192500K .......... .......... .......... .......... .......... 38% 12.1M 47s
192550K .......... .......... .......... .......... .......... 38% 25.0M 47s
192600K .......... .......... .......... .......... .......... 38% 11.9M 47s
192650K .......... .......... .......... .......... .......... 38% 9.38M 47s
192700K .......... .......... .......... .......... .......... 38% 30.3M 47s
192750K .......... .......... .......... .......... .......... 38% 18.4M 47s
192800K .......... .......... .......... .......... .......... 38% 8.77M 47s
192850K .......... .......... .......... .......... .......... 38% 12.9M 47s
192900K .......... .......... .......... .......... .......... 38% 25.8M 47s
192950K .......... .......... .......... .......... .......... 38% 12.4M 47s
193000K .......... .......... .......... .......... .......... 38% 12.7M 47s
193050K .......... .......... .......... .......... .......... 38% 14.6M 47s
193100K .......... .......... .......... .......... .......... 38% 10.7M 47s
193150K .......... .......... .......... .......... .......... 38% 11.5M 47s
193200K .......... .......... .......... .......... .......... 38% 11.4M 47s
193250K .......... .......... .......... .......... .......... 38% 17.2M 47s
193300K .......... .......... .......... .......... .......... 38% 15.6M 47s
193350K .......... .......... .......... .......... .......... 38% 10.2M 47s
193400K .......... .......... .......... .......... .......... 38% 18.6M 47s
193450K .......... .......... .......... .......... .......... 38% 8.71M 47s
193500K .......... .......... .......... .......... .......... 38% 144M 47s
193550K .......... .......... .......... .......... .......... 38% 13.3M 47s
193600K .......... .......... .......... .......... .......... 38% 9.80M 47s
193650K .......... .......... .......... .......... .......... 38% 11.3M 47s
193700K .......... .......... .......... .......... .......... 38% 6.46M 47s
193750K .......... .......... .......... .......... .......... 38% 12.0M 47s
193800K .......... .......... .......... .......... .......... 38% 17.9M 47s
193850K .......... .......... .......... .......... .......... 38% 8.60M 47s
193900K .......... .......... .......... .......... .......... 38% 11.5M 47s
193950K .......... .......... .......... .......... .......... 38% 5.23M 47s
194000K .......... .......... .......... .......... .......... 38% 7.33M 47s
194050K .......... .......... .......... .......... .......... 38% 9.38M 47s
194100K .......... .......... .......... .......... .......... 38% 5.26M 47s
194150K .......... .......... .......... .......... .......... 38% 9.16M 47s
194200K .......... .......... .......... .......... .......... 38% 7.12M 47s
194250K .......... .......... .......... .......... .......... 38% 5.97M 47s
194300K .......... .......... .......... .......... .......... 38% 8.48M 47s
194350K .......... .......... .......... .......... .......... 38% 7.40M 47s
194400K .......... .......... .......... .......... .......... 38% 10.8M 47s
194450K .......... .......... .......... .......... .......... 38% 9.49M 47s
194500K .......... .......... .......... .......... .......... 38% 13.0M 47s
194550K .......... .......... .......... .......... .......... 38% 11.3M 47s
194600K .......... .......... .......... .......... .......... 38% 11.3M 47s
194650K .......... .......... .......... .......... .......... 38% 11.9M 47s
194700K .......... .......... .......... .......... .......... 38% 9.15M 47s
194750K .......... .......... .......... .......... .......... 38% 17.3M 47s
194800K .......... .......... .......... .......... .......... 38% 18.6M 47s
194850K .......... .......... .......... .......... .......... 38% 8.94M 47s
194900K .......... .......... .......... .......... .......... 38% 11.8M 47s
194950K .......... .......... .......... .......... .......... 38% 17.1M 47s
195000K .......... .......... .......... .......... .......... 38% 12.4M 47s
195050K .......... .......... .......... .......... .......... 38% 12.1M 47s
195100K .......... .......... .......... .......... .......... 38% 9.27M 47s
195150K .......... .......... .......... .......... .......... 38% 12.7M 47s
195200K .......... .......... .......... .......... .......... 38% 17.1M 47s
195250K .......... .......... .......... .......... .......... 38% 9.10M 47s
195300K .......... .......... .......... .......... .......... 38% 13.3M 47s
195350K .......... .......... .......... .......... .......... 38% 12.2M 47s
195400K .......... .......... .......... .......... .......... 38% 11.6M 47s
195450K .......... .......... .......... .......... .......... 38% 15.5M 47s
195500K .......... .......... .......... .......... .......... 38% 8.95M 47s
195550K .......... .......... .......... .......... .......... 38% 27.3M 47s
195600K .......... .......... .......... .......... .......... 38% 12.5M 47s
195650K .......... .......... .......... .......... .......... 38% 12.4M 47s
195700K .......... .......... .......... .......... .......... 38% 11.3M 47s
195750K .......... .......... .......... .......... .......... 38% 12.5M 47s
195800K .......... .......... .......... .......... .......... 38% 11.8M 47s
195850K .......... .......... .......... .......... .......... 38% 9.09M 47s
195900K .......... .......... .......... .......... .......... 38% 8.83M 47s
195950K .......... .......... .......... .......... .......... 38% 11.1M 47s
196000K .......... .......... .......... .......... .......... 38% 9.13M 47s
196050K .......... .......... .......... .......... .......... 38% 9.47M 47s
196100K .......... .......... .......... .......... .......... 38% 16.3M 47s
196150K .......... .......... .......... .......... .......... 38% 11.8M 47s
196200K .......... .......... .......... .......... .......... 38% 17.1M 46s
196250K .......... .......... .......... .......... .......... 38% 11.3M 46s
196300K .......... .......... .......... .......... .......... 38% 18.3M 46s
196350K .......... .......... .......... .......... .......... 38% 16.9M 46s
196400K .......... .......... .......... .......... .......... 38% 18.1M 46s
196450K .......... .......... .......... .......... .......... 38% 13.0M 46s
196500K .......... .......... .......... .......... .......... 38% 17.4M 46s
196550K .......... .......... .......... .......... .......... 38% 16.9M 46s
196600K .......... .......... .......... .......... .......... 38% 17.2M 46s
196650K .......... .......... .......... .......... .......... 38% 16.6M 46s
196700K .......... .......... .......... .......... .......... 38% 17.9M 46s
196750K .......... .......... .......... .......... .......... 38% 250M 46s
196800K .......... .......... .......... .......... .......... 38% 8.12M 46s
196850K .......... .......... .......... .......... .......... 38% 178M 46s
196900K .......... .......... .......... .......... .......... 39% 10.1M 46s
196950K .......... .......... .......... .......... .......... 39% 12.7M 46s
197000K .......... .......... .......... .......... .......... 39% 12.5M 46s
197050K .......... .......... .......... .......... .......... 39% 12.0M 46s
197100K .......... .......... .......... .......... .......... 39% 12.0M 46s
197150K .......... .......... .......... .......... .......... 39% 17.4M 46s
197200K .......... .......... .......... .......... .......... 39% 9.36M 46s
197250K .......... .......... .......... .......... .......... 39% 12.5M 46s
197300K .......... .......... .......... .......... .......... 39% 18.4M 46s
197350K .......... .......... .......... .......... .......... 39% 12.1M 46s
197400K .......... .......... .......... .......... .......... 39% 16.2M 46s
197450K .......... .......... .......... .......... .......... 39% 8.55M 46s
197500K .......... .......... .......... .......... .......... 39% 17.8M 46s
197550K .......... .......... .......... .......... .......... 39% 16.5M 46s
197600K .......... .......... .......... .......... .......... 39% 15.7M 46s
197650K .......... .......... .......... .......... .......... 39% 9.36M 46s
197700K .......... .......... .......... .......... .......... 39% 11.5M 46s
197750K .......... .......... .......... .......... .......... 39% 13.1M 46s
197800K .......... .......... .......... .......... .......... 39% 12.6M 46s
197850K .......... .......... .......... .......... .......... 39% 16.9M 46s
197900K .......... .......... .......... .......... .......... 39% 22.6M 46s
197950K .......... .......... .......... .......... .......... 39% 10.1M 46s
198000K .......... .......... .......... .......... .......... 39% 12.2M 46s
198050K .......... .......... .......... .......... .......... 39% 16.5M 46s
198100K .......... .......... .......... .......... .......... 39% 23.1M 46s
198150K .......... .......... .......... .......... .......... 39% 23.0M 46s
198200K .......... .......... .......... .......... .......... 39% 18.6M 46s
198250K .......... .......... .......... .......... .......... 39% 11.9M 46s
198300K .......... .......... .......... .......... .......... 39% 32.6M 46s
198350K .......... .......... .......... .......... .......... 39% 17.6M 46s
198400K .......... .......... .......... .......... .......... 39% 30.1M 46s
198450K .......... .......... .......... .......... .......... 39% 10.9M 46s
198500K .......... .......... .......... .......... .......... 39% 18.7M 46s
198550K .......... .......... .......... .......... .......... 39% 28.8M 46s
198600K .......... .......... .......... .......... .......... 39% 13.6M 46s
198650K .......... .......... .......... .......... .......... 39% 18.4M 46s
198700K .......... .......... .......... .......... .......... 39% 16.2M 46s
198750K .......... .......... .......... .......... .......... 39% 12.4M 46s
198800K .......... .......... .......... .......... .......... 39% 8.46M 46s
198850K .......... .......... .......... .......... .......... 39% 18.7M 46s
198900K .......... .......... .......... .......... .......... 39% 15.4M 46s
198950K .......... .......... .......... .......... .......... 39% 11.3M 46s
199000K .......... .......... .......... .......... .......... 39% 13.2M 46s
199050K .......... .......... .......... .......... .......... 39% 19.5M 46s
199100K .......... .......... .......... .......... .......... 39% 8.55M 46s
199150K .......... .......... .......... .......... .......... 39% 29.1M 46s
199200K .......... .......... .......... .......... .......... 39% 15.7M 46s
199250K .......... .......... .......... .......... .......... 39% 15.9M 46s
199300K .......... .......... .......... .......... .......... 39% 14.8M 46s
199350K .......... .......... .......... .......... .......... 39% 16.6M 46s
199400K .......... .......... .......... .......... .......... 39% 18.3M 46s
199450K .......... .......... .......... .......... .......... 39% 17.9M 46s
199500K .......... .......... .......... .......... .......... 39% 16.6M 46s
199550K .......... .......... .......... .......... .......... 39% 12.9M 46s
199600K .......... .......... .......... .......... .......... 39% 9.40M 46s
199650K .......... .......... .......... .......... .......... 39% 128M 46s
199700K .......... .......... .......... .......... .......... 39% 18.7M 46s
199750K .......... .......... .......... .......... .......... 39% 29.0M 45s
199800K .......... .......... .......... .......... .......... 39% 17.9M 45s
199850K .......... .......... .......... .......... .......... 39% 12.6M 45s
199900K .......... .......... .......... .......... .......... 39% 15.8M 45s
199950K .......... .......... .......... .......... .......... 39% 27.6M 45s
200000K .......... .......... .......... .......... .......... 39% 19.1M 45s
200050K .......... .......... .......... .......... .......... 39% 18.7M 45s
200100K .......... .......... .......... .......... .......... 39% 14.0M 45s
200150K .......... .......... .......... .......... .......... 39% 17.4M 45s
200200K .......... .......... .......... .......... .......... 39% 27.0M 45s
200250K .......... .......... .......... .......... .......... 39% 36.8M 45s
200300K .......... .......... .......... .......... .......... 39% 12.4M 45s
200350K .......... .......... .......... .......... .......... 39% 7.33M 45s
200400K .......... .......... .......... .......... .......... 39% 36.0M 45s
200450K .......... .......... .......... .......... .......... 39% 32.6M 45s
200500K .......... .......... .......... .......... .......... 39% 18.2M 45s
200550K .......... .......... .......... .......... .......... 39% 11.8M 45s
200600K .......... .......... .......... .......... .......... 39% 17.4M 45s
200650K .......... .......... .......... .......... .......... 39% 12.3M 45s
200700K .......... .......... .......... .......... .......... 39% 13.8M 45s
200750K .......... .......... .......... .......... .......... 39% 18.1M 45s
200800K .......... .......... .......... .......... .......... 39% 11.7M 45s
200850K .......... .......... .......... .......... .......... 39% 25.4M 45s
200900K .......... .......... .......... .......... .......... 39% 15.3M 45s
200950K .......... .......... .......... .......... .......... 39% 12.4M 45s
201000K .......... .......... .......... .......... .......... 39% 7.34M 45s
201050K .......... .......... .......... .......... .......... 39% 19.1M 45s
201100K .......... .......... .......... .......... .......... 39% 26.2M 45s
201150K .......... .......... .......... .......... .......... 39% 15.5M 45s
201200K .......... .......... .......... .......... .......... 39% 10.8M 45s
201250K .......... .......... .......... .......... .......... 39% 16.0M 45s
201300K .......... .......... .......... .......... .......... 39% 15.3M 45s
201350K .......... .......... .......... .......... .......... 39% 11.7M 45s
201400K .......... .......... .......... .......... .......... 39% 33.7M 45s
201450K .......... .......... .......... .......... .......... 39% 17.7M 45s
201500K .......... .......... .......... .......... .......... 39% 17.0M 45s
201550K .......... .......... .......... .......... .......... 39% 27.3M 45s
201600K .......... .......... .......... .......... .......... 39% 17.4M 45s
201650K .......... .......... .......... .......... .......... 39% 14.8M 45s
201700K .......... .......... .......... .......... .......... 39% 19.8M 45s
201750K .......... .......... .......... .......... .......... 39% 107M 45s
201800K .......... .......... .......... .......... .......... 39% 19.5M 45s
201850K .......... .......... .......... .......... .......... 39% 17.2M 45s
201900K .......... .......... .......... .......... .......... 39% 37.0M 45s
201950K .......... .......... .......... .......... .......... 40% 6.95M 45s
202000K .......... .......... .......... .......... .......... 40% 159M 45s
202050K .......... .......... .......... .......... .......... 40% 214M 45s
202100K .......... .......... .......... .......... .......... 40% 13.4M 45s
202150K .......... .......... .......... .......... .......... 40% 21.4M 45s
202200K .......... .......... .......... .......... .......... 40% 18.0M 45s
202250K .......... .......... .......... .......... .......... 40% 24.2M 45s
202300K .......... .......... .......... .......... .......... 40% 38.6M 45s
202350K .......... .......... .......... .......... .......... 40% 16.8M 45s
202400K .......... .......... .......... .......... .......... 40% 23.0M 45s
202450K .......... .......... .......... .......... .......... 40% 21.1M 45s
202500K .......... .......... .......... .......... .......... 40% 19.3M 45s
202550K .......... .......... .......... .......... .......... 40% 21.3M 45s
202600K .......... .......... .......... .......... .......... 40% 34.8M 45s
202650K .......... .......... .......... .......... .......... 40% 25.1M 45s
202700K .......... .......... .......... .......... .......... 40% 20.6M 45s
202750K .......... .......... .......... .......... .......... 40% 26.1M 45s
202800K .......... .......... .......... .......... .......... 40% 21.8M 45s
202850K .......... .......... .......... .......... .......... 40% 27.4M 45s
202900K .......... .......... .......... .......... .......... 40% 8.76M 45s
202950K .......... .......... .......... .......... .......... 40% 12.0M 45s
203000K .......... .......... .......... .......... .......... 40% 19.8M 45s
203050K .......... .......... .......... .......... .......... 40% 17.3M 45s
203100K .......... .......... .......... .......... .......... 40% 11.4M 45s
203150K .......... .......... .......... .......... .......... 40% 27.5M 45s
203200K .......... .......... .......... .......... .......... 40% 11.7M 44s
203250K .......... .......... .......... .......... .......... 40% 28.3M 44s
203300K .......... .......... .......... .......... .......... 40% 11.5M 44s
203350K .......... .......... .......... .......... .......... 40% 11.4M 44s
203400K .......... .......... .......... .......... .......... 40% 23.0M 44s
203450K .......... .......... .......... .......... .......... 40% 15.4M 44s
203500K .......... .......... .......... .......... .......... 40% 17.4M 44s
203550K .......... .......... .......... .......... .......... 40% 18.5M 44s
203600K .......... .......... .......... .......... .......... 40% 14.4M 44s
203650K .......... .......... .......... .......... .......... 40% 18.0M 44s
203700K .......... .......... .......... .......... .......... 40% 15.6M 44s
203750K .......... .......... .......... .......... .......... 40% 10.1M 44s
203800K .......... .......... .......... .......... .......... 40% 18.1M 44s
203850K .......... .......... .......... .......... .......... 40% 12.0M 44s
203900K .......... .......... .......... .......... .......... 40% 19.8M 44s
203950K .......... .......... .......... .......... .......... 40% 9.30M 44s
204000K .......... .......... .......... .......... .......... 40% 14.2M 44s
204050K .......... .......... .......... .......... .......... 40% 34.9M 44s
204100K .......... .......... .......... .......... .......... 40% 16.3M 44s
204150K .......... .......... .......... .......... .......... 40% 11.2M 44s
204200K .......... .......... .......... .......... .......... 40% 16.9M 44s
204250K .......... .......... .......... .......... .......... 40% 15.0M 44s
204300K .......... .......... .......... .......... .......... 40% 18.7M 44s
204350K .......... .......... .......... .......... .......... 40% 9.01M 44s
204400K .......... .......... .......... .......... .......... 40% 15.9M 44s
204450K .......... .......... .......... .......... .......... 40% 10.6M 44s
204500K .......... .......... .......... .......... .......... 40% 19.3M 44s
204550K .......... .......... .......... .......... .......... 40% 14.8M 44s
204600K .......... .......... .......... .......... .......... 40% 14.2M 44s
204650K .......... .......... .......... .......... .......... 40% 18.8M 44s
204700K .......... .......... .......... .......... .......... 40% 12.1M 44s
204750K .......... .......... .......... .......... .......... 40% 31.4M 44s
204800K .......... .......... .......... .......... .......... 40% 12.8M 44s
204850K .......... .......... .......... .......... .......... 40% 10.7M 44s
204900K .......... .......... .......... .......... .......... 40% 16.1M 44s
204950K .......... .......... .......... .......... .......... 40% 16.2M 44s
205000K .......... .......... .......... .......... .......... 40% 15.2M 44s
205050K .......... .......... .......... .......... .......... 40% 9.60M 44s
205100K .......... .......... .......... .......... .......... 40% 12.6M 44s
205150K .......... .......... .......... .......... .......... 40% 15.5M 44s
205200K .......... .......... .......... .......... .......... 40% 15.6M 44s
205250K .......... .......... .......... .......... .......... 40% 11.4M 44s
205300K .......... .......... .......... .......... .......... 40% 16.4M 44s
205350K .......... .......... .......... .......... .......... 40% 9.33M 44s
205400K .......... .......... .......... .......... .......... 40% 9.20M 44s
205450K .......... .......... .......... .......... .......... 40% 11.8M 44s
205500K .......... .......... .......... .......... .......... 40% 10.7M 44s
205550K .......... .......... .......... .......... .......... 40% 21.6M 44s
205600K .......... .......... .......... .......... .......... 40% 17.7M 44s
205650K .......... .......... .......... .......... .......... 40% 9.00M 44s
205700K .......... .......... .......... .......... .......... 40% 126M 44s
205750K .......... .......... .......... .......... .......... 40% 26.9M 44s
205800K .......... .......... .......... .......... .......... 40% 22.1M 44s
205850K .......... .......... .......... .......... .......... 40% 22.5M 44s
205900K .......... .......... .......... .......... .......... 40% 22.4M 44s
205950K .......... .......... .......... .......... .......... 40% 21.4M 44s
206000K .......... .......... .......... .......... .......... 40% 23.6M 44s
206050K .......... .......... .......... .......... .......... 40% 34.0M 44s
206100K .......... .......... .......... .......... .......... 40% 16.2M 44s
206150K .......... .......... .......... .......... .......... 40% 21.3M 44s
206200K .......... .......... .......... .......... .......... 40% 17.1M 44s
206250K .......... .......... .......... .......... .......... 40% 28.5M 44s
206300K .......... .......... .......... .......... .......... 40% 27.1M 44s
206350K .......... .......... .......... .......... .......... 40% 29.0M 44s
206400K .......... .......... .......... .......... .......... 40% 27.3M 44s
206450K .......... .......... .......... .......... .......... 40% 13.1M 44s
206500K .......... .......... .......... .......... .......... 40% 36.0M 44s
206550K .......... .......... .......... .......... .......... 40% 18.8M 44s
206600K .......... .......... .......... .......... .......... 40% 17.5M 44s
206650K .......... .......... .......... .......... .......... 40% 9.19M 44s
206700K .......... .......... .......... .......... .......... 40% 17.1M 44s
206750K .......... .......... .......... .......... .......... 40% 29.1M 44s
206800K .......... .......... .......... .......... .......... 40% 49.8M 44s
206850K .......... .......... .......... .......... .......... 40% 15.2M 44s
206900K .......... .......... .......... .......... .......... 40% 14.7M 43s
206950K .......... .......... .......... .......... .......... 40% 15.1M 43s
207000K .......... .......... .......... .......... .......... 41% 21.4M 43s
207050K .......... .......... .......... .......... .......... 41% 12.7M 43s
207100K .......... .......... .......... .......... .......... 41% 16.3M 43s
207150K .......... .......... .......... .......... .......... 41% 15.6M 43s
207200K .......... .......... .......... .......... .......... 41% 16.8M 43s
207250K .......... .......... .......... .......... .......... 41% 12.6M 43s
207300K .......... .......... .......... .......... .......... 41% 26.5M 43s
207350K .......... .......... .......... .......... .......... 41% 9.23M 43s
207400K .......... .......... .......... .......... .......... 41% 18.3M 43s
207450K .......... .......... .......... .......... .......... 41% 11.5M 43s
207500K .......... .......... .......... .......... .......... 41% 36.6M 43s
207550K .......... .......... .......... .......... .......... 41% 96.3M 43s
207600K .......... .......... .......... .......... .......... 41% 12.1M 43s
207650K .......... .......... .......... .......... .......... 41% 30.8M 43s
207700K .......... .......... .......... .......... .......... 41% 14.9M 43s
207750K .......... .......... .......... .......... .......... 41% 32.5M 43s
207800K .......... .......... .......... .......... .......... 41% 22.3M 43s
207850K .......... .......... .......... .......... .......... 41% 19.2M 43s
207900K .......... .......... .......... .......... .......... 41% 18.8M 43s
207950K .......... .......... .......... .......... .......... 41% 19.0M 43s
208000K .......... .......... .......... .......... .......... 41% 27.2M 43s
208050K .......... .......... .......... .......... .......... 41% 31.0M 43s
208100K .......... .......... .......... .......... .......... 41% 22.2M 43s
208150K .......... .......... .......... .......... .......... 41% 20.2M 43s
208200K .......... .......... .......... .......... .......... 41% 17.0M 43s
208250K .......... .......... .......... .......... .......... 41% 28.0M 43s
208300K .......... .......... .......... .......... .......... 41% 11.8M 43s
208350K .......... .......... .......... .......... .......... 41% 40.1M 43s
208400K .......... .......... .......... .......... .......... 41% 18.5M 43s
208450K .......... .......... .......... .......... .......... 41% 18.9M 43s
208500K .......... .......... .......... .......... .......... 41% 13.9M 43s
208550K .......... .......... .......... .......... .......... 41% 21.6M 43s
208600K .......... .......... .......... .......... .......... 41% 26.2M 43s
208650K .......... .......... .......... .......... .......... 41% 23.6M 43s
208700K .......... .......... .......... .......... .......... 41% 27.3M 43s
208750K .......... .......... .......... .......... .......... 41% 26.5M 43s
208800K .......... .......... .......... .......... .......... 41% 21.7M 43s
208850K .......... .......... .......... .......... .......... 41% 11.7M 43s
208900K .......... .......... .......... .......... .......... 41% 19.0M 43s
208950K .......... .......... .......... .......... .......... 41% 19.1M 43s
209000K .......... .......... .......... .......... .......... 41% 26.2M 43s
209050K .......... .......... .......... .......... .......... 41% 24.6M 43s
209100K .......... .......... .......... .......... .......... 41% 18.6M 43s
209150K .......... .......... .......... .......... .......... 41% 19.8M 43s
209200K .......... .......... .......... .......... .......... 41% 12.0M 43s
209250K .......... .......... .......... .......... .......... 41% 12.6M 43s
209300K .......... .......... .......... .......... .......... 41% 105M 43s
209350K .......... .......... .......... .......... .......... 41% 10.5M 43s
209400K .......... .......... .......... .......... .......... 41% 17.5M 43s
209450K .......... .......... .......... .......... .......... 41% 14.9M 43s
209500K .......... .......... .......... .......... .......... 41% 15.4M 43s
209550K .......... .......... .......... .......... .......... 41% 18.0M 43s
209600K .......... .......... .......... .......... .......... 41% 17.3M 43s
209650K .......... .......... .......... .......... .......... 41% 12.3M 43s
209700K .......... .......... .......... .......... .......... 41% 12.3M 43s
209750K .......... .......... .......... .......... .......... 41% 17.2M 43s
209800K .......... .......... .......... .......... .......... 41% 18.1M 43s
209850K .......... .......... .......... .......... .......... 41% 9.01M 43s
209900K .......... .......... .......... .......... .......... 41% 10.8M 43s
209950K .......... .......... .......... .......... .......... 41% 31.7M 43s
210000K .......... .......... .......... .......... .......... 41% 16.9M 43s
210050K .......... .......... .......... .......... .......... 41% 30.4M 43s
210100K .......... .......... .......... .......... .......... 41% 14.0M 43s
210150K .......... .......... .......... .......... .......... 41% 30.4M 43s
210200K .......... .......... .......... .......... .......... 41% 11.3M 43s
210250K .......... .......... .......... .......... .......... 41% 18.1M 43s
210300K .......... .......... .......... .......... .......... 41% 18.1M 43s
210350K .......... .......... .......... .......... .......... 41% 29.3M 43s
210400K .......... .......... .......... .......... .......... 41% 13.1M 43s
210450K .......... .......... .......... .......... .......... 41% 20.1M 43s
210500K .......... .......... .......... .......... .......... 41% 20.7M 43s
210550K .......... .......... .......... .......... .......... 41% 15.6M 42s
210600K .......... .......... .......... .......... .......... 41% 12.4M 42s
210650K .......... .......... .......... .......... .......... 41% 8.99M 42s
210700K .......... .......... .......... .......... .......... 41% 19.0M 42s
210750K .......... .......... .......... .......... .......... 41% 16.8M 42s
210800K .......... .......... .......... .......... .......... 41% 17.2M 42s
210850K .......... .......... .......... .......... .......... 41% 18.3M 42s
210900K .......... .......... .......... .......... .......... 41% 12.2M 42s
210950K .......... .......... .......... .......... .......... 41% 15.8M 42s
211000K .......... .......... .......... .......... .......... 41% 15.2M 42s
211050K .......... .......... .......... .......... .......... 41% 17.2M 42s
211100K .......... .......... .......... .......... .......... 41% 11.4M 42s
211150K .......... .......... .......... .......... .......... 41% 12.7M 42s
211200K .......... .......... .......... .......... .......... 41% 13.1M 42s
211250K .......... .......... .......... .......... .......... 41% 8.89M 42s
211300K .......... .......... .......... .......... .......... 41% 9.19M 42s
211350K .......... .......... .......... .......... .......... 41% 11.4M 42s
211400K .......... .......... .......... .......... .......... 41% 11.0M 42s
211450K .......... .......... .......... .......... .......... 41% 16.8M 42s
211500K .......... .......... .......... .......... .......... 41% 11.9M 42s
211550K .......... .......... .......... .......... .......... 41% 9.13M 42s
211600K .......... .......... .......... .......... .......... 41% 12.2M 42s
211650K .......... .......... .......... .......... .......... 41% 15.9M 42s
211700K .......... .......... .......... .......... .......... 41% 12.2M 42s
211750K .......... .......... .......... .......... .......... 41% 10.5M 42s
211800K .......... .......... .......... .......... .......... 41% 18.5M 42s
211850K .......... .......... .......... .......... .......... 41% 17.8M 42s
211900K .......... .......... .......... .......... .......... 41% 97.7M 42s
211950K .......... .......... .......... .......... .......... 41% 9.74M 42s
212000K .......... .......... .......... .......... .......... 41% 18.8M 42s
212050K .......... .......... .......... .......... .......... 42% 19.6M 42s
212100K .......... .......... .......... .......... .......... 42% 12.1M 42s
212150K .......... .......... .......... .......... .......... 42% 11.7M 42s
212200K .......... .......... .......... .......... .......... 42% 12.5M 42s
212250K .......... .......... .......... .......... .......... 42% 17.3M 42s
212300K .......... .......... .......... .......... .......... 42% 9.10M 42s
212350K .......... .......... .......... .......... .......... 42% 11.8M 42s
212400K .......... .......... .......... .......... .......... 42% 17.4M 42s
212450K .......... .......... .......... .......... .......... 42% 9.37M 42s
212500K .......... .......... .......... .......... .......... 42% 17.1M 42s
212550K .......... .......... .......... .......... .......... 42% 8.99M 42s
212600K .......... .......... .......... .......... .......... 42% 9.24M 42s
212650K .......... .......... .......... .......... .......... 42% 15.9M 42s
212700K .......... .......... .......... .......... .......... 42% 11.5M 42s
212750K .......... .......... .......... .......... .......... 42% 10.8M 42s
212800K .......... .......... .......... .......... .......... 42% 17.7M 42s
212850K .......... .......... .......... .......... .......... 42% 10.9M 42s
212900K .......... .......... .......... .......... .......... 42% 25.0M 42s
212950K .......... .......... .......... .......... .......... 42% 11.7M 42s
213000K .......... .......... .......... .......... .......... 42% 16.6M 42s
213050K .......... .......... .......... .......... .......... 42% 17.8M 42s
213100K .......... .......... .......... .......... .......... 42% 17.3M 42s
213150K .......... .......... .......... .......... .......... 42% 11.0M 42s
213200K .......... .......... .......... .......... .......... 42% 23.4M 42s
213250K .......... .......... .......... .......... .......... 42% 19.1M 42s
213300K .......... .......... .......... .......... .......... 42% 10.8M 42s
213350K .......... .......... .......... .......... .......... 42% 94.6M 42s
213400K .......... .......... .......... .......... .......... 42% 13.0M 42s
213450K .......... .......... .......... .......... .......... 42% 39.5M 42s
213500K .......... .......... .......... .......... .......... 42% 16.9M 42s
213550K .......... .......... .......... .......... .......... 42% 12.5M 42s
213600K .......... .......... .......... .......... .......... 42% 9.31M 42s
213650K .......... .......... .......... .......... .......... 42% 29.3M 42s
213700K .......... .......... .......... .......... .......... 42% 11.5M 42s
213750K .......... .......... .......... .......... .......... 42% 17.3M 42s
213800K .......... .......... .......... .......... .......... 42% 11.7M 42s
213850K .......... .......... .......... .......... .......... 42% 12.7M 42s
213900K .......... .......... .......... .......... .......... 42% 17.4M 42s
213950K .......... .......... .......... .......... .......... 42% 11.9M 42s
214000K .......... .......... .......... .......... .......... 42% 18.3M 42s
214050K .......... .......... .......... .......... .......... 42% 18.5M 42s
214100K .......... .......... .......... .......... .......... 42% 9.33M 42s
214150K .......... .......... .......... .......... .......... 42% 13.1M 42s
214200K .......... .......... .......... .......... .......... 42% 12.3M 42s
214250K .......... .......... .......... .......... .......... 42% 16.4M 42s
214300K .......... .......... .......... .......... .......... 42% 17.1M 42s
214350K .......... .......... .......... .......... .......... 42% 12.0M 42s
214400K .......... .......... .......... .......... .......... 42% 11.4M 42s
214450K .......... .......... .......... .......... .......... 42% 11.8M 42s
214500K .......... .......... .......... .......... .......... 42% 8.88M 42s
214550K .......... .......... .......... .......... .......... 42% 15.2M 42s
214600K .......... .......... .......... .......... .......... 42% 11.8M 42s
214650K .......... .......... .......... .......... .......... 42% 9.25M 42s
214700K .......... .......... .......... .......... .......... 42% 8.65M 42s
214750K .......... .......... .......... .......... .......... 42% 10.4M 41s
214800K .......... .......... .......... .......... .......... 42% 12.7M 41s
214850K .......... .......... .......... .......... .......... 42% 10.1M 41s
214900K .......... .......... .......... .......... .......... 42% 22.8M 41s
214950K .......... .......... .......... .......... .......... 42% 16.3M 41s
215000K .......... .......... .......... .......... .......... 42% 17.5M 41s
215050K .......... .......... .......... .......... .......... 42% 17.0M 41s
215100K .......... .......... .......... .......... .......... 42% 11.4M 41s
215150K .......... .......... .......... .......... .......... 42% 18.5M 41s
215200K .......... .......... .......... .......... .......... 42% 14.0M 41s
215250K .......... .......... .......... .......... .......... 42% 16.8M 41s
215300K .......... .......... .......... .......... .......... 42% 29.9M 41s
215350K .......... .......... .......... .......... .......... 42% 8.19M 41s
215400K .......... .......... .......... .......... .......... 42% 19.8M 41s
215450K .......... .......... .......... .......... .......... 42% 15.9M 41s
215500K .......... .......... .......... .......... .......... 42% 18.2M 41s
215550K .......... .......... .......... .......... .......... 42% 9.65M 41s
215600K .......... .......... .......... .......... .......... 42% 15.5M 41s
215650K .......... .......... .......... .......... .......... 42% 16.0M 41s
215700K .......... .......... .......... .......... .......... 42% 12.1M 41s
215750K .......... .......... .......... .......... .......... 42% 12.7M 41s
215800K .......... .......... .......... .......... .......... 42% 15.2M 41s
215850K .......... .......... .......... .......... .......... 42% 15.5M 41s
215900K .......... .......... .......... .......... .......... 42% 18.2M 41s
215950K .......... .......... .......... .......... .......... 42% 11.1M 41s
216000K .......... .......... .......... .......... .......... 42% 19.0M 41s
216050K .......... .......... .......... .......... .......... 42% 12.5M 41s
216100K .......... .......... .......... .......... .......... 42% 9.74M 41s
216150K .......... .......... .......... .......... .......... 42% 36.8M 41s
216200K .......... .......... .......... .......... .......... 42% 11.4M 41s
216250K .......... .......... .......... .......... .......... 42% 24.7M 41s
216300K .......... .......... .......... .......... .......... 42% 26.6M 41s
216350K .......... .......... .......... .......... .......... 42% 14.4M 41s
216400K .......... .......... .......... .......... .......... 42% 19.2M 41s
216450K .......... .......... .......... .......... .......... 42% 17.2M 41s
216500K .......... .......... .......... .......... .......... 42% 26.0M 41s
216550K .......... .......... .......... .......... .......... 42% 18.4M 41s
216600K .......... .......... .......... .......... .......... 42% 22.5M 41s
216650K .......... .......... .......... .......... .......... 42% 19.2M 41s
216700K .......... .......... .......... .......... .......... 42% 17.1M 41s
216750K .......... .......... .......... .......... .......... 42% 15.9M 41s
216800K .......... .......... .......... .......... .......... 42% 18.5M 41s
216850K .......... .......... .......... .......... .......... 42% 12.2M 41s
216900K .......... .......... .......... .......... .......... 42% 211M 41s
216950K .......... .......... .......... .......... .......... 42% 8.81M 41s
217000K .......... .......... .......... .......... .......... 42% 78.6M 41s
217050K .......... .......... .......... .......... .......... 42% 10.6M 41s
217100K .......... .......... .......... .......... .......... 43% 87.5M 41s
217150K .......... .......... .......... .......... .......... 43% 25.4M 41s
217200K .......... .......... .......... .......... .......... 43% 23.1M 41s
217250K .......... .......... .......... .......... .......... 43% 26.5M 41s
217300K .......... .......... .......... .......... .......... 43% 17.4M 41s
217350K .......... .......... .......... .......... .......... 43% 12.1M 41s
217400K .......... .......... .......... .......... .......... 43% 22.7M 41s
217450K .......... .......... .......... .......... .......... 43% 25.1M 41s
217500K .......... .......... .......... .......... .......... 43% 18.3M 41s
217550K .......... .......... .......... .......... .......... 43% 31.5M 41s
217600K .......... .......... .......... .......... .......... 43% 17.0M 41s
217650K .......... .......... .......... .......... .......... 43% 17.9M 41s
217700K .......... .......... .......... .......... .......... 43% 33.4M 41s
217750K .......... .......... .......... .......... .......... 43% 30.5M 41s
217800K .......... .......... .......... .......... .......... 43% 18.0M 41s
217850K .......... .......... .......... .......... .......... 43% 17.8M 41s
217900K .......... .......... .......... .......... .......... 43% 18.5M 41s
217950K .......... .......... .......... .......... .......... 43% 15.4M 41s
218000K .......... .......... .......... .......... .......... 43% 17.6M 41s
218050K .......... .......... .......... .......... .......... 43% 16.6M 41s
218100K .......... .......... .......... .......... .......... 43% 16.6M 41s
218150K .......... .......... .......... .......... .......... 43% 45.3M 41s
218200K .......... .......... .......... .......... .......... 43% 17.5M 41s
218250K .......... .......... .......... .......... .......... 43% 13.1M 41s
218300K .......... .......... .......... .......... .......... 43% 16.7M 41s
218350K .......... .......... .......... .......... .......... 43% 17.2M 41s
218400K .......... .......... .......... .......... .......... 43% 16.0M 41s
218450K .......... .......... .......... .......... .......... 43% 14.5M 41s
218500K .......... .......... .......... .......... .......... 43% 22.7M 41s
218550K .......... .......... .......... .......... .......... 43% 16.8M 41s
218600K .......... .......... .......... .......... .......... 43% 31.9M 41s
218650K .......... .......... .......... .......... .......... 43% 18.8M 40s
218700K .......... .......... .......... .......... .......... 43% 27.7M 40s
218750K .......... .......... .......... .......... .......... 43% 18.1M 40s
218800K .......... .......... .......... .......... .......... 43% 9.42M 40s
218850K .......... .......... .......... .......... .......... 43% 18.7M 40s
218900K .......... .......... .......... .......... .......... 43% 17.0M 40s
218950K .......... .......... .......... .......... .......... 43% 18.6M 40s
219000K .......... .......... .......... .......... .......... 43% 17.0M 40s
219050K .......... .......... .......... .......... .......... 43% 24.7M 40s
219100K .......... .......... .......... .......... .......... 43% 25.2M 40s
219150K .......... .......... .......... .......... .......... 43% 18.6M 40s
219200K .......... .......... .......... .......... .......... 43% 11.3M 40s
219250K .......... .......... .......... .......... .......... 43% 23.1M 40s
219300K .......... .......... .......... .......... .......... 43% 26.7M 40s
219350K .......... .......... .......... .......... .......... 43% 16.8M 40s
219400K .......... .......... .......... .......... .......... 43% 15.8M 40s
219450K .......... .......... .......... .......... .......... 43% 18.0M 40s
219500K .......... .......... .......... .......... .......... 43% 15.5M 40s
219550K .......... .......... .......... .......... .......... 43% 27.3M 40s
219600K .......... .......... .......... .......... .......... 43% 16.4M 40s
219650K .......... .......... .......... .......... .......... 43% 24.8M 40s
219700K .......... .......... .......... .......... .......... 43% 11.6M 40s
219750K .......... .......... .......... .......... .......... 43% 18.6M 40s
219800K .......... .......... .......... .......... .......... 43% 34.0M 40s
219850K .......... .......... .......... .......... .......... 43% 8.16M 40s
219900K .......... .......... .......... .......... .......... 43% 38.4M 40s
219950K .......... .......... .......... .......... .......... 43% 15.9M 40s
220000K .......... .......... .......... .......... .......... 43% 33.6M 40s
220050K .......... .......... .......... .......... .......... 43% 26.3M 40s
220100K .......... .......... .......... .......... .......... 43% 13.0M 40s
220150K .......... .......... .......... .......... .......... 43% 14.0M 40s
220200K .......... .......... .......... .......... .......... 43% 16.4M 40s
220250K .......... .......... .......... .......... .......... 43% 30.0M 40s
220300K .......... .......... .......... .......... .......... 43% 11.1M 40s
220350K .......... .......... .......... .......... .......... 43% 15.4M 40s
220400K .......... .......... .......... .......... .......... 43% 16.9M 40s
220450K .......... .......... .......... .......... .......... 43% 12.4M 40s
220500K .......... .......... .......... .......... .......... 43% 15.2M 40s
220550K .......... .......... .......... .......... .......... 43% 26.8M 40s
220600K .......... .......... .......... .......... .......... 43% 17.9M 40s
220650K .......... .......... .......... .......... .......... 43% 9.44M 40s
220700K .......... .......... .......... .......... .......... 43% 32.1M 40s
220750K .......... .......... .......... .......... .......... 43% 17.8M 40s
220800K .......... .......... .......... .......... .......... 43% 37.2M 40s
220850K .......... .......... .......... .......... .......... 43% 10.7M 40s
220900K .......... .......... .......... .......... .......... 43% 18.2M 40s
220950K .......... .......... .......... .......... .......... 43% 16.4M 40s
221000K .......... .......... .......... .......... .......... 43% 16.0M 40s
221050K .......... .......... .......... .......... .......... 43% 16.8M 40s
221100K .......... .......... .......... .......... .......... 43% 11.4M 40s
221150K .......... .......... .......... .......... .......... 43% 17.9M 40s
221200K .......... .......... .......... .......... .......... 43% 16.7M 40s
221250K .......... .......... .......... .......... .......... 43% 17.4M 40s
221300K .......... .......... .......... .......... .......... 43% 27.3M 40s
221350K .......... .......... .......... .......... .......... 43% 6.23M 40s
221400K .......... .......... .......... .......... .......... 43% 13.7M 40s
221450K .......... .......... .......... .......... .......... 43% 9.46M 40s
221500K .......... .......... .......... .......... .......... 43% 10.5M 40s
221550K .......... .......... .......... .......... .......... 43% 12.3M 40s
221600K .......... .......... .......... .......... .......... 43% 11.1M 40s
221650K .......... .......... .......... .......... .......... 43% 9.08M 40s
221700K .......... .......... .......... .......... .......... 43% 8.86M 40s
221750K .......... .......... .......... .......... .......... 43% 11.1M 40s
221800K .......... .......... .......... .......... .......... 43% 9.38M 40s
221850K .......... .......... .......... .......... .......... 43% 8.77M 40s
221900K .......... .......... .......... .......... .......... 43% 9.89M 40s
221950K .......... .......... .......... .......... .......... 43% 8.95M 40s
222000K .......... .......... .......... .......... .......... 43% 15.8M 40s
222050K .......... .......... .......... .......... .......... 43% 10.8M 40s
222100K .......... .......... .......... .......... .......... 43% 17.0M 40s
222150K .......... .......... .......... .......... .......... 44% 12.5M 40s
222200K .......... .......... .......... .......... .......... 44% 12.1M 40s
222250K .......... .......... .......... .......... .......... 44% 17.3M 40s
222300K .......... .......... .......... .......... .......... 44% 11.8M 40s
222350K .......... .......... .......... .......... .......... 44% 12.1M 40s
222400K .......... .......... .......... .......... .......... 44% 12.9M 40s
222450K .......... .......... .......... .......... .......... 44% 17.7M 40s
222500K .......... .......... .......... .......... .......... 44% 11.4M 40s
222550K .......... .......... .......... .......... .......... 44% 20.2M 40s
222600K .......... .......... .......... .......... .......... 44% 12.3M 40s
222650K .......... .......... .......... .......... .......... 44% 15.3M 40s
222700K .......... .......... .......... .......... .......... 44% 11.1M 40s
222750K .......... .......... .......... .......... .......... 44% 16.8M 40s
222800K .......... .......... .......... .......... .......... 44% 11.5M 40s
222850K .......... .......... .......... .......... .......... 44% 7.28M 40s
222900K .......... .......... .......... .......... .......... 44% 16.8M 39s
222950K .......... .......... .......... .......... .......... 44% 7.41M 39s
223000K .......... .......... .......... .......... .......... 44% 16.9M 39s
223050K .......... .......... .......... .......... .......... 44% 18.2M 39s
223100K .......... .......... .......... .......... .......... 44% 10.1M 39s
223150K .......... .......... .......... .......... .......... 44% 26.3M 39s
223200K .......... .......... .......... .......... .......... 44% 19.0M 39s
223250K .......... .......... .......... .......... .......... 44% 23.4M 39s
223300K .......... .......... .......... .......... .......... 44% 33.9M 39s
223350K .......... .......... .......... .......... .......... 44% 15.5M 39s
223400K .......... .......... .......... .......... .......... 44% 25.0M 39s
223450K .......... .......... .......... .......... .......... 44% 19.7M 39s
223500K .......... .......... .......... .......... .......... 44% 15.2M 39s
223550K .......... .......... .......... .......... .......... 44% 32.9M 39s
223600K .......... .......... .......... .......... .......... 44% 15.1M 39s
223650K .......... .......... .......... .......... .......... 44% 17.6M 39s
223700K .......... .......... .......... .......... .......... 44% 30.1M 39s
223750K .......... .......... .......... .......... .......... 44% 30.7M 39s
223800K .......... .......... .......... .......... .......... 44% 7.63M 39s
223850K .......... .......... .......... .......... .......... 44% 39.6M 39s
223900K .......... .......... .......... .......... .......... 44% 11.8M 39s
223950K .......... .......... .......... .......... .......... 44% 16.0M 39s
224000K .......... .......... .......... .......... .......... 44% 27.9M 39s
224050K .......... .......... .......... .......... .......... 44% 11.1M 39s
224100K .......... .......... .......... .......... .......... 44% 12.0M 39s
224150K .......... .......... .......... .......... .......... 44% 22.4M 39s
224200K .......... .......... .......... .......... .......... 44% 16.6M 39s
224250K .......... .......... .......... .......... .......... 44% 14.3M 39s
224300K .......... .......... .......... .......... .......... 44% 13.7M 39s
224350K .......... .......... .......... .......... .......... 44% 7.02M 39s
224400K .......... .......... .......... .......... .......... 44% 13.3M 39s
224450K .......... .......... .......... .......... .......... 44% 9.76M 39s
224500K .......... .......... .......... .......... .......... 44% 10.9M 39s
224550K .......... .......... .......... .......... .......... 44% 9.19M 39s
224600K .......... .......... .......... .......... .......... 44% 8.99M 39s
224650K .......... .......... .......... .......... .......... 44% 8.49M 39s
224700K .......... .......... .......... .......... .......... 44% 12.4M 39s
224750K .......... .......... .......... .......... .......... 44% 4.08M 39s
224800K .......... .......... .......... .......... .......... 44% 12.9M 39s
224850K .......... .......... .......... .......... .......... 44% 9.57M 39s
224900K .......... .......... .......... .......... .......... 44% 7.79M 39s
224950K .......... .......... .......... .......... .......... 44% 9.10M 39s
225000K .......... .......... .......... .......... .......... 44% 12.1M 39s
225050K .......... .......... .......... .......... .......... 44% 6.24M 39s
225100K .......... .......... .......... .......... .......... 44% 5.24M 39s
225150K .......... .......... .......... .......... .......... 44% 7.44M 39s
225200K .......... .......... .......... .......... .......... 44% 8.93M 39s
225250K .......... .......... .......... .......... .......... 44% 18.3M 39s
225300K .......... .......... .......... .......... .......... 44% 11.7M 39s
225350K .......... .......... .......... .......... .......... 44% 11.9M 39s
225400K .......... .......... .......... .......... .......... 44% 12.5M 39s
225450K .......... .......... .......... .......... .......... 44% 10.9M 39s
225500K .......... .......... .......... .......... .......... 44% 12.0M 39s
225550K .......... .......... .......... .......... .......... 44% 7.53M 39s
225600K .......... .......... .......... .......... .......... 44% 9.15M 39s
225650K .......... .......... .......... .......... .......... 44% 17.9M 39s
225700K .......... .......... .......... .......... .......... 44% 9.22M 39s
225750K .......... .......... .......... .......... .......... 44% 11.5M 39s
225800K .......... .......... .......... .......... .......... 44% 31.6M 39s
225850K .......... .......... .......... .......... .......... 44% 15.0M 39s
225900K .......... .......... .......... .......... .......... 44% 11.3M 39s
225950K .......... .......... .......... .......... .......... 44% 12.6M 39s
226000K .......... .......... .......... .......... .......... 44% 16.8M 39s
226050K .......... .......... .......... .......... .......... 44% 17.9M 39s
226100K .......... .......... .......... .......... .......... 44% 11.7M 39s
226150K .......... .......... .......... .......... .......... 44% 12.3M 39s
226200K .......... .......... .......... .......... .......... 44% 27.9M 39s
226250K .......... .......... .......... .......... .......... 44% 13.2M 39s
226300K .......... .......... .......... .......... .......... 44% 30.1M 39s
226350K .......... .......... .......... .......... .......... 44% 9.22M 39s
226400K .......... .......... .......... .......... .......... 44% 8.53M 39s
226450K .......... .......... .......... .......... .......... 44% 13.5M 39s
226500K .......... .......... .......... .......... .......... 44% 14.6M 39s
226550K .......... .......... .......... .......... .......... 44% 12.4M 39s
226600K .......... .......... .......... .......... .......... 44% 7.41M 39s
226650K .......... .......... .......... .......... .......... 44% 16.2M 39s
226700K .......... .......... .......... .......... .......... 44% 17.7M 39s
226750K .......... .......... .......... .......... .......... 44% 10.9M 39s
226800K .......... .......... .......... .......... .......... 44% 16.1M 39s
226850K .......... .......... .......... .......... .......... 44% 17.7M 39s
226900K .......... .......... .......... .......... .......... 44% 9.52M 39s
226950K .......... .......... .......... .......... .......... 44% 6.25M 39s
227000K .......... .......... .......... .......... .......... 44% 17.4M 39s
227050K .......... .......... .......... .......... .......... 44% 12.6M 39s
227100K .......... .......... .......... .......... .......... 44% 8.93M 39s
227150K .......... .......... .......... .......... .......... 44% 11.2M 39s
227200K .......... .......... .......... .......... .......... 45% 7.20M 39s
227250K .......... .......... .......... .......... .......... 45% 3.60M 39s
227300K .......... .......... .......... .......... .......... 45% 133M 39s
227350K .......... .......... .......... .......... .......... 45% 6.27M 39s
227400K .......... .......... .......... .......... .......... 45% 11.7M 39s
227450K .......... .......... .......... .......... .......... 45% 11.7M 39s
227500K .......... .......... .......... .......... .......... 45% 15.6M 39s
227550K .......... .......... .......... .......... .......... 45% 17.4M 39s
227600K .......... .......... .......... .......... .......... 45% 15.3M 39s
227650K .......... .......... .......... .......... .......... 45% 11.9M 39s
227700K .......... .......... .......... .......... .......... 45% 9.09M 38s
227750K .......... .......... .......... .......... .......... 45% 15.5M 38s
227800K .......... .......... .......... .......... .......... 45% 17.6M 38s
227850K .......... .......... .......... .......... .......... 45% 18.1M 38s
227900K .......... .......... .......... .......... .......... 45% 17.2M 38s
227950K .......... .......... .......... .......... .......... 45% 14.7M 38s
228000K .......... .......... .......... .......... .......... 45% 11.5M 38s
228050K .......... .......... .......... .......... .......... 45% 9.27M 38s
228100K .......... .......... .......... .......... .......... 45% 7.60M 38s
228150K .......... .......... .......... .......... .......... 45% 10.8M 38s
228200K .......... .......... .......... .......... .......... 45% 7.45M 38s
228250K .......... .......... .......... .......... .......... 45% 11.9M 38s
228300K .......... .......... .......... .......... .......... 45% 7.82M 38s
228350K .......... .......... .......... .......... .......... 45% 8.87M 38s
228400K .......... .......... .......... .......... .......... 45% 11.6M 38s
228450K .......... .......... .......... .......... .......... 45% 6.05M 38s
228500K .......... .......... .......... .......... .......... 45% 18.4M 38s
228550K .......... .......... .......... .......... .......... 45% 6.47M 38s
228600K .......... .......... .......... .......... .......... 45% 9.11M 38s
228650K .......... .......... .......... .......... .......... 45% 9.07M 38s
228700K .......... .......... .......... .......... .......... 45% 8.99M 38s
228750K .......... .......... .......... .......... .......... 45% 9.15M 38s
228800K .......... .......... .......... .......... .......... 45% 7.58M 38s
228850K .......... .......... .......... .......... .......... 45% 8.67M 38s
228900K .......... .......... .......... .......... .......... 45% 12.1M 38s
228950K .......... .......... .......... .......... .......... 45% 7.13M 38s
229000K .......... .......... .......... .......... .......... 45% 17.2M 38s
229050K .......... .......... .......... .......... .......... 45% 12.6M 38s
229100K .......... .......... .......... .......... .......... 45% 8.73M 38s
229150K .......... .......... .......... .......... .......... 45% 12.6M 38s
229200K .......... .......... .......... .......... .......... 45% 11.7M 38s
229250K .......... .......... .......... .......... .......... 45% 12.4M 38s
229300K .......... .......... .......... .......... .......... 45% 16.3M 38s
229350K .......... .......... .......... .......... .......... 45% 7.81M 38s
229400K .......... .......... .......... .......... .......... 45% 9.26M 38s
229450K .......... .......... .......... .......... .......... 45% 6.20M 38s
229500K .......... .......... .......... .......... .......... 45% 9.41M 38s
229550K .......... .......... .......... .......... .......... 45% 7.20M 38s
229600K .......... .......... .......... .......... .......... 45% 6.29M 38s
229650K .......... .......... .......... .......... .......... 45% 9.31M 38s
229700K .......... .......... .......... .......... .......... 45% 6.37M 38s
229750K .......... .......... .......... .......... .......... 45% 7.27M 38s
229800K .......... .......... .......... .......... .......... 45% 5.38M 38s
229850K .......... .......... .......... .......... .......... 45% 7.56M 38s
229900K .......... .......... .......... .......... .......... 45% 11.8M 38s
229950K .......... .......... .......... .......... .......... 45% 11.7M 38s
230000K .......... .......... .......... .......... .......... 45% 8.44M 38s
230050K .......... .......... .......... .......... .......... 45% 11.0M 38s
230100K .......... .......... .......... .......... .......... 45% 7.36M 38s
230150K .......... .......... .......... .......... .......... 45% 16.7M 38s
230200K .......... .......... .......... .......... .......... 45% 6.33M 38s
230250K .......... .......... .......... .......... .......... 45% 16.6M 38s
230300K .......... .......... .......... .......... .......... 45% 15.5M 38s
230350K .......... .......... .......... .......... .......... 45% 10.9M 38s
230400K .......... .......... .......... .......... .......... 45% 18.2M 38s
230450K .......... .......... .......... .......... .......... 45% 15.2M 38s
230500K .......... .......... .......... .......... .......... 45% 17.9M 38s
230550K .......... .......... .......... .......... .......... 45% 13.4M 38s
230600K .......... .......... .......... .......... .......... 45% 15.0M 38s
230650K .......... .......... .......... .......... .......... 45% 15.8M 38s
230700K .......... .......... .......... .......... .......... 45% 16.0M 38s
230750K .......... .......... .......... .......... .......... 45% 32.2M 38s
230800K .......... .......... .......... .......... .......... 45% 11.3M 38s
230850K .......... .......... .......... .......... .......... 45% 17.6M 38s
230900K .......... .......... .......... .......... .......... 45% 16.7M 38s
230950K .......... .......... .......... .......... .......... 45% 204M 38s
231000K .......... .......... .......... .......... .......... 45% 17.3M 38s
231050K .......... .......... .......... .......... .......... 45% 9.07M 38s
231100K .......... .......... .......... .......... .......... 45% 19.1M 38s
231150K .......... .......... .......... .......... .......... 45% 23.6M 38s
231200K .......... .......... .......... .......... .......... 45% 33.5M 38s
231250K .......... .......... .......... .......... .......... 45% 16.0M 38s
231300K .......... .......... .......... .......... .......... 45% 18.3M 38s
231350K .......... .......... .......... .......... .......... 45% 18.6M 38s
231400K .......... .......... .......... .......... .......... 45% 11.4M 38s
231450K .......... .......... .......... .......... .......... 45% 19.0M 38s
231500K .......... .......... .......... .......... .......... 45% 16.2M 38s
231550K .......... .......... .......... .......... .......... 45% 23.2M 38s
231600K .......... .......... .......... .......... .......... 45% 13.5M 38s
231650K .......... .......... .......... .......... .......... 45% 32.7M 38s
231700K .......... .......... .......... .......... .......... 45% 17.4M 38s
231750K .......... .......... .......... .......... .......... 45% 18.4M 38s
231800K .......... .......... .......... .......... .......... 45% 12.0M 38s
231850K .......... .......... .......... .......... .......... 45% 10.6M 38s
231900K .......... .......... .......... .......... .......... 45% 7.96M 38s
231950K .......... .......... .......... .......... .......... 45% 111M 38s
232000K .......... .......... .......... .......... .......... 45% 15.7M 38s
232050K .......... .......... .......... .......... .......... 45% 15.8M 38s
232100K .......... .......... .......... .......... .......... 45% 11.6M 38s
232150K .......... .......... .......... .......... .......... 45% 16.1M 38s
232200K .......... .......... .......... .......... .......... 45% 16.4M 38s
232250K .......... .......... .......... .......... .......... 46% 16.0M 38s
232300K .......... .......... .......... .......... .......... 46% 11.5M 38s
232350K .......... .......... .......... .......... .......... 46% 11.2M 38s
232400K .......... .......... .......... .......... .......... 46% 17.1M 38s
232450K .......... .......... .......... .......... .......... 46% 7.81M 38s
232500K .......... .......... .......... .......... .......... 46% 9.06M 38s
232550K .......... .......... .......... .......... .......... 46% 13.3M 38s
232600K .......... .......... .......... .......... .......... 46% 17.7M 38s
232650K .......... .......... .......... .......... .......... 46% 10.6M 37s
232700K .......... .......... .......... .......... .......... 46% 11.3M 37s
232750K .......... .......... .......... .......... .......... 46% 16.1M 37s
232800K .......... .......... .......... .......... .......... 46% 15.2M 37s
232850K .......... .......... .......... .......... .......... 46% 8.81M 37s
232900K .......... .......... .......... .......... .......... 46% 17.3M 37s
232950K .......... .......... .......... .......... .......... 46% 11.9M 37s
233000K .......... .......... .......... .......... .......... 46% 6.21M 37s
233050K .......... .......... .......... .......... .......... 46% 6.09M 37s
233100K .......... .......... .......... .......... .......... 46% 6.21M 37s
233150K .......... .......... .......... .......... .......... 46% 11.6M 37s
233200K .......... .......... .......... .......... .......... 46% 6.00M 37s
233250K .......... .......... .......... .......... .......... 46% 9.39M 37s
233300K .......... .......... .......... .......... .......... 46% 9.19M 37s
233350K .......... .......... .......... .......... .......... 46% 6.14M 37s
233400K .......... .......... .......... .......... .......... 46% 11.0M 37s
233450K .......... .......... .......... .......... .......... 46% 24.2M 37s
233500K .......... .......... .......... .......... .......... 46% 29.2M 37s
233550K .......... .......... .......... .......... .......... 46% 18.2M 37s
233600K .......... .......... .......... .......... .......... 46% 25.0M 37s
233650K .......... .......... .......... .......... .......... 46% 19.2M 37s
233700K .......... .......... .......... .......... .......... 46% 26.4M 37s
233750K .......... .......... .......... .......... .......... 46% 18.3M 37s
233800K .......... .......... .......... .......... .......... 46% 26.2M 37s
233850K .......... .......... .......... .......... .......... 46% 23.0M 37s
233900K .......... .......... .......... .......... .......... 46% 18.8M 37s
233950K .......... .......... .......... .......... .......... 46% 25.1M 37s
234000K .......... .......... .......... .......... .......... 46% 11.8M 37s
234050K .......... .......... .......... .......... .......... 46% 15.7M 37s
234100K .......... .......... .......... .......... .......... 46% 33.5M 37s
234150K .......... .......... .......... .......... .......... 46% 12.7M 37s
234200K .......... .......... .......... .......... .......... 46% 15.2M 37s
234250K .......... .......... .......... .......... .......... 46% 9.33M 37s
234300K .......... .......... .......... .......... .......... 46% 30.6M 37s
234350K .......... .......... .......... .......... .......... 46% 12.9M 37s
234400K .......... .......... .......... .......... .......... 46% 13.1M 37s
234450K .......... .......... .......... .......... .......... 46% 10.9M 37s
234500K .......... .......... .......... .......... .......... 46% 14.2M 37s
234550K .......... .......... .......... .......... .......... 46% 15.1M 37s
234600K .......... .......... .......... .......... .......... 46% 9.53M 37s
234650K .......... .......... .......... .......... .......... 46% 16.0M 37s
234700K .......... .......... .......... .......... .......... 46% 9.15M 37s
234750K .......... .......... .......... .......... .......... 46% 9.41M 37s
234800K .......... .......... .......... .......... .......... 46% 17.7M 37s
234850K .......... .......... .......... .......... .......... 46% 11.2M 37s
234900K .......... .......... .......... .......... .......... 46% 13.9M 37s
234950K .......... .......... .......... .......... .......... 46% 18.7M 37s
235000K .......... .......... .......... .......... .......... 46% 16.1M 37s
235050K .......... .......... .......... .......... .......... 46% 15.2M 37s
235100K .......... .......... .......... .......... .......... 46% 12.3M 37s
235150K .......... .......... .......... .......... .......... 46% 16.4M 37s
235200K .......... .......... .......... .......... .......... 46% 16.6M 37s
235250K .......... .......... .......... .......... .......... 46% 15.6M 37s
235300K .......... .......... .......... .......... .......... 46% 12.6M 37s
235350K .......... .......... .......... .......... .......... 46% 16.3M 37s
235400K .......... .......... .......... .......... .......... 46% 10.9M 37s
235450K .......... .......... .......... .......... .......... 46% 12.1M 37s
235500K .......... .......... .......... .......... .......... 46% 12.5M 37s
235550K .......... .......... .......... .......... .......... 46% 10.6M 37s
235600K .......... .......... .......... .......... .......... 46% 18.2M 37s
235650K .......... .......... .......... .......... .......... 46% 16.7M 37s
235700K .......... .......... .......... .......... .......... 46% 12.6M 37s
235750K .......... .......... .......... .......... .......... 46% 15.2M 37s
235800K .......... .......... .......... .......... .......... 46% 11.4M 37s
235850K .......... .......... .......... .......... .......... 46% 16.8M 37s
235900K .......... .......... .......... .......... .......... 46% 15.4M 37s
235950K .......... .......... .......... .......... .......... 46% 10.8M 37s
236000K .......... .......... .......... .......... .......... 46% 17.0M 37s
236050K .......... .......... .......... .......... .......... 46% 12.5M 37s
236100K .......... .......... .......... .......... .......... 46% 9.82M 37s
236150K .......... .......... .......... .......... .......... 46% 10.4M 37s
236200K .......... .......... .......... .......... .......... 46% 34.9M 37s
236250K .......... .......... .......... .......... .......... 46% 11.7M 37s
236300K .......... .......... .......... .......... .......... 46% 12.0M 37s
236350K .......... .......... .......... .......... .......... 46% 12.3M 37s
236400K .......... .......... .......... .......... .......... 46% 16.4M 37s
236450K .......... .......... .......... .......... .......... 46% 9.50M 37s
236500K .......... .......... .......... .......... .......... 46% 12.9M 37s
236550K .......... .......... .......... .......... .......... 46% 16.9M 37s
236600K .......... .......... .......... .......... .......... 46% 17.6M 37s
236650K .......... .......... .......... .......... .......... 46% 17.7M 37s
236700K .......... .......... .......... .......... .......... 46% 11.1M 37s
236750K .......... .......... .......... .......... .......... 46% 9.21M 37s
236800K .......... .......... .......... .......... .......... 46% 19.3M 37s
236850K .......... .......... .......... .......... .......... 46% 12.0M 37s
236900K .......... .......... .......... .......... .......... 46% 15.8M 37s
236950K .......... .......... .......... .......... .......... 46% 14.8M 37s
237000K .......... .......... .......... .......... .......... 46% 15.4M 37s
237050K .......... .......... .......... .......... .......... 46% 19.9M 37s
237100K .......... .......... .......... .......... .......... 46% 8.96M 37s
237150K .......... .......... .......... .......... .......... 46% 17.4M 37s
237200K .......... .......... .......... .......... .......... 46% 10.9M 37s
237250K .......... .......... .......... .......... .......... 46% 17.6M 37s
237300K .......... .......... .......... .......... .......... 47% 12.0M 37s
237350K .......... .......... .......... .......... .......... 47% 12.0M 37s
237400K .......... .......... .......... .......... .......... 47% 17.4M 37s
237450K .......... .......... .......... .......... .......... 47% 7.72M 36s
237500K .......... .......... .......... .......... .......... 47% 116M 36s
237550K .......... .......... .......... .......... .......... 47% 23.1M 36s
237600K .......... .......... .......... .......... .......... 47% 15.4M 36s
237650K .......... .......... .......... .......... .......... 47% 18.9M 36s
237700K .......... .......... .......... .......... .......... 47% 20.8M 36s
237750K .......... .......... .......... .......... .......... 47% 10.1M 36s
237800K .......... .......... .......... .......... .......... 47% 159M 36s
237850K .......... .......... .......... .......... .......... 47% 13.0M 36s
237900K .......... .......... .......... .......... .......... 47% 13.1M 36s
237950K .......... .......... .......... .......... .......... 47% 13.9M 36s
238000K .......... .......... .......... .......... .......... 47% 16.3M 36s
238050K .......... .......... .......... .......... .......... 47% 18.8M 36s
238100K .......... .......... .......... .......... .......... 47% 10.8M 36s
238150K .......... .......... .......... .......... .......... 47% 12.6M 36s
238200K .......... .......... .......... .......... .......... 47% 17.6M 36s
238250K .......... .......... .......... .......... .......... 47% 25.8M 36s
238300K .......... .......... .......... .......... .......... 47% 15.8M 36s
238350K .......... .......... .......... .......... .......... 47% 26.0M 36s
238400K .......... .......... .......... .......... .......... 47% 5.07M 36s
238450K .......... .......... .......... .......... .......... 47% 44.9M 36s
238500K .......... .......... .......... .......... .......... 47% 11.4M 36s
238550K .......... .......... .......... .......... .......... 47% 13.4M 36s
238600K .......... .......... .......... .......... .......... 47% 10.8M 36s
238650K .......... .......... .......... .......... .......... 47% 11.6M 36s
238700K .......... .......... .......... .......... .......... 47% 8.92M 36s
238750K .......... .......... .......... .......... .......... 47% 17.1M 36s
238800K .......... .......... .......... .......... .......... 47% 11.4M 36s
238850K .......... .......... .......... .......... .......... 47% 11.7M 36s
238900K .......... .......... .......... .......... .......... 47% 16.1M 36s
238950K .......... .......... .......... .......... .......... 47% 7.14M 36s
239000K .......... .......... .......... .......... .......... 47% 8.89M 36s
239050K .......... .......... .......... .......... .......... 47% 20.3M 36s
239100K .......... .......... .......... .......... .......... 47% 11.3M 36s
239150K .......... .......... .......... .......... .......... 47% 18.5M 36s
239200K .......... .......... .......... .......... .......... 47% 10.6M 36s
239250K .......... .......... .......... .......... .......... 47% 15.6M 36s
239300K .......... .......... .......... .......... .......... 47% 11.4M 36s
239350K .......... .......... .......... .......... .......... 47% 11.8M 36s
239400K .......... .......... .......... .......... .......... 47% 18.3M 36s
239450K .......... .......... .......... .......... .......... 47% 16.0M 36s
239500K .......... .......... .......... .......... .......... 47% 7.28M 36s
239550K .......... .......... .......... .......... .......... 47% 23.1M 36s
239600K .......... .......... .......... .......... .......... 47% 15.0M 36s
239650K .......... .......... .......... .......... .......... 47% 17.3M 36s
239700K .......... .......... .......... .......... .......... 47% 11.8M 36s
239750K .......... .......... .......... .......... .......... 47% 44.4M 36s
239800K .......... .......... .......... .......... .......... 47% 11.2M 36s
239850K .......... .......... .......... .......... .......... 47% 23.8M 36s
239900K .......... .......... .......... .......... .......... 47% 17.3M 36s
239950K .......... .......... .......... .......... .......... 47% 10.2M 36s
240000K .......... .......... .......... .......... .......... 47% 31.4M 36s
240050K .......... .......... .......... .......... .......... 47% 12.4M 36s
240100K .......... .......... .......... .......... .......... 47% 18.4M 36s
240150K .......... .......... .......... .......... .......... 47% 15.1M 36s
240200K .......... .......... .......... .......... .......... 47% 12.0M 36s
240250K .......... .......... .......... .......... .......... 47% 11.9M 36s
240300K .......... .......... .......... .......... .......... 47% 18.4M 36s
240350K .......... .......... .......... .......... .......... 47% 8.83M 36s
240400K .......... .......... .......... .......... .......... 47% 35.3M 36s
240450K .......... .......... .......... .......... .......... 47% 14.4M 36s
240500K .......... .......... .......... .......... .......... 47% 18.5M 36s
240550K .......... .......... .......... .......... .......... 47% 12.2M 36s
240600K .......... .......... .......... .......... .......... 47% 28.5M 36s
240650K .......... .......... .......... .......... .......... 47% 15.8M 36s
240700K .......... .......... .......... .......... .......... 47% 13.3M 36s
240750K .......... .......... .......... .......... .......... 47% 15.7M 36s
240800K .......... .......... .......... .......... .......... 47% 24.0M 36s
240850K .......... .......... .......... .......... .......... 47% 15.1M 36s
240900K .......... .......... .......... .......... .......... 47% 27.2M 36s
240950K .......... .......... .......... .......... .......... 47% 13.0M 36s
241000K .......... .......... .......... .......... .......... 47% 29.5M 36s
241050K .......... .......... .......... .......... .......... 47% 14.4M 36s
241100K .......... .......... .......... .......... .......... 47% 17.7M 36s
241150K .......... .......... .......... .......... .......... 47% 274M 36s
241200K .......... .......... .......... .......... .......... 47% 12.3M 36s
241250K .......... .......... .......... .......... .......... 47% 27.3M 36s
241300K .......... .......... .......... .......... .......... 47% 18.1M 36s
241350K .......... .......... .......... .......... .......... 47% 11.0M 36s
241400K .......... .......... .......... .......... .......... 47% 19.3M 36s
241450K .......... .......... .......... .......... .......... 47% 21.0M 36s
241500K .......... .......... .......... .......... .......... 47% 23.3M 36s
241550K .......... .......... .......... .......... .......... 47% 18.3M 36s
241600K .......... .......... .......... .......... .......... 47% 24.6M 36s
241650K .......... .......... .......... .......... .......... 47% 33.8M 36s
241700K .......... .......... .......... .......... .......... 47% 11.7M 36s
241750K .......... .......... .......... .......... .......... 47% 18.3M 36s
241800K .......... .......... .......... .......... .......... 47% 20.2M 36s
241850K .......... .......... .......... .......... .......... 47% 20.3M 36s
241900K .......... .......... .......... .......... .......... 47% 34.3M 36s
241950K .......... .......... .......... .......... .......... 47% 13.2M 36s
242000K .......... .......... .......... .......... .......... 47% 12.4M 36s
242050K .......... .......... .......... .......... .......... 47% 12.6M 36s
242100K .......... .......... .......... .......... .......... 47% 12.7M 35s
242150K .......... .......... .......... .......... .......... 47% 17.3M 35s
242200K .......... .......... .......... .......... .......... 47% 10.4M 35s
242250K .......... .......... .......... .......... .......... 47% 12.4M 35s
242300K .......... .......... .......... .......... .......... 47% 16.5M 35s
242350K .......... .......... .......... .......... .......... 48% 9.02M 35s
242400K .......... .......... .......... .......... .......... 48% 12.5M 35s
242450K .......... .......... .......... .......... .......... 48% 12.1M 35s
242500K .......... .......... .......... .......... .......... 48% 11.0M 35s
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242600K .......... .......... .......... .......... .......... 48% 8.09M 35s
242650K .......... .......... .......... .......... .......... 48% 19.1M 35s
242700K .......... .......... .......... .......... .......... 48% 9.52M 35s
242750K .......... .......... .......... .......... .......... 48% 11.5M 35s
242800K .......... .......... .......... .......... .......... 48% 9.00M 35s
242850K .......... .......... .......... .......... .......... 48% 9.31M 35s
242900K .......... .......... .......... .......... .......... 48% 10.4M 35s
242950K .......... .......... .......... .......... .......... 48% 11.0M 35s
243000K .......... .......... .......... .......... .......... 48% 7.65M 35s
243050K .......... .......... .......... .......... .......... 48% 12.4M 35s
243100K .......... .......... .......... .......... .......... 48% 4.74M 35s
243150K .......... .......... .......... .......... .......... 48% 35.1M 35s
243200K .......... .......... .......... .......... .......... 48% 8.51M 35s
243250K .......... .......... .......... .......... .......... 48% 14.7M 35s
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243400K .......... .......... .......... .......... .......... 48% 15.3M 35s
243450K .......... .......... .......... .......... .......... 48% 7.33M 35s
243500K .......... .......... .......... .......... .......... 48% 17.7M 35s
243550K .......... .......... .......... .......... .......... 48% 10.9M 35s
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243650K .......... .......... .......... .......... .......... 48% 7.24M 35s
243700K .......... .......... .......... .......... .......... 48% 9.80M 35s
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243850K .......... .......... .......... .......... .......... 48% 7.45M 35s
243900K .......... .......... .......... .......... .......... 48% 7.28M 35s
243950K .......... .......... .......... .......... .......... 48% 10.7M 35s
244000K .......... .......... .......... .......... .......... 48% 9.06M 35s
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244100K .......... .......... .......... .......... .......... 48% 5.55M 35s
244150K .......... .......... .......... .......... .......... 48% 11.7M 35s
244200K .......... .......... .......... .......... .......... 48% 8.85M 35s
244250K .......... .......... .......... .......... .......... 48% 11.7M 35s
244300K .......... .......... .......... .......... .......... 48% 8.98M 35s
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244400K .......... .......... .......... .......... .......... 48% 7.54M 35s
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244700K .......... .......... .......... .......... .......... 48% 11.9M 35s
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244800K .......... .......... .......... .......... .......... 48% 11.1M 35s
244850K .......... .......... .......... .......... .......... 48% 14.9M 35s
244900K .......... .......... .......... .......... .......... 48% 12.8M 35s
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245000K .......... .......... .......... .......... .......... 48% 17.3M 35s
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245100K .......... .......... .......... .......... .......... 48% 14.4M 35s
245150K .......... .......... .......... .......... .......... 48% 33.4M 35s
245200K .......... .......... .......... .......... .......... 48% 20.5M 35s
245250K .......... .......... .......... .......... .......... 48% 32.6M 35s
245300K .......... .......... .......... .......... .......... 48% 17.4M 35s
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245400K .......... .......... .......... .......... .......... 48% 12.8M 35s
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245500K .......... .......... .......... .......... .......... 48% 34.1M 35s
245550K .......... .......... .......... .......... .......... 48% 12.1M 35s
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245650K .......... .......... .......... .......... .......... 48% 17.7M 35s
245700K .......... .......... .......... .......... .......... 48% 11.8M 35s
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245850K .......... .......... .......... .......... .......... 48% 11.9M 35s
245900K .......... .......... .......... .......... .......... 48% 17.4M 35s
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246000K .......... .......... .......... .......... .......... 48% 22.5M 35s
246050K .......... .......... .......... .......... .......... 48% 9.95M 35s
246100K .......... .......... .......... .......... .......... 48% 19.2M 35s
246150K .......... .......... .......... .......... .......... 48% 6.27M 35s
246200K .......... .......... .......... .......... .......... 48% 10.9M 35s
246250K .......... .......... .......... .......... .......... 48% 9.35M 35s
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246350K .......... .......... .......... .......... .......... 48% 7.23M 35s
246400K .......... .......... .......... .......... .......... 48% 11.7M 35s
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246700K .......... .......... .......... .......... .......... 48% 6.20M 35s
246750K .......... .......... .......... .......... .......... 48% 11.0M 35s
246800K .......... .......... .......... .......... .......... 48% 12.3M 35s
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246900K .......... .......... .......... .......... .......... 48% 5.45M 35s
246950K .......... .......... .......... .......... .......... 48% 13.0M 35s
247000K .......... .......... .......... .......... .......... 48% 16.0M 35s
247050K .......... .......... .......... .......... .......... 48% 16.1M 35s
247100K .......... .......... .......... .......... .......... 48% 12.1M 35s
247150K .......... .......... .......... .......... .......... 48% 12.1M 35s
247200K .......... .......... .......... .......... .......... 48% 9.98M 35s
247250K .......... .......... .......... .......... .......... 48% 14.0M 35s
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247400K .......... .......... .......... .......... .......... 49% 12.6M 35s
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247850K .......... .......... .......... .......... .......... 49% 32.7M 34s
247900K .......... .......... .......... .......... .......... 49% 10.3M 34s
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248000K .......... .......... .......... .......... .......... 49% 18.8M 34s
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248100K .......... .......... .......... .......... .......... 49% 20.5M 34s
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248200K .......... .......... .......... .......... .......... 49% 9.38M 34s
248250K .......... .......... .......... .......... .......... 49% 34.1M 34s
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248500K .......... .......... .......... .......... .......... 49% 11.8M 34s
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248900K .......... .......... .......... .......... .......... 49% 7.25M 34s
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249000K .......... .......... .......... .......... .......... 49% 10.9M 34s
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249100K .......... .......... .......... .......... .......... 49% 11.8M 34s
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249200K .......... .......... .......... .......... .......... 49% 6.22M 34s
249250K .......... .......... .......... .......... .......... 49% 9.06M 34s
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250000K .......... .......... .......... .......... .......... 49% 12.3M 34s
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250100K .......... .......... .......... .......... .......... 49% 8.35M 34s
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250200K .......... .......... .......... .......... .......... 49% 9.16M 34s
250250K .......... .......... .......... .......... .......... 49% 7.85M 34s
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251000K .......... .......... .......... .......... .......... 49% 9.69M 34s
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251100K .......... .......... .......... .......... .......... 49% 9.07M 34s
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251200K .......... .......... .......... .......... .......... 49% 5.91M 34s
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251500K .......... .......... .......... .......... .......... 49% 12.2M 34s
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251600K .......... .......... .......... .......... .......... 49% 11.7M 34s
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251750K .......... .......... .......... .......... .......... 49% 15.0M 34s
251800K .......... .......... .......... .......... .......... 49% 7.39M 34s
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251900K .......... .......... .......... .......... .......... 49% 16.4M 34s
251950K .......... .......... .......... .......... .......... 49% 7.19M 34s
252000K .......... .......... .......... .......... .......... 49% 12.1M 34s
252050K .......... .......... .......... .......... .......... 49% 16.6M 34s
252100K .......... .......... .......... .......... .......... 49% 7.38M 34s
252150K .......... .......... .......... .......... .......... 49% 10.8M 34s
252200K .......... .......... .......... .......... .......... 49% 8.14M 34s
252250K .......... .......... .......... .......... .......... 49% 11.2M 34s
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252350K .......... .......... .......... .......... .......... 49% 8.34M 34s
252400K .......... .......... .......... .......... .......... 49% 17.5M 34s
252450K .......... .......... .......... .......... .......... 50% 6.26M 34s
252500K .......... .......... .......... .......... .......... 50% 17.9M 34s
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252600K .......... .......... .......... .......... .......... 50% 11.6M 34s
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252700K .......... .......... .......... .......... .......... 50% 8.62M 34s
252750K .......... .......... .......... .......... .......... 50% 14.9M 34s
252800K .......... .......... .......... .......... .......... 50% 12.5M 34s
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252900K .......... .......... .......... .......... .......... 50% 18.0M 34s
252950K .......... .......... .......... .......... .......... 50% 7.14M 34s
253000K .......... .......... .......... .......... .......... 50% 27.4M 34s
253050K .......... .......... .......... .......... .......... 50% 16.0M 34s
253100K .......... .......... .......... .......... .......... 50% 6.08M 34s
253150K .......... .......... .......... .......... .......... 50% 11.3M 33s
253200K .......... .......... .......... .......... .......... 50% 9.16M 33s
253250K .......... .......... .......... .......... .......... 50% 12.3M 33s
253300K .......... .......... .......... .......... .......... 50% 9.91M 33s
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253400K .......... .......... .......... .......... .......... 50% 8.97M 33s
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253500K .......... .......... .......... .......... .......... 50% 9.64M 33s
253550K .......... .......... .......... .......... .......... 50% 15.7M 33s
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253700K .......... .......... .......... .......... .......... 50% 11.0M 33s
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254000K .......... .......... .......... .......... .......... 50% 30.5M 33s
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254100K .......... .......... .......... .......... .......... 50% 6.19M 33s
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254200K .......... .......... .......... .......... .......... 50% 7.01M 33s
254250K .......... .......... .......... .......... .......... 50% 12.5M 33s
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254400K .......... .......... .......... .......... .......... 50% 31.6M 33s
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254700K .......... .......... .......... .......... .......... 50% 9.65M 33s
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254900K .......... .......... .......... .......... .......... 50% 8.53M 33s
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255000K .......... .......... .......... .......... .......... 50% 9.32M 33s
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255100K .......... .......... .......... .......... .......... 50% 8.51M 33s
255150K .......... .......... .......... .......... .......... 50% 12.0M 33s
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255250K .......... .......... .......... .......... .......... 50% 11.7M 33s
255300K .......... .......... .......... .......... .......... 50% 11.5M 33s
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255400K .......... .......... .......... .......... .......... 50% 6.06M 33s
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255500K .......... .......... .......... .......... .......... 50% 7.45M 33s
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255700K .......... .......... .......... .......... .......... 50% 6.06M 33s
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255950K .......... .......... .......... .......... .......... 50% 7.03M 33s
256000K .......... .......... .......... .......... .......... 50% 11.7M 33s
256050K .......... .......... .......... .......... .......... 50% 9.05M 33s
256100K .......... .......... .......... .......... .......... 50% 9.29M 33s
256150K .......... .......... .......... .......... .......... 50% 10.6M 33s
256200K .......... .......... .......... .......... .......... 50% 27.1M 33s
256250K .......... .......... .......... .......... .......... 50% 11.6M 33s
256300K .......... .......... .......... .......... .......... 50% 14.3M 33s
256350K .......... .......... .......... .......... .......... 50% 17.3M 33s
256400K .......... .......... .......... .......... .......... 50% 11.4M 33s
256450K .......... .......... .......... .......... .......... 50% 15.6M 33s
256500K .......... .......... .......... .......... .......... 50% 33.1M 33s
256550K .......... .......... .......... .......... .......... 50% 9.70M 33s
256600K .......... .......... .......... .......... .......... 50% 16.8M 33s
256650K .......... .......... .......... .......... .......... 50% 17.9M 33s
256700K .......... .......... .......... .......... .......... 50% 9.35M 33s
256750K .......... .......... .......... .......... .......... 50% 18.3M 33s
256800K .......... .......... .......... .......... .......... 50% 17.8M 33s
256850K .......... .......... .......... .......... .......... 50% 9.36M 33s
256900K .......... .......... .......... .......... .......... 50% 97.1M 33s
256950K .......... .......... .......... .......... .......... 50% 20.7M 33s
257000K .......... .......... .......... .......... .......... 50% 14.9M 33s
257050K .......... .......... .......... .......... .......... 50% 15.8M 33s
257100K .......... .......... .......... .......... .......... 50% 17.0M 33s
257150K .......... .......... .......... .......... .......... 50% 15.6M 33s
257200K .......... .......... .......... .......... .......... 50% 26.9M 33s
257250K .......... .......... .......... .......... .......... 50% 19.4M 33s
257300K .......... .......... .......... .......... .......... 50% 29.7M 33s
257350K .......... .......... .......... .......... .......... 50% 15.6M 33s
257400K .......... .......... .......... .......... .......... 50% 26.6M 33s
257450K .......... .......... .......... .......... .......... 51% 11.7M 33s
257500K .......... .......... .......... .......... .......... 51% 35.6M 33s
257550K .......... .......... .......... .......... .......... 51% 18.0M 33s
257600K .......... .......... .......... .......... .......... 51% 15.5M 33s
257650K .......... .......... .......... .......... .......... 51% 17.4M 33s
257700K .......... .......... .......... .......... .......... 51% 11.7M 33s
257750K .......... .......... .......... .......... .......... 51% 35.5M 33s
257800K .......... .......... .......... .......... .......... 51% 29.2M 33s
257850K .......... .......... .......... .......... .......... 51% 18.5M 33s
257900K .......... .......... .......... .......... .......... 51% 12.9M 33s
257950K .......... .......... .......... .......... .......... 51% 17.7M 33s
258000K .......... .......... .......... .......... .......... 51% 17.3M 33s
258050K .......... .......... .......... .......... .......... 51% 15.3M 33s
258100K .......... .......... .......... .......... .......... 51% 28.8M 33s
258150K .......... .......... .......... .......... .......... 51% 34.2M 33s
258200K .......... .......... .......... .......... .......... 51% 17.2M 33s
258250K .......... .......... .......... .......... .......... 51% 27.3M 33s
258300K .......... .......... .......... .......... .......... 51% 17.6M 33s
258350K .......... .......... .......... .......... .......... 51% 12.4M 33s
258400K .......... .......... .......... .......... .......... 51% 26.4M 33s
258450K .......... .......... .......... .......... .......... 51% 33.2M 33s
258500K .......... .......... .......... .......... .......... 51% 24.5M 33s
258550K .......... .......... .......... .......... .......... 51% 18.7M 33s
258600K .......... .......... .......... .......... .......... 51% 18.6M 32s
258650K .......... .......... .......... .......... .......... 51% 8.47M 32s
258700K .......... .......... .......... .......... .......... 51% 18.5M 32s
258750K .......... .......... .......... .......... .......... 51% 21.1M 32s
258800K .......... .......... .......... .......... .......... 51% 18.4M 32s
258850K .......... .......... .......... .......... .......... 51% 15.6M 32s
258900K .......... .......... .......... .......... .......... 51% 12.2M 32s
258950K .......... .......... .......... .......... .......... 51% 11.3M 32s
259000K .......... .......... .......... .......... .......... 51% 9.82M 32s
259050K .......... .......... .......... .......... .......... 51% 12.1M 32s
259100K .......... .......... .......... .......... .......... 51% 11.1M 32s
259150K .......... .......... .......... .......... .......... 51% 14.6M 32s
259200K .......... .......... .......... .......... .......... 51% 7.61M 32s
259250K .......... .......... .......... .......... .......... 51% 8.93M 32s
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259350K .......... .......... .......... .......... .......... 51% 6.37M 32s
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259450K .......... .......... .......... .......... .......... 51% 8.76M 32s
259500K .......... .......... .......... .......... .......... 51% 12.4M 32s
259550K .......... .......... .......... .......... .......... 51% 8.85M 32s
259600K .......... .......... .......... .......... .......... 51% 11.4M 32s
259650K .......... .......... .......... .......... .......... 51% 7.32M 32s
259700K .......... .......... .......... .......... .......... 51% 9.27M 32s
259750K .......... .......... .......... .......... .......... 51% 16.0M 32s
259800K .......... .......... .......... .......... .......... 51% 13.1M 32s
259850K .......... .......... .......... .......... .......... 51% 6.13M 32s
259900K .......... .......... .......... .......... .......... 51% 7.38M 32s
259950K .......... .......... .......... .......... .......... 51% 11.8M 32s
260000K .......... .......... .......... .......... .......... 51% 11.8M 32s
260050K .......... .......... .......... .......... .......... 51% 6.61M 32s
260100K .......... .......... .......... .......... .......... 51% 9.37M 32s
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260200K .......... .......... .......... .......... .......... 51% 6.14M 32s
260250K .......... .......... .......... .......... .......... 51% 7.59M 32s
260300K .......... .......... .......... .......... .......... 51% 17.8M 32s
260350K .......... .......... .......... .......... .......... 51% 8.12M 32s
260400K .......... .......... .......... .......... .......... 51% 15.9M 32s
260450K .......... .......... .......... .......... .......... 51% 8.99M 32s
260500K .......... .......... .......... .......... .......... 51% 11.6M 32s
260550K .......... .......... .......... .......... .......... 51% 8.89M 32s
260600K .......... .......... .......... .......... .......... 51% 9.04M 32s
260650K .......... .......... .......... .......... .......... 51% 9.02M 32s
260700K .......... .......... .......... .......... .......... 51% 17.2M 32s
260750K .......... .......... .......... .......... .......... 51% 17.3M 32s
260800K .......... .......... .......... .......... .......... 51% 12.9M 32s
260850K .......... .......... .......... .......... .......... 51% 9.32M 32s
260900K .......... .......... .......... .......... .......... 51% 17.0M 32s
260950K .......... .......... .......... .......... .......... 51% 8.75M 32s
261000K .......... .......... .......... .......... .......... 51% 8.95M 32s
261050K .......... .......... .......... .......... .......... 51% 16.8M 32s
261100K .......... .......... .......... .......... .......... 51% 8.82M 32s
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261200K .......... .......... .......... .......... .......... 51% 13.8M 32s
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261400K .......... .......... .......... .......... .......... 51% 11.4M 32s
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261500K .......... .......... .......... .......... .......... 51% 12.2M 32s
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261600K .......... .......... .......... .......... .......... 51% 8.65M 32s
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261800K .......... .......... .......... .......... .......... 51% 184M 32s
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261900K .......... .......... .......... .......... .......... 51% 11.8M 32s
261950K .......... .......... .......... .......... .......... 51% 17.3M 32s
262000K .......... .......... .......... .......... .......... 51% 12.3M 32s
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262150K .......... .......... .......... .......... .......... 51% 8.88M 32s
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262250K .......... .......... .......... .......... .......... 51% 16.0M 32s
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262800K .......... .......... .......... .......... .......... 52% 9.39M 32s
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263000K .......... .......... .......... .......... .......... 52% 11.5M 32s
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263100K .......... .......... .......... .......... .......... 52% 8.98M 32s
263150K .......... .......... .......... .......... .......... 52% 12.0M 32s
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263250K .......... .......... .......... .......... .......... 52% 11.9M 32s
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263700K .......... .......... .......... .......... .......... 52% 5.11M 32s
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263800K .......... .......... .......... .......... .......... 52% 9.51M 32s
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263900K .......... .......... .......... .......... .......... 52% 7.18M 32s
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264000K .......... .......... .......... .......... .......... 52% 9.06M 32s
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264100K .......... .......... .......... .......... .......... 52% 9.20M 32s
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264200K .......... .......... .......... .......... .......... 52% 8.26M 32s
264250K .......... .......... .......... .......... .......... 52% 9.24M 32s
264300K .......... .......... .......... .......... .......... 52% 10.3M 32s
264350K .......... .......... .......... .......... .......... 52% 11.3M 32s
264400K .......... .......... .......... .......... .......... 52% 12.2M 32s
264450K .......... .......... .......... .......... .......... 52% 7.00M 32s
264500K .......... .......... .......... .......... .......... 52% 7.53M 32s
264550K .......... .......... .......... .......... .......... 52% 9.95M 32s
264600K .......... .......... .......... .......... .......... 52% 7.39M 32s
264650K .......... .......... .......... .......... .......... 52% 17.1M 32s
264700K .......... .......... .......... .......... .......... 52% 14.5M 32s
264750K .......... .......... .......... .......... .......... 52% 11.0M 31s
264800K .......... .......... .......... .......... .......... 52% 19.3M 31s
264850K .......... .......... .......... .......... .......... 52% 39.1M 31s
264900K .......... .......... .......... .......... .......... 52% 16.1M 31s
264950K .......... .......... .......... .......... .......... 52% 15.6M 31s
265000K .......... .......... .......... .......... .......... 52% 12.5M 31s
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265100K .......... .......... .......... .......... .......... 52% 13.3M 31s
265150K .......... .......... .......... .......... .......... 52% 17.1M 31s
265200K .......... .......... .......... .......... .......... 52% 11.4M 31s
265250K .......... .......... .......... .......... .......... 52% 11.8M 31s
265300K .......... .......... .......... .......... .......... 52% 14.1M 31s
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265400K .......... .......... .......... .......... .......... 52% 15.6M 31s
265450K .......... .......... .......... .......... .......... 52% 9.77M 31s
265500K .......... .......... .......... .......... .......... 52% 18.3M 31s
265550K .......... .......... .......... .......... .......... 52% 127M 31s
265600K .......... .......... .......... .......... .......... 52% 11.8M 31s
265650K .......... .......... .......... .......... .......... 52% 12.0M 31s
265700K .......... .......... .......... .......... .......... 52% 17.6M 31s
265750K .......... .......... .......... .......... .......... 52% 14.0M 31s
265800K .......... .......... .......... .......... .......... 52% 17.8M 31s
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265900K .......... .......... .......... .......... .......... 52% 15.6M 31s
265950K .......... .......... .......... .......... .......... 52% 10.8M 31s
266000K .......... .......... .......... .......... .......... 52% 9.08M 31s
266050K .......... .......... .......... .......... .......... 52% 27.5M 31s
266100K .......... .......... .......... .......... .......... 52% 4.58M 31s
266150K .......... .......... .......... .......... .......... 52% 268M 31s
266200K .......... .......... .......... .......... .......... 52% 12.8M 31s
266250K .......... .......... .......... .......... .......... 52% 17.0M 31s
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266350K .......... .......... .......... .......... .......... 52% 15.9M 31s
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266500K .......... .......... .......... .......... .......... 52% 11.6M 31s
266550K .......... .......... .......... .......... .......... 52% 18.7M 31s
266600K .......... .......... .......... .......... .......... 52% 12.4M 31s
266650K .......... .......... .......... .......... .......... 52% 17.0M 31s
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266750K .......... .......... .......... .......... .......... 52% 9.61M 31s
266800K .......... .......... .......... .......... .......... 52% 8.16M 31s
266850K .......... .......... .......... .......... .......... 52% 7.34M 31s
266900K .......... .......... .......... .......... .......... 52% 18.0M 31s
266950K .......... .......... .......... .......... .......... 52% 11.7M 31s
267000K .......... .......... .......... .......... .......... 52% 12.1M 31s
267050K .......... .......... .......... .......... .......... 52% 15.1M 31s
267100K .......... .......... .......... .......... .......... 52% 15.7M 31s
267150K .......... .......... .......... .......... .......... 52% 9.63M 31s
267200K .......... .......... .......... .......... .......... 52% 9.05M 31s
267250K .......... .......... .......... .......... .......... 52% 17.5M 31s
267300K .......... .......... .......... .......... .......... 52% 16.1M 31s
267350K .......... .......... .......... .......... .......... 52% 8.58M 31s
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267750K .......... .......... .......... .......... .......... 53% 9.23M 31s
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267850K .......... .......... .......... .......... .......... 53% 8.91M 31s
267900K .......... .......... .......... .......... .......... 53% 8.83M 31s
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268000K .......... .......... .......... .......... .......... 53% 8.43M 31s
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268100K .......... .......... .......... .......... .......... 53% 12.3M 31s
268150K .......... .......... .......... .......... .......... 53% 11.6M 31s
268200K .......... .......... .......... .......... .......... 53% 8.67M 31s
268250K .......... .......... .......... .......... .......... 53% 13.9M 31s
268300K .......... .......... .......... .......... .......... 53% 9.36M 31s
268350K .......... .......... .......... .......... .......... 53% 7.06M 31s
268400K .......... .......... .......... .......... .......... 53% 15.1M 31s
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268500K .......... .......... .......... .......... .......... 53% 33.8M 31s
268550K .......... .......... .......... .......... .......... 53% 16.8M 31s
268600K .......... .......... .......... .......... .......... 53% 24.5M 31s
268650K .......... .......... .......... .......... .......... 53% 11.1M 31s
268700K .......... .......... .......... .......... .......... 53% 14.6M 31s
268750K .......... .......... .......... .......... .......... 53% 16.2M 31s
268800K .......... .......... .......... .......... .......... 53% 16.9M 31s
268850K .......... .......... .......... .......... .......... 53% 10.7M 31s
268900K .......... .......... .......... .......... .......... 53% 17.6M 31s
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269000K .......... .......... .......... .......... .......... 53% 18.1M 31s
269050K .......... .......... .......... .......... .......... 53% 31.1M 31s
269100K .......... .......... .......... .......... .......... 53% 9.15M 31s
269150K .......... .......... .......... .......... .......... 53% 11.6M 31s
269200K .......... .......... .......... .......... .......... 53% 33.6M 31s
269250K .......... .......... .......... .......... .......... 53% 14.3M 31s
269300K .......... .......... .......... .......... .......... 53% 12.5M 31s
269350K .......... .......... .......... .......... .......... 53% 18.3M 31s
269400K .......... .......... .......... .......... .......... 53% 13.8M 31s
269450K .......... .......... .......... .......... .......... 53% 19.3M 31s
269500K .......... .......... .......... .......... .......... 53% 14.5M 31s
269550K .......... .......... .......... .......... .......... 53% 24.8M 31s
269600K .......... .......... .......... .......... .......... 53% 11.6M 31s
269650K .......... .......... .......... .......... .......... 53% 26.7M 31s
269700K .......... .......... .......... .......... .......... 53% 18.1M 31s
269750K .......... .......... .......... .......... .......... 53% 12.6M 31s
269800K .......... .......... .......... .......... .......... 53% 11.8M 31s
269850K .......... .......... .......... .......... .......... 53% 11.7M 31s
269900K .......... .......... .......... .......... .......... 53% 24.2M 31s
269950K .......... .......... .......... .......... .......... 53% 13.2M 31s
270000K .......... .......... .......... .......... .......... 53% 30.1M 31s
270050K .......... .......... .......... .......... .......... 53% 11.5M 31s
270100K .......... .......... .......... .......... .......... 53% 12.0M 31s
270150K .......... .......... .......... .......... .......... 53% 14.2M 31s
270200K .......... .......... .......... .......... .......... 53% 12.3M 31s
270250K .......... .......... .......... .......... .......... 53% 16.3M 31s
270300K .......... .......... .......... .......... .......... 53% 15.2M 30s
270350K .......... .......... .......... .......... .......... 53% 12.7M 30s
270400K .......... .......... .......... .......... .......... 53% 9.33M 30s
270450K .......... .......... .......... .......... .......... 53% 11.9M 30s
270500K .......... .......... .......... .......... .......... 53% 12.3M 30s
270550K .......... .......... .......... .......... .......... 53% 38.0M 30s
270600K .......... .......... .......... .......... .......... 53% 12.8M 30s
270650K .......... .......... .......... .......... .......... 53% 17.1M 30s
270700K .......... .......... .......... .......... .......... 53% 16.3M 30s
270750K .......... .......... .......... .......... .......... 53% 12.7M 30s
270800K .......... .......... .......... .......... .......... 53% 31.9M 30s
270850K .......... .......... .......... .......... .......... 53% 11.1M 30s
270900K .......... .......... .......... .......... .......... 53% 28.8M 30s
270950K .......... .......... .......... .......... .......... 53% 14.3M 30s
271000K .......... .......... .......... .......... .......... 53% 29.6M 30s
271050K .......... .......... .......... .......... .......... 53% 18.0M 30s
271100K .......... .......... .......... .......... .......... 53% 12.5M 30s
271150K .......... .......... .......... .......... .......... 53% 18.5M 30s
271200K .......... .......... .......... .......... .......... 53% 12.5M 30s
271250K .......... .......... .......... .......... .......... 53% 18.7M 30s
271300K .......... .......... .......... .......... .......... 53% 9.48M 30s
271350K .......... .......... .......... .......... .......... 53% 19.3M 30s
271400K .......... .......... .......... .......... .......... 53% 40.5M 30s
271450K .......... .......... .......... .......... .......... 53% 8.34M 30s
271500K .......... .......... .......... .......... .......... 53% 32.1M 30s
271550K .......... .......... .......... .......... .......... 53% 12.2M 30s
271600K .......... .......... .......... .......... .......... 53% 15.0M 30s
271650K .......... .......... .......... .......... .......... 53% 27.5M 30s
271700K .......... .......... .......... .......... .......... 53% 15.5M 30s
271750K .......... .......... .......... .......... .......... 53% 15.3M 30s
271800K .......... .......... .......... .......... .......... 53% 14.7M 30s
271850K .......... .......... .......... .......... .......... 53% 12.3M 30s
271900K .......... .......... .......... .......... .......... 53% 17.2M 30s
271950K .......... .......... .......... .......... .......... 53% 6.05M 30s
272000K .......... .......... .......... .......... .......... 53% 13.2M 30s
272050K .......... .......... .......... .......... .......... 53% 16.0M 30s
272100K .......... .......... .......... .......... .......... 53% 12.3M 30s
272150K .......... .......... .......... .......... .......... 53% 11.5M 30s
272200K .......... .......... .......... .......... .......... 53% 15.9M 30s
272250K .......... .......... .......... .......... .......... 53% 18.4M 30s
272300K .......... .......... .......... .......... .......... 53% 18.2M 30s
272350K .......... .......... .......... .......... .......... 53% 12.0M 30s
272400K .......... .......... .......... .......... .......... 53% 17.0M 30s
272450K .......... .......... .......... .......... .......... 53% 11.1M 30s
272500K .......... .......... .......... .......... .......... 53% 8.37M 30s
272550K .......... .......... .......... .......... .......... 53% 18.1M 30s
272600K .......... .......... .......... .......... .......... 54% 12.6M 30s
272650K .......... .......... .......... .......... .......... 54% 9.26M 30s
272700K .......... .......... .......... .......... .......... 54% 33.7M 30s
272750K .......... .......... .......... .......... .......... 54% 15.6M 30s
272800K .......... .......... .......... .......... .......... 54% 31.8M 30s
272850K .......... .......... .......... .......... .......... 54% 12.7M 30s
272900K .......... .......... .......... .......... .......... 54% 15.2M 30s
272950K .......... .......... .......... .......... .......... 54% 14.0M 30s
273000K .......... .......... .......... .......... .......... 54% 12.1M 30s
273050K .......... .......... .......... .......... .......... 54% 19.0M 30s
273100K .......... .......... .......... .......... .......... 54% 13.6M 30s
273150K .......... .......... .......... .......... .......... 54% 26.6M 30s
273200K .......... .......... .......... .......... .......... 54% 12.0M 30s
273250K .......... .......... .......... .......... .......... 54% 9.23M 30s
273300K .......... .......... .......... .......... .......... 54% 8.95M 30s
273350K .......... .......... .......... .......... .......... 54% 12.3M 30s
273400K .......... .......... .......... .......... .......... 54% 207M 30s
273450K .......... .......... .......... .......... .......... 54% 13.0M 30s
273500K .......... .......... .......... .......... .......... 54% 26.6M 30s
273550K .......... .......... .......... .......... .......... 54% 14.4M 30s
273600K .......... .......... .......... .......... .......... 54% 16.3M 30s
273650K .......... .......... .......... .......... .......... 54% 13.9M 30s
273700K .......... .......... .......... .......... .......... 54% 14.6M 30s
273750K .......... .......... .......... .......... .......... 54% 12.2M 30s
273800K .......... .......... .......... .......... .......... 54% 26.7M 30s
273850K .......... .......... .......... .......... .......... 54% 12.8M 30s
273900K .......... .......... .......... .......... .......... 54% 11.1M 30s
273950K .......... .......... .......... .......... .......... 54% 11.1M 30s
274000K .......... .......... .......... .......... .......... 54% 11.3M 30s
274050K .......... .......... .......... .......... .......... 54% 30.1M 30s
274100K .......... .......... .......... .......... .......... 54% 21.8M 30s
274150K .......... .......... .......... .......... .......... 54% 18.7M 30s
274200K .......... .......... .......... .......... .......... 54% 19.2M 30s
274250K .......... .......... .......... .......... .......... 54% 105M 30s
274300K .......... .......... .......... .......... .......... 54% 18.8M 30s
274350K .......... .......... .......... .......... .......... 54% 23.5M 30s
274400K .......... .......... .......... .......... .......... 54% 19.7M 30s
274450K .......... .......... .......... .......... .......... 54% 18.0M 30s
274500K .......... .......... .......... .......... .......... 54% 131M 30s
274550K .......... .......... .......... .......... .......... 54% 22.2M 30s
274600K .......... .......... .......... .......... .......... 54% 21.1M 30s
274650K .......... .......... .......... .......... .......... 54% 27.6M 30s
274700K .......... .......... .......... .......... .......... 54% 21.6M 30s
274750K .......... .......... .......... .......... .......... 54% 28.7M 30s
274800K .......... .......... .......... .......... .......... 54% 9.52M 30s
274850K .......... .......... .......... .......... .......... 54% 38.7M 30s
274900K .......... .......... .......... .......... .......... 54% 17.3M 30s
274950K .......... .......... .......... .......... .......... 54% 27.6M 30s
275000K .......... .......... .......... .......... .......... 54% 13.2M 30s
275050K .......... .......... .......... .......... .......... 54% 11.5M 30s
275100K .......... .......... .......... .......... .......... 54% 17.2M 30s
275150K .......... .......... .......... .......... .......... 54% 23.6M 30s
275200K .......... .......... .......... .......... .......... 54% 11.7M 30s
275250K .......... .......... .......... .......... .......... 54% 21.4M 30s
275300K .......... .......... .......... .......... .......... 54% 11.9M 30s
275350K .......... .......... .......... .......... .......... 54% 12.1M 30s
275400K .......... .......... .......... .......... .......... 54% 17.6M 30s
275450K .......... .......... .......... .......... .......... 54% 10.9M 30s
275500K .......... .......... .......... .......... .......... 54% 16.6M 30s
275550K .......... .......... .......... .......... .......... 54% 9.59M 30s
275600K .......... .......... .......... .......... .......... 54% 24.1M 30s
275650K .......... .......... .......... .......... .......... 54% 19.7M 30s
275700K .......... .......... .......... .......... .......... 54% 10.5M 29s
275750K .......... .......... .......... .......... .......... 54% 11.2M 29s
275800K .......... .......... .......... .......... .......... 54% 11.1M 29s
275850K .......... .......... .......... .......... .......... 54% 11.1M 29s
275900K .......... .......... .......... .......... .......... 54% 11.5M 29s
275950K .......... .......... .......... .......... .......... 54% 13.5M 29s
276000K .......... .......... .......... .......... .......... 54% 9.53M 29s
276050K .......... .......... .......... .......... .......... 54% 9.09M 29s
276100K .......... .......... .......... .......... .......... 54% 7.59M 29s
276150K .......... .......... .......... .......... .......... 54% 18.6M 29s
276200K .......... .......... .......... .......... .......... 54% 8.86M 29s
276250K .......... .......... .......... .......... .......... 54% 17.7M 29s
276300K .......... .......... .......... .......... .......... 54% 10.3M 29s
276350K .......... .......... .......... .......... .......... 54% 12.2M 29s
276400K .......... .......... .......... .......... .......... 54% 16.1M 29s
276450K .......... .......... .......... .......... .......... 54% 8.96M 29s
276500K .......... .......... .......... .......... .......... 54% 16.1M 29s
276550K .......... .......... .......... .......... .......... 54% 8.60M 29s
276600K .......... .......... .......... .......... .......... 54% 6.77M 29s
276650K .......... .......... .......... .......... .......... 54% 10.7M 29s
276700K .......... .......... .......... .......... .......... 54% 5.99M 29s
276750K .......... .......... .......... .......... .......... 54% 11.8M 29s
276800K .......... .......... .......... .......... .......... 54% 7.47M 29s
276850K .......... .......... .......... .......... .......... 54% 5.24M 29s
276900K .......... .......... .......... .......... .......... 54% 4.68M 29s
276950K .......... .......... .......... .......... .......... 54% 12.1M 29s
277000K .......... .......... .......... .......... .......... 54% 15.6M 29s
277050K .......... .......... .......... .......... .......... 54% 14.1M 29s
277100K .......... .......... .......... .......... .......... 54% 15.2M 29s
277150K .......... .......... .......... .......... .......... 54% 11.7M 29s
277200K .......... .......... .......... .......... .......... 54% 11.5M 29s
277250K .......... .......... .......... .......... .......... 54% 25.2M 29s
277300K .......... .......... .......... .......... .......... 54% 11.1M 29s
277350K .......... .......... .......... .......... .......... 54% 18.8M 29s
277400K .......... .......... .......... .......... .......... 54% 12.4M 29s
277450K .......... .......... .......... .......... .......... 54% 19.5M 29s
277500K .......... .......... .......... .......... .......... 54% 22.0M 29s
277550K .......... .......... .......... .......... .......... 54% 126M 29s
277600K .......... .......... .......... .......... .......... 54% 13.1M 29s
277650K .......... .......... .......... .......... .......... 55% 11.4M 29s
277700K .......... .......... .......... .......... .......... 55% 16.8M 29s
277750K .......... .......... .......... .......... .......... 55% 23.3M 29s
277800K .......... .......... .......... .......... .......... 55% 31.5M 29s
277850K .......... .......... .......... .......... .......... 55% 17.3M 29s
277900K .......... .......... .......... .......... .......... 55% 14.4M 29s
277950K .......... .......... .......... .......... .......... 55% 32.2M 29s
278000K .......... .......... .......... .......... .......... 55% 18.8M 29s
278050K .......... .......... .......... .......... .......... 55% 28.0M 29s
278100K .......... .......... .......... .......... .......... 55% 27.2M 29s
278150K .......... .......... .......... .......... .......... 55% 17.6M 29s
278200K .......... .......... .......... .......... .......... 55% 15.8M 29s
278250K .......... .......... .......... .......... .......... 55% 26.3M 29s
278300K .......... .......... .......... .......... .......... 55% 18.1M 29s
278350K .......... .......... .......... .......... .......... 55% 26.7M 29s
278400K .......... .......... .......... .......... .......... 55% 27.1M 29s
278450K .......... .......... .......... .......... .......... 55% 9.38M 29s
278500K .......... .......... .......... .......... .......... 55% 53.7M 29s
278550K .......... .......... .......... .......... .......... 55% 12.3M 29s
278600K .......... .......... .......... .......... .......... 55% 12.2M 29s
278650K .......... .......... .......... .......... .......... 55% 18.0M 29s
278700K .......... .......... .......... .......... .......... 55% 10.6M 29s
278750K .......... .......... .......... .......... .......... 55% 12.6M 29s
278800K .......... .......... .......... .......... .......... 55% 17.2M 29s
278850K .......... .......... .......... .......... .......... 55% 10.8M 29s
278900K .......... .......... .......... .......... .......... 55% 13.7M 29s
278950K .......... .......... .......... .......... .......... 55% 15.0M 29s
279000K .......... .......... .......... .......... .......... 55% 19.1M 29s
279050K .......... .......... .......... .......... .......... 55% 16.0M 29s
279100K .......... .......... .......... .......... .......... 55% 17.7M 29s
279150K .......... .......... .......... .......... .......... 55% 18.0M 29s
279200K .......... .......... .......... .......... .......... 55% 5.97M 29s
279250K .......... .......... .......... .......... .......... 55% 158M 29s
279300K .......... .......... .......... .......... .......... 55% 47.9M 29s
279350K .......... .......... .......... .......... .......... 55% 10.2M 29s
279400K .......... .......... .......... .......... .......... 55% 40.5M 29s
279450K .......... .......... .......... .......... .......... 55% 9.47M 29s
279500K .......... .......... .......... .......... .......... 55% 17.7M 29s
279550K .......... .......... .......... .......... .......... 55% 12.3M 29s
279600K .......... .......... .......... .......... .......... 55% 18.0M 29s
279650K .......... .......... .......... .......... .......... 55% 14.4M 29s
279700K .......... .......... .......... .......... .......... 55% 15.1M 29s
279750K .......... .......... .......... .......... .......... 55% 24.0M 29s
279800K .......... .......... .......... .......... .......... 55% 14.9M 29s
279850K .......... .......... .......... .......... .......... 55% 26.4M 29s
279900K .......... .......... .......... .......... .......... 55% 6.20M 29s
279950K .......... .......... .......... .......... .......... 55% 9.14M 29s
280000K .......... .......... .......... .......... .......... 55% 8.98M 29s
280050K .......... .......... .......... .......... .......... 55% 8.85M 29s
280100K .......... .......... .......... .......... .......... 55% 6.07M 29s
280150K .......... .......... .......... .......... .......... 55% 9.22M 29s
280200K .......... .......... .......... .......... .......... 55% 7.23M 29s
280250K .......... .......... .......... .......... .......... 55% 9.50M 29s
280300K .......... .......... .......... .......... .......... 55% 6.32M 29s
280350K .......... .......... .......... .......... .......... 55% 6.12M 29s
280400K .......... .......... .......... .......... .......... 55% 6.98M 29s
280450K .......... .......... .......... .......... .......... 55% 6.07M 29s
280500K .......... .......... .......... .......... .......... 55% 6.06M 29s
280550K .......... .......... .......... .......... .......... 55% 5.22M 29s
280600K .......... .......... .......... .......... .......... 55% 3.32M 29s
280650K .......... .......... .......... .......... .......... 55% 8.99M 29s
280700K .......... .......... .......... .......... .......... 55% 9.29M 29s
280750K .......... .......... .......... .......... .......... 55% 12.1M 29s
280800K .......... .......... .......... .......... .......... 55% 11.3M 29s
280850K .......... .......... .......... .......... .......... 55% 8.16M 29s
280900K .......... .......... .......... .......... .......... 55% 9.11M 29s
280950K .......... .......... .......... .......... .......... 55% 8.69M 29s
281000K .......... .......... .......... .......... .......... 55% 8.90M 29s
281050K .......... .......... .......... .......... .......... 55% 9.51M 29s
281100K .......... .......... .......... .......... .......... 55% 7.02M 29s
281150K .......... .......... .......... .......... .......... 55% 11.6M 29s
281200K .......... .......... .......... .......... .......... 55% 8.63M 29s
281250K .......... .......... .......... .......... .......... 55% 11.6M 29s
281300K .......... .......... .......... .......... .......... 55% 18.4M 29s
281350K .......... .......... .......... .......... .......... 55% 9.21M 29s
281400K .......... .......... .......... .......... .......... 55% 10.1M 29s
281450K .......... .......... .......... .......... .......... 55% 6.21M 29s
281500K .......... .......... .......... .......... .......... 55% 6.15M 29s
281550K .......... .......... .......... .......... .......... 55% 18.6M 29s
281600K .......... .......... .......... .......... .......... 55% 14.8M 29s
281650K .......... .......... .......... .......... .......... 55% 26.3M 29s
281700K .......... .......... .......... .......... .......... 55% 11.0M 29s
281750K .......... .......... .......... .......... .......... 55% 16.9M 29s
281800K .......... .......... .......... .......... .......... 55% 32.0M 29s
281850K .......... .......... .......... .......... .......... 55% 11.2M 29s
281900K .......... .......... .......... .......... .......... 55% 17.8M 28s
281950K .......... .......... .......... .......... .......... 55% 12.4M 28s
282000K .......... .......... .......... .......... .......... 55% 17.9M 28s
282050K .......... .......... .......... .......... .......... 55% 17.9M 28s
282100K .......... .......... .......... .......... .......... 55% 8.89M 28s
282150K .......... .......... .......... .......... .......... 55% 7.24M 28s
282200K .......... .......... .......... .......... .......... 55% 18.8M 28s
282250K .......... .......... .......... .......... .......... 55% 12.4M 28s
282300K .......... .......... .......... .......... .......... 55% 17.0M 28s
282350K .......... .......... .......... .......... .......... 55% 17.6M 28s
282400K .......... .......... .......... .......... .......... 55% 12.5M 28s
282450K .......... .......... .......... .......... .......... 55% 9.18M 28s
282500K .......... .......... .......... .......... .......... 55% 17.9M 28s
282550K .......... .......... .......... .......... .......... 55% 17.8M 28s
282600K .......... .......... .......... .......... .......... 55% 16.1M 28s
282650K .......... .......... .......... .......... .......... 55% 17.4M 28s
282700K .......... .......... .......... .......... .......... 56% 11.0M 28s
282750K .......... .......... .......... .......... .......... 56% 11.2M 28s
282800K .......... .......... .......... .......... .......... 56% 11.6M 28s
282850K .......... .......... .......... .......... .......... 56% 17.6M 28s
282900K .......... .......... .......... .......... .......... 56% 11.6M 28s
282950K .......... .......... .......... .......... .......... 56% 27.5M 28s
283000K .......... .......... .......... .......... .......... 56% 12.8M 28s
283050K .......... .......... .......... .......... .......... 56% 16.4M 28s
283100K .......... .......... .......... .......... .......... 56% 10.7M 28s
283150K .......... .......... .......... .......... .......... 56% 19.9M 28s
283200K .......... .......... .......... .......... .......... 56% 15.4M 28s
283250K .......... .......... .......... .......... .......... 56% 13.6M 28s
283300K .......... .......... .......... .......... .......... 56% 18.6M 28s
283350K .......... .......... .......... .......... .......... 56% 13.4M 28s
283400K .......... .......... .......... .......... .......... 56% 17.7M 28s
283450K .......... .......... .......... .......... .......... 56% 11.8M 28s
283500K .......... .......... .......... .......... .......... 56% 17.5M 28s
283550K .......... .......... .......... .......... .......... 56% 8.57M 28s
283600K .......... .......... .......... .......... .......... 56% 15.0M 28s
283650K .......... .......... .......... .......... .......... 56% 20.8M 28s
283700K .......... .......... .......... .......... .......... 56% 28.9M 28s
283750K .......... .......... .......... .......... .......... 56% 15.6M 28s
283800K .......... .......... .......... .......... .......... 56% 16.8M 28s
283850K .......... .......... .......... .......... .......... 56% 28.2M 28s
283900K .......... .......... .......... .......... .......... 56% 14.6M 28s
283950K .......... .......... .......... .......... .......... 56% 11.9M 28s
284000K .......... .......... .......... .......... .......... 56% 17.5M 28s
284050K .......... .......... .......... .......... .......... 56% 12.3M 28s
284100K .......... .......... .......... .......... .......... 56% 25.1M 28s
284150K .......... .......... .......... .......... .......... 56% 12.5M 28s
284200K .......... .......... .......... .......... .......... 56% 16.5M 28s
284250K .......... .......... .......... .......... .......... 56% 19.9M 28s
284300K .......... .......... .......... .......... .......... 56% 17.4M 28s
284350K .......... .......... .......... .......... .......... 56% 9.75M 28s
284400K .......... .......... .......... .......... .......... 56% 45.1M 28s
284450K .......... .......... .......... .......... .......... 56% 9.28M 28s
284500K .......... .......... .......... .......... .......... 56% 21.5M 28s
284550K .......... .......... .......... .......... .......... 56% 16.8M 28s
284600K .......... .......... .......... .......... .......... 56% 12.9M 28s
284650K .......... .......... .......... .......... .......... 56% 16.9M 28s
284700K .......... .......... .......... .......... .......... 56% 11.8M 28s
284750K .......... .......... .......... .......... .......... 56% 14.8M 28s
284800K .......... .......... .......... .......... .......... 56% 18.7M 28s
284850K .......... .......... .......... .......... .......... 56% 32.3M 28s
284900K .......... .......... .......... .......... .......... 56% 11.9M 28s
284950K .......... .......... .......... .......... .......... 56% 24.0M 28s
285000K .......... .......... .......... .......... .......... 56% 15.6M 28s
285050K .......... .......... .......... .......... .......... 56% 17.0M 28s
285100K .......... .......... .......... .......... .......... 56% 9.27M 28s
285150K .......... .......... .......... .......... .......... 56% 18.9M 28s
285200K .......... .......... .......... .......... .......... 56% 13.1M 28s
285250K .......... .......... .......... .......... .......... 56% 17.8M 28s
285300K .......... .......... .......... .......... .......... 56% 14.9M 28s
285350K .......... .......... .......... .......... .......... 56% 15.3M 28s
285400K .......... .......... .......... .......... .......... 56% 17.5M 28s
285450K .......... .......... .......... .......... .......... 56% 14.0M 28s
285500K .......... .......... .......... .......... .......... 56% 18.1M 28s
285550K .......... .......... .......... .......... .......... 56% 11.0M 28s
285600K .......... .......... .......... .......... .......... 56% 17.4M 28s
285650K .......... .......... .......... .......... .......... 56% 24.5M 28s
285700K .......... .......... .......... .......... .......... 56% 13.1M 28s
285750K .......... .......... .......... .......... .......... 56% 17.7M 28s
285800K .......... .......... .......... .......... .......... 56% 7.58M 28s
285850K .......... .......... .......... .......... .......... 56% 89.3M 28s
285900K .......... .......... .......... .......... .......... 56% 9.26M 28s
285950K .......... .......... .......... .......... .......... 56% 29.6M 28s
286000K .......... .......... .......... .......... .......... 56% 17.9M 28s
286050K .......... .......... .......... .......... .......... 56% 12.7M 28s
286100K .......... .......... .......... .......... .......... 56% 15.2M 28s
286150K .......... .......... .......... .......... .......... 56% 17.3M 28s
286200K .......... .......... .......... .......... .......... 56% 11.4M 28s
286250K .......... .......... .......... .......... .......... 56% 18.2M 28s
286300K .......... .......... .......... .......... .......... 56% 11.4M 28s
286350K .......... .......... .......... .......... .......... 56% 24.9M 28s
286400K .......... .......... .......... .......... .......... 56% 11.7M 28s
286450K .......... .......... .......... .......... .......... 56% 9.13M 28s
286500K .......... .......... .......... .......... .......... 56% 17.6M 28s
286550K .......... .......... .......... .......... .......... 56% 18.0M 28s
286600K .......... .......... .......... .......... .......... 56% 24.6M 28s
286650K .......... .......... .......... .......... .......... 56% 18.4M 28s
286700K .......... .......... .......... .......... .......... 56% 16.5M 28s
286750K .......... .......... .......... .......... .......... 56% 19.6M 28s
286800K .......... .......... .......... .......... .......... 56% 26.3M 28s
286850K .......... .......... .......... .......... .......... 56% 17.9M 28s
286900K .......... .......... .......... .......... .......... 56% 11.9M 28s
286950K .......... .......... .......... .......... .......... 56% 20.8M 28s
287000K .......... .......... .......... .......... .......... 56% 21.4M 28s
287050K .......... .......... .......... .......... .......... 56% 30.0M 28s
287100K .......... .......... .......... .......... .......... 56% 18.2M 28s
287150K .......... .......... .......... .......... .......... 56% 22.0M 28s
287200K .......... .......... .......... .......... .......... 56% 17.7M 28s
287250K .......... .......... .......... .......... .......... 56% 18.7M 28s
287300K .......... .......... .......... .......... .......... 56% 18.3M 28s
287350K .......... .......... .......... .......... .......... 56% 172M 28s
287400K .......... .......... .......... .......... .......... 56% 15.1M 28s
287450K .......... .......... .......... .......... .......... 56% 6.31M 28s
287500K .......... .......... .......... .......... .......... 56% 124M 28s
287550K .......... .......... .......... .......... .......... 56% 163M 27s
287600K .......... .......... .......... .......... .......... 56% 17.6M 27s
287650K .......... .......... .......... .......... .......... 56% 23.9M 27s
287700K .......... .......... .......... .......... .......... 56% 11.5M 27s
287750K .......... .......... .......... .......... .......... 57% 31.3M 27s
287800K .......... .......... .......... .......... .......... 57% 17.8M 27s
287850K .......... .......... .......... .......... .......... 57% 12.5M 27s
287900K .......... .......... .......... .......... .......... 57% 32.7M 27s
287950K .......... .......... .......... .......... .......... 57% 12.4M 27s
288000K .......... .......... .......... .......... .......... 57% 27.8M 27s
288050K .......... .......... .......... .......... .......... 57% 18.5M 27s
288100K .......... .......... .......... .......... .......... 57% 18.6M 27s
288150K .......... .......... .......... .......... .......... 57% 16.7M 27s
288200K .......... .......... .......... .......... .......... 57% 15.7M 27s
288250K .......... .......... .......... .......... .......... 57% 9.26M 27s
288300K .......... .......... .......... .......... .......... 57% 17.4M 27s
288350K .......... .......... .......... .......... .......... 57% 16.5M 27s
288400K .......... .......... .......... .......... .......... 57% 13.3M 27s
288450K .......... .......... .......... .......... .......... 57% 17.8M 27s
288500K .......... .......... .......... .......... .......... 57% 12.4M 27s
288550K .......... .......... .......... .......... .......... 57% 11.4M 27s
288600K .......... .......... .......... .......... .......... 57% 15.6M 27s
288650K .......... .......... .......... .......... .......... 57% 12.6M 27s
288700K .......... .......... .......... .......... .......... 57% 8.92M 27s
288750K .......... .......... .......... .......... .......... 57% 18.0M 27s
288800K .......... .......... .......... .......... .......... 57% 12.8M 27s
288850K .......... .......... .......... .......... .......... 57% 9.98M 27s
288900K .......... .......... .......... .......... .......... 57% 16.3M 27s
288950K .......... .......... .......... .......... .......... 57% 18.5M 27s
289000K .......... .......... .......... .......... .......... 57% 18.8M 27s
289050K .......... .......... .......... .......... .......... 57% 19.9M 27s
289100K .......... .......... .......... .......... .......... 57% 17.7M 27s
289150K .......... .......... .......... .......... .......... 57% 10.9M 27s
289200K .......... .......... .......... .......... .......... 57% 12.3M 27s
289250K .......... .......... .......... .......... .......... 57% 12.5M 27s
289300K .......... .......... .......... .......... .......... 57% 16.1M 27s
289350K .......... .......... .......... .......... .......... 57% 15.7M 27s
289400K .......... .......... .......... .......... .......... 57% 13.0M 27s
289450K .......... .......... .......... .......... .......... 57% 12.6M 27s
289500K .......... .......... .......... .......... .......... 57% 30.6M 27s
289550K .......... .......... .......... .......... .......... 57% 9.61M 27s
289600K .......... .......... .......... .......... .......... 57% 9.36M 27s
289650K .......... .......... .......... .......... .......... 57% 7.45M 27s
289700K .......... .......... .......... .......... .......... 57% 7.15M 27s
289750K .......... .......... .......... .......... .......... 57% 10.8M 27s
289800K .......... .......... .......... .......... .......... 57% 8.84M 27s
289850K .......... .......... .......... .......... .......... 57% 9.22M 27s
289900K .......... .......... .......... .......... .......... 57% 8.78M 27s
289950K .......... .......... .......... .......... .......... 57% 6.19M 27s
290000K .......... .......... .......... .......... .......... 57% 7.45M 27s
290050K .......... .......... .......... .......... .......... 57% 13.2M 27s
290100K .......... .......... .......... .......... .......... 57% 13.4M 27s
290150K .......... .......... .......... .......... .......... 57% 18.3M 27s
290200K .......... .......... .......... .......... .......... 57% 9.59M 27s
290250K .......... .......... .......... .......... .......... 57% 10.9M 27s
290300K .......... .......... .......... .......... .......... 57% 17.3M 27s
290350K .......... .......... .......... .......... .......... 57% 11.5M 27s
290400K .......... .......... .......... .......... .......... 57% 16.8M 27s
290450K .......... .......... .......... .......... .......... 57% 11.1M 27s
290500K .......... .......... .......... .......... .......... 57% 11.3M 27s
290550K .......... .......... .......... .......... .......... 57% 9.49M 27s
290600K .......... .......... .......... .......... .......... 57% 15.7M 27s
290650K .......... .......... .......... .......... .......... 57% 8.98M 27s
290700K .......... .......... .......... .......... .......... 57% 14.6M 27s
290750K .......... .......... .......... .......... .......... 57% 11.8M 27s
290800K .......... .......... .......... .......... .......... 57% 18.1M 27s
290850K .......... .......... .......... .......... .......... 57% 9.63M 27s
290900K .......... .......... .......... .......... .......... 57% 15.1M 27s
290950K .......... .......... .......... .......... .......... 57% 11.9M 27s
291000K .......... .......... .......... .......... .......... 57% 20.3M 27s
291050K .......... .......... .......... .......... .......... 57% 16.1M 27s
291100K .......... .......... .......... .......... .......... 57% 12.5M 27s
291150K .......... .......... .......... .......... .......... 57% 11.0M 27s
291200K .......... .......... .......... .......... .......... 57% 12.8M 27s
291250K .......... .......... .......... .......... .......... 57% 33.1M 27s
291300K .......... .......... .......... .......... .......... 57% 25.5M 27s
291350K .......... .......... .......... .......... .......... 57% 13.8M 27s
291400K .......... .......... .......... .......... .......... 57% 17.9M 27s
291450K .......... .......... .......... .......... .......... 57% 17.0M 27s
291500K .......... .......... .......... .......... .......... 57% 12.3M 27s
291550K .......... .......... .......... .......... .......... 57% 29.3M 27s
291600K .......... .......... .......... .......... .......... 57% 11.7M 27s
291650K .......... .......... .......... .......... .......... 57% 27.1M 27s
291700K .......... .......... .......... .......... .......... 57% 11.7M 27s
291750K .......... .......... .......... .......... .......... 57% 24.8M 27s
291800K .......... .......... .......... .......... .......... 57% 8.93M 27s
291850K .......... .......... .......... .......... .......... 57% 11.5M 27s
291900K .......... .......... .......... .......... .......... 57% 8.86M 27s
291950K .......... .......... .......... .......... .......... 57% 20.5M 27s
292000K .......... .......... .......... .......... .......... 57% 33.1M 27s
292050K .......... .......... .......... .......... .......... 57% 11.6M 27s
292100K .......... .......... .......... .......... .......... 57% 11.4M 27s
292150K .......... .......... .......... .......... .......... 57% 10.4M 27s
292200K .......... .......... .......... .......... .......... 57% 15.9M 27s
292250K .......... .......... .......... .......... .......... 57% 12.5M 27s
292300K .......... .......... .......... .......... .......... 57% 17.7M 27s
292350K .......... .......... .......... .......... .......... 57% 10.5M 27s
292400K .......... .......... .......... .......... .......... 57% 17.7M 27s
292450K .......... .......... .......... .......... .......... 57% 9.09M 27s
292500K .......... .......... .......... .......... .......... 57% 9.36M 27s
292550K .......... .......... .......... .......... .......... 57% 11.9M 27s
292600K .......... .......... .......... .......... .......... 57% 11.9M 27s
292650K .......... .......... .......... .......... .......... 57% 12.5M 27s
292700K .......... .......... .......... .......... .......... 57% 16.1M 27s
292750K .......... .......... .......... .......... .......... 57% 12.1M 27s
292800K .......... .......... .......... .......... .......... 58% 11.9M 27s
292850K .......... .......... .......... .......... .......... 58% 14.5M 27s
292900K .......... .......... .......... .......... .......... 58% 11.4M 27s
292950K .......... .......... .......... .......... .......... 58% 7.86M 27s
293000K .......... .......... .......... .......... .......... 58% 17.4M 27s
293050K .......... .......... .......... .......... .......... 58% 24.4M 27s
293100K .......... .......... .......... .......... .......... 58% 21.9M 27s
293150K .......... .......... .......... .......... .......... 58% 19.1M 27s
293200K .......... .......... .......... .......... .......... 58% 21.1M 27s
293250K .......... .......... .......... .......... .......... 58% 20.3M 27s
293300K .......... .......... .......... .......... .......... 58% 37.6M 27s
293350K .......... .......... .......... .......... .......... 58% 15.3M 27s
293400K .......... .......... .......... .......... .......... 58% 18.8M 27s
293450K .......... .......... .......... .......... .......... 58% 30.1M 27s
293500K .......... .......... .......... .......... .......... 58% 27.9M 27s
293550K .......... .......... .......... .......... .......... 58% 19.8M 26s
293600K .......... .......... .......... .......... .......... 58% 22.9M 26s
293650K .......... .......... .......... .......... .......... 58% 18.8M 26s
293700K .......... .......... .......... .......... .......... 58% 18.1M 26s
293750K .......... .......... .......... .......... .......... 58% 29.5M 26s
293800K .......... .......... .......... .......... .......... 58% 20.8M 26s
293850K .......... .......... .......... .......... .......... 58% 11.7M 26s
293900K .......... .......... .......... .......... .......... 58% 18.3M 26s
293950K .......... .......... .......... .......... .......... 58% 26.4M 26s
294000K .......... .......... .......... .......... .......... 58% 25.2M 26s
294050K .......... .......... .......... .......... .......... 58% 22.1M 26s
294100K .......... .......... .......... .......... .......... 58% 7.16M 26s
294150K .......... .......... .......... .......... .......... 58% 137M 26s
294200K .......... .......... .......... .......... .......... 58% 22.5M 26s
294250K .......... .......... .......... .......... .......... 58% 22.8M 26s
294300K .......... .......... .......... .......... .......... 58% 25.1M 26s
294350K .......... .......... .......... .......... .......... 58% 12.1M 26s
294400K .......... .......... .......... .......... .......... 58% 28.6M 26s
294450K .......... .......... .......... .......... .......... 58% 10.3M 26s
294500K .......... .......... .......... .......... .......... 58% 29.1M 26s
294550K .......... .......... .......... .......... .......... 58% 21.0M 26s
294600K .......... .......... .......... .......... .......... 58% 14.0M 26s
294650K .......... .......... .......... .......... .......... 58% 29.6M 26s
294700K .......... .......... .......... .......... .......... 58% 16.0M 26s
294750K .......... .......... .......... .......... .......... 58% 12.3M 26s
294800K .......... .......... .......... .......... .......... 58% 24.9M 26s
294850K .......... .......... .......... .......... .......... 58% 20.8M 26s
294900K .......... .......... .......... .......... .......... 58% 22.2M 26s
294950K .......... .......... .......... .......... .......... 58% 17.9M 26s
295000K .......... .......... .......... .......... .......... 58% 20.0M 26s
295050K .......... .......... .......... .......... .......... 58% 8.07M 26s
295100K .......... .......... .......... .......... .......... 58% 94.8M 26s
295150K .......... .......... .......... .......... .......... 58% 25.0M 26s
295200K .......... .......... .......... .......... .......... 58% 10.5M 26s
295250K .......... .......... .......... .......... .......... 58% 26.9M 26s
295300K .......... .......... .......... .......... .......... 58% 29.2M 26s
295350K .......... .......... .......... .......... .......... 58% 23.1M 26s
295400K .......... .......... .......... .......... .......... 58% 17.6M 26s
295450K .......... .......... .......... .......... .......... 58% 17.9M 26s
295500K .......... .......... .......... .......... .......... 58% 17.5M 26s
295550K .......... .......... .......... .......... .......... 58% 18.2M 26s
295600K .......... .......... .......... .......... .......... 58% 18.7M 26s
295650K .......... .......... .......... .......... .......... 58% 17.6M 26s
295700K .......... .......... .......... .......... .......... 58% 17.7M 26s
295750K .......... .......... .......... .......... .......... 58% 18.8M 26s
295800K .......... .......... .......... .......... .......... 58% 18.1M 26s
295850K .......... .......... .......... .......... .......... 58% 15.9M 26s
295900K .......... .......... .......... .......... .......... 58% 14.6M 26s
295950K .......... .......... .......... .......... .......... 58% 8.96M 26s
296000K .......... .......... .......... .......... .......... 58% 41.5M 26s
296050K .......... .......... .......... .......... .......... 58% 16.0M 26s
296100K .......... .......... .......... .......... .......... 58% 17.8M 26s
296150K .......... .......... .......... .......... .......... 58% 18.2M 26s
296200K .......... .......... .......... .......... .......... 58% 16.5M 26s
296250K .......... .......... .......... .......... .......... 58% 27.4M 26s
296300K .......... .......... .......... .......... .......... 58% 13.6M 26s
296350K .......... .......... .......... .......... .......... 58% 20.2M 26s
296400K .......... .......... .......... .......... .......... 58% 17.0M 26s
296450K .......... .......... .......... .......... .......... 58% 11.2M 26s
296500K .......... .......... .......... .......... .......... 58% 17.9M 26s
296550K .......... .......... .......... .......... .......... 58% 26.9M 26s
296600K .......... .......... .......... .......... .......... 58% 22.5M 26s
296650K .......... .......... .......... .......... .......... 58% 19.4M 26s
296700K .......... .......... .......... .......... .......... 58% 16.9M 26s
296750K .......... .......... .......... .......... .......... 58% 19.5M 26s
296800K .......... .......... .......... .......... .......... 58% 15.7M 26s
296850K .......... .......... .......... .......... .......... 58% 30.5M 26s
296900K .......... .......... .......... .......... .......... 58% 11.8M 26s
296950K .......... .......... .......... .......... .......... 58% 21.4M 26s
297000K .......... .......... .......... .......... .......... 58% 17.7M 26s
297050K .......... .......... .......... .......... .......... 58% 17.6M 26s
297100K .......... .......... .......... .......... .......... 58% 14.9M 26s
297150K .......... .......... .......... .......... .......... 58% 18.7M 26s
297200K .......... .......... .......... .......... .......... 58% 23.6M 26s
297250K .......... .......... .......... .......... .......... 58% 18.1M 26s
297300K .......... .......... .......... .......... .......... 58% 20.9M 26s
297350K .......... .......... .......... .......... .......... 58% 10.9M 26s
297400K .......... .......... .......... .......... .......... 58% 28.0M 26s
297450K .......... .......... .......... .......... .......... 58% 13.5M 26s
297500K .......... .......... .......... .......... .......... 58% 16.7M 26s
297550K .......... .......... .......... .......... .......... 58% 16.0M 26s
297600K .......... .......... .......... .......... .......... 58% 15.3M 26s
297650K .......... .......... .......... .......... .......... 58% 17.5M 26s
297700K .......... .......... .......... .......... .......... 58% 11.7M 26s
297750K .......... .......... .......... .......... .......... 58% 155M 26s
297800K .......... .......... .......... .......... .......... 58% 19.2M 26s
297850K .......... .......... .......... .......... .......... 59% 13.0M 26s
297900K .......... .......... .......... .......... .......... 59% 11.6M 26s
297950K .......... .......... .......... .......... .......... 59% 17.9M 26s
298000K .......... .......... .......... .......... .......... 59% 11.4M 26s
298050K .......... .......... .......... .......... .......... 59% 28.5M 26s
298100K .......... .......... .......... .......... .......... 59% 12.4M 26s
298150K .......... .......... .......... .......... .......... 59% 24.5M 26s
298200K .......... .......... .......... .......... .......... 59% 10.3M 26s
298250K .......... .......... .......... .......... .......... 59% 25.4M 26s
298300K .......... .......... .......... .......... .......... 59% 12.8M 26s
298350K .......... .......... .......... .......... .......... 59% 11.4M 26s
298400K .......... .......... .......... .......... .......... 59% 31.6M 26s
298450K .......... .......... .......... .......... .......... 59% 17.0M 26s
298500K .......... .......... .......... .......... .......... 59% 19.7M 26s
298550K .......... .......... .......... .......... .......... 59% 19.2M 26s
298600K .......... .......... .......... .......... .......... 59% 17.3M 26s
298650K .......... .......... .......... .......... .......... 59% 13.9M 26s
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298850K .......... .......... .......... .......... .......... 59% 92.3M 26s
298900K .......... .......... .......... .......... .......... 59% 9.89M 26s
298950K .......... .......... .......... .......... .......... 59% 184M 26s
299000K .......... .......... .......... .......... .......... 59% 9.58M 26s
299050K .......... .......... .......... .......... .......... 59% 18.2M 26s
299100K .......... .......... .......... .......... .......... 59% 22.4M 26s
299150K .......... .......... .......... .......... .......... 59% 21.0M 26s
299200K .......... .......... .......... .......... .......... 59% 19.9M 26s
299250K .......... .......... .......... .......... .......... 59% 17.5M 26s
299300K .......... .......... .......... .......... .......... 59% 11.4M 26s
299350K .......... .......... .......... .......... .......... 59% 16.6M 25s
299400K .......... .......... .......... .......... .......... 59% 25.0M 25s
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299500K .......... .......... .......... .......... .......... 59% 17.5M 25s
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299850K .......... .......... .......... .......... .......... 59% 20.5M 25s
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301300K .......... .......... .......... .......... .......... 59% 22.3M 25s
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301400K .......... .......... .......... .......... .......... 59% 40.2M 25s
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301500K .......... .......... .......... .......... .......... 59% 18.8M 25s
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301600K .......... .......... .......... .......... .......... 59% 41.5M 25s
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301800K .......... .......... .......... .......... .......... 59% 40.5M 25s
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302000K .......... .......... .......... .......... .......... 59% 164M 25s
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302150K .......... .......... .......... .......... .......... 59% 41.3M 25s
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302800K .......... .......... .......... .......... .......... 59% 20.7M 25s
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303150K .......... .......... .......... .......... .......... 60% 12.9M 25s
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303250K .......... .......... .......... .......... .......... 60% 31.7M 25s
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303900K .......... .......... .......... .......... .......... 60% 25.7M 25s
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304000K .......... .......... .......... .......... .......... 60% 20.6M 25s
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304100K .......... .......... .......... .......... .......... 60% 23.8M 25s
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304200K .......... .......... .......... .......... .......... 60% 26.3M 25s
304250K .......... .......... .......... .......... .......... 60% 17.9M 25s
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304850K .......... .......... .......... .......... .......... 60% 89.4M 25s
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305000K .......... .......... .......... .......... .......... 60% 206M 24s
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305150K .......... .......... .......... .......... .......... 60% 163M 24s
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307000K .......... .......... .......... .......... .......... 60% 20.1M 24s
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307100K .......... .......... .......... .......... .......... 60% 18.1M 24s
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307250K .......... .......... .......... .......... .......... 60% 17.1M 24s
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307850K .......... .......... .......... .......... .......... 60% 19.0M 24s
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308000K .......... .......... .......... .......... .......... 61% 176M 24s
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308150K .......... .......... .......... .......... .......... 61% 18.7M 24s
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309000K .......... .......... .......... .......... .......... 61% 16.7M 24s
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309100K .......... .......... .......... .......... .......... 61% 16.7M 24s
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310400K .......... .......... .......... .......... .......... 61% 150M 24s
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310500K .......... .......... .......... .......... .......... 61% 95.9M 24s
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310600K .......... .......... .......... .......... .......... 61% 18.4M 23s
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310800K .......... .......... .......... .......... .......... 61% 190M 23s
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311300K .......... .......... .......... .......... .......... 61% 16.5M 23s
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311400K .......... .......... .......... .......... .......... 61% 15.2M 23s
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311600K .......... .......... .......... .......... .......... 61% 88.9M 23s
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311800K .......... .......... .......... .......... .......... 61% 14.9M 23s
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312250K .......... .......... .......... .......... .......... 61% 98.4M 23s
312300K .......... .......... .......... .......... .......... 61% 14.2M 23s
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312400K .......... .......... .......... .......... .......... 61% 12.9M 23s
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312950K .......... .......... .......... .......... .......... 61% 16.2M 23s
313000K .......... .......... .......... .......... .......... 62% 208M 23s
313050K .......... .......... .......... .......... .......... 62% 97.3M 23s
313100K .......... .......... .......... .......... .......... 62% 14.0M 23s
313150K .......... .......... .......... .......... .......... 62% 103M 23s
313200K .......... .......... .......... .......... .......... 62% 15.7M 23s
313250K .......... .......... .......... .......... .......... 62% 144M 23s
313300K .......... .......... .......... .......... .......... 62% 100M 23s
313350K .......... .......... .......... .......... .......... 62% 17.5M 23s
313400K .......... .......... .......... .......... .......... 62% 135M 23s
313450K .......... .......... .......... .......... .......... 62% 16.5M 23s
313500K .......... .......... .......... .......... .......... 62% 72.0M 23s
313550K .......... .......... .......... .......... .......... 62% 146M 23s
313600K .......... .......... .......... .......... .......... 62% 16.1M 23s
313650K .......... .......... .......... .......... .......... 62% 89.1M 23s
313700K .......... .......... .......... .......... .......... 62% 82.9M 23s
313750K .......... .......... .......... .......... .......... 62% 15.1M 23s
313800K .......... .......... .......... .......... .......... 62% 98.0M 23s
313850K .......... .......... .......... .......... .......... 62% 98.2M 23s
313900K .......... .......... .......... .......... .......... 62% 19.5M 23s
313950K .......... .......... .......... .......... .......... 62% 142M 23s
314000K .......... .......... .......... .......... .......... 62% 165M 23s
314050K .......... .......... .......... .......... .......... 62% 13.4M 23s
314100K .......... .......... .......... .......... .......... 62% 103M 23s
314150K .......... .......... .......... .......... .......... 62% 263M 23s
314200K .......... .......... .......... .......... .......... 62% 12.6M 23s
314250K .......... .......... .......... .......... .......... 62% 142M 23s
314300K .......... .......... .......... .......... .......... 62% 141M 23s
314350K .......... .......... .......... .......... .......... 62% 13.6M 23s
314400K .......... .......... .......... .......... .......... 62% 123M 23s
314450K .......... .......... .......... .......... .......... 62% 15.4M 23s
314500K .......... .......... .......... .......... .......... 62% 94.4M 23s
314550K .......... .......... .......... .......... .......... 62% 133M 23s
314600K .......... .......... .......... .......... .......... 62% 13.6M 23s
314650K .......... .......... .......... .......... .......... 62% 175M 23s
314700K .......... .......... .......... .......... .......... 62% 131M 23s
314750K .......... .......... .......... .......... .......... 62% 13.8M 23s
314800K .......... .......... .......... .......... .......... 62% 27.5M 23s
314850K .......... .......... .......... .......... .......... 62% 202M 23s
314900K .......... .......... .......... .......... .......... 62% 256M 23s
314950K .......... .......... .......... .......... .......... 62% 15.0M 23s
315000K .......... .......... .......... .......... .......... 62% 156M 23s
315050K .......... .......... .......... .......... .......... 62% 14.7M 23s
315100K .......... .......... .......... .......... .......... 62% 199M 23s
315150K .......... .......... .......... .......... .......... 62% 247M 23s
315200K .......... .......... .......... .......... .......... 62% 16.0M 23s
315250K .......... .......... .......... .......... .......... 62% 169M 23s
315300K .......... .......... .......... .......... .......... 62% 170M 23s
315350K .......... .......... .......... .......... .......... 62% 14.1M 23s
315400K .......... .......... .......... .......... .......... 62% 182M 23s
315450K .......... .......... .......... .......... .......... 62% 104M 23s
315500K .......... .......... .......... .......... .......... 62% 15.6M 23s
315550K .......... .......... .......... .......... .......... 62% 183M 23s
315600K .......... .......... .......... .......... .......... 62% 118M 23s
315650K .......... .......... .......... .......... .......... 62% 13.3M 23s
315700K .......... .......... .......... .......... .......... 62% 175M 23s
315750K .......... .......... .......... .......... .......... 62% 124M 23s
315800K .......... .......... .......... .......... .......... 62% 14.3M 23s
315850K .......... .......... .......... .......... .......... 62% 130M 23s
315900K .......... .......... .......... .......... .......... 62% 191M 23s
315950K .......... .......... .......... .......... .......... 62% 12.8M 23s
316000K .......... .......... .......... .......... .......... 62% 168M 23s
316050K .......... .......... .......... .......... .......... 62% 110M 23s
316100K .......... .......... .......... .......... .......... 62% 14.7M 23s
316150K .......... .......... .......... .......... .......... 62% 196M 23s
316200K .......... .......... .......... .......... .......... 62% 96.1M 23s
316250K .......... .......... .......... .......... .......... 62% 13.6M 22s
316300K .......... .......... .......... .......... .......... 62% 279M 22s
316350K .......... .......... .......... .......... .......... 62% 113M 22s
316400K .......... .......... .......... .......... .......... 62% 12.1M 22s
316450K .......... .......... .......... .......... .......... 62% 99.0M 22s
316500K .......... .......... .......... .......... .......... 62% 185M 22s
316550K .......... .......... .......... .......... .......... 62% 13.7M 22s
316600K .......... .......... .......... .......... .......... 62% 137M 22s
316650K .......... .......... .......... .......... .......... 62% 117M 22s
316700K .......... .......... .......... .......... .......... 62% 14.5M 22s
316750K .......... .......... .......... .......... .......... 62% 150M 22s
316800K .......... .......... .......... .......... .......... 62% 100M 22s
316850K .......... .......... .......... .......... .......... 62% 14.5M 22s
316900K .......... .......... .......... .......... .......... 62% 198M 22s
316950K .......... .......... .......... .......... .......... 62% 107M 22s
317000K .......... .......... .......... .......... .......... 62% 16.5M 22s
317050K .......... .......... .......... .......... .......... 62% 231M 22s
317100K .......... .......... .......... .......... .......... 62% 86.1M 22s
317150K .......... .......... .......... .......... .......... 62% 16.5M 22s
317200K .......... .......... .......... .......... .......... 62% 119M 22s
317250K .......... .......... .......... .......... .......... 62% 122M 22s
317300K .......... .......... .......... .......... .......... 62% 12.2M 22s
317350K .......... .......... .......... .......... .......... 62% 134M 22s
317400K .......... .......... .......... .......... .......... 62% 184M 22s
317450K .......... .......... .......... .......... .......... 62% 9.87M 22s
317500K .......... .......... .......... .......... .......... 62% 127M 22s
317550K .......... .......... .......... .......... .......... 62% 70.2M 22s
317600K .......... .......... .......... .......... .......... 62% 125M 22s
317650K .......... .......... .......... .......... .......... 62% 17.4M 22s
317700K .......... .......... .......... .......... .......... 62% 94.1M 22s
317750K .......... .......... .......... .......... .......... 62% 148M 22s
317800K .......... .......... .......... .......... .......... 62% 14.8M 22s
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317900K .......... .......... .......... .......... .......... 62% 133M 22s
317950K .......... .......... .......... .......... .......... 62% 13.3M 22s
318000K .......... .......... .......... .......... .......... 62% 126M 22s
318050K .......... .......... .......... .......... .......... 63% 199M 22s
318100K .......... .......... .......... .......... .......... 63% 13.7M 22s
318150K .......... .......... .......... .......... .......... 63% 123M 22s
318200K .......... .......... .......... .......... .......... 63% 113M 22s
318250K .......... .......... .......... .......... .......... 63% 11.6M 22s
318300K .......... .......... .......... .......... .......... 63% 287M 22s
318350K .......... .......... .......... .......... .......... 63% 173M 22s
318400K .......... .......... .......... .......... .......... 63% 15.7M 22s
318450K .......... .......... .......... .......... .......... 63% 143M 22s
318500K .......... .......... .......... .......... .......... 63% 113M 22s
318550K .......... .......... .......... .......... .......... 63% 155M 22s
318600K .......... .......... .......... .......... .......... 63% 10.8M 22s
318650K .......... .......... .......... .......... .......... 63% 149M 22s
318700K .......... .......... .......... .......... .......... 63% 201M 22s
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318800K .......... .......... .......... .......... .......... 63% 237M 22s
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318900K .......... .......... .......... .......... .......... 63% 14.1M 22s
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319000K .......... .......... .......... .......... .......... 63% 171M 22s
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319100K .......... .......... .......... .......... .......... 63% 203M 22s
319150K .......... .......... .......... .......... .......... 63% 268M 22s
319200K .......... .......... .......... .......... .......... 63% 201M 22s
319250K .......... .......... .......... .......... .......... 63% 14.2M 22s
319300K .......... .......... .......... .......... .......... 63% 114M 22s
319350K .......... .......... .......... .......... .......... 63% 174M 22s
319400K .......... .......... .......... .......... .......... 63% 15.6M 22s
319450K .......... .......... .......... .......... .......... 63% 136M 22s
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319600K .......... .......... .......... .......... .......... 63% 79.7M 22s
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319700K .......... .......... .......... .......... .......... 63% 12.6M 22s
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319800K .......... .......... .......... .......... .......... 63% 133M 22s
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320000K .......... .......... .......... .......... .......... 63% 182M 22s
320050K .......... .......... .......... .......... .......... 63% 14.9M 22s
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320200K .......... .......... .......... .......... .......... 63% 14.3M 22s
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320700K .......... .......... .......... .......... .......... 63% 13.7M 22s
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320800K .......... .......... .......... .......... .......... 63% 112M 22s
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320900K .......... .......... .......... .......... .......... 63% 14.4M 22s
320950K .......... .......... .......... .......... .......... 63% 93.9M 22s
321000K .......... .......... .......... .......... .......... 63% 168M 22s
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321100K .......... .......... .......... .......... .......... 63% 71.4M 22s
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321500K .......... .......... .......... .......... .......... 63% 221M 22s
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321600K .......... .......... .......... .......... .......... 63% 13.9M 22s
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322150K .......... .......... .......... .......... .......... 63% 192M 21s
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322250K .......... .......... .......... .......... .......... 63% 138M 21s
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322800K .......... .......... .......... .......... .......... 63% 13.5M 21s
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323000K .......... .......... .......... .......... .......... 63% 273M 21s
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325400K .......... .......... .......... .......... .......... 64% 12.6M 21s
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325700K .......... .......... .......... .......... .......... 64% 220M 21s
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325800K .......... .......... .......... .......... .......... 64% 123M 21s
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325900K .......... .......... .......... .......... .......... 64% 191M 21s
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327100K .......... .......... .......... .......... .......... 64% 108M 21s
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327250K .......... .......... .......... .......... .......... 64% 173M 21s
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327850K .......... .......... .......... .......... .......... 64% 112M 21s
327900K .......... .......... .......... .......... .......... 64% 164M 21s
327950K .......... .......... .......... .......... .......... 64% 141M 21s
328000K .......... .......... .......... .......... .......... 64% 17.1M 21s
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328100K .......... .......... .......... .......... .......... 64% 153M 20s
328150K .......... .......... .......... .......... .......... 65% 18.2M 20s
328200K .......... .......... .......... .......... .......... 65% 147M 20s
328250K .......... .......... .......... .......... .......... 65% 227M 20s
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329100K .......... .......... .......... .......... .......... 65% 12.3M 20s
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330000K .......... .......... .......... .......... .......... 65% 18.2M 20s
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330200K .......... .......... .......... .......... .......... 65% 69.0M 20s
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331500K .......... .......... .......... .......... .......... 65% 111M 20s
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331600K .......... .......... .......... .......... .......... 65% 11.1M 20s
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331800K .......... .......... .......... .......... .......... 65% 16.5M 20s
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332300K .......... .......... .......... .......... .......... 65% 215M 20s
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332400K .......... .......... .......... .......... .......... 65% 96.9M 20s
332450K .......... .......... .......... .......... .......... 65% 194M 20s
332500K .......... .......... .......... .......... .......... 65% 128M 20s
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332600K .......... .......... .......... .......... .......... 65% 17.0M 20s
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332700K .......... .......... .......... .......... .......... 65% 138M 20s
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332800K .......... .......... .......... .......... .......... 65% 133M 20s
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332900K .......... .......... .......... .......... .......... 65% 13.6M 20s
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333000K .......... .......... .......... .......... .......... 65% 148M 20s
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333150K .......... .......... .......... .......... .......... 65% 10.8M 20s
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342750K .......... .......... .......... .......... .......... 67% 210M 18s
342800K .......... .......... .......... .......... .......... 67% 17.1M 18s
342850K .......... .......... .......... .......... .......... 67% 225M 18s
342900K .......... .......... .......... .......... .......... 67% 10.6M 18s
342950K .......... .......... .......... .......... .......... 67% 178M 18s
343000K .......... .......... .......... .......... .......... 67% 129M 18s
343050K .......... .......... .......... .......... .......... 67% 144M 18s
343100K .......... .......... .......... .......... .......... 67% 11.8M 18s
343150K .......... .......... .......... .......... .......... 67% 81.2M 18s
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343250K .......... .......... .......... .......... .......... 67% 242M 18s
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343350K .......... .......... .......... .......... .......... 68% 11.1M 18s
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343500K .......... .......... .......... .......... .......... 68% 97.1M 18s
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344200K .......... .......... .......... .......... .......... 68% 10.9M 18s
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357650K .......... .......... .......... .......... .......... 70% 156M 16s
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357900K .......... .......... .......... .......... .......... 70% 12.9M 16s
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358000K .......... .......... .......... .......... .......... 70% 243M 16s
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358100K .......... .......... .......... .......... .......... 70% 11.9M 16s
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358250K .......... .......... .......... .......... .......... 70% 271M 16s
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371500K .......... .......... .......... .......... .......... 73% 129M 14s
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371900K .......... .......... .......... .......... .......... 73% 205M 14s
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372650K .......... .......... .......... .......... .......... 73% 229M 14s
372700K .......... .......... .......... .......... .......... 73% 197M 14s
372750K .......... .......... .......... .......... .......... 73% 277M 14s
372800K .......... .......... .......... .......... .......... 73% 124M 14s
372850K .......... .......... .......... .......... .......... 73% 9.71M 14s
372900K .......... .......... .......... .......... .......... 73% 105M 14s
372950K .......... .......... .......... .......... .......... 73% 149M 14s
373000K .......... .......... .......... .......... .......... 73% 97.5M 14s
373050K .......... .......... .......... .......... .......... 73% 230M 14s
373100K .......... .......... .......... .......... .......... 73% 9.19M 14s
373150K .......... .......... .......... .......... .......... 73% 134M 14s
373200K .......... .......... .......... .......... .......... 73% 196M 14s
373250K .......... .......... .......... .......... .......... 73% 273M 14s
373300K .......... .......... .......... .......... .......... 73% 277M 14s
373350K .......... .......... .......... .......... .......... 73% 249M 14s
373400K .......... .......... .......... .......... .......... 73% 311M 14s
373450K .......... .......... .......... .......... .......... 73% 10.4M 14s
373500K .......... .......... .......... .......... .......... 73% 162M 14s
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373650K .......... .......... .......... .......... .......... 74% 112M 14s
373700K .......... .......... .......... .......... .......... 74% 8.93M 14s
373750K .......... .......... .......... .......... .......... 74% 114M 14s
373800K .......... .......... .......... .......... .......... 74% 166M 14s
373850K .......... .......... .......... .......... .......... 74% 189M 14s
373900K .......... .......... .......... .......... .......... 74% 10.1M 14s
373950K .......... .......... .......... .......... .......... 74% 103M 14s
374000K .......... .......... .......... .......... .......... 74% 191M 14s
374050K .......... .......... .......... .......... .......... 74% 184M 14s
374100K .......... .......... .......... .......... .......... 74% 258M 14s
374150K .......... .......... .......... .......... .......... 74% 339M 14s
374200K .......... .......... .......... .......... .......... 74% 164M 14s
374250K .......... .......... .......... .......... .......... 74% 10.7M 14s
374300K .......... .......... .......... .......... .......... 74% 198M 14s
374350K .......... .......... .......... .......... .......... 74% 190M 14s
374400K .......... .......... .......... .......... .......... 74% 131M 14s
374450K .......... .......... .......... .......... .......... 74% 196M 14s
374500K .......... .......... .......... .......... .......... 74% 8.51M 14s
374550K .......... .......... .......... .......... .......... 74% 179M 14s
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374800K .......... .......... .......... .......... .......... 74% 271M 14s
374850K .......... .......... .......... .......... .......... 74% 10.8M 14s
374900K .......... .......... .......... .......... .......... 74% 94.3M 14s
374950K .......... .......... .......... .......... .......... 74% 149M 14s
375000K .......... .......... .......... .......... .......... 74% 154M 14s
375050K .......... .......... .......... .......... .......... 74% 212M 14s
375100K .......... .......... .......... .......... .......... 74% 9.27M 14s
375150K .......... .......... .......... .......... .......... 74% 121M 14s
375200K .......... .......... .......... .......... .......... 74% 140M 14s
375250K .......... .......... .......... .......... .......... 74% 274M 14s
375300K .......... .......... .......... .......... .......... 74% 328M 14s
375350K .......... .......... .......... .......... .......... 74% 257M 13s
375400K .......... .......... .......... .......... .......... 74% 9.70M 13s
375450K .......... .......... .......... .......... .......... 74% 154M 13s
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375700K .......... .......... .......... .......... .......... 74% 10.0M 13s
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375900K .......... .......... .......... .......... .......... 74% 147M 13s
375950K .......... .......... .......... .......... .......... 74% 11.8M 13s
376000K .......... .......... .......... .......... .......... 74% 147M 13s
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376100K .......... .......... .......... .......... .......... 74% 113M 13s
376150K .......... .......... .......... .......... .......... 74% 291M 13s
376200K .......... .......... .......... .......... .......... 74% 257M 13s
376250K .......... .......... .......... .......... .......... 74% 7.68M 13s
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376450K .......... .......... .......... .......... .......... 74% 192M 13s
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376550K .......... .......... .......... .......... .......... 74% 9.84M 13s
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376800K .......... .......... .......... .......... .......... 74% 8.17M 13s
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376900K .......... .......... .......... .......... .......... 74% 130M 13s
376950K .......... .......... .......... .......... .......... 74% 9.47M 13s
377000K .......... .......... .......... .......... .......... 74% 100M 13s
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377100K .......... .......... .......... .......... .......... 74% 102M 13s
377150K .......... .......... .......... .......... .......... 74% 122M 13s
377200K .......... .......... .......... .......... .......... 74% 203M 13s
377250K .......... .......... .......... .......... .......... 74% 271M 13s
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377350K .......... .......... .......... .......... .......... 74% 126M 13s
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377450K .......... .......... .......... .......... .......... 74% 15.8M 13s
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377650K .......... .......... .......... .......... .......... 74% 9.38M 13s
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377800K .......... .......... .......... .......... .......... 74% 227M 13s
377850K .......... .......... .......... .......... .......... 74% 279M 13s
377900K .......... .......... .......... .......... .......... 74% 8.86M 13s
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378000K .......... .......... .......... .......... .......... 74% 146M 13s
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378100K .......... .......... .......... .......... .......... 74% 164M 13s
378150K .......... .......... .......... .......... .......... 74% 158M 13s
378200K .......... .......... .......... .......... .......... 74% 83.2M 13s
378250K .......... .......... .......... .......... .......... 74% 225M 13s
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378550K .......... .......... .......... .......... .......... 74% 17.3M 13s
378600K .......... .......... .......... .......... .......... 74% 99.0M 13s
378650K .......... .......... .......... .......... .......... 75% 143M 13s
378700K .......... .......... .......... .......... .......... 75% 9.24M 13s
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378850K .......... .......... .......... .......... .......... 75% 174M 13s
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379000K .......... .......... .......... .......... .......... 75% 10.8M 13s
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379100K .......... .......... .......... .......... .......... 75% 115M 13s
379150K .......... .......... .......... .......... .......... 75% 258M 13s
379200K .......... .......... .......... .......... .......... 75% 168M 13s
379250K .......... .......... .......... .......... .......... 75% 191M 13s
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379600K .......... .......... .......... .......... .......... 75% 11.2M 13s
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379850K .......... .......... .......... .......... .......... 75% 9.33M 13s
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380000K .......... .......... .......... .......... .......... 75% 11.0M 13s
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380200K .......... .......... .......... .......... .......... 75% 226M 13s
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380350K .......... .......... .......... .......... .......... 75% 173M 13s
380400K .......... .......... .......... .......... .......... 75% 9.56M 13s
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380500K .......... .......... .......... .......... .......... 75% 142M 13s
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380700K .......... .......... .......... .......... .......... 75% 8.82M 13s
380750K .......... .......... .......... .......... .......... 75% 159M 13s
380800K .......... .......... .......... .......... .......... 75% 132M 13s
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381000K .......... .......... .......... .......... .......... 75% 9.19M 13s
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381500K .......... .......... .......... .......... .......... 75% 287M 13s
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381600K .......... .......... .......... .......... .......... 75% 9.04M 13s
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382150K .......... .......... .......... .......... .......... 75% 131M 13s
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382250K .......... .......... .......... .......... .......... 75% 145M 13s
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382500K .......... .......... .......... .......... .......... 75% 216M 13s
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382600K .......... .......... .......... .......... .......... 75% 96.9M 13s
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382700K .......... .......... .......... .......... .......... 75% 8.46M 13s
382750K .......... .......... .......... .......... .......... 75% 128M 13s
382800K .......... .......... .......... .......... .......... 75% 214M 13s
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383000K .......... .......... .......... .......... .......... 75% 218M 13s
383050K .......... .......... .......... .......... .......... 75% 8.28M 12s
383100K .......... .......... .......... .......... .......... 75% 9.34M 12s
383150K .......... .......... .......... .......... .......... 75% 136M 12s
383200K .......... .......... .......... .......... .......... 75% 239M 12s
383250K .......... .......... .......... .......... .......... 75% 145M 12s
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383600K .......... .......... .......... .......... .......... 75% 15.1M 12s
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383850K .......... .......... .......... .......... .......... 76% 8.65M 12s
383900K .......... .......... .......... .......... .......... 76% 157M 12s
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384000K .......... .......... .......... .......... .......... 76% 97.1M 12s
384050K .......... .......... .......... .......... .......... 76% 271M 12s
384100K .......... .......... .......... .......... .......... 76% 9.24M 12s
384150K .......... .......... .......... .......... .......... 76% 187M 12s
384200K .......... .......... .......... .......... .......... 76% 134M 12s
384250K .......... .......... .......... .......... .......... 76% 284M 12s
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384400K .......... .......... .......... .......... .......... 76% 10.1M 12s
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384700K .......... .......... .......... .......... .......... 76% 11.0M 12s
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384900K .......... .......... .......... .......... .......... 76% 10.7M 12s
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385000K .......... .......... .......... .......... .......... 76% 82.3M 12s
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385100K .......... .......... .......... .......... .......... 76% 111M 12s
385150K .......... .......... .......... .......... .......... 76% 14.2M 12s
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385350K .......... .......... .......... .......... .......... 76% 10.3M 12s
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385650K .......... .......... .......... .......... .......... 76% 10.1M 12s
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385800K .......... .......... .......... .......... .......... 76% 151M 12s
385850K .......... .......... .......... .......... .......... 76% 12.2M 12s
385900K .......... .......... .......... .......... .......... 76% 174M 12s
385950K .......... .......... .......... .......... .......... 76% 99.6M 12s
386000K .......... .......... .......... .......... .......... 76% 164M 12s
386050K .......... .......... .......... .......... .......... 76% 174M 12s
386100K .......... .......... .......... .......... .......... 76% 187M 12s
386150K .......... .......... .......... .......... .......... 76% 11.0M 12s
386200K .......... .......... .......... .......... .......... 76% 122M 12s
386250K .......... .......... .......... .......... .......... 76% 167M 12s
386300K .......... .......... .......... .......... .......... 76% 118M 12s
386350K .......... .......... .......... .......... .......... 76% 9.68M 12s
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386450K .......... .......... .......... .......... .......... 76% 99.2M 12s
386500K .......... .......... .......... .......... .......... 76% 175M 12s
386550K .......... .......... .......... .......... .......... 76% 257M 12s
386600K .......... .......... .......... .......... .......... 76% 224M 12s
386650K .......... .......... .......... .......... .......... 76% 10.9M 12s
386700K .......... .......... .......... .......... .......... 76% 162M 12s
386750K .......... .......... .......... .......... .......... 76% 176M 12s
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386850K .......... .......... .......... .......... .......... 76% 117M 12s
386900K .......... .......... .......... .......... .......... 76% 10.6M 12s
386950K .......... .......... .......... .......... .......... 76% 184M 12s
387000K .......... .......... .......... .......... .......... 76% 164M 12s
387050K .......... .......... .......... .......... .......... 76% 282M 12s
387100K .......... .......... .......... .......... .......... 76% 238M 12s
387150K .......... .......... .......... .......... .......... 76% 11.5M 12s
387200K .......... .......... .......... .......... .......... 76% 10.2M 12s
387250K .......... .......... .......... .......... .......... 76% 125M 12s
387300K .......... .......... .......... .......... .......... 76% 200M 12s
387350K .......... .......... .......... .......... .......... 76% 168M 12s
387400K .......... .......... .......... .......... .......... 76% 54.6M 12s
387450K .......... .......... .......... .......... .......... 76% 79.9M 12s
387500K .......... .......... .......... .......... .......... 76% 104M 12s
387550K .......... .......... .......... .......... .......... 76% 126M 12s
387600K .......... .......... .......... .......... .......... 76% 157M 12s
387650K .......... .......... .......... .......... .......... 76% 12.1M 12s
387700K .......... .......... .......... .......... .......... 76% 141M 12s
387750K .......... .......... .......... .......... .......... 76% 136M 12s
387800K .......... .......... .......... .......... .......... 76% 186M 12s
387850K .......... .......... .......... .......... .......... 76% 98.6M 12s
387900K .......... .......... .......... .......... .......... 76% 194M 12s
387950K .......... .......... .......... .......... .......... 76% 7.01M 12s
388000K .......... .......... .......... .......... .......... 76% 138M 12s
388050K .......... .......... .......... .......... .......... 76% 167M 12s
388100K .......... .......... .......... .......... .......... 76% 187M 12s
388150K .......... .......... .......... .......... .......... 76% 217M 12s
388200K .......... .......... .......... .......... .......... 76% 11.3M 12s
388250K .......... .......... .......... .......... .......... 76% 174M 12s
388300K .......... .......... .......... .......... .......... 76% 183M 12s
388350K .......... .......... .......... .......... .......... 76% 99.4M 12s
388400K .......... .......... .......... .......... .......... 76% 247M 12s
388450K .......... .......... .......... .......... .......... 76% 164M 12s
388500K .......... .......... .......... .......... .......... 76% 129M 12s
388550K .......... .......... .......... .......... .......... 76% 6.71M 12s
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388900K .......... .......... .......... .......... .......... 77% 9.06M 12s
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389000K .......... .......... .......... .......... .......... 77% 228M 12s
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389100K .......... .......... .......... .......... .......... 77% 239M 12s
389150K .......... .......... .......... .......... .......... 77% 244M 12s
389200K .......... .......... .......... .......... .......... 77% 155M 12s
389250K .......... .......... .......... .......... .......... 77% 10.4M 12s
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389500K .......... .......... .......... .......... .......... 77% 11.8M 12s
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389750K .......... .......... .......... .......... .......... 77% 10.2M 12s
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390000K .......... .......... .......... .......... .......... 77% 10.1M 12s
390050K .......... .......... .......... .......... .......... 77% 141M 12s
390100K .......... .......... .......... .......... .......... 77% 162M 12s
390150K .......... .......... .......... .......... .......... 77% 224M 12s
390200K .......... .......... .......... .......... .......... 77% 230M 12s
390250K .......... .......... .......... .......... .......... 77% 10.9M 12s
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390450K .......... .......... .......... .......... .......... 77% 270M 12s
390500K .......... .......... .......... .......... .......... 77% 10.1M 12s
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390750K .......... .......... .......... .......... .......... 77% 14.2M 12s
390800K .......... .......... .......... .......... .......... 77% 93.2M 12s
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390900K .......... .......... .......... .......... .......... 77% 230M 12s
390950K .......... .......... .......... .......... .......... 77% 204M 12s
391000K .......... .......... .......... .......... .......... 77% 9.84M 11s
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391100K .......... .......... .......... .......... .......... 77% 142M 11s
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391200K .......... .......... .......... .......... .......... 77% 185M 11s
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391300K .......... .......... .......... .......... .......... 77% 7.18M 11s
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391500K .......... .......... .......... .......... .......... 77% 107M 11s
391550K .......... .......... .......... .......... .......... 77% 237M 11s
391600K .......... .......... .......... .......... .......... 77% 131M 11s
391650K .......... .......... .......... .......... .......... 77% 8.20M 11s
391700K .......... .......... .......... .......... .......... 77% 99.4M 11s
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391800K .......... .......... .......... .......... .......... 77% 137M 11s
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391900K .......... .......... .......... .......... .......... 77% 249M 11s
391950K .......... .......... .......... .......... .......... 77% 228M 11s
392000K .......... .......... .......... .......... .......... 77% 10.4M 11s
392050K .......... .......... .......... .......... .......... 77% 236M 11s
392100K .......... .......... .......... .......... .......... 77% 205M 11s
392150K .......... .......... .......... .......... .......... 77% 146M 11s
392200K .......... .......... .......... .......... .......... 77% 143M 11s
392250K .......... .......... .......... .......... .......... 77% 158M 11s
392300K .......... .......... .......... .......... .......... 77% 4.11M 11s
392350K .......... .......... .......... .......... .......... 77% 71.9M 11s
392400K .......... .......... .......... .......... .......... 77% 148M 11s
392450K .......... .......... .......... .......... .......... 77% 128M 11s
392500K .......... .......... .......... .......... .......... 77% 271M 11s
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392700K .......... .......... .......... .......... .......... 77% 200M 11s
392750K .......... .......... .......... .......... .......... 77% 219M 11s
392800K .......... .......... .......... .......... .......... 77% 273M 11s
392850K .......... .......... .......... .......... .......... 77% 287M 11s
392900K .......... .......... .......... .......... .......... 77% 313M 11s
392950K .......... .......... .......... .......... .......... 77% 23.9M 11s
393000K .......... .......... .......... .......... .......... 77% 129M 11s
393050K .......... .......... .......... .......... .......... 77% 8.92M 11s
393100K .......... .......... .......... .......... .......... 77% 128M 11s
393150K .......... .......... .......... .......... .......... 77% 178M 11s
393200K .......... .......... .......... .......... .......... 77% 112M 11s
393250K .......... .......... .......... .......... .......... 77% 7.71M 11s
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393350K .......... .......... .......... .......... .......... 77% 9.54M 11s
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393850K .......... .......... .......... .......... .......... 78% 18.6M 11s
393900K .......... .......... .......... .......... .......... 78% 169M 11s
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394000K .......... .......... .......... .......... .......... 78% 184M 11s
394050K .......... .......... .......... .......... .......... 78% 7.92M 11s
394100K .......... .......... .......... .......... .......... 78% 119M 11s
394150K .......... .......... .......... .......... .......... 78% 114M 11s
394200K .......... .......... .......... .......... .......... 78% 91.1M 11s
394250K .......... .......... .......... .......... .......... 78% 105M 11s
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394350K .......... .......... .......... .......... .......... 78% 10.5M 11s
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394700K .......... .......... .......... .......... .......... 78% 6.74M 11s
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394800K .......... .......... .......... .......... .......... 78% 82.1M 11s
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394900K .......... .......... .......... .......... .......... 78% 303M 11s
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395000K .......... .......... .......... .......... .......... 78% 9.05M 11s
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395100K .......... .......... .......... .......... .......... 78% 111M 11s
395150K .......... .......... .......... .......... .......... 78% 291M 11s
395200K .......... .......... .......... .......... .......... 78% 261M 11s
395250K .......... .......... .......... .......... .......... 78% 311M 11s
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399100K .......... .......... .......... .......... .......... 79% 96.3M 11s
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399200K .......... .......... .......... .......... .......... 79% 168M 10s
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399500K .......... .......... .......... .......... .......... 79% 652K 10s
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399750K .......... .......... .......... .......... .......... 79% 95.4M 10s
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401400K .......... .......... .......... .......... .......... 79% 142M 10s
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401800K .......... .......... .......... .......... .......... 79% 113M 10s
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402550K .......... .......... .......... .......... .......... 79% 11.6M 10s
402600K .......... .......... .......... .......... .......... 79% 137M 10s
402650K .......... .......... .......... .......... .......... 79% 135M 10s
402700K .......... .......... .......... .......... .......... 79% 151M 10s
402750K .......... .......... .......... .......... .......... 79% 147M 10s
402800K .......... .......... .......... .......... .......... 79% 57.2M 10s
402850K .......... .......... .......... .......... .......... 79% 120M 10s
402900K .......... .......... .......... .......... .......... 79% 4.28M 10s
402950K .......... .......... .......... .......... .......... 79% 108M 10s
403000K .......... .......... .......... .......... .......... 79% 158M 10s
403050K .......... .......... .......... .......... .......... 79% 309M 10s
403100K .......... .......... .......... .......... .......... 79% 103M 10s
403150K .......... .......... .......... .......... .......... 79% 144M 10s
403200K .......... .......... .......... .......... .......... 79% 88.8M 10s
403250K .......... .......... .......... .......... .......... 79% 105M 10s
403300K .......... .......... .......... .......... .......... 79% 7.48M 10s
403350K .......... .......... .......... .......... .......... 79% 119M 10s
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403600K .......... .......... .......... .......... .......... 79% 8.93M 10s
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403700K .......... .......... .......... .......... .......... 79% 215M 10s
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404000K .......... .......... .......... .......... .......... 80% 156M 10s
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404100K .......... .......... .......... .......... .......... 80% 101M 10s
404150K .......... .......... .......... .......... .......... 80% 108M 10s
404200K .......... .......... .......... .......... .......... 80% 99.6M 10s
404250K .......... .......... .......... .......... .......... 80% 215M 10s
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404350K .......... .......... .......... .......... .......... 80% 9.32M 10s
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404600K .......... .......... .......... .......... .......... 80% 6.92M 10s
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404800K .......... .......... .......... .......... .......... 80% 188M 10s
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405000K .......... .......... .......... .......... .......... 80% 221M 10s
405050K .......... .......... .......... .......... .......... 80% 8.18M 10s
405100K .......... .......... .......... .......... .......... 80% 161M 10s
405150K .......... .......... .......... .......... .......... 80% 152M 10s
405200K .......... .......... .......... .......... .......... 80% 150M 10s
405250K .......... .......... .......... .......... .......... 80% 292M 10s
405300K .......... .......... .......... .......... .......... 80% 8.22M 10s
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405600K .......... .......... .......... .......... .......... 80% 11.6M 10s
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405850K .......... .......... .......... .......... .......... 80% 9.09M 10s
405900K .......... .......... .......... .......... .......... 80% 112M 10s
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406000K .......... .......... .......... .......... .......... 80% 276M 10s
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406100K .......... .......... .......... .......... .......... 80% 11.0M 10s
406150K .......... .......... .......... .......... .......... 80% 198M 10s
406200K .......... .......... .......... .......... .......... 80% 96.9M 10s
406250K .......... .......... .......... .......... .......... 80% 130M 10s
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406400K .......... .......... .......... .......... .......... 80% 6.62M 10s
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406650K .......... .......... .......... .......... .......... 80% 7.38M 10s
406700K .......... .......... .......... .......... .......... 80% 95.4M 10s
406750K .......... .......... .......... .......... .......... 80% 107M 10s
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406850K .......... .......... .......... .......... .......... 80% 125M 10s
406900K .......... .......... .......... .......... .......... 80% 168M 10s
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407000K .......... .......... .......... .......... .......... 80% 98.4M 10s
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407100K .......... .......... .......... .......... .......... 80% 89.9M 10s
407150K .......... .......... .......... .......... .......... 80% 248M 10s
407200K .......... .......... .......... .......... .......... 80% 6.57M 10s
407250K .......... .......... .......... .......... .......... 80% 215M 10s
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407600K .......... .......... .......... .......... .......... 80% 9.33M 10s
407650K .......... .......... .......... .......... .......... 80% 6.62M 10s
407700K .......... .......... .......... .......... .......... 80% 57.0M 10s
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407800K .......... .......... .......... .......... .......... 80% 174M 10s
407850K .......... .......... .......... .......... .......... 80% 123M 10s
407900K .......... .......... .......... .......... .......... 80% 248M 9s
407950K .......... .......... .......... .......... .......... 80% 106M 9s
408000K .......... .......... .......... .......... .......... 80% 328M 9s
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408100K .......... .......... .......... .......... .......... 80% 113M 9s
408150K .......... .......... .......... .......... .......... 80% 140M 9s
408200K .......... .......... .......... .......... .......... 80% 102M 9s
408250K .......... .......... .......... .......... .......... 80% 24.3M 9s
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409150K .......... .......... .......... .......... .......... 81% 8.06M 9s
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410100K .......... .......... .......... .......... .......... 81% 144M 9s
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410200K .......... .......... .......... .......... .......... 81% 11.4M 9s
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410300K .......... .......... .......... .......... .......... 81% 150M 9s
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410400K .......... .......... .......... .......... .......... 81% 274M 9s
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410500K .......... .......... .......... .......... .......... 81% 7.35M 9s
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410600K .......... .......... .......... .......... .......... 81% 136M 9s
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410800K .......... .......... .......... .......... .......... 81% 217M 9s
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412000K .......... .......... .......... .......... .......... 81% 200M 9s
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412300K .......... .......... .......... .......... .......... 81% 11.1M 9s
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412400K .......... .......... .......... .......... .......... 81% 121M 9s
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417350K .......... .......... .......... .......... .......... 82% 192M 8s
417400K .......... .......... .......... .......... .......... 82% 13.7M 8s
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417500K .......... .......... .......... .......... .......... 82% 179M 8s
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417600K .......... .......... .......... .......... .......... 82% 205M 8s
417650K .......... .......... .......... .......... .......... 82% 7.86M 8s
417700K .......... .......... .......... .......... .......... 82% 107M 8s
417750K .......... .......... .......... .......... .......... 82% 151M 8s
417800K .......... .......... .......... .......... .......... 82% 108M 8s
417850K .......... .......... .......... .......... .......... 82% 111M 8s
417900K .......... .......... .......... .......... .......... 82% 8.35M 8s
417950K .......... .......... .......... .......... .......... 82% 109M 8s
418000K .......... .......... .......... .......... .......... 82% 124M 8s
418050K .......... .......... .......... .......... .......... 82% 172M 8s
418100K .......... .......... .......... .......... .......... 82% 108M 8s
418150K .......... .......... .......... .......... .......... 82% 230M 8s
418200K .......... .......... .......... .......... .......... 82% 129M 8s
418250K .......... .......... .......... .......... .......... 82% 191M 8s
418300K .......... .......... .......... .......... .......... 82% 157M 8s
418350K .......... .......... .......... .......... .......... 82% 9.07M 8s
418400K .......... .......... .......... .......... .......... 82% 115M 8s
418450K .......... .......... .......... .......... .......... 82% 134M 8s
418500K .......... .......... .......... .......... .......... 82% 114M 8s
418550K .......... .......... .......... .......... .......... 82% 144M 8s
418600K .......... .......... .......... .......... .......... 82% 118M 8s
418650K .......... .......... .......... .......... .......... 82% 127M 8s
418700K .......... .......... .......... .......... .......... 82% 6.48M 8s
418750K .......... .......... .......... .......... .......... 82% 130M 8s
418800K .......... .......... .......... .......... .......... 82% 170M 8s
418850K .......... .......... .......... .......... .......... 82% 108M 8s
418900K .......... .......... .......... .......... .......... 82% 170M 8s
418950K .......... .......... .......... .......... .......... 82% 6.39M 8s
419000K .......... .......... .......... .......... .......... 82% 190M 8s
419050K .......... .......... .......... .......... .......... 83% 87.2M 8s
419100K .......... .......... .......... .......... .......... 83% 50.7M 8s
419150K .......... .......... .......... .......... .......... 83% 156M 8s
419200K .......... .......... .......... .......... .......... 83% 135M 8s
419250K .......... .......... .......... .......... .......... 83% 147M 8s
419300K .......... .......... .......... .......... .......... 83% 148M 8s
419350K .......... .......... .......... .......... .......... 83% 94.8M 8s
419400K .......... .......... .......... .......... .......... 83% 220M 8s
419450K .......... .......... .......... .......... .......... 83% 252M 8s
419500K .......... .......... .......... .......... .......... 83% 6.64M 8s
419550K .......... .......... .......... .......... .......... 83% 117M 8s
419600K .......... .......... .......... .......... .......... 83% 130M 8s
419650K .......... .......... .......... .......... .......... 83% 136M 8s
419700K .......... .......... .......... .......... .......... 83% 235M 8s
419750K .......... .......... .......... .......... .......... 83% 313M 8s
419800K .......... .......... .......... .......... .......... 83% 321M 8s
419850K .......... .......... .......... .......... .......... 83% 190M 8s
419900K .......... .......... .......... .......... .......... 83% 162M 8s
419950K .......... .......... .......... .......... .......... 83% 6.48M 8s
420000K .......... .......... .......... .......... .......... 83% 155M 8s
420050K .......... .......... .......... .......... .......... 83% 279M 8s
420100K .......... .......... .......... .......... .......... 83% 256M 8s
420150K .......... .......... .......... .......... .......... 83% 186M 8s
420200K .......... .......... .......... .......... .......... 83% 219M 8s
420250K .......... .......... .......... .......... .......... 83% 214M 8s
420300K .......... .......... .......... .......... .......... 83% 156M 8s
420350K .......... .......... .......... .......... .......... 83% 8.56M 8s
420400K .......... .......... .......... .......... .......... 83% 162M 8s
420450K .......... .......... .......... .......... .......... 83% 144M 8s
420500K .......... .......... .......... .......... .......... 83% 142M 8s
420550K .......... .......... .......... .......... .......... 83% 171M 8s
420600K .......... .......... .......... .......... .......... 83% 124M 8s
420650K .......... .......... .......... .......... .......... 83% 7.25M 8s
420700K .......... .......... .......... .......... .......... 83% 111M 8s
420750K .......... .......... .......... .......... .......... 83% 140M 8s
420800K .......... .......... .......... .......... .......... 83% 195M 8s
420850K .......... .......... .......... .......... .......... 83% 219M 8s
420900K .......... .......... .......... .......... .......... 83% 144M 8s
420950K .......... .......... .......... .......... .......... 83% 110M 8s
421000K .......... .......... .......... .......... .......... 83% 9.73M 8s
421050K .......... .......... .......... .......... .......... 83% 133M 8s
421100K .......... .......... .......... .......... .......... 83% 116M 8s
421150K .......... .......... .......... .......... .......... 83% 165M 8s
421200K .......... .......... .......... .......... .......... 83% 267M 8s
421250K .......... .......... .......... .......... .......... 83% 172M 8s
421300K .......... .......... .......... .......... .......... 83% 157M 8s
421350K .......... .......... .......... .......... .......... 83% 8.28M 8s
421400K .......... .......... .......... .......... .......... 83% 252M 8s
421450K .......... .......... .......... .......... .......... 83% 126M 8s
421500K .......... .......... .......... .......... .......... 83% 142M 8s
421550K .......... .......... .......... .......... .......... 83% 138M 8s
421600K .......... .......... .......... .......... .......... 83% 186M 8s
421650K .......... .......... .......... .......... .......... 83% 6.41M 8s
421700K .......... .......... .......... .......... .......... 83% 114M 8s
421750K .......... .......... .......... .......... .......... 83% 184M 8s
421800K .......... .......... .......... .......... .......... 83% 103M 8s
421850K .......... .......... .......... .......... .......... 83% 158M 8s
421900K .......... .......... .......... .......... .......... 83% 196M 8s
421950K .......... .......... .......... .......... .......... 83% 188M 8s
422000K .......... .......... .......... .......... .......... 83% 7.56M 8s
422050K .......... .......... .......... .......... .......... 83% 99.6M 8s
422100K .......... .......... .......... .......... .......... 83% 140M 8s
422150K .......... .......... .......... .......... .......... 83% 184M 8s
422200K .......... .......... .......... .......... .......... 83% 118M 8s
422250K .......... .......... .......... .......... .......... 83% 101M 8s
422300K .......... .......... .......... .......... .......... 83% 133M 8s
422350K .......... .......... .......... .......... .......... 83% 221M 8s
422400K .......... .......... .......... .......... .......... 83% 247M 8s
422450K .......... .......... .......... .......... .......... 83% 96.7M 8s
422500K .......... .......... .......... .......... .......... 83% 10.9M 8s
422550K .......... .......... .......... .......... .......... 83% 121M 8s
422600K .......... .......... .......... .......... .......... 83% 126M 8s
422650K .......... .......... .......... .......... .......... 83% 119M 8s
422700K .......... .......... .......... .......... .......... 83% 220M 8s
422750K .......... .......... .......... .......... .......... 83% 267M 8s
422800K .......... .......... .......... .......... .......... 83% 6.15M 8s
422850K .......... .......... .......... .......... .......... 83% 176M 8s
422900K .......... .......... .......... .......... .......... 83% 140M 8s
422950K .......... .......... .......... .......... .......... 83% 118M 8s
423000K .......... .......... .......... .......... .......... 83% 187M 8s
423050K .......... .......... .......... .......... .......... 83% 7.00M 8s
423100K .......... .......... .......... .......... .......... 83% 132M 8s
423150K .......... .......... .......... .......... .......... 83% 141M 8s
423200K .......... .......... .......... .......... .......... 83% 111M 8s
423250K .......... .......... .......... .......... .......... 83% 154M 8s
423300K .......... .......... .......... .......... .......... 83% 182M 8s
423350K .......... .......... .......... .......... .......... 83% 286M 8s
423400K .......... .......... .......... .......... .......... 83% 249M 8s
423450K .......... .......... .......... .......... .......... 83% 148M 8s
423500K .......... .......... .......... .......... .......... 83% 117M 8s
423550K .......... .......... .......... .......... .......... 83% 223M 8s
423600K .......... .......... .......... .......... .......... 83% 241M 8s
423650K .......... .......... .......... .......... .......... 83% 12.3M 8s
423700K .......... .......... .......... .......... .......... 83% 123M 8s
423750K .......... .......... .......... .......... .......... 83% 152M 8s
423800K .......... .......... .......... .......... .......... 83% 298M 8s
423850K .......... .......... .......... .......... .......... 83% 112M 8s
423900K .......... .......... .......... .......... .......... 83% 7.88M 8s
423950K .......... .......... .......... .......... .......... 83% 131M 8s
424000K .......... .......... .......... .......... .......... 83% 197M 8s
424050K .......... .......... .......... .......... .......... 83% 8.03M 8s
424100K .......... .......... .......... .......... .......... 84% 112M 8s
424150K .......... .......... .......... .......... .......... 84% 217M 8s
424200K .......... .......... .......... .......... .......... 84% 123M 8s
424250K .......... .......... .......... .......... .......... 84% 228M 8s
424300K .......... .......... .......... .......... .......... 84% 187M 8s
424350K .......... .......... .......... .......... .......... 84% 70.7M 8s
424400K .......... .......... .......... .......... .......... 84% 214M 8s
424450K .......... .......... .......... .......... .......... 84% 196M 8s
424500K .......... .......... .......... .......... .......... 84% 294M 8s
424550K .......... .......... .......... .......... .......... 84% 321M 8s
424600K .......... .......... .......... .......... .......... 84% 8.68M 8s
424650K .......... .......... .......... .......... .......... 84% 123M 8s
424700K .......... .......... .......... .......... .......... 84% 119M 8s
424750K .......... .......... .......... .......... .......... 84% 249M 8s
424800K .......... .......... .......... .......... .......... 84% 104M 8s
424850K .......... .......... .......... .......... .......... 84% 174M 8s
424900K .......... .......... .......... .......... .......... 84% 6.53M 8s
424950K .......... .......... .......... .......... .......... 84% 157M 8s
425000K .......... .......... .......... .......... .......... 84% 122M 8s
425050K .......... .......... .......... .......... .......... 84% 267M 8s
425100K .......... .......... .......... .......... .......... 84% 6.51M 8s
425150K .......... .......... .......... .......... .......... 84% 151M 8s
425200K .......... .......... .......... .......... .......... 84% 133M 8s
425250K .......... .......... .......... .......... .......... 84% 140M 8s
425300K .......... .......... .......... .......... .......... 84% 186M 8s
425350K .......... .......... .......... .......... .......... 84% 165M 8s
425400K .......... .......... .......... .......... .......... 84% 173M 8s
425450K .......... .......... .......... .......... .......... 84% 160M 8s
425500K .......... .......... .......... .......... .......... 84% 102M 8s
425550K .......... .......... .......... .......... .......... 84% 150M 8s
425600K .......... .......... .......... .......... .......... 84% 131M 8s
425650K .......... .......... .......... .......... .......... 84% 109M 8s
425700K .......... .......... .......... .......... .......... 84% 120M 8s
425750K .......... .......... .......... .......... .......... 84% 25.0M 7s
425800K .......... .......... .......... .......... .......... 84% 168M 7s
425850K .......... .......... .......... .......... .......... 84% 126M 7s
425900K .......... .......... .......... .......... .......... 84% 6.06M 7s
425950K .......... .......... .......... .......... .......... 84% 107M 7s
426000K .......... .......... .......... .......... .......... 84% 121M 7s
426050K .......... .......... .......... .......... .......... 84% 156M 7s
426100K .......... .......... .......... .......... .......... 84% 8.83M 7s
426150K .......... .......... .......... .......... .......... 84% 109M 7s
426200K .......... .......... .......... .......... .......... 84% 94.6M 7s
426250K .......... .......... .......... .......... .......... 84% 163M 7s
426300K .......... .......... .......... .......... .......... 84% 224M 7s
426350K .......... .......... .......... .......... .......... 84% 194M 7s
426400K .......... .......... .......... .......... .......... 84% 230M 7s
426450K .......... .......... .......... .......... .......... 84% 263M 7s
426500K .......... .......... .......... .......... .......... 84% 211M 7s
426550K .......... .......... .......... .......... .......... 84% 261M 7s
426600K .......... .......... .......... .......... .......... 84% 11.2M 7s
426650K .......... .......... .......... .......... .......... 84% 153M 7s
426700K .......... .......... .......... .......... .......... 84% 173M 7s
426750K .......... .......... .......... .......... .......... 84% 282M 7s
426800K .......... .......... .......... .......... .......... 84% 313M 7s
426850K .......... .......... .......... .......... .......... 84% 148M 7s
426900K .......... .......... .......... .......... .......... 84% 142M 7s
426950K .......... .......... .......... .......... .......... 84% 6.29M 7s
427000K .......... .......... .......... .......... .......... 84% 170M 7s
427050K .......... .......... .......... .......... .......... 84% 119M 7s
427100K .......... .......... .......... .......... .......... 84% 8.15M 7s
427150K .......... .......... .......... .......... .......... 84% 85.7M 7s
427200K .......... .......... .......... .......... .......... 84% 76.2M 7s
427250K .......... .......... .......... .......... .......... 84% 151M 7s
427300K .......... .......... .......... .......... .......... 84% 294M 7s
427350K .......... .......... .......... .......... .......... 84% 261M 7s
427400K .......... .......... .......... .......... .......... 84% 317M 7s
427450K .......... .......... .......... .......... .......... 84% 203M 7s
427500K .......... .......... .......... .......... .......... 84% 233M 7s
427550K .......... .......... .......... .......... .......... 84% 249M 7s
427600K .......... .......... .......... .......... .......... 84% 204M 7s
427650K .......... .......... .......... .......... .......... 84% 106M 7s
427700K .......... .......... .......... .......... .......... 84% 196M 7s
427750K .......... .......... .......... .......... .......... 84% 17.9M 7s
427800K .......... .......... .......... .......... .......... 84% 159M 7s
427850K .......... .......... .......... .......... .......... 84% 120M 7s
427900K .......... .......... .......... .......... .......... 84% 239M 7s
427950K .......... .......... .......... .......... .......... 84% 181M 7s
428000K .......... .......... .......... .......... .......... 84% 7.55M 7s
428050K .......... .......... .......... .......... .......... 84% 109M 7s
428100K .......... .......... .......... .......... .......... 84% 159M 7s
428150K .......... .......... .......... .......... .......... 84% 7.28M 7s
428200K .......... .......... .......... .......... .......... 84% 117M 7s
428250K .......... .......... .......... .......... .......... 84% 142M 7s
428300K .......... .......... .......... .......... .......... 84% 110M 7s
428350K .......... .......... .......... .......... .......... 84% 191M 7s
428400K .......... .......... .......... .......... .......... 84% 286M 7s
428450K .......... .......... .......... .......... .......... 84% 182M 7s
428500K .......... .......... .......... .......... .......... 84% 298M 7s
428550K .......... .......... .......... .......... .......... 84% 300M 7s
428600K .......... .......... .......... .......... .......... 84% 203M 7s
428650K .......... .......... .......... .......... .......... 84% 180M 7s
428700K .......... .......... .......... .......... .......... 84% 229M 7s
428750K .......... .......... .......... .......... .......... 84% 307M 7s
428800K .......... .......... .......... .......... .......... 84% 17.0M 7s
428850K .......... .......... .......... .......... .......... 84% 132M 7s
428900K .......... .......... .......... .......... .......... 84% 279M 7s
428950K .......... .......... .......... .......... .......... 84% 257M 7s
429000K .......... .......... .......... .......... .......... 84% 187M 7s
429050K .......... .......... .......... .......... .......... 84% 7.03M 7s
429100K .......... .......... .......... .......... .......... 84% 152M 7s
429150K .......... .......... .......... .......... .......... 85% 160M 7s
429200K .......... .......... .......... .......... .......... 85% 7.01M 7s
429250K .......... .......... .......... .......... .......... 85% 179M 7s
429300K .......... .......... .......... .......... .......... 85% 86.0M 7s
429350K .......... .......... .......... .......... .......... 85% 160M 7s
429400K .......... .......... .......... .......... .......... 85% 237M 7s
429450K .......... .......... .......... .......... .......... 85% 206M 7s
429500K .......... .......... .......... .......... .......... 85% 223M 7s
429550K .......... .......... .......... .......... .......... 85% 216M 7s
429600K .......... .......... .......... .......... .......... 85% 203M 7s
429650K .......... .......... .......... .......... .......... 85% 220M 7s
429700K .......... .......... .......... .......... .......... 85% 219M 7s
429750K .......... .......... .......... .......... .......... 85% 229M 7s
429800K .......... .......... .......... .......... .......... 85% 11.1M 7s
429850K .......... .......... .......... .......... .......... 85% 140M 7s
429900K .......... .......... .......... .......... .......... 85% 298M 7s
429950K .......... .......... .......... .......... .......... 85% 153M 7s
430000K .......... .......... .......... .......... .......... 85% 229M 7s
430050K .......... .......... .......... .......... .......... 85% 6.44M 7s
430100K .......... .......... .......... .......... .......... 85% 137M 7s
430150K .......... .......... .......... .......... .......... 85% 109M 7s
430200K .......... .......... .......... .......... .......... 85% 6.90M 7s
430250K .......... .......... .......... .......... .......... 85% 128M 7s
430300K .......... .......... .......... .......... .......... 85% 148M 7s
430350K .......... .......... .......... .......... .......... 85% 114M 7s
430400K .......... .......... .......... .......... .......... 85% 119M 7s
430450K .......... .......... .......... .......... .......... 85% 234M 7s
430500K .......... .......... .......... .......... .......... 85% 245M 7s
430550K .......... .......... .......... .......... .......... 85% 277M 7s
430600K .......... .......... .......... .......... .......... 85% 131M 7s
430650K .......... .......... .......... .......... .......... 85% 211M 7s
430700K .......... .......... .......... .......... .......... 85% 210M 7s
430750K .......... .......... .......... .......... .......... 85% 177M 7s
430800K .......... .......... .......... .......... .......... 85% 12.8M 7s
430850K .......... .......... .......... .......... .......... 85% 131M 7s
430900K .......... .......... .......... .......... .......... 85% 205M 7s
430950K .......... .......... .......... .......... .......... 85% 136M 7s
431000K .......... .......... .......... .......... .......... 85% 132M 7s
431050K .......... .......... .......... .......... .......... 85% 7.25M 7s
431100K .......... .......... .......... .......... .......... 85% 85.8M 7s
431150K .......... .......... .......... .......... .......... 85% 189M 7s
431200K .......... .......... .......... .......... .......... 85% 7.04M 7s
431250K .......... .......... .......... .......... .......... 85% 110M 7s
431300K .......... .......... .......... .......... .......... 85% 146M 7s
431350K .......... .......... .......... .......... .......... 85% 137M 7s
431400K .......... .......... .......... .......... .......... 85% 94.3M 7s
431450K .......... .......... .......... .......... .......... 85% 173M 7s
431500K .......... .......... .......... .......... .......... 85% 167M 7s
431550K .......... .......... .......... .......... .......... 85% 138M 7s
431600K .......... .......... .......... .......... .......... 85% 196M 7s
431650K .......... .......... .......... .......... .......... 85% 223M 7s
431700K .......... .......... .......... .......... .......... 85% 167M 7s
431750K .......... .......... .......... .......... .......... 85% 152M 7s
431800K .......... .......... .......... .......... .......... 85% 15.4M 7s
431850K .......... .......... .......... .......... .......... 85% 119M 7s
431900K .......... .......... .......... .......... .......... 85% 152M 7s
431950K .......... .......... .......... .......... .......... 85% 174M 7s
432000K .......... .......... .......... .......... .......... 85% 276M 7s
432050K .......... .......... .......... .......... .......... 85% 170M 7s
432100K .......... .......... .......... .......... .......... 85% 6.71M 7s
432150K .......... .......... .......... .......... .......... 85% 186M 7s
432200K .......... .......... .......... .......... .......... 85% 132M 7s
432250K .......... .......... .......... .......... .......... 85% 6.67M 7s
432300K .......... .......... .......... .......... .......... 85% 97.7M 7s
432350K .......... .......... .......... .......... .......... 85% 162M 7s
432400K .......... .......... .......... .......... .......... 85% 178M 7s
432450K .......... .......... .......... .......... .......... 85% 153M 7s
432500K .......... .......... .......... .......... .......... 85% 147M 7s
432550K .......... .......... .......... .......... .......... 85% 215M 7s
432600K .......... .......... .......... .......... .......... 85% 130M 7s
432650K .......... .......... .......... .......... .......... 85% 221M 7s
432700K .......... .......... .......... .......... .......... 85% 129M 7s
432750K .......... .......... .......... .......... .......... 85% 152M 7s
432800K .......... .......... .......... .......... .......... 85% 162M 7s
432850K .......... .......... .......... .......... .......... 85% 9.83M 7s
432900K .......... .......... .......... .......... .......... 85% 144M 7s
432950K .......... .......... .......... .......... .......... 85% 148M 7s
433000K .......... .......... .......... .......... .......... 85% 181M 7s
433050K .......... .......... .......... .......... .......... 85% 140M 7s
433100K .......... .......... .......... .......... .......... 85% 69.8M 7s
433150K .......... .......... .......... .......... .......... 85% 6.35M 7s
433200K .......... .......... .......... .......... .......... 85% 121M 7s
433250K .......... .......... .......... .......... .......... 85% 7.64M 7s
433300K .......... .......... .......... .......... .......... 85% 96.1M 7s
433350K .......... .......... .......... .......... .......... 85% 156M 7s
433400K .......... .......... .......... .......... .......... 85% 138M 7s
433450K .......... .......... .......... .......... .......... 85% 185M 7s
433500K .......... .......... .......... .......... .......... 85% 215M 7s
433550K .......... .......... .......... .......... .......... 85% 309M 7s
433600K .......... .......... .......... .......... .......... 85% 286M 7s
433650K .......... .......... .......... .......... .......... 85% 276M 7s
433700K .......... .......... .......... .......... .......... 85% 263M 7s
433750K .......... .......... .......... .......... .......... 85% 298M 7s
433800K .......... .......... .......... .......... .......... 85% 253M 7s
433850K .......... .......... .......... .......... .......... 85% 97.1M 7s
433900K .......... .......... .......... .......... .......... 85% 10.4M 7s
433950K .......... .......... .......... .......... .......... 85% 89.1M 7s
434000K .......... .......... .......... .......... .......... 85% 136M 7s
434050K .......... .......... .......... .......... .......... 85% 123M 7s
434100K .......... .......... .......... .......... .......... 85% 197M 7s
434150K .......... .......... .......... .......... .......... 85% 226M 7s
434200K .......... .......... .......... .......... .......... 86% 8.02M 7s
434250K .......... .......... .......... .......... .......... 86% 153M 7s
434300K .......... .......... .......... .......... .......... 86% 5.63M 7s
434350K .......... .......... .......... .......... .......... 86% 109M 7s
434400K .......... .......... .......... .......... .......... 86% 100M 7s
434450K .......... .......... .......... .......... .......... 86% 184M 7s
434500K .......... .......... .......... .......... .......... 86% 270M 7s
434550K .......... .......... .......... .......... .......... 86% 268M 7s
434600K .......... .......... .......... .......... .......... 86% 185M 7s
434650K .......... .......... .......... .......... .......... 86% 215M 7s
434700K .......... .......... .......... .......... .......... 86% 148M 7s
434750K .......... .......... .......... .......... .......... 86% 194M 7s
434800K .......... .......... .......... .......... .......... 86% 209M 7s
434850K .......... .......... .......... .......... .......... 86% 208M 7s
434900K .......... .......... .......... .......... .......... 86% 178M 7s
434950K .......... .......... .......... .......... .......... 86% 227M 7s
435000K .......... .......... .......... .......... .......... 86% 18.4M 7s
435050K .......... .......... .......... .......... .......... 86% 222M 7s
435100K .......... .......... .......... .......... .......... 86% 144M 7s
435150K .......... .......... .......... .......... .......... 86% 145M 6s
435200K .......... .......... .......... .......... .......... 86% 5.65M 6s
435250K .......... .......... .......... .......... .......... 86% 150M 6s
435300K .......... .......... .......... .......... .......... 86% 8.06M 6s
435350K .......... .......... .......... .......... .......... 86% 115M 6s
435400K .......... .......... .......... .......... .......... 86% 95.2M 6s
435450K .......... .......... .......... .......... .......... 86% 95.2M 6s
435500K .......... .......... .......... .......... .......... 86% 140M 6s
435550K .......... .......... .......... .......... .......... 86% 254M 6s
435600K .......... .......... .......... .......... .......... 86% 124M 6s
435650K .......... .......... .......... .......... .......... 86% 110M 6s
435700K .......... .......... .......... .......... .......... 86% 234M 6s
435750K .......... .......... .......... .......... .......... 86% 109M 6s
435800K .......... .......... .......... .......... .......... 86% 134M 6s
435850K .......... .......... .......... .......... .......... 86% 140M 6s
435900K .......... .......... .......... .......... .......... 86% 242M 6s
435950K .......... .......... .......... .......... .......... 86% 9.95M 6s
436000K .......... .......... .......... .......... .......... 86% 210M 6s
436050K .......... .......... .......... .......... .......... 86% 107M 6s
436100K .......... .......... .......... .......... .......... 86% 109M 6s
436150K .......... .......... .......... .......... .......... 86% 220M 6s
436200K .......... .......... .......... .......... .......... 86% 109M 6s
436250K .......... .......... .......... .......... .......... 86% 8.15M 6s
436300K .......... .......... .......... .......... .......... 86% 263M 6s
436350K .......... .......... .......... .......... .......... 86% 93.4M 6s
436400K .......... .......... .......... .......... .......... 86% 153M 6s
436450K .......... .......... .......... .......... .......... 86% 140M 6s
436500K .......... .......... .......... .......... .......... 86% 146M 6s
436550K .......... .......... .......... .......... .......... 86% 196M 6s
436600K .......... .......... .......... .......... .......... 86% 8.18M 6s
436650K .......... .......... .......... .......... .......... 86% 135M 6s
436700K .......... .......... .......... .......... .......... 86% 133M 6s
436750K .......... .......... .......... .......... .......... 86% 149M 6s
436800K .......... .......... .......... .......... .......... 86% 235M 6s
436850K .......... .......... .......... .......... .......... 86% 140M 6s
436900K .......... .......... .......... .......... .......... 86% 8.42M 6s
436950K .......... .......... .......... .......... .......... 86% 153M 6s
437000K .......... .......... .......... .......... .......... 86% 138M 6s
437050K .......... .......... .......... .......... .......... 86% 140M 6s
437100K .......... .......... .......... .......... .......... 86% 81.7M 6s
437150K .......... .......... .......... .......... .......... 86% 116M 6s
437200K .......... .......... .......... .......... .......... 86% 8.92M 6s
437250K .......... .......... .......... .......... .......... 86% 157M 6s
437300K .......... .......... .......... .......... .......... 86% 123M 6s
437350K .......... .......... .......... .......... .......... 86% 7.07M 6s
437400K .......... .......... .......... .......... .......... 86% 157M 6s
437450K .......... .......... .......... .......... .......... 86% 158M 6s
437500K .......... .......... .......... .......... .......... 86% 155M 6s
437550K .......... .......... .......... .......... .......... 86% 140M 6s
437600K .......... .......... .......... .......... .......... 86% 111M 6s
437650K .......... .......... .......... .......... .......... 86% 124M 6s
437700K .......... .......... .......... .......... .......... 86% 132M 6s
437750K .......... .......... .......... .......... .......... 86% 156M 6s
437800K .......... .......... .......... .......... .......... 86% 148M 6s
437850K .......... .......... .......... .......... .......... 86% 6.78M 6s
437900K .......... .......... .......... .......... .......... 86% 237M 6s
437950K .......... .......... .......... .......... .......... 86% 113M 6s
438000K .......... .......... .......... .......... .......... 86% 217M 6s
438050K .......... .......... .......... .......... .......... 86% 126M 6s
438100K .......... .......... .......... .......... .......... 86% 252M 6s
438150K .......... .......... .......... .......... .......... 86% 253M 6s
438200K .......... .......... .......... .......... .......... 86% 241M 6s
438250K .......... .......... .......... .......... .......... 86% 167M 6s
438300K .......... .......... .......... .......... .......... 86% 8.93M 6s
438350K .......... .......... .......... .......... .......... 86% 108M 6s
438400K .......... .......... .......... .......... .......... 86% 5.63M 6s
438450K .......... .......... .......... .......... .......... 86% 119M 6s
438500K .......... .......... .......... .......... .......... 86% 98.8M 6s
438550K .......... .......... .......... .......... .......... 86% 284M 6s
438600K .......... .......... .......... .......... .......... 86% 219M 6s
438650K .......... .......... .......... .......... .......... 86% 146M 6s
438700K .......... .......... .......... .......... .......... 86% 284M 6s
438750K .......... .......... .......... .......... .......... 86% 339M 6s
438800K .......... .......... .......... .......... .......... 86% 337M 6s
438850K .......... .......... .......... .......... .......... 86% 274M 6s
438900K .......... .......... .......... .......... .......... 86% 321M 6s
438950K .......... .......... .......... .......... .......... 86% 175M 6s
439000K .......... .......... .......... .......... .......... 86% 248M 6s
439050K .......... .......... .......... .......... .......... 86% 27.1M 6s
439100K .......... .......... .......... .......... .......... 86% 109M 6s
439150K .......... .......... .......... .......... .......... 86% 97.1M 6s
439200K .......... .......... .......... .......... .......... 86% 178M 6s
439250K .......... .......... .......... .......... .......... 87% 5.69M 6s
439300K .......... .......... .......... .......... .......... 87% 144M 6s
439350K .......... .......... .......... .......... .......... 87% 123M 6s
439400K .......... .......... .......... .......... .......... 87% 7.51M 6s
439450K .......... .......... .......... .......... .......... 87% 57.7M 6s
439500K .......... .......... .......... .......... .......... 87% 133M 6s
439550K .......... .......... .......... .......... .......... 87% 188M 6s
439600K .......... .......... .......... .......... .......... 87% 146M 6s
439650K .......... .......... .......... .......... .......... 87% 223M 6s
439700K .......... .......... .......... .......... .......... 87% 168M 6s
439750K .......... .......... .......... .......... .......... 87% 228M 6s
439800K .......... .......... .......... .......... .......... 87% 273M 6s
439850K .......... .......... .......... .......... .......... 87% 202M 6s
439900K .......... .......... .......... .......... .......... 87% 179M 6s
439950K .......... .......... .......... .......... .......... 87% 126M 6s
440000K .......... .......... .......... .......... .......... 87% 12.3M 6s
440050K .......... .......... .......... .......... .......... 87% 153M 6s
440100K .......... .......... .......... .......... .......... 87% 121M 6s
440150K .......... .......... .......... .......... .......... 87% 123M 6s
440200K .......... .......... .......... .......... .......... 87% 158M 6s
440250K .......... .......... .......... .......... .......... 87% 222M 6s
440300K .......... .......... .......... .......... .......... 87% 7.33M 6s
440350K .......... .......... .......... .......... .......... 87% 90.8M 6s
440400K .......... .......... .......... .......... .......... 87% 142M 6s
440450K .......... .......... .......... .......... .......... 87% 5.77M 6s
440500K .......... .......... .......... .......... .......... 87% 92.7M 6s
440550K .......... .......... .......... .......... .......... 87% 120M 6s
440600K .......... .......... .......... .......... .......... 87% 221M 6s
440650K .......... .......... .......... .......... .......... 87% 210M 6s
440700K .......... .......... .......... .......... .......... 87% 208M 6s
440750K .......... .......... .......... .......... .......... 87% 276M 6s
440800K .......... .......... .......... .......... .......... 87% 301M 6s
440850K .......... .......... .......... .......... .......... 87% 188M 6s
440900K .......... .......... .......... .......... .......... 87% 178M 6s
440950K .......... .......... .......... .......... .......... 87% 159M 6s
441000K .......... .......... .......... .......... .......... 87% 132M 6s
441050K .......... .......... .......... .......... .......... 87% 148M 6s
441100K .......... .......... .......... .......... .......... 87% 12.6M 6s
441150K .......... .......... .......... .......... .......... 87% 127M 6s
441200K .......... .......... .......... .......... .......... 87% 155M 6s
441250K .......... .......... .......... .......... .......... 87% 258M 6s
441300K .......... .......... .......... .......... .......... 87% 225M 6s
441350K .......... .......... .......... .......... .......... 87% 5.94M 6s
441400K .......... .......... .......... .......... .......... 87% 186M 6s
441450K .......... .......... .......... .......... .......... 87% 6.76M 6s
441500K .......... .......... .......... .......... .......... 87% 109M 6s
441550K .......... .......... .......... .......... .......... 87% 178M 6s
441600K .......... .......... .......... .......... .......... 87% 159M 6s
441650K .......... .......... .......... .......... .......... 87% 189M 6s
441700K .......... .......... .......... .......... .......... 87% 101M 6s
441750K .......... .......... .......... .......... .......... 87% 85.2M 6s
441800K .......... .......... .......... .......... .......... 87% 96.3M 6s
441850K .......... .......... .......... .......... .......... 87% 79.3M 6s
441900K .......... .......... .......... .......... .......... 87% 193M 6s
441950K .......... .......... .......... .......... .......... 87% 239M 6s
442000K .......... .......... .......... .......... .......... 87% 241M 6s
442050K .......... .......... .......... .......... .......... 87% 111M 6s
442100K .......... .......... .......... .......... .......... 87% 10.9M 6s
442150K .......... .......... .......... .......... .......... 87% 142M 6s
442200K .......... .......... .......... .......... .......... 87% 151M 6s
442250K .......... .......... .......... .......... .......... 87% 291M 6s
442300K .......... .......... .......... .......... .......... 87% 311M 6s
442350K .......... .......... .......... .......... .......... 87% 184M 6s
442400K .......... .......... .......... .......... .......... 87% 6.42M 6s
442450K .......... .......... .......... .......... .......... 87% 122M 6s
442500K .......... .......... .......... .......... .......... 87% 5.84M 6s
442550K .......... .......... .......... .......... .......... 87% 150M 6s
442600K .......... .......... .......... .......... .......... 87% 159M 6s
442650K .......... .......... .......... .......... .......... 87% 198M 6s
442700K .......... .......... .......... .......... .......... 87% 241M 6s
442750K .......... .......... .......... .......... .......... 87% 176M 6s
442800K .......... .......... .......... .......... .......... 87% 321M 6s
442850K .......... .......... .......... .......... .......... 87% 157M 6s
442900K .......... .......... .......... .......... .......... 87% 132M 6s
442950K .......... .......... .......... .......... .......... 87% 203M 6s
443000K .......... .......... .......... .......... .......... 87% 317M 6s
443050K .......... .......... .......... .......... .......... 87% 268M 6s
443100K .......... .......... .......... .......... .......... 87% 174M 6s
443150K .......... .......... .......... .......... .......... 87% 208M 6s
443200K .......... .......... .......... .......... .......... 87% 20.9M 6s
443250K .......... .......... .......... .......... .......... 87% 207M 6s
443300K .......... .......... .......... .......... .......... 87% 108M 6s
443350K .......... .......... .......... .......... .......... 87% 5.99M 6s
443400K .......... .......... .......... .......... .......... 87% 162M 6s
443450K .......... .......... .......... .......... .......... 87% 184M 6s
443500K .......... .......... .......... .......... .......... 87% 5.74M 6s
443550K .......... .......... .......... .......... .......... 87% 277M 6s
443600K .......... .......... .......... .......... .......... 87% 177M 6s
443650K .......... .......... .......... .......... .......... 87% 136M 6s
443700K .......... .......... .......... .......... .......... 87% 95.0M 6s
443750K .......... .......... .......... .......... .......... 87% 159M 6s
443800K .......... .......... .......... .......... .......... 87% 165M 6s
443850K .......... .......... .......... .......... .......... 87% 161M 6s
443900K .......... .......... .......... .......... .......... 87% 209M 6s
443950K .......... .......... .......... .......... .......... 87% 124M 6s
444000K .......... .......... .......... .......... .......... 87% 204M 6s
444050K .......... .......... .......... .......... .......... 87% 174M 6s
444100K .......... .......... .......... .......... .......... 87% 195M 6s
444150K .......... .......... .......... .......... .......... 87% 219M 6s
444200K .......... .......... .......... .......... .......... 87% 158M 6s
444250K .......... .......... .......... .......... .......... 87% 27.6M 6s
444300K .......... .......... .......... .......... .......... 88% 109M 6s
444350K .......... .......... .......... .......... .......... 88% 170M 6s
444400K .......... .......... .......... .......... .......... 88% 153M 6s
444450K .......... .......... .......... .......... .......... 88% 5.34M 6s
444500K .......... .......... .......... .......... .......... 88% 146M 6s
444550K .......... .......... .......... .......... .......... 88% 119M 6s
444600K .......... .......... .......... .......... .......... 88% 127M 6s
444650K .......... .......... .......... .......... .......... 88% 97.1M 6s
444700K .......... .......... .......... .......... .......... 88% 121M 6s
444750K .......... .......... .......... .......... .......... 88% 110M 6s
444800K .......... .......... .......... .......... .......... 88% 127M 6s
444850K .......... .......... .......... .......... .......... 88% 122M 6s
444900K .......... .......... .......... .......... .......... 88% 6.23M 5s
444950K .......... .......... .......... .......... .......... 88% 191M 5s
445000K .......... .......... .......... .......... .......... 88% 118M 5s
445050K .......... .......... .......... .......... .......... 88% 108M 5s
445100K .......... .......... .......... .......... .......... 88% 228M 5s
445150K .......... .......... .......... .......... .......... 88% 152M 5s
445200K .......... .......... .......... .......... .......... 88% 178M 5s
445250K .......... .......... .......... .......... .......... 88% 164M 5s
445300K .......... .......... .......... .......... .......... 88% 182M 5s
445350K .......... .......... .......... .......... .......... 88% 8.44M 5s
445400K .......... .......... .......... .......... .......... 88% 190M 5s
445450K .......... .......... .......... .......... .......... 88% 116M 5s
445500K .......... .......... .......... .......... .......... 88% 133M 5s
445550K .......... .......... .......... .......... .......... 88% 7.63M 5s
445600K .......... .......... .......... .......... .......... 88% 96.5M 5s
445650K .......... .......... .......... .......... .......... 88% 100M 5s
445700K .......... .......... .......... .......... .......... 88% 144M 5s
445750K .......... .......... .......... .......... .......... 88% 160M 5s
445800K .......... .......... .......... .......... .......... 88% 191M 5s
445850K .......... .......... .......... .......... .......... 88% 103M 5s
445900K .......... .......... .......... .......... .......... 88% 182M 5s
445950K .......... .......... .......... .......... .......... 88% 211M 5s
446000K .......... .......... .......... .......... .......... 88% 6.52M 5s
446050K .......... .......... .......... .......... .......... 88% 135M 5s
446100K .......... .......... .......... .......... .......... 88% 105M 5s
446150K .......... .......... .......... .......... .......... 88% 121M 5s
446200K .......... .......... .......... .......... .......... 88% 104M 5s
446250K .......... .......... .......... .......... .......... 88% 296M 5s
446300K .......... .......... .......... .......... .......... 88% 140M 5s
446350K .......... .......... .......... .......... .......... 88% 113M 5s
446400K .......... .......... .......... .......... .......... 88% 8.55M 5s
446450K .......... .......... .......... .......... .......... 88% 129M 5s
446500K .......... .......... .......... .......... .......... 88% 141M 5s
446550K .......... .......... .......... .......... .......... 88% 241M 5s
446600K .......... .......... .......... .......... .......... 88% 6.65M 5s
446650K .......... .......... .......... .......... .......... 88% 80.8M 5s
446700K .......... .......... .......... .......... .......... 88% 145M 5s
446750K .......... .......... .......... .......... .......... 88% 234M 5s
446800K .......... .......... .......... .......... .......... 88% 154M 5s
446850K .......... .......... .......... .......... .......... 88% 91.4M 5s
446900K .......... .......... .......... .......... .......... 88% 132M 5s
446950K .......... .......... .......... .......... .......... 88% 123M 5s
447000K .......... .......... .......... .......... .......... 88% 115M 5s
447050K .......... .......... .......... .......... .......... 88% 276M 5s
447100K .......... .......... .......... .......... .......... 88% 105M 5s
447150K .......... .......... .......... .......... .......... 88% 137M 5s
447200K .......... .......... .......... .......... .......... 88% 12.1M 5s
447250K .......... .......... .......... .......... .......... 88% 138M 5s
447300K .......... .......... .......... .......... .......... 88% 150M 5s
447350K .......... .......... .......... .......... .......... 88% 157M 5s
447400K .......... .......... .......... .......... .......... 88% 91.6M 5s
447450K .......... .......... .......... .......... .......... 88% 126M 5s
447500K .......... .......... .......... .......... .......... 88% 298M 5s
447550K .......... .......... .......... .......... .......... 88% 7.37M 5s
447600K .......... .......... .......... .......... .......... 88% 7.11M 5s
447650K .......... .......... .......... .......... .......... 88% 227M 5s
447700K .......... .......... .......... .......... .......... 88% 109M 5s
447750K .......... .......... .......... .......... .......... 88% 94.6M 5s
447800K .......... .......... .......... .......... .......... 88% 211M 5s
447850K .......... .......... .......... .......... .......... 88% 209M 5s
447900K .......... .......... .......... .......... .......... 88% 139M 5s
447950K .......... .......... .......... .......... .......... 88% 136M 5s
448000K .......... .......... .......... .......... .......... 88% 265M 5s
448050K .......... .......... .......... .......... .......... 88% 264M 5s
448100K .......... .......... .......... .......... .......... 88% 136M 5s
448150K .......... .......... .......... .......... .......... 88% 127M 5s
448200K .......... .......... .......... .......... .......... 88% 9.66M 5s
448250K .......... .......... .......... .......... .......... 88% 128M 5s
448300K .......... .......... .......... .......... .......... 88% 119M 5s
448350K .......... .......... .......... .......... .......... 88% 225M 5s
448400K .......... .......... .......... .......... .......... 88% 294M 5s
448450K .......... .......... .......... .......... .......... 88% 214M 5s
448500K .......... .......... .......... .......... .......... 88% 131M 5s
448550K .......... .......... .......... .......... .......... 88% 154M 5s
448600K .......... .......... .......... .......... .......... 88% 6.23M 5s
448650K .......... .......... .......... .......... .......... 88% 6.90M 5s
448700K .......... .......... .......... .......... .......... 88% 82.3M 5s
448750K .......... .......... .......... .......... .......... 88% 155M 5s
448800K .......... .......... .......... .......... .......... 88% 137M 5s
448850K .......... .......... .......... .......... .......... 88% 140M 5s
448900K .......... .......... .......... .......... .......... 88% 243M 5s
448950K .......... .......... .......... .......... .......... 88% 207M 5s
449000K .......... .......... .......... .......... .......... 88% 176M 5s
449050K .......... .......... .......... .......... .......... 88% 235M 5s
449100K .......... .......... .......... .......... .......... 88% 155M 5s
449150K .......... .......... .......... .......... .......... 88% 241M 5s
449200K .......... .......... .......... .......... .......... 88% 200M 5s
449250K .......... .......... .......... .......... .......... 88% 309M 5s
449300K .......... .......... .......... .......... .......... 88% 260M 5s
449350K .......... .......... .......... .......... .......... 89% 203M 5s
449400K .......... .......... .......... .......... .......... 89% 19.6M 5s
449450K .......... .......... .......... .......... .......... 89% 86.0M 5s
449500K .......... .......... .......... .......... .......... 89% 182M 5s
449550K .......... .......... .......... .......... .......... 89% 156M 5s
449600K .......... .......... .......... .......... .......... 89% 5.28M 5s
449650K .......... .......... .......... .......... .......... 89% 6.96M 5s
449700K .......... .......... .......... .......... .......... 89% 83.0M 5s
449750K .......... .......... .......... .......... .......... 89% 140M 5s
449800K .......... .......... .......... .......... .......... 89% 223M 5s
449850K .......... .......... .......... .......... .......... 89% 176M 5s
449900K .......... .......... .......... .......... .......... 89% 317M 5s
449950K .......... .......... .......... .......... .......... 89% 117M 5s
450000K .......... .......... .......... .......... .......... 89% 136M 5s
450050K .......... .......... .......... .......... .......... 89% 138M 5s
450100K .......... .......... .......... .......... .......... 89% 182M 5s
450150K .......... .......... .......... .......... .......... 89% 116M 5s
450200K .......... .......... .......... .......... .......... 89% 118M 5s
450250K .......... .......... .......... .......... .......... 89% 252M 5s
450300K .......... .......... .......... .......... .......... 89% 163M 5s
450350K .......... .......... .......... .......... .......... 89% 152M 5s
450400K .......... .......... .......... .......... .......... 89% 250M 5s
450450K .......... .......... .......... .......... .......... 89% 37.4M 5s
450500K .......... .......... .......... .......... .......... 89% 114M 5s
450550K .......... .......... .......... .......... .......... 89% 274M 5s
450600K .......... .......... .......... .......... .......... 89% 8.89M 5s
450650K .......... .......... .......... .......... .......... 89% 218M 5s
450700K .......... .......... .......... .......... .......... 89% 6.79M 5s
450750K .......... .......... .......... .......... .......... 89% 133M 5s
450800K .......... .......... .......... .......... .......... 89% 218M 5s
450850K .......... .......... .......... .......... .......... 89% 115M 5s
450900K .......... .......... .......... .......... .......... 89% 258M 5s
450950K .......... .......... .......... .......... .......... 89% 228M 5s
451000K .......... .......... .......... .......... .......... 89% 145M 5s
451050K .......... .......... .......... .......... .......... 89% 273M 5s
451100K .......... .......... .......... .......... .......... 89% 268M 5s
451150K .......... .......... .......... .......... .......... 89% 277M 5s
451200K .......... .......... .......... .......... .......... 89% 164M 5s
451250K .......... .......... .......... .......... .......... 89% 7.55M 5s
451300K .......... .......... .......... .......... .......... 89% 143M 5s
451350K .......... .......... .......... .......... .......... 89% 110M 5s
451400K .......... .......... .......... .......... .......... 89% 175M 5s
451450K .......... .......... .......... .......... .......... 89% 89.8M 5s
451500K .......... .......... .......... .......... .......... 89% 118M 5s
451550K .......... .......... .......... .......... .......... 89% 113M 5s
451600K .......... .......... .......... .......... .......... 89% 129M 5s
451650K .......... .......... .......... .......... .......... 89% 8.34M 5s
451700K .......... .......... .......... .......... .......... 89% 5.96M 5s
451750K .......... .......... .......... .......... .......... 89% 171M 5s
451800K .......... .......... .......... .......... .......... 89% 151M 5s
451850K .......... .......... .......... .......... .......... 89% 161M 5s
451900K .......... .......... .......... .......... .......... 89% 116M 5s
451950K .......... .......... .......... .......... .......... 89% 198M 5s
452000K .......... .......... .......... .......... .......... 89% 129M 5s
452050K .......... .......... .......... .......... .......... 89% 203M 5s
452100K .......... .......... .......... .......... .......... 89% 238M 5s
452150K .......... .......... .......... .......... .......... 89% 196M 5s
452200K .......... .......... .......... .......... .......... 89% 166M 5s
452250K .......... .......... .......... .......... .......... 89% 277M 5s
452300K .......... .......... .......... .......... .......... 89% 215M 5s
452350K .......... .......... .......... .......... .......... 89% 139M 5s
452400K .......... .......... .......... .......... .......... 89% 147M 5s
452450K .......... .......... .......... .......... .......... 89% 15.8M 5s
452500K .......... .......... .......... .......... .......... 89% 248M 5s
452550K .......... .......... .......... .......... .......... 89% 164M 5s
452600K .......... .......... .......... .......... .......... 89% 112M 5s
452650K .......... .......... .......... .......... .......... 89% 111M 5s
452700K .......... .......... .......... .......... .......... 89% 5.59M 5s
452750K .......... .......... .......... .......... .......... 89% 101M 5s
452800K .......... .......... .......... .......... .......... 89% 146M 5s
452850K .......... .......... .......... .......... .......... 89% 243M 5s
452900K .......... .......... .......... .......... .......... 89% 128M 5s
452950K .......... .......... .......... .......... .......... 89% 146M 5s
453000K .......... .......... .......... .......... .......... 89% 203M 5s
453050K .......... .......... .......... .......... .......... 89% 228M 5s
453100K .......... .......... .......... .......... .......... 89% 6.60M 5s
453150K .......... .......... .......... .......... .......... 89% 153M 5s
453200K .......... .......... .......... .......... .......... 89% 201M 5s
453250K .......... .......... .......... .......... .......... 89% 112M 5s
453300K .......... .......... .......... .......... .......... 89% 286M 5s
453350K .......... .......... .......... .......... .......... 89% 135M 5s
453400K .......... .......... .......... .......... .......... 89% 287M 5s
453450K .......... .......... .......... .......... .......... 89% 115M 5s
453500K .......... .......... .......... .......... .......... 89% 6.68M 5s
453550K .......... .......... .......... .......... .......... 89% 108M 5s
453600K .......... .......... .......... .......... .......... 89% 126M 5s
453650K .......... .......... .......... .......... .......... 89% 198M 5s
453700K .......... .......... .......... .......... .......... 89% 260M 5s
453750K .......... .......... .......... .......... .......... 89% 6.71M 5s
453800K .......... .......... .......... .......... .......... 89% 99.2M 5s
453850K .......... .......... .......... .......... .......... 89% 115M 5s
453900K .......... .......... .......... .......... .......... 89% 133M 5s
453950K .......... .......... .......... .......... .......... 89% 213M 5s
454000K .......... .......... .......... .......... .......... 89% 195M 5s
454050K .......... .......... .......... .......... .......... 89% 163M 5s
454100K .......... .......... .......... .......... .......... 89% 170M 5s
454150K .......... .......... .......... .......... .......... 89% 270M 5s
454200K .......... .......... .......... .......... .......... 89% 256M 5s
454250K .......... .......... .......... .......... .......... 89% 218M 5s
454300K .......... .......... .......... .......... .......... 89% 181M 5s
454350K .......... .......... .......... .......... .......... 89% 8.20M 5s
454400K .......... .......... .......... .......... .......... 90% 153M 5s
454450K .......... .......... .......... .......... .......... 90% 165M 5s
454500K .......... .......... .......... .......... .......... 90% 223M 5s
454550K .......... .......... .......... .......... .......... 90% 196M 5s
454600K .......... .......... .......... .......... .......... 90% 245M 5s
454650K .......... .......... .......... .......... .......... 90% 213M 5s
454700K .......... .......... .......... .......... .......... 90% 6.51M 5s
454750K .......... .......... .......... .......... .......... 90% 6.95M 5s
454800K .......... .......... .......... .......... .......... 90% 88.8M 5s
454850K .......... .......... .......... .......... .......... 90% 114M 5s
454900K .......... .......... .......... .......... .......... 90% 158M 5s
454950K .......... .......... .......... .......... .......... 90% 155M 5s
455000K .......... .......... .......... .......... .......... 90% 264M 4s
455050K .......... .......... .......... .......... .......... 90% 230M 4s
455100K .......... .......... .......... .......... .......... 90% 156M 4s
455150K .......... .......... .......... .......... .......... 90% 198M 4s
455200K .......... .......... .......... .......... .......... 90% 204M 4s
455250K .......... .......... .......... .......... .......... 90% 176M 4s
455300K .......... .......... .......... .......... .......... 90% 150M 4s
455350K .......... .......... .......... .......... .......... 90% 190M 4s
455400K .......... .......... .......... .......... .......... 90% 145M 4s
455450K .......... .......... .......... .......... .......... 90% 166M 4s
455500K .......... .......... .......... .......... .......... 90% 245M 4s
455550K .......... .......... .......... .......... .......... 90% 30.6M 4s
455600K .......... .......... .......... .......... .......... 90% 184M 4s
455650K .......... .......... .......... .......... .......... 90% 168M 4s
455700K .......... .......... .......... .......... .......... 90% 118M 4s
455750K .......... .......... .......... .......... .......... 90% 5.19M 4s
455800K .......... .......... .......... .......... .......... 90% 5.97M 4s
455850K .......... .......... .......... .......... .......... 90% 103M 4s
455900K .......... .......... .......... .......... .......... 90% 192M 4s
455950K .......... .......... .......... .......... .......... 90% 108M 4s
456000K .......... .......... .......... .......... .......... 90% 122M 4s
456050K .......... .......... .......... .......... .......... 90% 127M 4s
456100K .......... .......... .......... .......... .......... 90% 177M 4s
456150K .......... .......... .......... .......... .......... 90% 100M 4s
456200K .......... .......... .......... .......... .......... 90% 169M 4s
456250K .......... .......... .......... .......... .......... 90% 152M 4s
456300K .......... .......... .......... .......... .......... 90% 237M 4s
456350K .......... .......... .......... .......... .......... 90% 191M 4s
456400K .......... .......... .......... .......... .......... 90% 237M 4s
456450K .......... .......... .......... .......... .......... 90% 184M 4s
456500K .......... .......... .......... .......... .......... 90% 203M 4s
456550K .......... .......... .......... .......... .......... 90% 116M 4s
456600K .......... .......... .......... .......... .......... 90% 113M 4s
456650K .......... .......... .......... .......... .......... 90% 210M 4s
456700K .......... .......... .......... .......... .......... 90% 149M 4s
456750K .......... .......... .......... .......... .......... 90% 5.95M 4s
456800K .......... .......... .......... .......... .......... 90% 130M 4s
456850K .......... .......... .......... .......... .......... 90% 5.99M 4s
456900K .......... .......... .......... .......... .......... 90% 195M 4s
456950K .......... .......... .......... .......... .......... 90% 103M 4s
457000K .......... .......... .......... .......... .......... 90% 132M 4s
457050K .......... .......... .......... .......... .......... 90% 224M 4s
457100K .......... .......... .......... .......... .......... 90% 125M 4s
457150K .......... .......... .......... .......... .......... 90% 242M 4s
457200K .......... .......... .......... .......... .......... 90% 129M 4s
457250K .......... .......... .......... .......... .......... 90% 226M 4s
457300K .......... .......... .......... .......... .......... 90% 113M 4s
457350K .......... .......... .......... .......... .......... 90% 147M 4s
457400K .......... .......... .......... .......... .......... 90% 303M 4s
457450K .......... .......... .......... .......... .......... 90% 204M 4s
457500K .......... .......... .......... .......... .......... 90% 236M 4s
457550K .......... .......... .......... .......... .......... 90% 267M 4s
457600K .......... .......... .......... .......... .......... 90% 21.9M 4s
457650K .......... .......... .......... .......... .......... 90% 143M 4s
457700K .......... .......... .......... .......... .......... 90% 168M 4s
457750K .......... .......... .......... .......... .......... 90% 154M 4s
457800K .......... .......... .......... .......... .......... 90% 5.98M 4s
457850K .......... .......... .......... .......... .......... 90% 95.6M 4s
457900K .......... .......... .......... .......... .......... 90% 173M 4s
457950K .......... .......... .......... .......... .......... 90% 146M 4s
458000K .......... .......... .......... .......... .......... 90% 138M 4s
458050K .......... .......... .......... .......... .......... 90% 191M 4s
458100K .......... .......... .......... .......... .......... 90% 190M 4s
458150K .......... .......... .......... .......... .......... 90% 257M 4s
458200K .......... .......... .......... .......... .......... 90% 8.66M 4s
458250K .......... .......... .......... .......... .......... 90% 93.7M 4s
458300K .......... .......... .......... .......... .......... 90% 157M 4s
458350K .......... .......... .......... .......... .......... 90% 136M 4s
458400K .......... .......... .......... .......... .......... 90% 138M 4s
458450K .......... .......... .......... .......... .......... 90% 124M 4s
458500K .......... .......... .......... .......... .......... 90% 143M 4s
458550K .......... .......... .......... .......... .......... 90% 190M 4s
458600K .......... .......... .......... .......... .......... 90% 6.81M 4s
458650K .......... .......... .......... .......... .......... 90% 95.0M 4s
458700K .......... .......... .......... .......... .......... 90% 128M 4s
458750K .......... .......... .......... .......... .......... 90% 101M 4s
458800K .......... .......... .......... .......... .......... 90% 196M 4s
458850K .......... .......... .......... .......... .......... 90% 7.60M 4s
458900K .......... .......... .......... .......... .......... 90% 168M 4s
458950K .......... .......... .......... .......... .......... 90% 88.9M 4s
459000K .......... .......... .......... .......... .......... 90% 132M 4s
459050K .......... .......... .......... .......... .......... 90% 153M 4s
459100K .......... .......... .......... .......... .......... 90% 161M 4s
459150K .......... .......... .......... .......... .......... 90% 148M 4s
459200K .......... .......... .......... .......... .......... 90% 109M 4s
459250K .......... .......... .......... .......... .......... 90% 142M 4s
459300K .......... .......... .......... .......... .......... 90% 174M 4s
459350K .......... .......... .......... .......... .......... 90% 110M 4s
459400K .......... .......... .......... .......... .......... 90% 119M 4s
459450K .......... .......... .......... .......... .......... 91% 9.85M 4s
459500K .......... .......... .......... .......... .......... 91% 201M 4s
459550K .......... .......... .......... .......... .......... 91% 195M 4s
459600K .......... .......... .......... .......... .......... 91% 121M 4s
459650K .......... .......... .......... .......... .......... 91% 163M 4s
459700K .......... .......... .......... .......... .......... 91% 187M 4s
459750K .......... .......... .......... .......... .......... 91% 321M 4s
459800K .......... .......... .......... .......... .......... 91% 5.85M 4s
459850K .......... .......... .......... .......... .......... 91% 106M 4s
459900K .......... .......... .......... .......... .......... 91% 6.98M 4s
459950K .......... .......... .......... .......... .......... 91% 86.4M 4s
460000K .......... .......... .......... .......... .......... 91% 106M 4s
460050K .......... .......... .......... .......... .......... 91% 180M 4s
460100K .......... .......... .......... .......... .......... 91% 126M 4s
460150K .......... .......... .......... .......... .......... 91% 136M 4s
460200K .......... .......... .......... .......... .......... 91% 124M 4s
460250K .......... .......... .......... .......... .......... 91% 136M 4s
460300K .......... .......... .......... .......... .......... 91% 169M 4s
460350K .......... .......... .......... .......... .......... 91% 226M 4s
460400K .......... .......... .......... .......... .......... 91% 230M 4s
460450K .......... .......... .......... .......... .......... 91% 150M 4s
460500K .......... .......... .......... .......... .......... 91% 159M 4s
460550K .......... .......... .......... .......... .......... 91% 142M 4s
460600K .......... .......... .......... .......... .......... 91% 108M 4s
460650K .......... .......... .......... .......... .......... 91% 44.4M 4s
460700K .......... .......... .......... .......... .......... 91% 114M 4s
460750K .......... .......... .......... .......... .......... 91% 144M 4s
460800K .......... .......... .......... .......... .......... 91% 203M 4s
460850K .......... .......... .......... .......... .......... 91% 4.54M 4s
460900K .......... .......... .......... .......... .......... 91% 6.33M 4s
460950K .......... .......... .......... .......... .......... 91% 89.1M 4s
461000K .......... .......... .......... .......... .......... 91% 160M 4s
461050K .......... .......... .......... .......... .......... 91% 178M 4s
461100K .......... .......... .......... .......... .......... 91% 100M 4s
461150K .......... .......... .......... .......... .......... 91% 142M 4s
461200K .......... .......... .......... .......... .......... 91% 166M 4s
461250K .......... .......... .......... .......... .......... 91% 311M 4s
461300K .......... .......... .......... .......... .......... 91% 307M 4s
461350K .......... .......... .......... .......... .......... 91% 215M 4s
461400K .......... .......... .......... .......... .......... 91% 287M 4s
461450K .......... .......... .......... .......... .......... 91% 206M 4s
461500K .......... .......... .......... .......... .......... 91% 178M 4s
461550K .......... .......... .......... .......... .......... 91% 296M 4s
461600K .......... .......... .......... .......... .......... 91% 134M 4s
461650K .......... .......... .......... .......... .......... 91% 112M 4s
461700K .......... .......... .......... .......... .......... 91% 152M 4s
461750K .......... .......... .......... .......... .......... 91% 121M 4s
461800K .......... .......... .......... .......... .......... 91% 167M 4s
461850K .......... .......... .......... .......... .......... 91% 135M 4s
461900K .......... .......... .......... .......... .......... 91% 6.36M 4s
461950K .......... .......... .......... .......... .......... 91% 7.52M 4s
462000K .......... .......... .......... .......... .......... 91% 108M 4s
462050K .......... .......... .......... .......... .......... 91% 161M 4s
462100K .......... .......... .......... .......... .......... 91% 75.2M 4s
462150K .......... .......... .......... .......... .......... 91% 141M 4s
462200K .......... .......... .......... .......... .......... 91% 156M 4s
462250K .......... .......... .......... .......... .......... 91% 309M 4s
462300K .......... .......... .......... .......... .......... 91% 326M 4s
462350K .......... .......... .......... .......... .......... 91% 238M 4s
462400K .......... .......... .......... .......... .......... 91% 286M 4s
462450K .......... .......... .......... .......... .......... 91% 200M 4s
462500K .......... .......... .......... .......... .......... 91% 282M 4s
462550K .......... .......... .......... .......... .......... 91% 8.61M 4s
462600K .......... .......... .......... .......... .......... 91% 184M 4s
462650K .......... .......... .......... .......... .......... 91% 144M 4s
462700K .......... .......... .......... .......... .......... 91% 198M 4s
462750K .......... .......... .......... .......... .......... 91% 154M 4s
462800K .......... .......... .......... .......... .......... 91% 117M 4s
462850K .......... .......... .......... .......... .......... 91% 129M 4s
462900K .......... .......... .......... .......... .......... 91% 6.05M 4s
462950K .......... .......... .......... .......... .......... 91% 6.77M 4s
463000K .......... .......... .......... .......... .......... 91% 156M 4s
463050K .......... .......... .......... .......... .......... 91% 104M 4s
463100K .......... .......... .......... .......... .......... 91% 114M 4s
463150K .......... .......... .......... .......... .......... 91% 172M 4s
463200K .......... .......... .......... .......... .......... 91% 186M 4s
463250K .......... .......... .......... .......... .......... 91% 289M 4s
463300K .......... .......... .......... .......... .......... 91% 94.3M 4s
463350K .......... .......... .......... .......... .......... 91% 113M 4s
463400K .......... .......... .......... .......... .......... 91% 150M 4s
463450K .......... .......... .......... .......... .......... 91% 131M 4s
463500K .......... .......... .......... .......... .......... 91% 270M 4s
463550K .......... .......... .......... .......... .......... 91% 189M 4s
463600K .......... .......... .......... .......... .......... 91% 185M 4s
463650K .......... .......... .......... .......... .......... 91% 219M 4s
463700K .......... .......... .......... .......... .......... 91% 165M 4s
463750K .......... .......... .......... .......... .......... 91% 23.2M 4s
463800K .......... .......... .......... .......... .......... 91% 120M 4s
463850K .......... .......... .......... .......... .......... 91% 117M 4s
463900K .......... .......... .......... .......... .......... 91% 80.4M 4s
463950K .......... .......... .......... .......... .......... 91% 6.17M 4s
464000K .......... .......... .......... .......... .......... 91% 6.79M 4s
464050K .......... .......... .......... .......... .......... 91% 130M 4s
464100K .......... .......... .......... .......... .......... 91% 141M 4s
464150K .......... .......... .......... .......... .......... 91% 117M 4s
464200K .......... .......... .......... .......... .......... 91% 118M 4s
464250K .......... .......... .......... .......... .......... 91% 123M 4s
464300K .......... .......... .......... .......... .......... 91% 216M 4s
464350K .......... .......... .......... .......... .......... 91% 202M 4s
464400K .......... .......... .......... .......... .......... 91% 311M 4s
464450K .......... .......... .......... .......... .......... 91% 203M 4s
464500K .......... .......... .......... .......... .......... 92% 114M 4s
464550K .......... .......... .......... .......... .......... 92% 135M 4s
464600K .......... .......... .......... .......... .......... 92% 147M 4s
464650K .......... .......... .......... .......... .......... 92% 156M 4s
464700K .......... .......... .......... .......... .......... 92% 230M 4s
464750K .......... .......... .......... .......... .......... 92% 12.4M 4s
464800K .......... .......... .......... .......... .......... 92% 110M 4s
464850K .......... .......... .......... .......... .......... 92% 109M 4s
464900K .......... .......... .......... .......... .......... 92% 210M 4s
464950K .......... .......... .......... .......... .......... 92% 228M 4s
465000K .......... .......... .......... .......... .......... 92% 6.78M 4s
465050K .......... .......... .......... .......... .......... 92% 264M 4s
465100K .......... .......... .......... .......... .......... 92% 177M 4s
465150K .......... .......... .......... .......... .......... 92% 122M 4s
465200K .......... .......... .......... .......... .......... 92% 231M 4s
465250K .......... .......... .......... .......... .......... 92% 245M 4s
465300K .......... .......... .......... .......... .......... 92% 294M 4s
465350K .......... .......... .......... .......... .......... 92% 199M 4s
465400K .......... .......... .......... .......... .......... 92% 216M 3s
465450K .......... .......... .......... .......... .......... 92% 6.42M 3s
465500K .......... .......... .......... .......... .......... 92% 204M 3s
465550K .......... .......... .......... .......... .......... 92% 121M 3s
465600K .......... .......... .......... .......... .......... 92% 270M 3s
465650K .......... .......... .......... .......... .......... 92% 261M 3s
465700K .......... .......... .......... .......... .......... 92% 167M 3s
465750K .......... .......... .......... .......... .......... 92% 187M 3s
465800K .......... .......... .......... .......... .......... 92% 181M 3s
465850K .......... .......... .......... .......... .......... 92% 168M 3s
465900K .......... .......... .......... .......... .......... 92% 8.11M 3s
465950K .......... .......... .......... .......... .......... 92% 165M 3s
466000K .......... .......... .......... .......... .......... 92% 193M 3s
466050K .......... .......... .......... .......... .......... 92% 6.11M 3s
466100K .......... .......... .......... .......... .......... 92% 166M 3s
466150K .......... .......... .......... .......... .......... 92% 103M 3s
466200K .......... .......... .......... .......... .......... 92% 154M 3s
466250K .......... .......... .......... .......... .......... 92% 132M 3s
466300K .......... .......... .......... .......... .......... 92% 239M 3s
466350K .......... .......... .......... .......... .......... 92% 298M 3s
466400K .......... .......... .......... .......... .......... 92% 307M 3s
466450K .......... .......... .......... .......... .......... 92% 102M 3s
466500K .......... .......... .......... .......... .......... 92% 145M 3s
466550K .......... .......... .......... .......... .......... 92% 244M 3s
466600K .......... .......... .......... .......... .......... 92% 164M 3s
466650K .......... .......... .......... .......... .......... 92% 189M 3s
466700K .......... .......... .......... .......... .......... 92% 219M 3s
466750K .......... .......... .......... .......... .......... 92% 12.2M 3s
466800K .......... .......... .......... .......... .......... 92% 228M 3s
466850K .......... .......... .......... .......... .......... 92% 260M 3s
466900K .......... .......... .......... .......... .......... 92% 276M 3s
466950K .......... .......... .......... .......... .......... 92% 229M 3s
467000K .......... .......... .......... .......... .......... 92% 305M 3s
467050K .......... .......... .......... .......... .......... 92% 6.68M 3s
467100K .......... .......... .......... .......... .......... 92% 106M 3s
467150K .......... .......... .......... .......... .......... 92% 242M 3s
467200K .......... .......... .......... .......... .......... 92% 113M 3s
467250K .......... .......... .......... .......... .......... 92% 166M 3s
467300K .......... .......... .......... .......... .......... 92% 161M 3s
467350K .......... .......... .......... .......... .......... 92% 192M 3s
467400K .......... .......... .......... .......... .......... 92% 286M 3s
467450K .......... .......... .......... .......... .......... 92% 6.99M 3s
467500K .......... .......... .......... .......... .......... 92% 140M 3s
467550K .......... .......... .......... .......... .......... 92% 159M 3s
467600K .......... .......... .......... .......... .......... 92% 171M 3s
467650K .......... .......... .......... .......... .......... 92% 180M 3s
467700K .......... .......... .......... .......... .......... 92% 109M 3s
467750K .......... .......... .......... .......... .......... 92% 170M 3s
467800K .......... .......... .......... .......... .......... 92% 219M 3s
467850K .......... .......... .......... .......... .......... 92% 148M 3s
467900K .......... .......... .......... .......... .......... 92% 9.08M 3s
467950K .......... .......... .......... .......... .......... 92% 143M 3s
468000K .......... .......... .......... .......... .......... 92% 138M 3s
468050K .......... .......... .......... .......... .......... 92% 171M 3s
468100K .......... .......... .......... .......... .......... 92% 5.32M 3s
468150K .......... .......... .......... .......... .......... 92% 149M 3s
468200K .......... .......... .......... .......... .......... 92% 205M 3s
468250K .......... .......... .......... .......... .......... 92% 209M 3s
468300K .......... .......... .......... .......... .......... 92% 198M 3s
468350K .......... .......... .......... .......... .......... 92% 140M 3s
468400K .......... .......... .......... .......... .......... 92% 210M 3s
468450K .......... .......... .......... .......... .......... 92% 157M 3s
468500K .......... .......... .......... .......... .......... 92% 161M 3s
468550K .......... .......... .......... .......... .......... 92% 222M 3s
468600K .......... .......... .......... .......... .......... 92% 234M 3s
468650K .......... .......... .......... .......... .......... 92% 203M 3s
468700K .......... .......... .......... .......... .......... 92% 10.2M 3s
468750K .......... .......... .......... .......... .......... 92% 140M 3s
468800K .......... .......... .......... .......... .......... 92% 241M 3s
468850K .......... .......... .......... .......... .......... 92% 206M 3s
468900K .......... .......... .......... .......... .......... 92% 161M 3s
468950K .......... .......... .......... .......... .......... 92% 261M 3s
469000K .......... .......... .......... .......... .......... 92% 317M 3s
469050K .......... .......... .......... .......... .......... 92% 8.66M 3s
469100K .......... .......... .......... .......... .......... 92% 7.69M 3s
469150K .......... .......... .......... .......... .......... 92% 152M 3s
469200K .......... .......... .......... .......... .......... 92% 97.5M 3s
469250K .......... .......... .......... .......... .......... 92% 99.2M 3s
469300K .......... .......... .......... .......... .......... 92% 93.7M 3s
469350K .......... .......... .......... .......... .......... 92% 160M 3s
469400K .......... .......... .......... .......... .......... 92% 197M 3s
469450K .......... .......... .......... .......... .......... 92% 85.7M 3s
469500K .......... .......... .......... .......... .......... 92% 114M 3s
469550K .......... .......... .......... .......... .......... 93% 132M 3s
469600K .......... .......... .......... .......... .......... 93% 98.6M 3s
469650K .......... .......... .......... .......... .......... 93% 224M 3s
469700K .......... .......... .......... .......... .......... 93% 9.22M 3s
469750K .......... .......... .......... .......... .......... 93% 149M 3s
469800K .......... .......... .......... .......... .......... 93% 124M 3s
469850K .......... .......... .......... .......... .......... 93% 113M 3s
469900K .......... .......... .......... .......... .......... 93% 200M 3s
469950K .......... .......... .......... .......... .......... 93% 108M 3s
470000K .......... .......... .......... .......... .......... 93% 222M 3s
470050K .......... .......... .......... .......... .......... 93% 264M 3s
470100K .......... .......... .......... .......... .......... 93% 5.88M 3s
470150K .......... .......... .......... .......... .......... 93% 6.37M 3s
470200K .......... .......... .......... .......... .......... 93% 140M 3s
470250K .......... .......... .......... .......... .......... 93% 112M 3s
470300K .......... .......... .......... .......... .......... 93% 117M 3s
470350K .......... .......... .......... .......... .......... 93% 114M 3s
470400K .......... .......... .......... .......... .......... 93% 50.8M 3s
470450K .......... .......... .......... .......... .......... 93% 131M 3s
470500K .......... .......... .......... .......... .......... 93% 292M 3s
470550K .......... .......... .......... .......... .......... 93% 212M 3s
470600K .......... .......... .......... .......... .......... 93% 239M 3s
470650K .......... .......... .......... .......... .......... 93% 230M 3s
470700K .......... .......... .......... .......... .......... 93% 216M 3s
470750K .......... .......... .......... .......... .......... 93% 315M 3s
470800K .......... .......... .......... .......... .......... 93% 277M 3s
470850K .......... .......... .......... .......... .......... 93% 239M 3s
470900K .......... .......... .......... .......... .......... 93% 23.6M 3s
470950K .......... .......... .......... .......... .......... 93% 121M 3s
471000K .......... .......... .......... .......... .......... 93% 245M 3s
471050K .......... .......... .......... .......... .......... 93% 167M 3s
471100K .......... .......... .......... .......... .......... 93% 227M 3s
471150K .......... .......... .......... .......... .......... 93% 5.56M 3s
471200K .......... .......... .......... .......... .......... 93% 177M 3s
471250K .......... .......... .......... .......... .......... 93% 159M 3s
471300K .......... .......... .......... .......... .......... 93% 131M 3s
471350K .......... .......... .......... .......... .......... 93% 235M 3s
471400K .......... .......... .......... .......... .......... 93% 123M 3s
471450K .......... .......... .......... .......... .......... 93% 139M 3s
471500K .......... .......... .......... .......... .......... 93% 207M 3s
471550K .......... .......... .......... .......... .......... 93% 114M 3s
471600K .......... .......... .......... .......... .......... 93% 8.67M 3s
471650K .......... .......... .......... .......... .......... 93% 165M 3s
471700K .......... .......... .......... .......... .......... 93% 151M 3s
471750K .......... .......... .......... .......... .......... 93% 91.3M 3s
471800K .......... .......... .......... .......... .......... 93% 167M 3s
471850K .......... .......... .......... .......... .......... 93% 218M 3s
471900K .......... .......... .......... .......... .......... 93% 237M 3s
471950K .......... .......... .......... .......... .......... 93% 203M 3s
472000K .......... .......... .......... .......... .......... 93% 6.60M 3s
472050K .......... .......... .......... .......... .......... 93% 170M 3s
472100K .......... .......... .......... .......... .......... 93% 174M 3s
472150K .......... .......... .......... .......... .......... 93% 152M 3s
472200K .......... .......... .......... .......... .......... 93% 6.72M 3s
472250K .......... .......... .......... .......... .......... 93% 123M 3s
472300K .......... .......... .......... .......... .......... 93% 248M 3s
472350K .......... .......... .......... .......... .......... 93% 169M 3s
472400K .......... .......... .......... .......... .......... 93% 215M 3s
472450K .......... .......... .......... .......... .......... 93% 157M 3s
472500K .......... .......... .......... .......... .......... 93% 305M 3s
472550K .......... .......... .......... .......... .......... 93% 305M 3s
472600K .......... .......... .......... .......... .......... 93% 228M 3s
472650K .......... .......... .......... .......... .......... 93% 157M 3s
472700K .......... .......... .......... .......... .......... 93% 116M 3s
472750K .......... .......... .......... .......... .......... 93% 165M 3s
472800K .......... .......... .......... .......... .......... 93% 274M 3s
472850K .......... .......... .......... .......... .......... 93% 11.2M 3s
472900K .......... .......... .......... .......... .......... 93% 161M 3s
472950K .......... .......... .......... .......... .......... 93% 163M 3s
473000K .......... .......... .......... .......... .......... 93% 125M 3s
473050K .......... .......... .......... .......... .......... 93% 176M 3s
473100K .......... .......... .......... .......... .......... 93% 152M 3s
473150K .......... .......... .......... .......... .......... 93% 6.20M 3s
473200K .......... .......... .......... .......... .......... 93% 5.59M 3s
473250K .......... .......... .......... .......... .......... 93% 110M 3s
473300K .......... .......... .......... .......... .......... 93% 163M 3s
473350K .......... .......... .......... .......... .......... 93% 121M 3s
473400K .......... .......... .......... .......... .......... 93% 131M 3s
473450K .......... .......... .......... .......... .......... 93% 173M 3s
473500K .......... .......... .......... .......... .......... 93% 163M 3s
473550K .......... .......... .......... .......... .......... 93% 138M 3s
473600K .......... .......... .......... .......... .......... 93% 263M 3s
473650K .......... .......... .......... .......... .......... 93% 282M 3s
473700K .......... .......... .......... .......... .......... 93% 284M 3s
473750K .......... .......... .......... .......... .......... 93% 303M 3s
473800K .......... .......... .......... .......... .......... 93% 136M 3s
473850K .......... .......... .......... .......... .......... 93% 125M 3s
473900K .......... .......... .......... .......... .......... 93% 175M 3s
473950K .......... .......... .......... .......... .......... 93% 126M 3s
474000K .......... .......... .......... .......... .......... 93% 19.8M 3s
474050K .......... .......... .......... .......... .......... 93% 144M 3s
474100K .......... .......... .......... .......... .......... 93% 138M 3s
474150K .......... .......... .......... .......... .......... 93% 264M 3s
474200K .......... .......... .......... .......... .......... 93% 5.06M 3s
474250K .......... .......... .......... .......... .......... 93% 92.5M 3s
474300K .......... .......... .......... .......... .......... 93% 196M 3s
474350K .......... .......... .......... .......... .......... 93% 210M 3s
474400K .......... .......... .......... .......... .......... 93% 197M 3s
474450K .......... .......... .......... .......... .......... 93% 140M 3s
474500K .......... .......... .......... .......... .......... 93% 128M 3s
474550K .......... .......... .......... .......... .......... 93% 163M 3s
474600K .......... .......... .......... .......... .......... 94% 198M 3s
474650K .......... .......... .......... .......... .......... 94% 210M 3s
474700K .......... .......... .......... .......... .......... 94% 6.24M 3s
474750K .......... .......... .......... .......... .......... 94% 117M 3s
474800K .......... .......... .......... .......... .......... 94% 279M 3s
474850K .......... .......... .......... .......... .......... 94% 118M 3s
474900K .......... .......... .......... .......... .......... 94% 281M 3s
474950K .......... .......... .......... .......... .......... 94% 263M 3s
475000K .......... .......... .......... .......... .......... 94% 210M 3s
475050K .......... .......... .......... .......... .......... 94% 242M 3s
475100K .......... .......... .......... .......... .......... 94% 253M 3s
475150K .......... .......... .......... .......... .......... 94% 235M 3s
475200K .......... .......... .......... .......... .......... 94% 6.72M 3s
475250K .......... .......... .......... .......... .......... 94% 5.98M 3s
475300K .......... .......... .......... .......... .......... 94% 118M 3s
475350K .......... .......... .......... .......... .......... 94% 159M 3s
475400K .......... .......... .......... .......... .......... 94% 101M 3s
475450K .......... .......... .......... .......... .......... 94% 99.6M 3s
475500K .......... .......... .......... .......... .......... 94% 151M 3s
475550K .......... .......... .......... .......... .......... 94% 92.7M 3s
475600K .......... .......... .......... .......... .......... 94% 139M 3s
475650K .......... .......... .......... .......... .......... 94% 117M 3s
475700K .......... .......... .......... .......... .......... 94% 189M 3s
475750K .......... .......... .......... .......... .......... 94% 214M 3s
475800K .......... .......... .......... .......... .......... 94% 271M 3s
475850K .......... .......... .......... .......... .......... 94% 244M 3s
475900K .......... .......... .......... .......... .......... 94% 300M 3s
475950K .......... .......... .......... .......... .......... 94% 214M 3s
476000K .......... .......... .......... .......... .......... 94% 199M 3s
476050K .......... .......... .......... .......... .......... 94% 18.0M 3s
476100K .......... .......... .......... .......... .......... 94% 150M 3s
476150K .......... .......... .......... .......... .......... 94% 176M 3s
476200K .......... .......... .......... .......... .......... 94% 123M 2s
476250K .......... .......... .......... .......... .......... 94% 137M 2s
476300K .......... .......... .......... .......... .......... 94% 5.59M 2s
476350K .......... .......... .......... .......... .......... 94% 159M 2s
476400K .......... .......... .......... .......... .......... 94% 209M 2s
476450K .......... .......... .......... .......... .......... 94% 134M 2s
476500K .......... .......... .......... .......... .......... 94% 330M 2s
476550K .......... .......... .......... .......... .......... 94% 274M 2s
476600K .......... .......... .......... .......... .......... 94% 256M 2s
476650K .......... .......... .......... .......... .......... 94% 247M 2s
476700K .......... .......... .......... .......... .......... 94% 229M 2s
476750K .......... .......... .......... .......... .......... 94% 6.37M 2s
476800K .......... .......... .......... .......... .......... 94% 194M 2s
476850K .......... .......... .......... .......... .......... 94% 117M 2s
476900K .......... .......... .......... .......... .......... 94% 274M 2s
476950K .......... .......... .......... .......... .......... 94% 177M 2s
477000K .......... .......... .......... .......... .......... 94% 188M 2s
477050K .......... .......... .......... .......... .......... 94% 181M 2s
477100K .......... .......... .......... .......... .......... 94% 159M 2s
477150K .......... .......... .......... .......... .......... 94% 143M 2s
477200K .......... .......... .......... .......... .......... 94% 6.61M 2s
477250K .......... .......... .......... .......... .......... 94% 155M 2s
477300K .......... .......... .......... .......... .......... 94% 10.9M 2s
477350K .......... .......... .......... .......... .......... 94% 77.8M 2s
477400K .......... .......... .......... .......... .......... 94% 160M 2s
477450K .......... .......... .......... .......... .......... 94% 103M 2s
477500K .......... .......... .......... .......... .......... 94% 121M 2s
477550K .......... .......... .......... .......... .......... 94% 218M 2s
477600K .......... .......... .......... .......... .......... 94% 241M 2s
477650K .......... .......... .......... .......... .......... 94% 163M 2s
477700K .......... .......... .......... .......... .......... 94% 87.7M 2s
477750K .......... .......... .......... .......... .......... 94% 120M 2s
477800K .......... .......... .......... .......... .......... 94% 156M 2s
477850K .......... .......... .......... .......... .......... 94% 8.30M 2s
477900K .......... .......... .......... .......... .......... 94% 171M 2s
477950K .......... .......... .......... .......... .......... 94% 114M 2s
478000K .......... .......... .......... .......... .......... 94% 111M 2s
478050K .......... .......... .......... .......... .......... 94% 154M 2s
478100K .......... .......... .......... .......... .......... 94% 154M 2s
478150K .......... .......... .......... .......... .......... 94% 194M 2s
478200K .......... .......... .......... .......... .......... 94% 7.58M 2s
478250K .......... .......... .......... .......... .......... 94% 99.6M 2s
478300K .......... .......... .......... .......... .......... 94% 161M 2s
478350K .......... .......... .......... .......... .......... 94% 9.56M 2s
478400K .......... .......... .......... .......... .......... 94% 98.0M 2s
478450K .......... .......... .......... .......... .......... 94% 98.0M 2s
478500K .......... .......... .......... .......... .......... 94% 124M 2s
478550K .......... .......... .......... .......... .......... 94% 203M 2s
478600K .......... .......... .......... .......... .......... 94% 189M 2s
478650K .......... .......... .......... .......... .......... 94% 291M 2s
478700K .......... .......... .......... .......... .......... 94% 9.34M 2s
478750K .......... .......... .......... .......... .......... 94% 191M 2s
478800K .......... .......... .......... .......... .......... 94% 103M 2s
478850K .......... .......... .......... .......... .......... 94% 250M 2s
478900K .......... .......... .......... .......... .......... 94% 326M 2s
478950K .......... .......... .......... .......... .......... 94% 271M 2s
479000K .......... .......... .......... .......... .......... 94% 10.9M 2s
479050K .......... .......... .......... .......... .......... 94% 139M 2s
479100K .......... .......... .......... .......... .......... 94% 113M 2s
479150K .......... .......... .......... .......... .......... 94% 198M 2s
479200K .......... .......... .......... .......... .......... 94% 130M 2s
479250K .......... .......... .......... .......... .......... 94% 149M 2s
479300K .......... .......... .......... .......... .......... 94% 8.72M 2s
479350K .......... .......... .......... .......... .......... 94% 9.73M 2s
479400K .......... .......... .......... .......... .......... 94% 186M 2s
479450K .......... .......... .......... .......... .......... 94% 144M 2s
479500K .......... .......... .......... .......... .......... 94% 127M 2s
479550K .......... .......... .......... .......... .......... 94% 92.7M 2s
479600K .......... .......... .......... .......... .......... 94% 103M 2s
479650K .......... .......... .......... .......... .......... 95% 106M 2s
479700K .......... .......... .......... .......... .......... 95% 88.9M 2s
479750K .......... .......... .......... .......... .......... 95% 153M 2s
479800K .......... .......... .......... .......... .......... 95% 203M 2s
479850K .......... .......... .......... .......... .......... 95% 8.08M 2s
479900K .......... .......... .......... .......... .......... 95% 132M 2s
479950K .......... .......... .......... .......... .......... 95% 85.2M 2s
480000K .......... .......... .......... .......... .......... 95% 263M 2s
480050K .......... .......... .......... .......... .......... 95% 277M 2s
480100K .......... .......... .......... .......... .......... 95% 100M 2s
480150K .......... .......... .......... .......... .......... 95% 107M 2s
480200K .......... .......... .......... .......... .......... 95% 11.9M 2s
480250K .......... .......... .......... .......... .......... 95% 289M 2s
480300K .......... .......... .......... .......... .......... 95% 202M 2s
480350K .......... .......... .......... .......... .......... 95% 7.02M 2s
480400K .......... .......... .......... .......... .......... 95% 159M 2s
480450K .......... .......... .......... .......... .......... 95% 166M 2s
480500K .......... .......... .......... .......... .......... 95% 149M 2s
480550K .......... .......... .......... .......... .......... 95% 166M 2s
480600K .......... .......... .......... .......... .......... 95% 129M 2s
480650K .......... .......... .......... .......... .......... 95% 213M 2s
480700K .......... .......... .......... .......... .......... 95% 136M 2s
480750K .......... .......... .......... .......... .......... 95% 12.1M 2s
480800K .......... .......... .......... .......... .......... 95% 111M 2s
480850K .......... .......... .......... .......... .......... 95% 159M 2s
480900K .......... .......... .......... .......... .......... 95% 125M 2s
480950K .......... .......... .......... .......... .......... 95% 127M 2s
481000K .......... .......... .......... .......... .......... 95% 8.69M 2s
481050K .......... .......... .......... .......... .......... 95% 157M 2s
481100K .......... .......... .......... .......... .......... 95% 160M 2s
481150K .......... .......... .......... .......... .......... 95% 206M 2s
481200K .......... .......... .......... .......... .......... 95% 193M 2s
481250K .......... .......... .......... .......... .......... 95% 254M 2s
481300K .......... .......... .......... .......... .......... 95% 194M 2s
481350K .......... .......... .......... .......... .......... 95% 17.0M 2s
481400K .......... .......... .......... .......... .......... 95% 9.29M 2s
481450K .......... .......... .......... .......... .......... 95% 127M 2s
481500K .......... .......... .......... .......... .......... 95% 127M 2s
481550K .......... .......... .......... .......... .......... 95% 143M 2s
481600K .......... .......... .......... .......... .......... 95% 265M 2s
481650K .......... .......... .......... .......... .......... 95% 238M 2s
481700K .......... .......... .......... .......... .......... 95% 12.2M 2s
481750K .......... .......... .......... .......... .......... 95% 176M 2s
481800K .......... .......... .......... .......... .......... 95% 144M 2s
481850K .......... .......... .......... .......... .......... 95% 199M 2s
481900K .......... .......... .......... .......... .......... 95% 6.95M 2s
481950K .......... .......... .......... .......... .......... 95% 92.5M 2s
482000K .......... .......... .......... .......... .......... 95% 208M 2s
482050K .......... .......... .......... .......... .......... 95% 313M 2s
482100K .......... .......... .......... .......... .......... 95% 291M 2s
482150K .......... .......... .......... .......... .......... 95% 277M 2s
482200K .......... .......... .......... .......... .......... 95% 120M 2s
482250K .......... .......... .......... .......... .......... 95% 14.4M 2s
482300K .......... .......... .......... .......... .......... 95% 209M 2s
482350K .......... .......... .......... .......... .......... 95% 233M 2s
482400K .......... .......... .......... .......... .......... 95% 5.68M 2s
482450K .......... .......... .......... .......... .......... 95% 76.9M 2s
482500K .......... .......... .......... .......... .......... 95% 190M 2s
482550K .......... .......... .......... .......... .......... 95% 154M 2s
482600K .......... .......... .......... .......... .......... 95% 105M 2s
482650K .......... .......... .......... .......... .......... 95% 213M 2s
482700K .......... .......... .......... .......... .......... 95% 114M 2s
482750K .......... .......... .......... .......... .......... 95% 165M 2s
482800K .......... .......... .......... .......... .......... 95% 205M 2s
482850K .......... .......... .......... .......... .......... 95% 7.94M 2s
482900K .......... .......... .......... .......... .......... 95% 151M 2s
482950K .......... .......... .......... .......... .......... 95% 105M 2s
483000K .......... .......... .......... .......... .......... 95% 268M 2s
483050K .......... .......... .......... .......... .......... 95% 203M 2s
483100K .......... .......... .......... .......... .......... 95% 176M 2s
483150K .......... .......... .......... .......... .......... 95% 238M 2s
483200K .......... .......... .......... .......... .......... 95% 11.5M 2s
483250K .......... .......... .......... .......... .......... 95% 113M 2s
483300K .......... .......... .......... .......... .......... 95% 154M 2s
483350K .......... .......... .......... .......... .......... 95% 263M 2s
483400K .......... .......... .......... .......... .......... 95% 7.67M 2s
483450K .......... .......... .......... .......... .......... 95% 83.8M 2s
483500K .......... .......... .......... .......... .......... 95% 163M 2s
483550K .......... .......... .......... .......... .......... 95% 167M 2s
483600K .......... .......... .......... .......... .......... 95% 163M 2s
483650K .......... .......... .......... .......... .......... 95% 130M 2s
483700K .......... .......... .......... .......... .......... 95% 96.3M 2s
483750K .......... .......... .......... .......... .......... 95% 191M 2s
483800K .......... .......... .......... .......... .......... 95% 12.3M 2s
483850K .......... .......... .......... .......... .......... 95% 197M 2s
483900K .......... .......... .......... .......... .......... 95% 284M 2s
483950K .......... .......... .......... .......... .......... 95% 11.0M 2s
484000K .......... .......... .......... .......... .......... 95% 123M 2s
484050K .......... .......... .......... .......... .......... 95% 199M 2s
484100K .......... .......... .......... .......... .......... 95% 13.2M 2s
484150K .......... .......... .......... .......... .......... 95% 248M 2s
484200K .......... .......... .......... .......... .......... 95% 234M 2s
484250K .......... .......... .......... .......... .......... 95% 186M 2s
484300K .......... .......... .......... .......... .......... 95% 14.7M 2s
484350K .......... .......... .......... .......... .......... 95% 133M 2s
484400K .......... .......... .......... .......... .......... 95% 196M 2s
484450K .......... .......... .......... .......... .......... 95% 14.0M 2s
484500K .......... .......... .......... .......... .......... 95% 110M 2s
484550K .......... .......... .......... .......... .......... 95% 210M 2s
484600K .......... .......... .......... .......... .......... 95% 158M 2s
484650K .......... .......... .......... .......... .......... 95% 245M 2s
484700K .......... .......... .......... .......... .......... 96% 11.8M 2s
484750K .......... .......... .......... .......... .......... 96% 284M 2s
484800K .......... .......... .......... .......... .......... 96% 126M 2s
484850K .......... .......... .......... .......... .......... 96% 11.5M 2s
484900K .......... .......... .......... .......... .......... 96% 229M 2s
484950K .......... .......... .......... .......... .......... 96% 153M 2s
485000K .......... .......... .......... .......... .......... 96% 210M 2s
485050K .......... .......... .......... .......... .......... 96% 13.8M 2s
485100K .......... .......... .......... .......... .......... 96% 107M 2s
485150K .......... .......... .......... .......... .......... 96% 96.7M 2s
485200K .......... .......... .......... .......... .......... 96% 12.7M 2s
485250K .......... .......... .......... .......... .......... 96% 111M 2s
485300K .......... .......... .......... .......... .......... 96% 99.2M 2s
485350K .......... .......... .......... .......... .......... 96% 115M 2s
485400K .......... .......... .......... .......... .......... 96% 18.6M 2s
485450K .......... .......... .......... .......... .......... 96% 84.3M 2s
485500K .......... .......... .......... .......... .......... 96% 11.7M 2s
485550K .......... .......... .......... .......... .......... 96% 98.4M 2s
485600K .......... .......... .......... .......... .......... 96% 132M 2s
485650K .......... .......... .......... .......... .......... 96% 129M 2s
485700K .......... .......... .......... .......... .......... 96% 105M 2s
485750K .......... .......... .......... .......... .......... 96% 10.0M 2s
485800K .......... .......... .......... .......... .......... 96% 138M 2s
485850K .......... .......... .......... .......... .......... 96% 126M 2s
485900K .......... .......... .......... .......... .......... 96% 282M 2s
485950K .......... .......... .......... .......... .......... 96% 241M 2s
486000K .......... .......... .......... .......... .......... 96% 8.48M 2s
486050K .......... .......... .......... .......... .......... 96% 174M 2s
486100K .......... .......... .......... .......... .......... 96% 227M 2s
486150K .......... .......... .......... .......... .......... 96% 170M 2s
486200K .......... .......... .......... .......... .......... 96% 191M 2s
486250K .......... .......... .......... .......... .......... 96% 247M 2s
486300K .......... .......... .......... .......... .......... 96% 183M 2s
486350K .......... .......... .......... .......... .......... 96% 11.1M 2s
486400K .......... .......... .......... .......... .......... 96% 178M 2s
486450K .......... .......... .......... .......... .......... 96% 229M 2s
486500K .......... .......... .......... .......... .......... 96% 8.09M 2s
486550K .......... .......... .......... .......... .......... 96% 122M 2s
486600K .......... .......... .......... .......... .......... 96% 156M 2s
486650K .......... .......... .......... .......... .......... 96% 224M 2s
486700K .......... .......... .......... .......... .......... 96% 112M 2s
486750K .......... .......... .......... .......... .......... 96% 148M 2s
486800K .......... .......... .......... .......... .......... 96% 120M 2s
486850K .......... .......... .......... .......... .......... 96% 95.6M 2s
486900K .......... .......... .......... .......... .......... 96% 11.2M 2s
486950K .......... .......... .......... .......... .......... 96% 118M 2s
487000K .......... .......... .......... .......... .......... 96% 219M 2s
487050K .......... .......... .......... .......... .......... 96% 292M 2s
487100K .......... .......... .......... .......... .......... 96% 108M 2s
487150K .......... .......... .......... .......... .......... 96% 8.15M 2s
487200K .......... .......... .......... .......... .......... 96% 117M 2s
487250K .......... .......... .......... .......... .......... 96% 144M 2s
487300K .......... .......... .......... .......... .......... 96% 178M 2s
487350K .......... .......... .......... .......... .......... 96% 158M 2s
487400K .......... .......... .......... .......... .......... 96% 73.0M 1s
487450K .......... .......... .......... .......... .......... 96% 10.7M 1s
487500K .......... .......... .......... .......... .......... 96% 151M 1s
487550K .......... .......... .......... .......... .......... 96% 7.86M 1s
487600K .......... .......... .......... .......... .......... 96% 141M 1s
487650K .......... .......... .......... .......... .......... 96% 166M 1s
487700K .......... .......... .......... .......... .......... 96% 185M 1s
487750K .......... .......... .......... .......... .......... 96% 112M 1s
487800K .......... .......... .......... .......... .......... 96% 237M 1s
487850K .......... .......... .......... .......... .......... 96% 174M 1s
487900K .......... .......... .......... .......... .......... 96% 244M 1s
487950K .......... .......... .......... .......... .......... 96% 231M 1s
488000K .......... .......... .......... .......... .......... 96% 307M 1s
488050K .......... .......... .......... .......... .......... 96% 11.9M 1s
488100K .......... .......... .......... .......... .......... 96% 114M 1s
488150K .......... .......... .......... .......... .......... 96% 94.1M 1s
488200K .......... .......... .......... .......... .......... 96% 99.4M 1s
488250K .......... .......... .......... .......... .......... 96% 126M 1s
488300K .......... .......... .......... .......... .......... 96% 8.93M 1s
488350K .......... .......... .......... .......... .......... 96% 104M 1s
488400K .......... .......... .......... .......... .......... 96% 113M 1s
488450K .......... .......... .......... .......... .......... 96% 121M 1s
488500K .......... .......... .......... .......... .......... 96% 263M 1s
488550K .......... .......... .......... .......... .......... 96% 11.3M 1s
488600K .......... .......... .......... .......... .......... 96% 161M 1s
488650K .......... .......... .......... .......... .......... 96% 103M 1s
488700K .......... .......... .......... .......... .......... 96% 119M 1s
488750K .......... .......... .......... .......... .......... 96% 178M 1s
488800K .......... .......... .......... .......... .......... 96% 135M 1s
488850K .......... .......... .......... .......... .......... 96% 7.34M 1s
488900K .......... .......... .......... .......... .......... 96% 105M 1s
488950K .......... .......... .......... .......... .......... 96% 130M 1s
489000K .......... .......... .......... .......... .......... 96% 184M 1s
489050K .......... .......... .......... .......... .......... 96% 184M 1s
489100K .......... .......... .......... .......... .......... 96% 284M 1s
489150K .......... .......... .......... .......... .......... 96% 268M 1s
489200K .......... .......... .......... .......... .......... 96% 249M 1s
489250K .......... .......... .......... .......... .......... 96% 11.5M 1s
489300K .......... .......... .......... .......... .......... 96% 123M 1s
489350K .......... .......... .......... .......... .......... 96% 135M 1s
489400K .......... .......... .......... .......... .......... 96% 116M 1s
489450K .......... .......... .......... .......... .......... 96% 7.25M 1s
489500K .......... .......... .......... .......... .......... 96% 115M 1s
489550K .......... .......... .......... .......... .......... 96% 119M 1s
489600K .......... .......... .......... .......... .......... 96% 10.4M 1s
489650K .......... .......... .......... .......... .......... 96% 171M 1s
489700K .......... .......... .......... .......... .......... 96% 92.0M 1s
489750K .......... .......... .......... .......... .......... 97% 140M 1s
489800K .......... .......... .......... .......... .......... 97% 103M 1s
489850K .......... .......... .......... .......... .......... 97% 148M 1s
489900K .......... .......... .......... .......... .......... 97% 128M 1s
489950K .......... .......... .......... .......... .......... 97% 167M 1s
490000K .......... .......... .......... .......... .......... 97% 12.3M 1s
490050K .......... .......... .......... .......... .......... 97% 139M 1s
490100K .......... .......... .......... .......... .......... 97% 159M 1s
490150K .......... .......... .......... .......... .......... 97% 154M 1s
490200K .......... .......... .......... .......... .......... 97% 9.37M 1s
490250K .......... .......... .......... .......... .......... 97% 102M 1s
490300K .......... .......... .......... .......... .......... 97% 122M 1s
490350K .......... .......... .......... .......... .......... 97% 137M 1s
490400K .......... .......... .......... .......... .......... 97% 14.0M 1s
490450K .......... .......... .......... .......... .......... 97% 118M 1s
490500K .......... .......... .......... .......... .......... 97% 224M 1s
490550K .......... .......... .......... .......... .......... 97% 311M 1s
490600K .......... .......... .......... .......... .......... 97% 12.0M 1s
490650K .......... .......... .......... .......... .......... 97% 117M 1s
490700K .......... .......... .......... .......... .......... 97% 188M 1s
490750K .......... .......... .......... .......... .......... 97% 113M 1s
490800K .......... .......... .......... .......... .......... 97% 12.1M 1s
490850K .......... .......... .......... .......... .......... 97% 102M 1s
490900K .......... .......... .......... .......... .......... 97% 145M 1s
490950K .......... .......... .......... .......... .......... 97% 11.7M 1s
491000K .......... .......... .......... .......... .......... 97% 245M 1s
491050K .......... .......... .......... .......... .......... 97% 83.0M 1s
491100K .......... .......... .......... .......... .......... 97% 188M 1s
491150K .......... .......... .......... .......... .......... 97% 13.0M 1s
491200K .......... .......... .......... .......... .......... 97% 107M 1s
491250K .......... .......... .......... .......... .......... 97% 161M 1s
491300K .......... .......... .......... .......... .......... 97% 161M 1s
491350K .......... .......... .......... .......... .......... 97% 12.0M 1s
491400K .......... .......... .......... .......... .......... 97% 170M 1s
491450K .......... .......... .......... .......... .......... 97% 117M 1s
491500K .......... .......... .......... .......... .......... 97% 243M 1s
491550K .......... .......... .......... .......... .......... 97% 13.3M 1s
491600K .......... .......... .......... .......... .......... 97% 152M 1s
491650K .......... .......... .......... .......... .......... 97% 12.1M 1s
491700K .......... .......... .......... .......... .......... 97% 93.4M 1s
491750K .......... .......... .......... .......... .......... 97% 174M 1s
491800K .......... .......... .......... .......... .......... 97% 167M 1s
491850K .......... .......... .......... .......... .......... 97% 130M 1s
491900K .......... .......... .......... .......... .......... 97% 11.6M 1s
491950K .......... .......... .......... .......... .......... 97% 97.3M 1s
492000K .......... .......... .......... .......... .......... 97% 96.9M 1s
492050K .......... .......... .......... .......... .......... 97% 137M 1s
492100K .......... .......... .......... .......... .......... 97% 126M 1s
492150K .......... .......... .......... .......... .......... 97% 8.15M 1s
492200K .......... .......... .......... .......... .......... 97% 168M 1s
492250K .......... .......... .......... .......... .......... 97% 148M 1s
492300K .......... .......... .......... .......... .......... 97% 160M 1s
492350K .......... .......... .......... .......... .......... 97% 163M 1s
492400K .......... .......... .......... .......... .......... 97% 163M 1s
492450K .......... .......... .......... .......... .......... 97% 132M 1s
492500K .......... .......... .......... .......... .......... 97% 11.4M 1s
492550K .......... .......... .......... .......... .......... 97% 159M 1s
492600K .......... .......... .......... .......... .......... 97% 110M 1s
492650K .......... .......... .......... .......... .......... 97% 6.60M 1s
492700K .......... .......... .......... .......... .......... 97% 72.7M 1s
492750K .......... .......... .......... .......... .......... 97% 167M 1s
492800K .......... .......... .......... .......... .......... 97% 159M 1s
492850K .......... .......... .......... .......... .......... 97% 256M 1s
492900K .......... .......... .......... .......... .......... 97% 128M 1s
492950K .......... .......... .......... .......... .......... 97% 142M 1s
493000K .......... .......... .......... .......... .......... 97% 193M 1s
493050K .......... .......... .......... .......... .......... 97% 137M 1s
493100K .......... .......... .......... .......... .......... 97% 12.7M 1s
493150K .......... .......... .......... .......... .......... 97% 191M 1s
493200K .......... .......... .......... .......... .......... 97% 234M 1s
493250K .......... .......... .......... .......... .......... 97% 176M 1s
493300K .......... .......... .......... .......... .......... 97% 6.64M 1s
493350K .......... .......... .......... .......... .......... 97% 118M 1s
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493450K .......... .......... .......... .......... .......... 97% 138M 1s
493500K .......... .......... .......... .......... .......... 97% 154M 1s
493550K .......... .......... .......... .......... .......... 97% 133M 1s
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493650K .......... .......... .......... .......... .......... 97% 254M 1s
493700K .......... .......... .......... .......... .......... 97% 14.9M 1s
493750K .......... .......... .......... .......... .......... 97% 183M 1s
493800K .......... .......... .......... .......... .......... 97% 126M 1s
493850K .......... .......... .......... .......... .......... 97% 195M 1s
493900K .......... .......... .......... .......... .......... 97% 6.26M 1s
493950K .......... .......... .......... .......... .......... 97% 109M 1s
494000K .......... .......... .......... .......... .......... 97% 114M 1s
494050K .......... .......... .......... .......... .......... 97% 172M 1s
494100K .......... .......... .......... .......... .......... 97% 238M 1s
494150K .......... .......... .......... .......... .......... 97% 128M 1s
494200K .......... .......... .......... .......... .......... 97% 82.9M 1s
494250K .......... .......... .......... .......... .......... 97% 8.27M 1s
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494350K .......... .......... .......... .......... .......... 97% 132M 1s
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494450K .......... .......... .......... .......... .......... 97% 95.2M 1s
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494650K .......... .......... .......... .......... .......... 97% 11.7M 1s
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494750K .......... .......... .......... .......... .......... 97% 86.9M 1s
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494850K .......... .......... .......... .......... .......... 98% 134M 1s
494900K .......... .......... .......... .......... .......... 98% 123M 1s
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495000K .......... .......... .......... .......... .......... 98% 147M 1s
495050K .......... .......... .......... .......... .......... 98% 267M 1s
495100K .......... .......... .......... .......... .......... 98% 253M 1s
495150K .......... .......... .......... .......... .......... 98% 195M 1s
495200K .......... .......... .......... .......... .......... 98% 119M 1s
495250K .......... .......... .......... .......... .......... 98% 9.33M 1s
495300K .......... .......... .......... .......... .......... 98% 151M 1s
495350K .......... .......... .......... .......... .......... 98% 211M 1s
495400K .......... .......... .......... .......... .......... 98% 120M 1s
495450K .......... .......... .......... .......... .......... 98% 117M 1s
495500K .......... .......... .......... .......... .......... 98% 189M 1s
495550K .......... .......... .......... .......... .......... 98% 158M 1s
495600K .......... .......... .......... .......... .......... 98% 10.4M 1s
495650K .......... .......... .......... .......... .......... 98% 122M 1s
495700K .......... .......... .......... .......... .......... 98% 168M 1s
495750K .......... .......... .......... .......... .......... 98% 8.16M 1s
495800K .......... .......... .......... .......... .......... 98% 120M 1s
495850K .......... .......... .......... .......... .......... 98% 159M 1s
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496150K .......... .......... .......... .......... .......... 98% 7.12M 1s
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496550K .......... .......... .......... .......... .......... 98% 7.95M 1s
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496750K .......... .......... .......... .......... .......... 98% 7.31M 1s
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496850K .......... .......... .......... .......... .......... 98% 85.1M 1s
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497000K .......... .......... .......... .......... .......... 98% 182M 1s
497050K .......... .......... .......... .......... .......... 98% 254M 1s
497100K .......... .......... .......... .......... .......... 98% 207M 1s
497150K .......... .......... .......... .......... .......... 98% 268M 1s
497200K .......... .......... .......... .......... .......... 98% 270M 1s
497250K .......... .......... .......... .......... .......... 98% 201M 1s
497300K .......... .......... .......... .......... .......... 98% 215M 1s
497350K .......... .......... .......... .......... .......... 98% 12.3M 1s
497400K .......... .......... .......... .......... .......... 98% 201M 1s
497450K .......... .......... .......... .......... .......... 98% 176M 1s
497500K .......... .......... .......... .......... .......... 98% 213M 1s
497550K .......... .......... .......... .......... .......... 98% 276M 1s
497600K .......... .......... .......... .......... .......... 98% 202M 1s
497650K .......... .......... .......... .......... .......... 98% 8.21M 1s
497700K .......... .......... .......... .......... .......... 98% 254M 1s
497750K .......... .......... .......... .......... .......... 98% 228M 1s
497800K .......... .......... .......... .......... .......... 98% 9.20M 1s
497850K .......... .......... .......... .......... .......... 98% 119M 1s
497900K .......... .......... .......... .......... .......... 98% 268M 1s
497950K .......... .......... .......... .......... .......... 98% 203M 1s
498000K .......... .......... .......... .......... .......... 98% 274M 1s
498050K .......... .......... .......... .......... .......... 98% 233M 1s
498100K .......... .......... .......... .......... .......... 98% 228M 1s
498150K .......... .......... .......... .......... .......... 98% 305M 1s
498200K .......... .......... .......... .......... .......... 98% 189M 1s
498250K .......... .......... .......... .......... .......... 98% 11.1M 1s
498300K .......... .......... .......... .......... .......... 98% 215M 1s
498350K .......... .......... .......... .......... .......... 98% 188M 1s
498400K .......... .......... .......... .......... .......... 98% 307M 1s
498450K .......... .......... .......... .......... .......... 98% 237M 1s
498500K .......... .......... .......... .......... .......... 98% 10.0M 1s
498550K .......... .......... .......... .......... .......... 98% 253M 1s
498600K .......... .......... .......... .......... .......... 98% 212M 1s
498650K .......... .......... .......... .......... .......... 98% 253M 1s
498700K .......... .......... .......... .......... .......... 98% 189M 1s
498750K .......... .......... .......... .......... .......... 98% 292M 1s
498800K .......... .......... .......... .......... .......... 98% 10.8M 1s
498850K .......... .......... .......... .......... .......... 98% 82.5M 1s
498900K .......... .......... .......... .......... .......... 98% 233M 1s
498950K .......... .......... .......... .......... .......... 98% 210M 0s
499000K .......... .......... .......... .......... .......... 98% 311M 0s
499050K .......... .......... .......... .......... .......... 98% 292M 0s
499100K .......... .......... .......... .......... .......... 98% 9.35M 0s
499150K .......... .......... .......... .......... .......... 98% 193M 0s
499200K .......... .......... .......... .......... .......... 98% 211M 0s
499250K .......... .......... .......... .......... .......... 98% 138M 0s
499300K .......... .......... .......... .......... .......... 98% 157M 0s
499350K .......... .......... .......... .......... .......... 98% 143M 0s
499400K .......... .......... .......... .......... .......... 98% 11.6M 0s
499450K .......... .......... .......... .......... .......... 98% 117M 0s
499500K .......... .......... .......... .......... .......... 98% 313M 0s
499550K .......... .......... .......... .......... .......... 98% 252M 0s
499600K .......... .......... .......... .......... .......... 98% 198M 0s
499650K .......... .......... .......... .......... .......... 98% 282M 0s
499700K .......... .......... .......... .......... .......... 98% 10.3M 0s
499750K .......... .......... .......... .......... .......... 98% 159M 0s
499800K .......... .......... .......... .......... .......... 98% 125M 0s
499850K .......... .......... .......... .......... .......... 99% 8.41M 0s
499900K .......... .......... .......... .......... .......... 99% 143M 0s
499950K .......... .......... .......... .......... .......... 99% 94.4M 0s
500000K .......... .......... .......... .......... .......... 99% 111M 0s
500050K .......... .......... .......... .......... .......... 99% 292M 0s
500100K .......... .......... .......... .......... .......... 99% 161M 0s
500150K .......... .......... .......... .......... .......... 99% 227M 0s
500200K .......... .......... .......... .......... .......... 99% 119M 0s
500250K .......... .......... .......... .......... .......... 99% 142M 0s
500300K .......... .......... .......... .......... .......... 99% 13.1M 0s
500350K .......... .......... .......... .......... .......... 99% 131M 0s
500400K .......... .......... .......... .......... .......... 99% 120M 0s
500450K .......... .......... .......... .......... .......... 99% 170M 0s
500500K .......... .......... .......... .......... .......... 99% 236M 0s
500550K .......... .......... .......... .......... .......... 99% 8.35M 0s
500600K .......... .......... .......... .......... .......... 99% 131M 0s
500650K .......... .......... .......... .......... .......... 99% 154M 0s
500700K .......... .......... .......... .......... .......... 99% 151M 0s
500750K .......... .......... .......... .......... .......... 99% 159M 0s
500800K .......... .......... .......... .......... .......... 99% 200M 0s
500850K .......... .......... .......... .......... .......... 99% 11.0M 0s
500900K .......... .......... .......... .......... .......... 99% 98.2M 0s
500950K .......... .......... .......... .......... .......... 99% 149M 0s
501000K .......... .......... .......... .......... .......... 99% 210M 0s
501050K .......... .......... .......... .......... .......... 99% 265M 0s
501100K .......... .......... .......... .......... .......... 99% 196M 0s
501150K .......... .......... .......... .......... .......... 99% 9.31M 0s
501200K .......... .......... .......... .......... .......... 99% 116M 0s
501250K .......... .......... .......... .......... .......... 99% 110M 0s
501300K .......... .......... .......... .......... .......... 99% 176M 0s
501350K .......... .......... .......... .......... .......... 99% 155M 0s
501400K .......... .......... .......... .......... .......... 99% 298M 0s
501450K .......... .......... .......... .......... .......... 99% 9.00M 0s
501500K .......... .......... .......... .......... .......... 99% 169M 0s
501550K .......... .......... .......... .......... .......... 99% 168M 0s
501600K .......... .......... .......... .......... .......... 99% 117M 0s
501650K .......... .......... .......... .......... .......... 99% 160M 0s
501700K .......... .......... .......... .......... .......... 99% 191M 0s
501750K .......... .......... .......... .......... .......... 99% 9.74M 0s
501800K .......... .......... .......... .......... .......... 99% 110M 0s
501850K .......... .......... .......... .......... .......... 99% 203M 0s
501900K .......... .......... .......... .......... .......... 99% 7.00M 0s
501950K .......... .......... .......... .......... .......... 99% 79.1M 0s
502000K .......... .......... .......... .......... .......... 99% 143M 0s
502050K .......... .......... .......... .......... .......... 99% 125M 0s
502100K .......... .......... .......... .......... .......... 99% 286M 0s
502150K .......... .......... .......... .......... .......... 99% 346M 0s
502200K .......... .......... .......... .......... .......... 99% 286M 0s
502250K .......... .......... .......... .......... .......... 99% 212M 0s
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502350K .......... .......... .......... .......... .......... 99% 9.63M 0s
502400K .......... .......... .......... .......... .......... 99% 205M 0s
502450K .......... .......... .......... .......... .......... 99% 138M 0s
502500K .......... .......... .......... .......... .......... 99% 114M 0s
502550K .......... .......... .......... .......... .......... 99% 180M 0s
502600K .......... .......... .......... .......... .......... 99% 8.49M 0s
502650K .......... .......... .......... .......... .......... 99% 209M 0s
502700K .......... .......... .......... .......... .......... 99% 125M 0s
502750K .......... .......... .......... .......... .......... 99% 135M 0s
502800K .......... .......... .......... .......... .......... 99% 144M 0s
502850K .......... .......... .......... .......... .......... 99% 108M 0s
502900K .......... .......... .......... .......... .......... 99% 10.8M 0s
502950K .......... .......... .......... .......... .......... 99% 67.3M 0s
503000K .......... .......... .......... .......... .......... 99% 171M 0s
503050K .......... .......... .......... .......... .......... 99% 226M 0s
503100K .......... .......... .......... .......... .......... 99% 261M 0s
503150K .......... .......... .......... .......... .......... 99% 305M 0s
503200K .......... .......... .......... .......... .......... 99% 8.09M 0s
503250K .......... .......... .......... .......... .......... 99% 204M 0s
503300K .......... .......... .......... .......... .......... 99% 159M 0s
503350K .......... .......... .......... .......... .......... 99% 141M 0s
503400K .......... .......... .......... .......... .......... 99% 162M 0s
503450K .......... .......... .......... .......... .......... 99% 196M 0s
503500K .......... .......... .......... .......... .......... 99% 147M 0s
503550K .......... .......... .......... .......... .......... 99% 9.88M 0s
503600K .......... .......... .......... .......... .......... 99% 140M 0s
503650K .......... .......... .......... .......... .......... 99% 125M 0s
503700K .......... .......... .......... .......... .......... 99% 87.2M 0s
503750K .......... .......... .......... .......... .......... 99% 125M 0s
503800K .......... .......... .......... .......... .......... 99% 9.16M 0s
503850K .......... .......... .......... .......... .......... 99% 109M 0s
503900K .......... .......... .......... .......... .......... 99% 210M 0s
503950K .......... .......... .......... .......... .......... 99% 10.3M 0s
504000K .......... .......... .......... .......... .......... 99% 186M 0s
504050K .......... .......... .......... .......... .......... 99% 170M 0s
504100K .......... .......... .......... .......... .......... 99% 140M 0s
504150K .......... .......... .......... .......... .......... 99% 260M 0s
504200K .......... .......... .......... .......... .......... 99% 173M 0s
504250K .......... .......... .......... .......... .......... 99% 138M 0s
504300K .......... .......... .......... .......... .......... 99% 183M 0s
504350K .......... .......... .......... .......... .......... 99% 10.4M 0s
504400K .......... .......... .......... .......... .......... 99% 245M 0s
504450K .......... .......... .......... .......... .......... 99% 149M 0s
504500K .......... .......... .......... .......... .......... 99% 220M 0s
504550K .......... .......... .......... .......... .......... 99% 270M 0s
504600K .......... .......... .......... .......... .......... 99% 168M 0s
504650K .......... .......... .......... .......... .......... 99% 247M 0s
504700K .......... .......... .......... .......... .......... 99% 13.2M 0s
504750K .......... .......... .......... .......... .......... 99% 146M 0s
504800K .......... .......... .......... .......... .......... 99% 94.6M 0s
504850K .......... .......... .......... .......... .......... 99% 146M 0s
504900K 100% 13.7K=42s
2024-04-28 13:00:20 (11.7 MB/s) - ‘ESPbeta-macos-x86_64.tgz’ saved [517018302/517018302]
+ tar -xf ESPbeta-macos-x86_64.tgz
+ cd ESPbeta
+ rm -rf /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Custom icon assigned to '/Users/jenkins/Desktop/runESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/idle3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pyftsubset'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_op4'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/ttx'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/wingproj'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_op2'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pip3'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/undill'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/run_om_test'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/f90nml'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/webview'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/fonttools'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/openmdao'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pyNastranGUI'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/f2py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pydoc3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/2to3-3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pip3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_pynastrangui'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/numba'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/normalizer'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/virtualenv'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/reset_notebook'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/abaqus_to_nastran'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/get_gprof'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/format_converter'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pyftmerge'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/python3.11-config'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/f06'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/get_objgraph'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/config-3.11-darwin/Makefile'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/config-3.11-darwin/python-config.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/pkgconfig/python-3.11-embed.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/pkgconfig/python-3.11.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/_sysconfigdata__darwin_darwin.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/site-packages/mpi4py/mpi.cfg'
Patching 'bin/ompi_info'
Patching 'bin/orte-info'
Patching 'lib/libmpi.40.dylib'
Patching 'lib/libopen-pal.40.dylib'
Patching 'lib/openmpi/mca_io_romio321.so'
Patching 'lib/openmpi/mca_pmix_pmix3x.so'
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/orte.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/openmpi/ortecc-wrapper-data.txt'
+ rm -rf '/Users/jenkins/Desktop/*ESPbeta.command'
+ source /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN64
++ ESP_ARCH=DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad
++ export CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/OpenCASCADE-7.8.0
++ CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/OpenCASCADE-7.8.0
++ export CARARCH=.
++ CARARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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-v8.0.0/bin
++ PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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-v8.0.0/bin
++ export PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/include/python3.11
++ PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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-v8.0.0/bin
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/ESP-localhost7681.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/ESP-localhost7681.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/wvClient/wv.html'
+ which python
/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/python
+ python --version
Python 3.11.9
+ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:169]]
ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,0,999)"
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
--> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000158 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:176]]
ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,14,999)"
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
--> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000164 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:183]]
iend must not be less than ibeg when evaluating "slice(e3,4,-1)"
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
--> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (illegal_pmtr_index) in Branch Brch_000317 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:384]]
index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000332 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:402]]
index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000346 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:418]]
row index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000360 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:434]]
row index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000367 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:442]]
row index must be between 1 and 2
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000374 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:450]]
column index must be between 1 and 3
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000381 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:458]]
column index must be between 1 and 3
--> catching signal -262 (illegal_pmtr_index)
ERROR:: (UNKNOWN) in Branch Brch_001805 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1914]]
signal 1 thrown by user
--> catching signal 1 (UNKNOWN)
ERROR:: (illegal_value) in Branch Brch_001813 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1924]]
vertex and base must be different
--> catching signal -225 (illegal_value)
==> serveESP completed successfully with no verification data
real 0m3.672s
user 0m0.034s
sys 0m0.021s
+ set +x
=============================================
ESP verification case 01 passed (as expected)
=============================================
+ expectSuccess 02 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.204s
user 0m0.241s
sys 0m0.036s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m1.952s
user 0m2.873s
sys 0m0.710s
+ set +x
=============================================
ESP verification case 03 passed (as expected)
=============================================
+ expectSuccess 04 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.416s
user 0m0.471s
sys 0m0.052s
+ set +x
=============================================
ESP verification case 04 passed (as expected)
=============================================
+ expectSuccess 05 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.339s
user 0m0.503s
sys 0m0.055s
+ set +x
=============================================
ESP verification case 05 passed (as expected)
=============================================
+ expectSuccess 06 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.379s
user 0m0.534s
sys 0m0.034s
+ set +x
=============================================
ESP verification case 06 passed (as expected)
=============================================
+ expectSuccess 07 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m2.612s
user 0m4.280s
sys 0m0.701s
+ set +x
=============================================
ESP verification case 07 passed (as expected)
=============================================
+ expectSuccess 08 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data
real 0m20.370s
user 0m34.370s
sys 0m2.181s
+ set +x
=============================================
ESP verification case 08 passed (as expected)
=============================================
+ expectSuccess 09 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.446s
user 0m0.577s
sys 0m0.034s
+ set +x
=============================================
ESP verification case 09 passed (as expected)
=============================================
+ expectSuccess 10 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data
real 0m25.757s
user 0m58.856s
sys 0m16.128s
+ set +x
=============================================
ESP verification case 10 passed (as expected)
=============================================
+ expectSuccess 11 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
==> serveESP completed successfully with 1 warnings and no verification data
real 0m0.213s
user 0m0.185s
sys 0m0.033s
+ set +x
=============================================
ESP verification case 11 passed (as expected)
=============================================
+ expectSuccess 12 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.360s
user 0m0.576s
sys 0m0.016s
+ set +x
=============================================
ESP verification case 12 passed (as expected)
=============================================
+ expectSuccess 13 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.099s
user 0m0.124s
sys 0m0.014s
+ set +x
=============================================
ESP verification case 13 passed (as expected)
=============================================
+ expectSuccess 14 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data
real 0m0.298s
user 0m0.365s
sys 0m0.020s
+ set +x
=============================================
ESP verification case 14 passed (as expected)
=============================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
.................................................... PCurve Map: 48 (alloc 48)!
Surface Map: 12 (alloc 24)!
Curve Map: 28 (alloc 28)!
Writing PCurves...
Writing Curves...
Writing Surfaces...
Writing 16 Nodes...
Writing 28 Edges...
Writing 12 Loops...
Writing 12 Faces...
Writing 1 Shells...
EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 71 tests in 1.661s
OK
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m4.701s
user 0m7.019s
sys 0m0.200s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 24.309s
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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.024 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4283 6322
AFLR2 GG : Nodes, Faces = 6128 10012
AFLR2 GG : Nodes, Faces = 7863 13482
AFLR2 GG : Nodes, Faces = 9464 16684
AFLR2 GG : Nodes, Faces = 10948 19652
AFLR2 GG : Nodes, Faces = 12322 22400
AFLR2 GG : Nodes, Faces = 13619 24994
AFLR2 GG : Nodes, Faces = 14829 27414
AFLR2 GG : Nodes, Faces = 15981 29718
AFLR2 GG : Nodes, Faces = 17082 31920
AFLR2 GG : Nodes, Faces = 18110 33976
AFLR2 GG : Nodes, Faces = 19081 35918
AFLR2 GG : Nodes, Faces = 20014 37784
AFLR2 GG : Nodes, Faces = 20924 39604
AFLR2 GG : Nodes, Faces = 21782 41320
AFLR2 GG : Nodes, Faces = 22595 42946
AFLR2 GG : Nodes, Faces = 23377 44510
AFLR2 GG : Nodes, Faces = 24129 46014
AFLR2 GG : Nodes, Faces = 24840 47436
AFLR2 GG : Nodes, Faces = 25522 48800
AFLR2 GG : Nodes, Faces = 26170 50096
AFLR2 GG : Nodes, Faces = 26793 51342
AFLR2 GG : Nodes, Faces = 27346 52448
AFLR2 GG : Nodes, Faces = 27846 53448
AFLR2 GG : Nodes, Faces = 28280 54316
AFLR2 GG : Nodes, Faces = 28652 55060
AFLR2 GG : Nodes, Faces = 28920 55596
AFLR2 GG : Nodes, Faces = 29143 56042
AFLR2 GG : Nodes, Faces = 29358 56472
AFLR2 GG : Nodes, Faces = 29550 56856
AFLR2 GG : Nodes, Faces = 29693 57142
AFLR2 GG : Nodes, Faces = 29805 57366
AFLR2 GG : Nodes, Faces = 29875 57506
AFLR2 GG : Nodes, Faces = 29895 57546
AFLR2 GG : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.060 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.006 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2224 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2224 2224
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 446 894
AFLR2 IG : Nodes, Faces = 892 1786
AFLR2 IG : Nodes, Faces = 918 1838
AFLR2 IG : Nodes, Faces = 1033 2068
AFLR2 IG : Nodes, Faces = 1133 2268
AFLR2 IG : Nodes, Faces = 1233 2468
AFLR2 IG : Nodes, Faces = 1333 2668
AFLR2 IG : Nodes, Faces = 1338 2678
AFLR2 IG : Nodes, Faces = 1433 2868
AFLR2 IG : Nodes, Faces = 1533 3068
AFLR2 IG : Nodes, Faces = 1633 3268
AFLR2 IG : Nodes, Faces = 1733 3468
AFLR2 IG : Nodes, Faces = 1784 3570
AFLR2 IG : Nodes, Faces = 1833 3668
AFLR2 IG : Nodes, Faces = 1858 3718
AFLR2 IG : Nodes, Faces = 2224 4450
AFLR2 IG : Nodes, Faces = 2228 4450
AFLR2 IG : Nodes, Faces = 2224 2224
AFLR2 : CPU Time = 0.025 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2224 2224
AFLR2 GG : Nodes, Faces = 4122 6020
AFLR2 GG : Nodes, Faces = 5812 9400
AFLR2 GG : Nodes, Faces = 7299 12374
AFLR2 GG : Nodes, Faces = 8574 14924
AFLR2 GG : Nodes, Faces = 9729 17234
AFLR2 GG : Nodes, Faces = 10787 19350
AFLR2 GG : Nodes, Faces = 11767 21310
AFLR2 GG : Nodes, Faces = 12683 23142
AFLR2 GG : Nodes, Faces = 13516 24808
AFLR2 GG : Nodes, Faces = 14278 26332
AFLR2 GG : Nodes, Faces = 14999 27774
AFLR2 GG : Nodes, Faces = 15682 29140
AFLR2 GG : Nodes, Faces = 16312 30400
AFLR2 GG : Nodes, Faces = 16899 31574
AFLR2 GG : Nodes, Faces = 17451 32678
AFLR2 GG : Nodes, Faces = 17959 33694
AFLR2 GG : Nodes, Faces = 18443 34662
AFLR2 GG : Nodes, Faces = 18877 35530
AFLR2 GG : Nodes, Faces = 19283 36342
AFLR2 GG : Nodes, Faces = 19650 37076
AFLR2 GG : Nodes, Faces = 19994 37764
AFLR2 GG : Nodes, Faces = 20325 38426
AFLR2 GG : Nodes, Faces = 20638 39052
AFLR2 GG : Nodes, Faces = 20940 39656
AFLR2 GG : Nodes, Faces = 21240 40256
AFLR2 GG : Nodes, Faces = 21523 40822
AFLR2 GG : Nodes, Faces = 21792 41360
AFLR2 GG : Nodes, Faces = 22053 41882
AFLR2 GG : Nodes, Faces = 22305 42386
AFLR2 GG : Nodes, Faces = 22521 42818
AFLR2 GG : Nodes, Faces = 22696 43168
AFLR2 GG : Nodes, Faces = 22829 43434
AFLR2 GG : Nodes, Faces = 22953 43682
AFLR2 GG : Nodes, Faces = 23050 43876
AFLR2 GG : Nodes, Faces = 23110 43996
AFLR2 GG : Nodes, Faces = 23139 44054
AFLR2 GG : Nodes, Faces = 23157 44090
AFLR2 GG : Nodes, Faces = 23175 44126
AFLR2 GG : Nodes, Faces = 23183 44142
AFLR2 GG : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.053 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.005 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.024 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 = 0.061 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.006 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2224 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2224 2224
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 446 894
AFLR2 IG : Nodes, Faces = 892 1786
AFLR2 IG : Nodes, Faces = 918 1838
AFLR2 IG : Nodes, Faces = 1033 2068
AFLR2 IG : Nodes, Faces = 1133 2268
AFLR2 IG : Nodes, Faces = 1233 2468
AFLR2 IG : Nodes, Faces = 1333 2668
AFLR2 IG : Nodes, Faces = 1338 2678
AFLR2 IG : Nodes, Faces = 1433 2868
AFLR2 IG : Nodes, Faces = 1533 3068
AFLR2 IG : Nodes, Faces = 1633 3268
AFLR2 IG : Nodes, Faces = 1733 3468
AFLR2 IG : Nodes, Faces = 1784 3570
AFLR2 IG : Nodes, Faces = 1833 3668
AFLR2 IG : Nodes, Faces = 1858 3718
AFLR2 IG : Nodes, Faces = 2224 4450
AFLR2 IG : Nodes, Faces = 2228 4450
AFLR2 IG : Nodes, Faces = 2224 2224
AFLR2 : CPU Time = 0.024 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2224 2224
AFLR2 GG : Nodes, Faces = 4122 6020
AFLR2 GG : Nodes, Faces = 5812 9400
AFLR2 GG : Nodes, Faces = 7299 12374
AFLR2 GG : Nodes, Faces = 8574 14924
AFLR2 GG : Nodes, Faces = 9729 17234
AFLR2 GG : Nodes, Faces = 10787 19350
AFLR2 GG : Nodes, Faces = 11767 21310
AFLR2 GG : Nodes, Faces = 12683 23142
AFLR2 GG : Nodes, Faces = 13516 24808
AFLR2 GG : Nodes, Faces = 14278 26332
AFLR2 GG : Nodes, Faces = 14999 27774
AFLR2 GG : Nodes, Faces = 15682 29140
AFLR2 GG : Nodes, Faces = 16312 30400
AFLR2 GG : Nodes, Faces = 16899 31574
AFLR2 GG : Nodes, Faces = 17451 32678
AFLR2 GG : Nodes, Faces = 17959 33694
AFLR2 GG : Nodes, Faces = 18443 34662
AFLR2 GG : Nodes, Faces = 18877 35530
AFLR2 GG : Nodes, Faces = 19283 36342
AFLR2 GG : Nodes, Faces = 19650 37076
AFLR2 GG : Nodes, Faces = 19994 37764
AFLR2 GG : Nodes, Faces = 20325 38426
AFLR2 GG : Nodes, Faces = 20638 39052
AFLR2 GG : Nodes, Faces = 20940 39656
AFLR2 GG : Nodes, Faces = 21240 40256
AFLR2 GG : Nodes, Faces = 21523 40822
AFLR2 GG : Nodes, Faces = 21792 41360
AFLR2 GG : Nodes, Faces = 22053 41882
AFLR2 GG : Nodes, Faces = 22305 42386
AFLR2 GG : Nodes, Faces = 22521 42818
AFLR2 GG : Nodes, Faces = 22696 43168
AFLR2 GG : Nodes, Faces = 22829 43434
AFLR2 GG : Nodes, Faces = 22953 43682
AFLR2 GG : Nodes, Faces = 23050 43876
AFLR2 GG : Nodes, Faces = 23110 43996
AFLR2 GG : Nodes, Faces = 23139 44054
AFLR2 GG : Nodes, Faces = 23157 44090
AFLR2 GG : Nodes, Faces = 23175 44126
AFLR2 GG : Nodes, Faces = 23183 44142
AFLR2 GG : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.054 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.005 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
ok
test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.025 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 = 0.061 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.005 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 48 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 10 22
AFLR2 IG : Nodes, Faces = 20 42
AFLR2 IG : Nodes, Faces = 30 62
AFLR2 IG : Nodes, Faces = 40 82
AFLR2 IG : Nodes, Faces = 45 92
AFLR2 IG : Nodes, Faces = 46 94
AFLR2 IG : Nodes, Faces = 48 98
AFLR2 IG : Nodes, Faces = 52 98
AFLR2 IG : Nodes, Faces = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 48 48
AFLR2 GG : Nodes, Faces = 88 128
AFLR2 GG : Nodes, Faces = 109 170
AFLR2 GG : Nodes, Faces = 124 200
AFLR2 GG : Nodes, Faces = 136 224
AFLR2 GG : Nodes, Faces = 148 248
AFLR2 GG : Nodes, Faces = 161 274
AFLR2 GG : Nodes, Faces = 171 294
AFLR2 GG : Nodes, Faces = 181 314
AFLR2 GG : Nodes, Faces = 187 326
AFLR2 GG : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 344 344
AFLR2 GG : Nodes, Faces = 679 1014
AFLR2 GG : Nodes, Faces = 1006 1668
AFLR2 GG : Nodes, Faces = 1321 2298
AFLR2 GG : Nodes, Faces = 1604 2864
AFLR2 GG : Nodes, Faces = 1886 3428
AFLR2 GG : Nodes, Faces = 2155 3966
AFLR2 GG : Nodes, Faces = 2409 4474
AFLR2 GG : Nodes, Faces = 2649 4954
AFLR2 GG : Nodes, Faces = 2867 5390
AFLR2 GG : Nodes, Faces = 3063 5782
AFLR2 GG : Nodes, Faces = 3243 6142
AFLR2 GG : Nodes, Faces = 3400 6456
AFLR2 GG : Nodes, Faces = 3540 6736
AFLR2 GG : Nodes, Faces = 3665 6986
AFLR2 GG : Nodes, Faces = 3786 7228
AFLR2 GG : Nodes, Faces = 3900 7456
AFLR2 GG : Nodes, Faces = 4010 7676
AFLR2 GG : Nodes, Faces = 4114 7884
AFLR2 GG : Nodes, Faces = 4209 8074
AFLR2 GG : Nodes, Faces = 4292 8240
AFLR2 GG : Nodes, Faces = 4368 8392
AFLR2 GG : Nodes, Faces = 4439 8534
AFLR2 GG : Nodes, Faces = 4503 8662
AFLR2 GG : Nodes, Faces = 4560 8776
AFLR2 GG : Nodes, Faces = 4611 8878
AFLR2 GG : Nodes, Faces = 4650 8956
AFLR2 GG : Nodes, Faces = 4677 9010
AFLR2 GG : Nodes, Faces = 4695 9046
AFLR2 GG : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.011 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.002 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.010 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4058 7772
AFLR2 QI : Nodes, Faces = 4057 364
AFLR2 QI : Nodes, Faces = 4057 3703
AFLR2 QI : Nodes, Faces = 4057 7770
AFLR2 QI : Nodes, Faces = 4056 344
AFLR2 QI : Nodes, Faces = 4056 3712
AFLR2 QI : Nodes, Faces = 4056 7768
AFLR2 QI : Nodes, Faces = 4055 348
AFLR2 QI : Nodes, Faces = 4055 3709
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 392
AFLR2 QI : Nodes, Faces = 4055 3687
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 : CPU Time = 0.006 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.011 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4058 7772
AFLR2 QI : Nodes, Faces = 4057 364
AFLR2 QI : Nodes, Faces = 4057 3703
AFLR2 QI : Nodes, Faces = 4057 7770
AFLR2 QI : Nodes, Faces = 4056 344
AFLR2 QI : Nodes, Faces = 4056 3712
AFLR2 QI : Nodes, Faces = 4056 7768
AFLR2 QI : Nodes, Faces = 4055 348
AFLR2 QI : Nodes, Faces = 4055 3709
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 392
AFLR2 QI : Nodes, Faces = 4055 3687
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 : CPU Time = 0.005 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1189
Number of elements = 6249
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 6237
Number of elements = 34620
Number of triangles = 4438
Number of quadrilatarals = 0
Number of tetrahedrals = 30182
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 13613
Number of elements = 76414
Number of triangles = 8142
Number of quadrilatarals = 0
Number of tetrahedrals = 68272
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 41618
Number of elements = 236483
Number of triangles = 19838
Number of quadrilatarals = 0
Number of tetrahedrals = 216645
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 4369
Number of elements = 24223
Number of triangles = 3016
Number of quadrilatarals = 0
Number of tetrahedrals = 21207
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 11007
Number of elements = 60837
Number of triangles = 8632
Number of quadrilatarals = 0
Number of tetrahedrals = 52205
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 10474
Number of elements = 58678
Number of triangles = 6352
Number of quadrilatarals = 0
Number of tetrahedrals = 52326
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 88507
Number of elements = 497504
Number of triangles = 51750
Number of quadrilatarals = 0
Number of tetrahedrals = 445754
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16456
Number of elements = 93635
Number of triangles = 7926
Number of quadrilatarals = 0
Number of tetrahedrals = 85709
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2589
Number of elements = 13809
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11051
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3654
Number of elements = 19800
Number of triangles = 3394
Number of quadrilatarals = 0
Number of tetrahedrals = 16406
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5456
Number of elements = 30308
Number of triangles = 3656
Number of quadrilatarals = 0
Number of tetrahedrals = 26652
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4694
Number of elements = 25935
Number of triangles = 3326
Number of quadrilatarals = 0
Number of tetrahedrals = 22609
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5554
Number of elements = 30862
Number of triangles = 3756
Number of quadrilatarals = 0
Number of tetrahedrals = 27106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2260
Number of elements = 12133
Number of triangles = 2222
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2392
Number of elements = 12577
Number of triangles = 2666
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3341
Number of elements = 18069
Number of triangles = 3110
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3606
Number of elements = 18961
Number of triangles = 4002
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4414
Number of elements = 23974
Number of triangles = 3998
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4811
Number of elements = 25310
Number of triangles = 5334
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 4):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 4):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 4):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 4):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5490
Number of elements = 29891
Number of triangles = 4886
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6019
Number of elements = 31671
Number of triangles = 6666
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6542
Number of elements = 35667
Number of triangles = 5774
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7203
Number of elements = 37891
Number of triangles = 7998
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 6):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 6):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 6):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 6):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 6):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 6):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7601
Number of elements = 41489
Number of triangles = 6662
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8394
Number of elements = 44157
Number of triangles = 9330
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 19800
Number of elements = 109798
Number of triangles = 15540
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 22741
Number of elements = 119570
Number of triangles = 25312
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 19):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 19):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 19):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 19):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 19):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 19):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 19):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 8 (of 19):
Number of nodes = 1193
Number of elements = 6272
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4940
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 9 (of 19):
Number of nodes = 1176
Number of elements = 6165
Number of triangles = 1330
Number of quadrilatarals = 0
Number of tetrahedrals = 4835
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 10 (of 19):
Number of nodes = 1203
Number of elements = 6314
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4982
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 11 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 12 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 13 (of 19):
Number of nodes = 1198
Number of elements = 6296
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4964
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 14 (of 19):
Number of nodes = 1223
Number of elements = 6443
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5111
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 15 (of 19):
Number of nodes = 1184
Number of elements = 6224
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4892
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 16 (of 19):
Number of nodes = 1195
Number of elements = 6287
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4955
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 17 (of 19):
Number of nodes = 1197
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 18 (of 19):
Number of nodes = 1203
Number of elements = 6310
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4978
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 19 (of 19):
Number of nodes = 1191
Number of elements = 6253
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4921
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8857
Number of elements = 49191
Number of triangles = 6284
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8989
Number of elements = 49635
Number of triangles = 6728
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 7796
Number of elements = 43368
Number of triangles = 5396
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1193
Number of elements = 6267
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4935
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9944
Number of elements = 55193
Number of triangles = 7174
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10218
Number of elements = 56081
Number of triangles = 8062
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7818
Number of elements = 43469
Number of triangles = 5398
Number of quadrilatarals = 0
Number of tetrahedrals = 38071
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1202
Number of elements = 6320
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4988
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1198
Number of elements = 6292
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4960
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9609
Number of elements = 53228
Number of triangles = 6994
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9829
Number of elements = 53956
Number of triangles = 7722
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7789
Number of elements = 43295
Number of triangles = 5394
Number of quadrilatarals = 0
Number of tetrahedrals = 37901
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1186
Number of elements = 6230
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4898
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 854
Number of elements = 4431
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3435
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9348
Number of elements = 51734
Number of triangles = 6812
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9531
Number of elements = 52330
Number of triangles = 7408
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7804
Number of elements = 43358
Number of triangles = 5386
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1200
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9183
Number of elements = 50871
Number of triangles = 6632
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9322
Number of elements = 51307
Number of triangles = 7068
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7927
Number of elements = 44116
Number of triangles = 5382
Number of quadrilatarals = 0
Number of tetrahedrals = 38734
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 868
Number of elements = 4530
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3534
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10181
Number of elements = 56797
Number of triangles = 6782
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10671
Number of elements = 58561
Number of triangles = 8546
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7741
Number of elements = 43010
Number of triangles = 5362
Number of quadrilatarals = 0
Number of tetrahedrals = 37648
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 2692
Number of elements = 14435
Number of triangles = 2800
Number of quadrilatarals = 0
Number of tetrahedrals = 11635
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 238
Number of elements = 1116
Number of triangles = 384
Number of quadrilatarals = 0
Number of tetrahedrals = 732
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1500
Number of elements = 7757
Number of triangles = 1986
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1564
Number of elements = 7881
Number of triangles = 2110
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1160
Number of elements = 6087
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4779
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 360
Number of elements = 1635
Number of triangles = 718
Number of quadrilatarals = 0
Number of tetrahedrals = 917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 44
Number of elements = 159
Number of triangles = 84
Number of quadrilatarals = 0
Number of tetrahedrals = 75
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5075
Number of elements = 27761
Number of triangles = 4072
Number of quadrilatarals = 0
Number of tetrahedrals = 23689
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5221
Number of elements = 28313
Number of triangles = 4624
Number of quadrilatarals = 0
Number of tetrahedrals = 23689
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 4882
Number of elements = 26790
Number of triangles = 4040
Number of quadrilatarals = 0
Number of tetrahedrals = 22750
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 339
Number of elements = 1523
Number of triangles = 584
Number of quadrilatarals = 0
Number of tetrahedrals = 939
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 32776
Number of elements = 189806
Number of triangles = 8496
Number of quadrilatarals = 0
Number of tetrahedrals = 181310
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 36115
Number of elements = 203130
Number of triangles = 21820
Number of quadrilatarals = 0
Number of tetrahedrals = 181310
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 28584
Number of elements = 162362
Number of triangles = 15158
Number of quadrilatarals = 0
Number of tetrahedrals = 147204
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1425
Number of elements = 7592
Number of triangles = 1456
Number of quadrilatarals = 0
Number of tetrahedrals = 6136
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 4138
Number of elements = 22901
Number of triangles = 2938
Number of quadrilatarals = 0
Number of tetrahedrals = 19963
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 711
Number of elements = 3685
Number of triangles = 844
Number of quadrilatarals = 0
Number of tetrahedrals = 2841
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1257
Number of elements = 6590
Number of triangles = 1424
Number of quadrilatarals = 0
Number of tetrahedrals = 5166
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16639
Number of elements = 94369
Number of triangles = 8800
Number of quadrilatarals = 0
Number of tetrahedrals = 85569
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18563
Number of elements = 101745
Number of triangles = 16176
Number of quadrilatarals = 0
Number of tetrahedrals = 85569
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 12009
Number of elements = 67436
Number of triangles = 7140
Number of quadrilatarals = 0
Number of tetrahedrals = 60296
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 6554
Number of elements = 34309
Number of triangles = 9036
Number of quadrilatarals = 0
Number of tetrahedrals = 25273
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4989
Number of elements = 27641
Number of triangles = 3462
Number of quadrilatarals = 0
Number of tetrahedrals = 24179
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6401
Number of elements = 35742
Number of triangles = 4048
Number of quadrilatarals = 0
Number of tetrahedrals = 31694
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59702
Number of elements = 348382
Number of triangles = 12928
Number of quadrilatarals = 0
Number of tetrahedrals = 335454
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 58332
Number of elements = 339688
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 327260
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59702
Number of elements = 347882
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 335454
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
ok
test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - trailingEdge
Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Rib_Root, index = 1
Name = Skin, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 46
Number of elements = 44
Number of triangle elements = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes = 47
Total number of elements = 44
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 46
Number of elements = 44
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 44
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 47
Combined Number of elements = 45
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 44
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 3
Surface 2: Number of points found for aero-spline = 6
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
8 automatic connections were made for capsConnect Rib_Root (node id 1)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
ok
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice control surface data
VLM control surface name - Elevator
VLM control surface name - LeftAileron
VLM control surface name - RightAileron
VLM control surface name - Rudder
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... skipped 'No flowCart executable'
test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable'
test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable'
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable'
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable'
test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Wing1, index = 1
Name = trailingEdge, index = 2
Writing FAST file ....
Finished writing FAST file
Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 9
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = nodeBody, index = 8
Name = farfield, index = 9
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000082F5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7000082F5000 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
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000082F5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7000082F5000 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
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000082F5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7000082F5000 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
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000082F5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7000082F5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ok
test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = nodeBody, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ok
test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_setInput (test_egadsTess.TestEGADS.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_egadsTess.TestEGADS.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7820
Number of elements = 15636
Number of triangle elements = 15636
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5889
Number of elements = 11774
Number of triangle elements = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 524
Number of elements = 1044
Number of triangle elements = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14233
Total number of elements = 28454
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14233, elements - 28454
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.142292
Creating surface mesh ...
Surface mesh seconds: 0.029537
Recovering boundaries...
Boundary recovery seconds: 0.109503
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.037965
Recovering Delaunayness...
Delaunay recovery seconds: 0.050881
Refining mesh...
18972 insertions, added 13254 points, 701278 tetrahedra in queue.
6317 insertions, added 2883 points, 614952 tetrahedra in queue.
8421 insertions, added 2047 points, 103425 tetrahedra in queue.
Refinement seconds: 2.02433
Smoothing vertices...
Mesh smoothing seconds: 1.74608
Improving mesh...
Mesh improvement seconds: 0.038613
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.012586
Total running seconds: 4.19263
Statistics:
Input points: 14233
Input facets: 28454
Input segments: 42681
Input holes: 2
Input regions: 0
Mesh points: 33078
Mesh tetrahedra: 159812
Mesh faces: 333851
Mesh faces on exterior boundary: 28454
Mesh faces on input facets: 28454
Mesh edges on input segments: 42681
Steiner points inside domain: 18845
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 5
Design Variable name - Mach
Warning: No initial value set for Mach
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 6
Design Variable name - Alpha
Design Variable name - Beta
Warning: No initial value set for Beta
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Composite
Objective name - Lift^2
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Overwrite_NML is set to 'True' - a new namelist will be created
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - Alpha
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Composite
Objective name - Lift^2
Done getting CFD functional
Creating FUN3D directory tree
DesignVariable = Alpha
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Overwrite_NML is set to 'True' - a new namelist will be created
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data
ok
test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 6
Design Variable name - Alpha
Design Variable name - Beta
Warning: No initial value set for Beta
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Composite
Objective name - Lift^2
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
ok
test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7820
Number of elements = 15636
Number of triangle elements = 15636
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5889
Number of elements = 11774
Number of triangle elements = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 524
Number of elements = 1044
Number of triangle elements = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14233
Total number of elements = 28454
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14233, elements - 28454
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.143695
Creating surface mesh ...
Surface mesh seconds: 0.031688
Recovering boundaries...
Boundary recovery seconds: 0.109003
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.042754
Recovering Delaunayness...
Delaunay recovery seconds: 0.054358
Refining mesh...
18972 insertions, added 13254 points, 701278 tetrahedra in queue.
6317 insertions, added 2883 points, 614952 tetrahedra in queue.
8421 insertions, added 2047 points, 103425 tetrahedra in queue.
Refinement seconds: 1.94718
Smoothing vertices...
Mesh smoothing seconds: 1.75178
Improving mesh...
Mesh improvement seconds: 0.032718
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.012237
Total running seconds: 4.1265
Statistics:
Input points: 14233
Input facets: 28454
Input segments: 42681
Input holes: 2
Input regions: 0
Mesh points: 33078
Mesh tetrahedra: 159812
Mesh faces: 333851
Mesh faces on exterior boundary: 28454
Mesh faces on input facets: 28454
Mesh edges on input segments: 42681
Steiner points inside domain: 18845
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/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/ESPbeta/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5079, elements - 10146
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5079, elements - 10146
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
ok
test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Writing moving_body.input
ok
test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14233, elements - 28454
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ...
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - alowervar
Design Variable name - auppervar
Design Variable name - classvar
Design Variable name - ztailvar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - avar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ...
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - camber
Design Variable name - thick
Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 54 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 54 54
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 12 26
AFLR2 IG : Nodes, Faces = 24 50
AFLR2 IG : Nodes, Faces = 36 74
AFLR2 IG : Nodes, Faces = 48 98
AFLR2 IG : Nodes, Faces = 52 106
AFLR2 IG : Nodes, Faces = 53 108
AFLR2 IG : Nodes, Faces = 54 110
AFLR2 IG : Nodes, Faces = 58 110
AFLR2 IG : Nodes, Faces = 54 54
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 54 54
AFLR2 GG : Nodes, Faces = 100 146
AFLR2 GG : Nodes, Faces = 122 190
AFLR2 GG : Nodes, Faces = 138 222
AFLR2 GG : Nodes, Faces = 153 252
AFLR2 GG : Nodes, Faces = 168 282
AFLR2 GG : Nodes, Faces = 180 306
AFLR2 GG : Nodes, Faces = 192 330
AFLR2 GG : Nodes, Faces = 201 348
AFLR2 GG : Nodes, Faces = 210 366
AFLR2 GG : Nodes, Faces = 216 378
AFLR2 GG : Nodes, Faces = 221 388
AFLR2 GG : Nodes, Faces = 224 394
AFLR2 GG : Nodes, Faces = 225 396
AFLR2 : CPU Time = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 225 396
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 225
Number of elements = 450
Number of tris = 396
Number of quad = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1602
Number of elements = 8758
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7518
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2600
Number of elements = 13864
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1071
Number of elements = 5705
Number of triangles = 998
Number of quadrilatarals = 0
Number of tetrahedrals = 4707
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 15544
Number of elements = 89331
Number of triangles = 4632
Number of quadrilatarals = 0
Number of tetrahedrals = 84699
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1602
Number of elements = 8758
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7518
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_inputs (test_refine.TestREFINE.test_inputs) ... ok
test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 438
Number of elements = 2179
Number of triangles = 644
Number of quadrilatarals = 0
Number of tetrahedrals = 1535
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 936
Number of elements = 4999
Number of triangles = 758
Number of quadrilatarals = 0
Number of tetrahedrals = 4241
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 3 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 8 Faces
EGADS : Body 0 has 15 Edges
EGADS : Body 0 has 8 Loops
EGADS : Body 0 has 9 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 8 Faces
EGADS : Body 1 has 15 Edges
EGADS : Body 1 has 8 Loops
EGADS : Body 1 has 9 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 2 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 2 Loops
EGADS : Body 2 has 2 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 4 5
EGADS : 2 Yes 0 0 1 1 1 1 3 4 6
EGADS : 3 Yes 0 0 1 1 1 1 2 4 7
EGADS : 4 Yes 0 0 1 1 1 1 2 3
EGADS : 5 Yes 0 0 1 1 1 1 6 7 8
EGADS : 6 Yes 0 0 1 1 1 2 5 7 8
EGADS : 7 Yes 0 0 1 1 1 3 5 6 8
EGADS : 8 Yes 0 0 1 1 1 5 6 7
EGADS : 9 Yes 1 0 1 0 10 10 11 12 13
EGADS : 10 Yes 1 0 1 0 10 9 11 12 14
EGADS : 11 Yes 1 0 1 0 10 9 10 12 15
EGADS : 12 Yes 1 0 1 0 10 9 10 11
EGADS : 13 Yes 1 0 1 0 10 9 14 15 16
EGADS : 14 Yes 1 0 1 0 10 10 13 15 16
EGADS : 15 Yes 1 0 1 0 10 11 13 14 16
EGADS : 16 Yes 1 0 1 0 10 13 14 15
EGADS : 17 Yes 2 0 1 NA NA 18
EGADS : 18 Yes 2 0 1 NA NA 17
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 4 -3 -2
EGADS : 2 3 7 -6 -5
EGADS : 3 6 9 -1 -8
EGADS : 4 -4 -9 -7
EGADS : 5 -10 2 11 -12
EGADS : 6 -11 5 13 -14
EGADS : 7 -13 8 10 -15
EGADS : 8 12 14 15
EGADS : 9 16 19 -18 -17
EGADS : 10 18 22 -21 -20
EGADS : 11 21 24 -16 -23
EGADS : 12 -19 -24 -22
EGADS : 13 -25 17 26 -27
EGADS : 14 -26 20 28 -29
EGADS : 15 -28 23 25 -30
EGADS : 16 27 29 30
EGADS : 17 -31 -32 33 34
EGADS : 18 -35 -34 36 32
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 4 -3 -2
EGADS : 2 Yes 3 7 -6 -5
EGADS : 3 Yes 6 9 -1 -8
EGADS : 4 Yes -4 -9 -7
EGADS : 5 Yes -10 2 11 -12
EGADS : 6 Yes -11 5 13 -14
EGADS : 7 Yes -13 8 10 -15
EGADS : 8 Yes 12 14 15
EGADS : 9 Yes 16 19 -18 -17
EGADS : 10 Yes 18 22 -21 -20
EGADS : 11 Yes 21 24 -16 -23
EGADS : 12 Yes -19 -24 -22
EGADS : 13 Yes -25 17 26 -27
EGADS : 14 Yes -26 20 28 -29
EGADS : 15 Yes -28 23 25 -30
EGADS : 16 Yes 27 29 30
EGADS : 17 Yes -31 -32 33 34
EGADS : 18 Yes -35 -34 36 32
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 5
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 4
EGADS : 5 0 Yes 3 5 1 2 6
EGADS : 6 0 Yes 5 6 1 2 3
EGADS : 7 0 Yes 4 6 1 2 4
EGADS : 8 0 Yes 5 1 1 3 7
EGADS : 9 0 Yes 6 2 1 3 4
EGADS : 10 0 Yes 1 7 1 5 7
EGADS : 11 0 Yes 3 8 1 5 6
EGADS : 12 0 Yes 7 8 1 5 8
EGADS : 13 0 Yes 5 9 1 6 7
EGADS : 14 0 Yes 8 9 1 6 8
EGADS : 15 0 Yes 9 7 1 7 8
EGADS : 16 1 Yes 10 11 1 9 11
EGADS : 17 1 Yes 10 12 1 9 13
EGADS : 18 1 Yes 12 13 1 9 10
EGADS : 19 1 Yes 11 13 1 9 12
EGADS : 20 1 Yes 12 14 1 10 14
EGADS : 21 1 Yes 14 15 1 10 11
EGADS : 22 1 Yes 13 15 1 10 12
EGADS : 23 1 Yes 14 10 1 11 15
EGADS : 24 1 Yes 15 11 1 11 12
EGADS : 25 1 Yes 10 16 1 13 15
EGADS : 26 1 Yes 12 17 1 13 14
EGADS : 27 1 Yes 16 17 1 13 16
EGADS : 28 1 Yes 14 18 1 14 15
EGADS : 29 1 Yes 17 18 1 14 16
EGADS : 30 1 Yes 18 16 1 15 16
EGADS : 31 2 DEGEN 19 19 - 17
EGADS : 32 2 Yes 20 19 NA 17 18
EGADS : 33 2 DEGEN 20 20 - 17
EGADS : 34 2 Yes 20 19 NA 17 18
EGADS : 35 2 DEGEN 19 19 - 18
EGADS : 36 2 DEGEN 20 20 - 18
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 3.77246052 0 0.00459131419
EGADS : 2 Yes 5.90487498 7.07106781 0
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 4.0824829 7.07106781 0.123425948
EGADS : 5 Yes 3.77001182 0 0
EGADS : 6 Yes 5.90282524 7.07106781 0
EGADS : 7 Yes 5.90487498 0 0
EGADS : 8 Yes 4.0824829 0 0.123425948
EGADS : 9 Yes 5.90282524 0 0
EGADS : 10 Yes 11.5089842 0 0.00183652568
EGADS : 11 Yes 12.36195 2.82842712 0
EGADS : 12 Yes 10 0 0
EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791
EGADS : 14 Yes 11.5080047 0 0
EGADS : 15 Yes 12.3611301 2.82842712 0
EGADS : 16 Yes 12.36195 0 0
EGADS : 17 Yes 11.6329932 0 0.0493703791
EGADS : 18 Yes 12.3611301 0 0
EGADS : 19 Yes 0 0 80
EGADS : 20 Yes 0 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 160
AFLR4 : Min Bounding Box Length = 160
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 0.890888
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 15.6122
AFLR4 : Abs Min Surf Spacing = 0.00222722
AFLR4 : Min Surf Spacing = 0.00445444
AFLR4 : Max Surf Spacing = 0.0890888
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 STD
AFLR4 : 12 CAD geometry 0 STD
AFLR4 : 13 CAD geometry 0 STD
AFLR4 : 14 CAD geometry 0 STD
AFLR4 : 15 CAD geometry 0 STD
AFLR4 : 16 CAD geometry 0 STD
AFLR4 : 17 CAD geometry 0 FARFIELD
AFLR4 : 18 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 12428
AFLR43 : Nodes = 6220
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 6220 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 Solid
UG3 : 12 Solid
UG3 : 13 Solid
UG3 : 14 Solid
UG3 : 15 Solid
UG3 : 16 Solid
UG3 : 17 FarField
UG3 : 18 FarField
AFLR3 : CPU Time = 0.013 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 6220 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1246 7333
AFLR3 IG : Nodes, Elements = 2492 16261
AFLR3 IG : Nodes, Elements = 3738 25021
AFLR3 IG : Nodes, Elements = 4984 34304
AFLR3 IG : Nodes, Elements = 6227 43518
AFLR3 IG : Nodes, Elements = 6227 43440
AFLR3 IG : Nodes, Elements = 6227 43474
AFLR3 IG : Nodes, Elements = 6227 43437
AFLR3 IG : Nodes, Elements = 6220 26107
AFLR3 IG : Nodes, Elements = 6220 26133
AFLR3 IG : Nodes, Elements = 6220 21538
AFLR3 IG : Nodes, Elements = 6220 19141
AFLR3 : CPU Time = 0.128 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6220 19141
AFLR3 GG : Nodes, Elements = 9092 27970
AFLR3 GG : Nodes, Elements = 9092 39349
AFLR3 GG : Nodes, Elements = 9092 36380
AFLR3 GG : Nodes, Elements = 9092 34923
AFLR3 GG : Nodes, Elements = 11659 42981
AFLR3 GG : Nodes, Elements = 11659 53807
AFLR3 GG : Nodes, Elements = 11659 50702
AFLR3 GG : Nodes, Elements = 11659 49815
AFLR3 GG : Nodes, Elements = 14477 58553
AFLR3 GG : Nodes, Elements = 14477 70855
AFLR3 GG : Nodes, Elements = 14477 67465
AFLR3 GG : Nodes, Elements = 14477 66533
AFLR3 GG : Nodes, Elements = 17443 75634
AFLR3 GG : Nodes, Elements = 17443 88707
AFLR3 GG : Nodes, Elements = 17443 85026
AFLR3 GG : Nodes, Elements = 17443 84166
AFLR3 GG : Nodes, Elements = 20625 93912
AFLR3 GG : Nodes, Elements = 20625 107483
AFLR3 GG : Nodes, Elements = 20625 103837
AFLR3 GG : Nodes, Elements = 20625 103014
AFLR3 GG : Nodes, Elements = 23983 113245
AFLR3 GG : Nodes, Elements = 23983 127691
AFLR3 GG : Nodes, Elements = 23983 123762
AFLR3 GG : Nodes, Elements = 23983 122939
AFLR3 GG : Nodes, Elements = 27471 133562
AFLR3 GG : Nodes, Elements = 27471 148246
AFLR3 GG : Nodes, Elements = 27471 144367
AFLR3 GG : Nodes, Elements = 27471 143483
AFLR3 GG : Nodes, Elements = 31049 154330
AFLR3 GG : Nodes, Elements = 31049 169629
AFLR3 GG : Nodes, Elements = 31049 165573
AFLR3 GG : Nodes, Elements = 31049 164719
AFLR3 GG : Nodes, Elements = 34642 175591
AFLR3 GG : Nodes, Elements = 34642 190772
AFLR3 GG : Nodes, Elements = 34642 186857
AFLR3 GG : Nodes, Elements = 34642 186049
AFLR3 GG : Nodes, Elements = 38204 196811
AFLR3 GG : Nodes, Elements = 38204 211769
AFLR3 GG : Nodes, Elements = 38204 208011
AFLR3 GG : Nodes, Elements = 38204 207203
AFLR3 GG : Nodes, Elements = 41735 217867
AFLR3 GG : Nodes, Elements = 41735 232734
AFLR3 GG : Nodes, Elements = 41735 228893
AFLR3 GG : Nodes, Elements = 41735 228199
AFLR3 GG : Nodes, Elements = 45118 238407
AFLR3 GG : Nodes, Elements = 45118 252771
AFLR3 GG : Nodes, Elements = 45118 249083
AFLR3 GG : Nodes, Elements = 45118 248399
AFLR3 GG : Nodes, Elements = 48432 258383
AFLR3 GG : Nodes, Elements = 48432 272398
AFLR3 GG : Nodes, Elements = 48432 268767
AFLR3 GG : Nodes, Elements = 48432 268040
AFLR3 GG : Nodes, Elements = 51632 277673
AFLR3 GG : Nodes, Elements = 51632 291124
AFLR3 GG : Nodes, Elements = 51632 287737
AFLR3 GG : Nodes, Elements = 51632 287138
AFLR3 GG : Nodes, Elements = 54742 296489
AFLR3 GG : Nodes, Elements = 54742 309545
AFLR3 GG : Nodes, Elements = 54742 306294
AFLR3 GG : Nodes, Elements = 54742 305700
AFLR3 GG : Nodes, Elements = 57753 314750
AFLR3 GG : Nodes, Elements = 57753 327393
AFLR3 GG : Nodes, Elements = 57753 324205
AFLR3 GG : Nodes, Elements = 57753 323671
AFLR3 GG : Nodes, Elements = 60589 332185
AFLR3 GG : Nodes, Elements = 60589 344195
AFLR3 GG : Nodes, Elements = 60589 341132
AFLR3 GG : Nodes, Elements = 60589 340678
AFLR3 GG : Nodes, Elements = 63303 348823
AFLR3 GG : Nodes, Elements = 63303 360078
AFLR3 GG : Nodes, Elements = 63303 357259
AFLR3 GG : Nodes, Elements = 63303 356861
AFLR3 GG : Nodes, Elements = 65821 364418
AFLR3 GG : Nodes, Elements = 65821 375019
AFLR3 GG : Nodes, Elements = 65821 372315
AFLR3 GG : Nodes, Elements = 65821 371973
AFLR3 GG : Nodes, Elements = 68056 378682
AFLR3 GG : Nodes, Elements = 68056 387933
AFLR3 GG : Nodes, Elements = 68056 385584
AFLR3 GG : Nodes, Elements = 68056 385301
AFLR3 GG : Nodes, Elements = 69951 390988
AFLR3 GG : Nodes, Elements = 69951 398948
AFLR3 GG : Nodes, Elements = 69951 396934
AFLR3 GG : Nodes, Elements = 69951 396704
AFLR3 GG : Nodes, Elements = 71446 401190
AFLR3 GG : Nodes, Elements = 71446 407532
AFLR3 GG : Nodes, Elements = 71446 405836
AFLR3 GG : Nodes, Elements = 71446 405665
AFLR3 GG : Nodes, Elements = 72588 409091
AFLR3 GG : Nodes, Elements = 72588 414051
AFLR3 GG : Nodes, Elements = 72588 412698
AFLR3 GG : Nodes, Elements = 72588 412555
AFLR3 GG : Nodes, Elements = 73412 415028
AFLR3 GG : Nodes, Elements = 73412 418465
AFLR3 GG : Nodes, Elements = 73412 417560
AFLR3 GG : Nodes, Elements = 73412 417491
AFLR3 GG : Nodes, Elements = 73970 419165
AFLR3 GG : Nodes, Elements = 73970 421515
AFLR3 GG : Nodes, Elements = 73970 420850
AFLR3 GG : Nodes, Elements = 73970 420801
AFLR3 GG : Nodes, Elements = 74329 421878
AFLR3 GG : Nodes, Elements = 74329 423409
AFLR3 GG : Nodes, Elements = 74329 422967
AFLR3 GG : Nodes, Elements = 74329 422934
AFLR3 GG : Nodes, Elements = 74527 423528
AFLR3 GG : Nodes, Elements = 74527 424406
AFLR3 GG : Nodes, Elements = 74527 424145
AFLR3 GG : Nodes, Elements = 74527 424123
AFLR3 GG : Nodes, Elements = 74619 424399
AFLR3 GG : Nodes, Elements = 74619 424805
AFLR3 GG : Nodes, Elements = 74619 424686
AFLR3 GG : Nodes, Elements = 74619 424681
AFLR3 GG : Nodes, Elements = 74657 424795
AFLR3 GG : Nodes, Elements = 74657 424951
AFLR3 GG : Nodes, Elements = 74657 424897
AFLR3 GG : Nodes, Elements = 74672 424942
AFLR3 GG : Nodes, Elements = 74672 425006
AFLR3 GG : Nodes, Elements = 74672 424985
AFLR3 GG : Nodes, Elements = 74672 424986
AFLR3 GG : Nodes, Elements = 74673 424989
AFLR3 GG : Nodes, Elements = 74673 424992
AFLR3 GG : Nodes, Elements = 74673 424991
AFLR3 GG : Nodes, Elements = 74696 425060
AFLR3 GG : Nodes, Elements = 74696 425133
AFLR3 GG : Nodes, Elements = 74696 425114
AFLR3 GG : Nodes, Elements = 74696 425117
AFLR3 GG : Nodes, Elements = 74700 425129
AFLR3 GG : Nodes, Elements = 74700 425145
AFLR3 GG : Nodes, Elements = 74700 425140
AFLR3 GG : Nodes, Elements = 74702 425146
AFLR3 GG : Nodes, Elements = 74702 425155
AFLR3 GG : Nodes, Elements = 74702 425152
AFLR3 GG : Nodes, Elements = 74702 425150
AFLR3 : CPU Time = 3.516 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 74702 425150
AFLR3 QI : Nodes, Elements = 73200 416638
AFLR3 QI : Nodes, Elements = 72976 415359
AFLR3 QI : Nodes, Elements = 72961 415273
AFLR3 QI : Nodes, Elements = 72960 415266
AFLR3 QI : Nodes, Elements = 72960 419161
AFLR3 QI : Nodes, Elements = 72960 415035
AFLR3 QI : Nodes, Elements = 72960 414621
AFLR3 QI : Nodes, Elements = 72960 415001
AFLR3 QI : Nodes, Elements = 72960 414373
AFLR3 QI : Nodes, Elements = 72960 414178
AFLR3 QI : Nodes, Elements = 72960 414472
AFLR3 QI : Nodes, Elements = 72960 414145
AFLR3 QI : Nodes, Elements = 72960 414045
AFLR3 QI : Nodes, Elements = 72960 414288
AFLR3 QI : Nodes, Elements = 72960 414039
AFLR3 QI : Nodes, Elements = 72960 413980
AFLR3 QI : Nodes, Elements = 72960 414224
AFLR3 QI : Nodes, Elements = 72960 413989
AFLR3 QI : Nodes, Elements = 72960 413938
AFLR3 QI : Nodes, Elements = 72966 413964
AFLR3 QI : Nodes, Elements = 72966 414196
AFLR3 QI : Nodes, Elements = 72966 413985
AFLR3 QI : Nodes, Elements = 72966 413966
AFLR3 QI : Nodes, Elements = 72966 414195
AFLR3 QI : Nodes, Elements = 72966 413976
AFLR3 QI : Nodes, Elements = 72966 413935
AFLR3 : CPU Time = 1.208 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 72966 413935
AFLR3 QRG: Nodes, Elements = 72978 413998
AFLR3 QRG: Nodes, Elements = 72988 414052
AFLR3 QRG: Nodes, Elements = 72990 414061
AFLR3 QRG: Nodes, Elements = 72991 414065
AFLR3 QRG: Nodes, Elements = 72990 414059
AFLR3 QRG: Nodes, Elements = 72998 414101
AFLR3 QRG: Nodes, Elements = 72998 414099
AFLR3 QRG: Nodes, Elements = 73000 414112
AFLR3 QRG: Nodes, Elements = 73007 414152
AFLR3 : CPU Time = 0.040 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Ang = 1.137 170.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 61
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 414152
UG3 : Min Vol = 6.36e-10
UG3 : Average Vol = 5.12
UG3 : Total-Tet-Vol = 2.12e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Q = 0.0734 1
UG3 : Average Q = 0.894
UG3 : No. Q< 0.1 = 29
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 5.269 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Ang = 1.137 170.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 61
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 414152
UG3 : Min Vol = 6.36e-10
UG3 : Average Vol = 5.12
UG3 : Total-Tet-Vol = 2.12e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Q = 0.223 1
UG3 : Average Q = 0.859
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 1
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
ok
test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting surface mesh for body 1 (of 7)
Getting surface mesh for body 2 (of 7)
Getting surface mesh for body 3 (of 7)
Getting surface mesh for body 4 (of 7)
Getting surface mesh for body 5 (of 7)
Getting surface mesh for body 6 (of 7)
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1125FCE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7000082F5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7000082F5000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes = 294
Number of elements = 584
Number of triangle elements = 584
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes = 2048
Number of elements = 4096
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes = 152
Number of elements = 300
Number of triangle elements = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes = 624
Number of elements = 1248
Number of triangle elements = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4192
Total number of elements = 8364
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 294, elements - 584
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 294, elements - 584
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4192, elements - 8364
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 374
Number of elements = 744
Number of triangle elements = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 472
Total number of elements = 936
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 386
Number of elements = 768
Number of triangle elements = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 351
Number of elements = 698
Number of triangle elements = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 491
Total number of elements = 970
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 376
Number of elements = 748
Number of triangle elements = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 454
Total number of elements = 896
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 126
Number of elements = 252
Number of triangle elements = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 109
Number of elements = 214
Number of triangle elements = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 48
Number of elements = 96
Number of triangle elements = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 12
Number of elements = 20
Number of triangle elements = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 169
Total number of elements = 330
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 536
Number of elements = 1072
Number of triangle elements = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 544
Number of elements = 1084
Number of triangle elements = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes = 1351
Number of elements = 2682
Number of triangle elements = 2682
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 288
Number of elements = 572
Number of triangle elements = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 174
Number of elements = 344
Number of triangle elements = 344
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 26
Number of elements = 48
Number of triangle elements = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 482
Number of elements = 960
Number of triangle elements = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 174, elements - 344
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 174, elements - 344
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 444
Number of elements = 884
Number of triangle elements = 884
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 522
Number of elements = 1044
Number of triangle elements = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 966
Total number of elements = 1928
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 444, elements - 884
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 444, elements - 884
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 7173, elements - 14338
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9601
Number of elements = 19194
Number of triangle elements = 19194
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9601
Total number of elements = 19194
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1220
Number of elements = 2680
Number of triangle elements = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1221
Total number of elements = 2680
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1220
Number of elements = 2680
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 2680
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 1221
Combined Number of elements = 2681
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 2680
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 6
Property name - Rib_Root
Property name - Rib_Root_Point
Property name - Ribs
Property name - Skin
Property name - Spar1
Property name - Spar2
Done getting FEA properties
Updating mesh element types based on properties input
'Smart_Restart' is ON
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting vortex lattice control surface data
VLM control surface name - CntrlLE
VLM control surface name - CntrlTE
Done getting vortex lattice control surface data
Getting FEA vortex lattice mesh
Getting ZAERO UAIC Configurations.......
Number of UAIC Configurations - 2
UAIC Configuration: climb, id = 1
- Mach Number : 0.200000
- Reduced Freq: [0.020000, ... , 0.250000]
UAIC Configuration: cruise, id = 2
- Mach Number : 0.700000
- Reduced Freq: [0.040000, ... , 0.350000]
Getting ZAERO Analysis Subcases.......
Number of Analysis Subcases - 2
Analysis Subcase: FlutterCruise, id = 1
- Discipline : flutter
- UAIC : cruise
Analysis Subcase: Trim, id = 2
- Discipline : Trim
- UAIC : climb
Getting ZAERO Trim Variables.......
Number of Trim Variables - 2
Trim Variable: ANGLEA
- Label : ALPHA
- Value : free
Trim Variable: URDD3
- Label : NZ
- Value : 1.0
Updating StaticAeroelastic subcase: Trim
- vectorToCG -> [0.345898, 1.652951, -0.041403]
- weight -> 476456.149985
- weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813290, 6179.981375, 19723.152207, 370546.335523]
ok
----------------------------------------------------------------------
Ran 143 tests in 482.765s
OK (skipped=15)
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./avlTest test;
+ ./avlTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m0.439s
user 0m0.248s
sys 0m0.141s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./avlTest passed (as expected)
=============================================
=================================================
+ echo './msesTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./msesTest test;
+ ./msesTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm
Value of CL = 0.276892
real 0m1.400s
user 0m1.139s
sys 0m0.097s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./msesTest passed (as expected)
=============================================
=================================================
+ echo './frictionTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./frictionTest test;
+ ./frictionTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m0.371s
user 0m0.097s
sys 0m0.048s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dAFLR2Test test;
+ ./fun3dAFLR2Test 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 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 = 0.005 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 = 0.064 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 = 0.028 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 0m1.071s
user 0m0.904s
sys 0m0.473s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./fun3dAFLR2Test passed (as expected)
=============================================
=================================================
+ echo './fun3dTetgenTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dTetgenTest test;
+ ./fun3dTetgenTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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: 0.127007
Creating surface mesh ...
Surface mesh seconds: 0.030664
Recovering boundaries...
Boundary recovery seconds: 0.113007
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.042593
Recovering Delaunayness...
Delaunay recovery seconds: 0.057464
Refining mesh...
21363 insertions, added 16942 points, 799712 tetrahedra in queue.
7113 insertions, added 2754 points, 343153 tetrahedra in queue.
Refinement seconds: 1.41223
Smoothing vertices...
Mesh smoothing seconds: 1.92302
Improving mesh...
Mesh improvement seconds: 0.036711
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.011172
Total running seconds: 3.75457
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 0m5.982s
user 0m6.395s
sys 0m0.275s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./interferenceTest test;
+ ./interferenceTest
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m2.443s
user 0m4.333s
sys 0m0.111s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./interferenceTest passed (as expected)
=============================================
=================================================
+ echo './hsmCantileverPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmCantileverPlateTest test;
+ ./hsmCantileverPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m0.481s
user 0m0.276s
sys 0m0.065s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected)
=============================================
=================================================
+ echo './hsmSimplePlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmSimplePlateTest test;
+ ./hsmSimplePlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m0.774s
user 0m0.664s
sys 0m0.063s
+ status=0
+ set +x
=============================================
CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected)
=============================================
=================================================
+ echo './hsmJoinedPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmJoinedPlateTest test;
+ ./hsmJoinedPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
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 0m0.351s
user 0m0.241s
sys 0m0.066s
+ 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/ESPbeta/Python-3.11.9/bin/python
=================================================
No options provided...defaulting to ALL
Running.... LINEARAERO PyTests
avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/avl
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m1.356s
user 0m0.836s
sys 0m0.522s
+ 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/ESPbeta/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/ESPbeta/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 0m11.939s
user 0m12.809s
sys 0m5.041s
+ 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/ESPbeta/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/ESPbeta/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 0m37.194s
user 0m14.785s
sys 0m18.695s
+ 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/ESPbeta/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/ESPbeta/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 0m1.843s
user 0m0.896s
sys 0m0.509s
+ 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/ESPbeta/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/ESPbeta/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 0m1.379s
user 0m0.874s
sys 0m0.561s
+ 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/ESPbeta/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/ESPbeta/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
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 0m24.332s
user 0m4.622s
sys 0m1.703s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected)
=================================================
friction: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/friction
=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
real 0m0.763s
user 0m0.699s
sys 0m0.204s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m0.873s
user 0m0.695s
sys 0m0.176s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/mses
=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = 0.37837932402995744
Cd = 0.0077758580442312715
Cm = 0.005262576090327783
real 0m2.551s
user 0m2.425s
sys 0m0.259s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
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 0m18.215s
user 0m17.288s
sys 0m0.926s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected)
=================================================
xfoil: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/xfoil
=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m3.286s
user 0m3.190s
sys 0m0.234s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m6.973s
user 0m13.673s
sys 0m4.620s
+ 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/ESPbeta/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/ESPbeta/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 0m4.181s
user 0m4.680s
sys 0m0.166s
+ 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/ESPbeta/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/ESPbeta/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 0m6.076s
user 0m8.420s
sys 0m0.247s
+ 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/ESPbeta/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/ESPbeta/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 0m3.370s
user 0m3.628s
sys 0m0.222s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 316 634
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 681 1018
AFLR2 GGp: Nodes, Faces = 1013 1682
AFLR2 GGp: Nodes, Faces = 1339 2334
AFLR2 GGp: Nodes, Faces = 1652 2960
AFLR2 GGp: Nodes, Faces = 1957 3570
AFLR2 GGp: Nodes, Faces = 2252 4160
AFLR2 GGp: Nodes, Faces = 2526 4708
AFLR2 GGp: Nodes, Faces = 2809 5274
AFLR2 GGp: Nodes, Faces = 3083 5822
AFLR2 GGp: Nodes, Faces = 3327 6310
AFLR2 GGp: Nodes, Faces = 3564 6784
AFLR2 GGp: Nodes, Faces = 3788 7232
AFLR2 GGp: Nodes, Faces = 3995 7646
AFLR2 GGp: Nodes, Faces = 4194 8044
AFLR2 GGp: Nodes, Faces = 4394 8444
AFLR2 GGp: Nodes, Faces = 4585 8826
AFLR2 GGp: Nodes, Faces = 4772 9200
AFLR2 GGp: Nodes, Faces = 4943 9542
AFLR2 GGp: Nodes, Faces = 5129 9914
AFLR2 GGp: Nodes, Faces = 5293 10242
AFLR2 GGp: Nodes, Faces = 5447 10550
AFLR2 GGp: Nodes, Faces = 5594 10844
AFLR2 GGp: Nodes, Faces = 5716 11088
AFLR2 GGp: Nodes, Faces = 5830 11316
AFLR2 GGp: Nodes, Faces = 5909 11474
AFLR2 GGp: Nodes, Faces = 5964 11584
AFLR2 GGp: Nodes, Faces = 6006 11668
AFLR2 GGp: Nodes, Faces = 6025 11706
AFLR2 GGp: Nodes, Faces = 6034 11724
AFLR2 : CPU Time = 0.022 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 6034 11724
AFLR2 QI : Nodes, Faces = 6033 454
AFLR2 QI : Nodes, Faces = 6033 5634
AFLR2 QI : Nodes, Faces = 6033 11722
AFLR2 QI : Nodes, Faces = 6032 462
AFLR2 QI : Nodes, Faces = 6032 5629
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 456
AFLR2 QI : Nodes, Faces = 6032 5632
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 474
AFLR2 QI : Nodes, Faces = 6032 5623
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6031 486
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 QI : Nodes, Faces = 6031 488
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 : CPU Time = 0.010 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
real 0m1.167s
user 0m1.144s
sys 0m0.534s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_PyTest.py test;
+ python -u aflr4_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m1.283s
user 0m1.129s
sys 0m0.253s
+ 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/ESPbeta/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/ESPbeta/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 0m2.242s
user 0m2.128s
sys 0m0.328s
+ 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/ESPbeta/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/ESPbeta/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 0m5.497s
user 0m7.859s
sys 0m0.579s
+ 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/ESPbeta/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/ESPbeta/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 0m6.843s
user 0m6.309s
sys 0m0.453s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 150173
Number of elements = 449915
Number of triangles = 14380
Number of quadrilatarals = 0
Number of tetrahedrals = 214483
Number of pyramids = 425
Number of prisms = 220627
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m12.634s
user 0m11.954s
sys 0m0.630s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 0m23.569s
user 0m22.425s
sys 0m0.989s
+ 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/ESPbeta/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/ESPbeta/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 0m8.326s
user 0m14.312s
sys 0m5.620s
+ 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/ESPbeta/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/ESPbeta/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 0m10.340s
user 0m9.690s
sys 0m0.570s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 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 = 0.102 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
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: 0.009086
Creating surface mesh ...
Surface mesh seconds: 0.001897
Recovering boundaries...
Boundary recovery seconds: 0.004389
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.00067
Recovering Delaunayness...
Delaunay recovery seconds: 0.002038
Refining mesh...
Refinement seconds: 0.009365
Smoothing vertices...
Mesh smoothing seconds: 0.012449
Improving mesh...
Mesh improvement seconds: 0.001147
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000422
Total running seconds: 0.041653
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 0m1.096s
user 0m0.818s
sys 0m0.248s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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: 0.017714
Creating surface mesh ...
Surface mesh seconds: 0.005354
Recovering boundaries...
Boundary recovery seconds: 0.055728
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.005767
Suppressing Steiner points ...
Steiner suppression seconds: 2.3e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.008869
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: 0.607873
Smoothing vertices...
Mesh smoothing seconds: 0.309603
Improving mesh...
Mesh improvement seconds: 0.008368
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.002171
Total running seconds: 1.0218
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 0m4.707s
user 0m4.247s
sys 0m0.357s
+ 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/ESPbeta/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/ESPbeta/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
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: 0.151539
Creating surface mesh ...
Surface mesh seconds: 0.013147
Recovering boundaries...
Boundary recovery seconds: 0.065201
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.009973
Recovering Delaunayness...
Delaunay recovery seconds: 0.037617
Refining mesh...
Refinement seconds: 0.172786
Smoothing vertices...
Mesh smoothing seconds: 0.201949
Improving mesh...
Mesh improvement seconds: 0.008044
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.003726
Total running seconds: 0.664801
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 FAST file ....
Finished writing FAST file
real 0m1.966s
user 0m1.806s
sys 0m0.284s
+ 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/ESPbeta/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/ESPbeta/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
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: 0.15176
Creating surface mesh ...
Surface mesh seconds: 0.013419
Recovering boundaries...
Boundary recovery seconds: 0.068915
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.00752
Recovering Delaunayness...
Delaunay recovery seconds: 0.072688
Refining mesh...
Refinement seconds: 0.3695
Smoothing vertices...
Mesh smoothing seconds: 0.485769
Improving mesh...
Mesh improvement seconds: 0.01382
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.005351
Total running seconds: 1.18962
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
real 0m2.329s
user 0m2.248s
sys 0m0.238s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Getting mesh sizing parameters
Mesh sizing name - Airfoil
Mesh sizing name - AirfoilTE
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m0.963s
user 0m0.897s
sys 0m0.514s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 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 = 0.009 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 3715 7206
AFLR2 : CPU Time = 0.001 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_SU2_aflr2.
Volume file name: flow_pyCAPS_SU2_aflr2.
Restart file name: restart_flow_pyCAPS_SU2_aflr2.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
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| 2.8881e-02| -0.385358| 2.453598| 1.625650| 5.369499| 0.360138|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.7265e-02| -0.512634| 2.087781| 1.374671| 4.973554| 1.183036|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6597e-02| -0.792582| 1.733529| 1.142729| 4.657622| 3.896320|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.6291e-02| -0.880738| 1.486539| 1.023158| 4.334759| 14.592265|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.6034e-02| -0.987528| 1.351478| 0.932491| 4.191092| 111.166022|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 2.5870e-02| -1.104038| 1.188715| 0.874764| 3.951825| -483.924340|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 2.5799e-02| -1.178622| 1.124587| 0.844310| 3.820426| 127.331200|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 2.5745e-02| -1.243517| 1.097463| 0.824869| 3.768858| 40.162273|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 2.5714e-02| -1.287932| 1.075843| 0.810639| 3.733440| 25.154653|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 2.5803e-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 0m1.738s
user 0m1.349s
sys 0m0.746s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 545 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 545 545
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 110 222
AFLR2 IG : Nodes, Faces = 220 442
AFLR2 IG : Nodes, Faces = 330 662
AFLR2 IG : Nodes, Faces = 440 882
AFLR2 IG : Nodes, Faces = 517 1036
AFLR2 IG : Nodes, Faces = 545 1092
AFLR2 IG : Nodes, Faces = 549 1092
AFLR2 IG : Nodes, Faces = 545 545
AFLR2 : CPU Time = 0.002 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 545 545
AFLR2 GGp: Nodes, Faces = 1083 1621
AFLR2 GGp: Nodes, Faces = 1616 2687
AFLR2 GGp: Nodes, Faces = 2144 3743
AFLR2 GGp: Nodes, Faces = 2661 4777
AFLR2 GGp: Nodes, Faces = 3171 5797
AFLR2 GGp: Nodes, Faces = 3672 6799
AFLR2 GGp: Nodes, Faces = 4158 7771
AFLR2 GGp: Nodes, Faces = 4653 8761
AFLR2 GGp: Nodes, Faces = 5142 9739
AFLR2 GGp: Nodes, Faces = 5608 10671
AFLR2 GGp: Nodes, Faces = 6055 11565
AFLR2 GGp: Nodes, Faces = 6482 12419
AFLR2 GGp: Nodes, Faces = 6880 13215
AFLR2 GGp: Nodes, Faces = 7257 13969
AFLR2 GGp: Nodes, Faces = 7614 14683
AFLR2 GGp: Nodes, Faces = 7947 15349
AFLR2 GGp: Nodes, Faces = 8276 16007
AFLR2 GGp: Nodes, Faces = 8575 16605
AFLR2 GGp: Nodes, Faces = 8869 17193
AFLR2 GGp: Nodes, Faces = 9140 17735
AFLR2 GGp: Nodes, Faces = 9401 18257
AFLR2 GGp: Nodes, Faces = 9654 18763
AFLR2 GGp: Nodes, Faces = 9887 19229
AFLR2 GGp: Nodes, Faces = 10110 19675
AFLR2 GGp: Nodes, Faces = 10315 20085
AFLR2 GGp: Nodes, Faces = 10497 20449
AFLR2 GGp: Nodes, Faces = 10656 20767
AFLR2 GGp: Nodes, Faces = 10791 21037
AFLR2 GGp: Nodes, Faces = 10919 21293
AFLR2 GGp: Nodes, Faces = 11022 21499
AFLR2 GGp: Nodes, Faces = 11092 21639
AFLR2 GGp: Nodes, Faces = 11145 21745
AFLR2 GGp: Nodes, Faces = 11156 21767
AFLR2 : CPU Time = 0.035 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 = 0.015 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 49.3184| 90|
| CV Face Area Aspect Ratio| 1.00035| 33.4982|
| CV Sub-Volume Ratio| 1.00001| 7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11153| 1/1.00| 10|
| 1| 2702| 1/4.13| 7.38309|
| 2| 549| 1/4.92| 4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 7.0409e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 6.7501e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 6.7641e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 6.6818e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 6.7329e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 6.6821e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 6.6745e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 6.6480e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 6.6904e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 6.7201e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.22124| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file |surface_flow_pyCAPS_su2_aflr2.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary |flow_pyCAPS_su2_aflr2.szplt |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.072253 Cd = -0.01151
Cmz = 0.070975
Cx = -0.01151 Cy = 0.072253
Pressure Contribution
Cl_p = 0.072253 Cd_p = -0.01151
Cmz_p = 0.070975
Cx_p = -0.01151 Cy_p = 0.072253
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m2.297s
user 0m2.089s
sys 0m0.748s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
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| 9.0386e-01| -0.065995| 2.296266| 2.031890| 5.424900| 1.969324|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 8.9929e-01| -0.000146| 2.503192| 2.184653| 5.504433| 2.669994|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 8.8616e-01| 0.022836| 2.578793| 2.419949| 5.523561| 4.081575|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 8.9050e-01| -0.041097| 2.580097| 2.548191| 5.445039| 6.003651|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 8.8309e-01| -0.101756| 2.566392| 2.598258| 5.370190| 7.692754|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 8.8049e-01| -0.114949| 2.558251| 2.609841| 5.363328| 8.911043|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 8.7985e-01| -0.124738| 2.541827| 2.614192| 5.362516| 9.794574|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 8.7968e-01| -0.166905| 2.494151| 2.620861| 5.317920| 10.317284|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 8.8113e-01| -0.223036| 2.429312| 2.616363| 5.252496| 10.445731|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 8.8217e-01| -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 0m28.516s
user 0m27.454s
sys 0m0.974s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
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| 1.4266e+00| -0.458238| 1.872911| 1.656342| 5.032658| 0.747356|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.4237e+00| -0.474495| 2.012416| 1.722531| 5.023251| 1.417645|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.4224e+00| -0.411436| 2.112682| 1.938918| 5.080139| 3.206640|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.4124e+00| -0.401624| 2.160654| 2.076942| 5.079456| 6.873640|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.4048e+00| -0.411670| 2.180863| 2.151230| 5.057111| 12.470424|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.3972e+00| -0.425533| 2.184395| 2.189878| 5.041713| 19.530915|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.3916e+00| -0.436222| 2.170558| 2.217712| 5.036784| 27.444937|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.3796e+00| -0.438251| 2.130034| 2.242936| 5.037249| 32.489152|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.3717e+00| -0.443916| 2.073807| 2.259407| 5.025917| 31.208484|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.3673e+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 8.0.0 "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 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- 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 6.523589 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
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| 1.5358e+00| -0.397716| 1.978508| 1.645118| 5.093179| 1.915087|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.4928e+00| -0.257369| 2.241094| 1.916257| 5.249805| 2.557622|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.4500e+00| -0.191638| 2.350399| 2.185809| 5.310465| 3.925162|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.4348e+00| -0.217261| 2.380880| 2.338313| 5.269941| 5.872036|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.4324e+00| -0.261506| 2.381321| 2.406007| 5.209923| 7.749274|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.4091e+00| -0.289071| 2.378299| 2.432486| 5.189120| 9.267784|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.3980e+00| -0.307559| 2.365345| 2.449297| 5.186812| 10.504429|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.3905e+00| -0.325707| 2.326921| 2.468701| 5.171814| 11.399364|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.3866e+00| -0.348872| 2.267332| 2.478078| 5.139102| 11.874957|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.3861e+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 1m0.253s
user 0m55.953s
sys 0m2.720s
+ 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/ESPbeta/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/ESPbeta/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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../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| 5.4381e-02| -1.163171| 1.073770| 1.341444| 4.312165| 0.062120|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.3050e-02| -1.561828| 0.808636| 0.967487| 3.922716| 0.139775|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.2648e-02| -1.601698| 0.943793| 1.009036| 3.876382| 0.373708|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.2719e-02| -1.659374| 1.008221| 1.015635| 3.799753| 0.952935|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 5.2798e-02| -1.663585| 1.011627| 0.956487| 3.788246| 2.344781|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 5.2447e-02| -1.633451| 0.991734| 0.872954| 3.829708| 6.259549|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 5.2606e-02| -1.626398| 0.990123| 0.847075| 3.843511| 26.349556|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 5.2803e-02| -1.643439| 1.009125| 0.895796| 3.825758| -56.104876|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 5.2589e-02| -1.659565| 1.020774| 0.939260| 3.804303| -24.431167|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 5.2495e-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 0m2.017s
user 0m1.780s
sys 0m0.817s
+ 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/ESPbeta/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/ESPbeta/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: 0.020422
Creating surface mesh ...
Surface mesh seconds: 0.005953
Recovering boundaries...
Boundary recovery seconds: 0.061863
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.005728
Suppressing Steiner points ...
Steiner suppression seconds: 2.4e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.00786
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: 0.509587
Smoothing vertices...
Mesh smoothing seconds: 0.287608
Improving mesh...
Mesh improvement seconds: 0.009488
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.002881
Total running seconds: 0.911887
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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
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| 1.6968e-01| 0.619384| 3.051344| 2.094590| 6.110279| 1.812161|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.6276e-01| 0.785542| 3.264371| 2.974872| 6.285549| 2.181906|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.6143e-01| 0.724139| 3.334285| 3.249736| 6.229534| 3.226648|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.6142e-01| 0.621976| 3.305627| 3.334988| 6.113861| 4.648342|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.6118e-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 0m47.111s
user 0m46.301s
sys 0m0.750s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = x43A, index = 1
Name = Farfield, 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 = 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 = 2
Name = x43A, index = 1
Name = Farfield, index = 2
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: 0.060959
Creating surface mesh ...
Surface mesh seconds: 0.018573
Recovering boundaries...
Warning: 6 segments are not recovered.
Boundary recovery seconds: 0.175098
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.014248
Suppressing Steiner points ...
Steiner suppression seconds: 4.9e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.022764
Refining mesh...
12616 insertions, added 5241 points, 5767 tetrahedra in queue.
Refinement seconds: 0.576191
Smoothing vertices...
Mesh smoothing seconds: 0.489678
Improving mesh...
Mesh improvement seconds: 0.022808
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.007148
Total running seconds: 1.39227
Statistics:
Input points: 9462
Input facets: 18920
Input segments: 28380
Input holes: 1
Input regions: 0
Mesh points: 14821
Mesh tetrahedra: 61094
Mesh faces: 131651
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: 5356
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 - x43A
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)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 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.
Reference origin for moment evaluation is (0, 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: ../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|
+-----------------------------------------------------------------------+
| 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.
14821 grid points.
61094 volume elements.
2 surface markers.
7622 boundary elements in index 0 (Marker = BC_1).
11304 boundary elements in index 1 (Marker = BC_2).
61094 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: 0.525061. Standard deviation K: 2.57978.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.87942| 84.6357|
| CV Face Area Aspect Ratio| 1.46889| 6493|
| CV Sub-Volume Ratio| 1| 6.13247e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 14821| 1/1.00| 10|
| 1| 2666| 1/5.56| 8.46744|
| 2| 478| 1/5.58| 7.16197|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13597.1 m^2.
Area projection in the x-plane = 761.676 m^2, y-plane = 2062.72 m^2, z-plane = 5463.61 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.
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| 3.2106e-01| 2.731802| 5.665841| 4.729515| 8.731277| -0.432085|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.2136e-01| 3.137591| 6.181212| 5.718209| 9.153091| -0.138681|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.1492e-01| 3.230131| 6.302675| 5.765314| 9.201154| -0.035407|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.1314e-01| 3.248992| 6.311106| 5.682179| 9.209371| -0.014648|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 3.1068e-01| 3.211631| 6.270139| 5.549009| 9.178618| -0.041111|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.21163| < -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 87 non-physical points in the solution.
Warning: 39 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 = -4.908144 Cd = 119.388853
Cmx = 15.62437 Cmy = 9303.232175 Cmz = 79.61054
Cx = 119.482107 Cy = 0.463396 Cz = 1.346912
real 0m8.891s
user 0m10.526s
sys 0m1.168s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 0m10.728s
user 0m9.105s
sys 0m0.859s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m6.407s
user 0m9.586s
sys 0m6.997s
+ 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/ESPbeta/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/ESPbeta/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 0m0.641s
user 0m0.590s
sys 0m0.193s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
real 0m0.911s
user 0m0.909s
sys 0m0.144s
+ 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/ESPbeta/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/ESPbeta/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 0m0.799s
user 0m0.800s
sys 0m0.145s
+ 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/ESPbeta/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/ESPbeta/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 0m10.494s
user 0m16.822s
sys 0m5.262s
+ 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/ESPbeta/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/ESPbeta/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 0m1.321s
user 0m0.701s
sys 0m0.262s
+ 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/ESPbeta/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/ESPbeta/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 0m0.978s
user 0m0.778s
sys 0m0.274s
+ 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/ESPbeta/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/ESPbeta/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 0m41.824s
user 0m40.235s
sys 0m0.962s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
real 0m1.300s
user 0m0.976s
sys 0m0.384s
+ 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/ESPbeta/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/ESPbeta/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 0m1.234s
user 0m0.887s
sys 0m0.309s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m14.806s
user 0m17.290s
sys 0m7.496s
+ 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/ESPbeta/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/ESPbeta/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 0m0.911s
user 0m0.753s
sys 0m0.275s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ python -u astros_ThreeBarFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
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 0m0.946s
user 0m0.773s
sys 0m0.273s
+ 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/ESPbeta/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/ESPbeta/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 0m1.309s
user 0m0.872s
sys 0m0.269s
+ 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/ESPbeta/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/ESPbeta/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 0m1.190s
user 0m0.785s
sys 0m0.268s
+ 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/ESPbeta/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/ESPbeta/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 0m1.011s
user 0m0.760s
sys 0m0.291s
+ 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/ESPbeta/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/ESPbeta/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 0m1.260s
user 0m0.973s
sys 0m0.366s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================
Running.... AEROELASTIC PyTests
=================================================
+ echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 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 : Auto Mode Turned OFF
OVERALL : CPU Time = 0.128 seconds
Body 1 (of 1)
Number of nodes = 9344
Number of elements = 18684
Number of triangle elements = 18684
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9344
Total number of elements = 18684
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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 57971
Number of elements = 333716
Number of triangles = 18684
Number of quadrilatarals = 0
Number of tetrahedrals = 315032
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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
57971 grid points.
315032 volume elements.
3 surface markers.
12290 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
315032 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: 102.753. Mean K: 0.746817. Standard deviation K: 4.38935.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 48.3512| 85.8306|
| CV Face Area Aspect Ratio| 1.14045| 31.4315|
| CV Sub-Volume Ratio| 1| 18.8988|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 57971| 1/1.00| 10|
| 1| 9882| 1/5.87| 8.31705|
| 2| 1748| 1/5.65| 7.00314|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.04169 m^2.
Area projection in the x-plane = 0.644461 m^2, y-plane = 0.295795 m^2, z-plane = 4.29819 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.379751 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86125e-18 m, z-direction = -0.0467278 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| 1.4473e+00| -1.301420| 0.995200| 0.625797| 4.167686| -1.057342|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.4319e+00| -1.707965| 0.838200| 0.448053| 3.749040| -0.626750|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.4304e+00| -1.710972| 0.654912| 0.274296| 3.746128| 1.211163|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.71097| < -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 = 273
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 3.102378e+09, tgt = 3.102377e+09, diff = 2.969126e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 273
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 3.017966e+09, tgt = 3.017966e+09, diff = 2.078335e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
Number of variables = 16
Number of data points = 273
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 4.336225e+07, tgt = 4.336225e+07, diff = 2.093896e-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
real 0m15.289s
user 0m14.354s
sys 0m1.748s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 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 : Auto Mode Turned OFF
OVERALL : CPU Time = 0.127 seconds
Body 1 (of 1)
Number of nodes = 9344
Number of elements = 18684
Number of triangle elements = 18684
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9344
Total number of elements = 18684
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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 57971
Number of elements = 333716
Number of triangles = 18684
Number of quadrilatarals = 0
Number of tetrahedrals = 315032
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 8.0.0 "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 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- 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.
57971 grid points.
315032 volume elements.
3 surface markers.
12290 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
315032 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 14.555672 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
57971 grid points.
315032 volume elements.
3 surface markers.
12290 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
315032 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 1 TETRAHEDRON volume elements.
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: 84.836. Mean K: 0.750948. Standard deviation K: 3.83823.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 45.6439| 85.8629|
| CV Face Area Aspect Ratio| 1.14586| 29.4281|
| CV Sub-Volume Ratio| 1| 383.004|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 57971| 1/1.00| 10|
| 1| 9882| 1/5.87| 8.31705|
| 2| 1748| 1/5.65| 7.00314|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89964 m.
Wetted area = 11.4382 m^2.
Area projection in the x-plane = 2.82758 m^2, y-plane = 1.25436 m^2, z-plane = 4.17954 m^2.
Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89964 m, z-direction = 0.526515 m.
Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86125e-18 m, z-direction = -0.705261 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| 1.4235e+00| -0.623692| 1.811758| 1.304943| 4.845414| 0.044089|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.4300e+00| -1.097077| 1.517974| 1.157653| 4.375064| 0.036828|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.4171e+00| -1.114058| 1.275810| 0.953312| 4.353416| 0.078289|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.11406| < -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 0m35.370s
user 0m32.644s
sys 0m2.932s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 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 : Auto Mode Turned OFF
OVERALL : CPU Time = 0.144 seconds
Body 1 (of 1)
Number of nodes = 2592
Number of elements = 5180
Number of triangle elements = 5180
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2592
Total number of elements = 5180
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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10507
Number of elements = 59441
Number of triangles = 5180
Number of quadrilatarals = 0
Number of tetrahedrals = 54261
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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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: 51.6883. Mean K: 0.709649. Standard deviation K: 3.22583.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 47.3226| 85.2324|
| CV Face Area Aspect Ratio| 1.1684| 20.6612|
| CV Sub-Volume Ratio| 1| 47.6073|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 10507| 1/1.00| 10|
| 1| 1887| 1/5.57| 8.46296|
| 2| 390| 1/4.84| 7.50547|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 7.82006 m^2.
Area projection in the x-plane = 0.576038 m^2, y-plane = 0.250011 m^2, z-plane = 3.65657 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.37624 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.47212e-18 m, z-direction = -0.0403729 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| 2.4605e-01| -0.750454| 1.605234| 1.225426| 4.718652| -1.376163|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.4147e-01| -1.062854| 1.498939| 1.098101| 4.394115| -1.125962|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.4050e-01| -1.149358| 1.367392| 0.963522| 4.304567| -0.359410|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.14936| < -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 = 89
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 3.095408e+09, tgt = 3.095408e+09, diff = 1.068540e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 3.013302e+09, tgt = 3.013302e+09, diff = 1.983646e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 3.927402e+07, tgt = 3.927402e+07, diff = 8.714199e-05
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 8.0.0 "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 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- 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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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 0.904206 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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 804 TETRAHEDRON volume elements.
There has been a re-orientation of 21 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 64473.1.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 23.5521. Mean K: 0.528789. Standard deviation K: 1.74045.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 7.66041| 85.5114|
| CV Face Area Aspect Ratio| 1.25587| 202.76|
| CV Sub-Volume Ratio| 1| 271782|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 10507| 1/1.00| 10|
| 1| 1887| 1/5.57| 8.46296|
| 2| 390| 1/4.84| 7.50547|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 4.37812 m.
Wetted area = 164.85 m^2.
Area projection in the x-plane = 65.7669 m^2, y-plane = 36.294 m^2, z-plane = 5.33932 m^2.
Max. coordinate in the x-direction = 2.78271 m, y-direction = 4.37812 m, z-direction = 16.9899 m.
Min. coordinate in the x-direction = -0.641697 m, y-direction = -0.050867 m, z-direction = -19.3086 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| 2.6025e-01| 1.820197| 4.775771| 4.897088| 7.289302| -0.034366|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.6608e-01| 2.137045| 4.784403| 4.877876| 7.618312| 0.009116|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6768e-01| 2.250000| 4.781209| 4.873868| 7.719326| -0.039142|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 2.25| < -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 34 non-physical points in the solution.
Warning: 1 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 = 89
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 1.536427e+09, tgt = 1.536428e+09, diff = 2.295131e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.234838e+09, tgt = 1.234837e+09, diff = 3.180435e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 1.949674e+07, tgt = 1.949674e+07, diff = 8.351915e-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 8.0.0 "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 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- 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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 804 TETRAHEDRON volume elements.
There has been a re-orientation of 21 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 64473.1.
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 13.055863 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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 14310 TETRAHEDRON volume elements.
There has been a re-orientation of 440 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 93990.1.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 432.976. Mean K: 2.26256. Standard deviation K: 13.2218.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.993574| 83.001|
| CV Face Area Aspect Ratio| 1.25431| 663.666|
| CV Sub-Volume Ratio| 1| 39793.3|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 10507| 1/1.00| 10|
| 1| 1862| 1/5.64| 8.42542|
| 2| 380| 1/4.9| 7.44076|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 9.34591 m.
Wetted area = 333.899 m^2.
Area projection in the x-plane = 98.9122 m^2, y-plane = 121.26 m^2, z-plane = 8.50121 m^2.
Max. coordinate in the x-direction = 4.37557 m, y-direction = 9.34591 m, z-direction = 7.91011 m.
Min. coordinate in the x-direction = 0.00811606 m, y-direction = -2.47212e-18 m, z-direction = -83.695 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| 2.4949e-01| 2.958965| 5.923322| 5.829651| 8.428070| -0.053456|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.6101e-01| 3.190359| 5.848824| 5.710948| 8.596266| -0.067996|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6302e-01| 3.306288| 5.926725| 5.746675| 8.681176| -0.063709|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.30629| < -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 297 non-physical points in the solution.
Warning: 14 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 = 89
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 1.516978e+09, tgt = 1.516979e+09, diff = 1.580333e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.852427e+09, tgt = 1.852426e+09, diff = 9.218352e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 9.963337e+06, tgt = 9.963337e+06, diff = 4.220347e-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 8.0.0 "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 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- 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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 14310 TETRAHEDRON volume elements.
There has been a re-orientation of 440 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 93990.1.
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 30.262051 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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 17305 TETRAHEDRON volume elements.
There has been a re-orientation of 1452 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 4.344e+09.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 85.9848. Mean K: 0.903436. Standard deviation K: 3.15511.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.30251| 82.4975|
| CV Face Area Aspect Ratio| 1.20319| 3379.04|
| CV Sub-Volume Ratio| 1| 1.50908e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 10507| 1/1.00| 10|
| 1| 1868| 1/5.62| 8.43446|
| 2| 390| 1/4.79| 7.50547|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30.7472 m.
Wetted area = 3993.35 m^2.
Area projection in the x-plane = 2011.33 m^2, y-plane = 491.545 m^2, z-plane = 51.2913 m^2.
Max. coordinate in the x-direction = 2.09966 m, y-direction = 30.7472 m, z-direction = 0.151749 m.
Min. coordinate in the x-direction = -3.24788 m, y-direction = -0.0168109 m, z-direction = -345.593 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| 2.4144e-01| 6.147495| 9.114350| 9.073167| 11.616601| 0.010350|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.5766e-01| 6.565061| 9.194501| 9.126459| 12.079221| 0.010934|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6282e-01| 6.687439| 9.327431| 9.156299| 12.149979| 0.017064|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 6.68744| < -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 383 non-physical points in the solution.
Warning: 34 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 = 55.140294
Cd = 3231.431574
real 0m58.514s
user 0m55.736s
sys 0m3.219s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 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 : Auto Mode Turned OFF
OVERALL : CPU Time = 0.067 seconds
Body 1 (of 1)
Number of nodes = 2592
Number of elements = 5180
Number of triangle elements = 5180
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2592
Total number of elements = 5180
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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10507
Number of elements = 59441
Number of triangles = 5180
Number of quadrilatarals = 0
Number of tetrahedrals = 54261
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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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: 51.6883. Mean K: 0.709649. Standard deviation K: 3.22583.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 47.3226| 85.2324|
| CV Face Area Aspect Ratio| 1.1684| 20.6612|
| CV Sub-Volume Ratio| 1| 47.6073|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 10507| 1/1.00| 10|
| 1| 1887| 1/5.57| 8.46296|
| 2| 390| 1/4.84| 7.50547|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 7.82006 m^2.
Area projection in the x-plane = 0.576038 m^2, y-plane = 0.250011 m^2, z-plane = 3.65657 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.37624 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.47212e-18 m, z-direction = -0.0403729 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| 2.4371e-01| -0.750454| 1.605234| 1.225426| 4.718652| -1.376163|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.4207e-01| -1.062854| 1.498939| 1.098101| 4.394115| -1.125962|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.4124e-01| -1.149358| 1.367392| 0.963522| 4.304567| -0.359410|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.14936| < -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 = 89
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 3.095408e+09, tgt = 3.095408e+09, diff = 7.825720e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 3.013302e+09, tgt = 3.013302e+09, diff = 9.294739e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 3.927402e+07, tgt = 3.927402e+07, diff = 2.399312e-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 8.0.0 "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 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- 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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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 0.855164 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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 13523 TETRAHEDRON volume elements.
There has been a re-orientation of 748 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 123782.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 415.11. Mean K: 2.16584. Standard deviation K: 13.332.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.92562| 84.7646|
| CV Face Area Aspect Ratio| 1.27744| 292.927|
| CV Sub-Volume Ratio| 1| 118306|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 10507| 1/1.00| 10|
| 1| 1877| 1/5.6| 8.44798|
| 2| 390| 1/4.81| 7.50547|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 13.8398 m.
Wetted area = 1402.36 m^2.
Area projection in the x-plane = 384.002 m^2, y-plane = 378.143 m^2, z-plane = 57.7119 m^2.
Max. coordinate in the x-direction = 3.39449 m, y-direction = 13.8398 m, z-direction = 29.1726 m.
Min. coordinate in the x-direction = -12.2926 m, y-direction = -0.275699 m, z-direction = -103.414 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| 2.4812e-01| 2.868480| 5.821230| 6.352316| 8.337585| 0.563893|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.5337e-01| 3.320850| 5.847228| 6.171194| 8.710496| 0.274128|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.5282e-01| 3.419093| 5.974174| 6.100774| 8.825893| 0.278686|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.41909| < -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 141 non-physical points in the solution.
Warning: 10 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 = 89
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 1.114856e+09, tgt = 1.114856e+09, diff = 2.558384e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 8.090012e+08, tgt = 8.090013e+08, diff = 1.173934e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 3.900116e+06, tgt = 3.900129e+06, diff = 1.300269e+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 8.0.0 "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 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- 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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 13523 TETRAHEDRON volume elements.
There has been a re-orientation of 748 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 123782.
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 30.203248 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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 29922 TETRAHEDRON volume elements.
There has been a re-orientation of 1538 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 8.84987e+09.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 14.4836. Mean K: 0.288226. Standard deviation K: 0.896469.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.121201| 75.7125|
| CV Face Area Aspect Ratio| 1.79914| 60705.6|
| CV Sub-Volume Ratio| 1| 140265|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 10507| 1/1.00| 10|
| 1| 1882| 1/5.58| 8.45548|
| 2| 386| 1/4.88| 7.47972|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 13.0689 m.
Wetted area = 542994 m^2.
Area projection in the x-plane = 117432 m^2, y-plane = 152826 m^2, z-plane = 11877.2 m^2.
Max. coordinate in the x-direction = 41.6804 m, y-direction = 13.0689 m, z-direction = 4288.86 m.
Min. coordinate in the x-direction = -9.10052 m, y-direction = -321.423 m, z-direction = -0.0403729 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| 2.4482e-01| 6.415350| 9.378832| 9.486602| 11.884456| -0.030484|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.5934e-01| 6.725858| 9.354846| 9.374443| 12.131450| -0.030492|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6297e-01| 6.819940| 9.399878| 9.389989| 12.163719| -0.030706|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 6.81994| < -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 311 non-physical points in the solution.
Warning: 38 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 = 89
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
Rank 0: src = 2.150956e+09, tgt = 2.150956e+09, diff = 2.010757e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
Rank 0: src = 1.766195e+09, tgt = 1.766195e+09, diff = 8.162825e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
Number of variables = 16
Number of data points = 89
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
Rank 0: src = 9.920224e+06, tgt = 9.920274e+06, diff = 5.020026e+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 8.0.0 "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 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- 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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 29922 TETRAHEDRON volume elements.
There has been a re-orientation of 1538 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 8.84987e+09.
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 30.072084 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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
10507 grid points.
54261 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54261 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 30070 TETRAHEDRON volume elements.
There has been a re-orientation of 2841 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 4.4513e+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: 6.61287. Mean K: 0.212418. Standard deviation K: 0.770655.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 0.51726| 80.4987|
| CV Face Area Aspect Ratio| 1.8032| 1.41276e+07|
| CV Sub-Volume Ratio| 1| 1.64182e+08|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 10507| 1/1.00| 10|
| 1| 1879| 1/5.59| 8.45098|
| 2| 389| 1/4.83| 7.49905|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 197.836 m.
Wetted area = 368247 m^2.
Area projection in the x-plane = 250520 m^2, y-plane = 23963.8 m^2, z-plane = 2133.43 m^2.
Max. coordinate in the x-direction = 80.0706 m, y-direction = 197.836 m, z-direction = 49.432 m.
Min. coordinate in the x-direction = -1.14639 m, y-direction = -12.6475 m, z-direction = -3036 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| 2.8338e-01| 8.733273| 11.700128| 11.624192| 14.202379| -0.008746|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.8016e-01| 9.180734| 11.757029| 11.723172| 14.610100| -0.004968|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.6998e-01| 9.320666| 11.834719| 11.818968| 14.689679| 0.005390|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 9.32067| < -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 721 non-physical points in the solution.
Warning: 78 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 1m40.906s
user 1m43.790s
sys 0m8.431s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 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 : Auto Mode Turned OFF
OVERALL : CPU Time = 0.128 seconds
Body 1 (of 1)
Number of nodes = 9344
Number of elements = 18684
Number of triangle elements = 18684
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9344
Total number of elements = 18684
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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 57971
Number of elements = 333716
Number of triangles = 18684
Number of quadrilatarals = 0
Number of tetrahedrals = 315032
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 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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.
57971 grid points.
315032 volume elements.
3 surface markers.
12290 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
315032 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: 102.753. Mean K: 0.746817. Standard deviation K: 4.38935.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 48.3512| 85.8306|
| CV Face Area Aspect Ratio| 1.14045| 31.4315|
| CV Sub-Volume Ratio| 1| 18.8988|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 57971| 1/1.00| 10|
| 1| 9882| 1/5.87| 8.31705|
| 2| 1748| 1/5.65| 7.00314|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.04169 m^2.
Area projection in the x-plane = 0.644461 m^2, y-plane = 0.295795 m^2, z-plane = 4.29819 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.379751 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86125e-18 m, z-direction = -0.0467278 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| 2.0386e+00| -1.301420| 0.995200| 0.625797| 4.167686| -1.057342|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.7325e+00| -1.707965| 0.838200| 0.448053| 3.749040| -0.626750|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.6307e+00| -1.710972| 0.654912| 0.274296| 3.746128| 1.211163|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.71097| < -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 = 273
CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature'
Rank 0: src = 1.497561e+03, tgt = 1.497561e+03, diff = 3.981737e-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 = 273
CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature'
Rank 0: src = 1.453823e+03, tgt = 1.453823e+03, diff = 2.471332e-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 = 273
CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature'
Rank 0: src = 2.083918e+01, tgt = 2.083918e+01, diff = 0.000000e+00
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 0m16.362s
user 0m15.308s
sys 0m1.716s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
gp.py test;
+ python -u gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m7.628s
user 0m1.504s
sys 0m0.260s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
qp.py test;
+ python -u qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m1.422s
user 0m1.397s
sys 0m0.151s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
sp.py test;
+ python -u sp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m1.323s
user 0m1.341s
sys 0m0.181s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
boydBox.py test;
+ python -u boydBox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m1.104s
user 0m1.161s
sys 0m0.154s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_gp.py test;
+ python -u hoburg_gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m9.575s
user 0m9.218s
sys 0m0.486s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_blackbox.py test;
+ python -u hoburg_blackbox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m36.006s
user 0m35.716s
sys 0m0.404s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/sizeWing.py test;
+ python -u pyCAPS/sizeWing.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m1.703s
user 0m1.699s
sys 0m0.218s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case pyCAPS/sizeWing.py passed (as expected)
=================================================
avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/avl
=================================================
+ echo 'pyCAPS/optTaperAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optTaperAvl.py test;
+ python -u pyCAPS/optTaperAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m6.725s
user 0m4.212s
sys 0m2.372s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optWingAvl.py test;
+ python -u pyCAPS/optWingAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2
Starting iteration 0 at 0.3021 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 1.4696 seconds
Got sol from cvxopt at 1.4955 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 2.8866 seconds
Starting iteration 1 at 2.9193 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 2.9292 seconds
Got sol from cvxopt at 2.9556 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 4.2202 seconds
Starting iteration 2 at 4.2550 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 4.2657 seconds
Got sol from cvxopt at 4.2912 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 5.6065 seconds
Starting iteration 3 at 5.6417 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 5.6550 seconds
Got sol from cvxopt at 5.7025 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 6.9507 seconds
Starting iteration 4 at 6.9882 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 6.9990 seconds
Got sol from cvxopt at 7.0268 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 8.2465 seconds
Starting iteration 5 at 8.2812 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 8.2917 seconds
Got sol from cvxopt at 8.3318 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 9.5089 seconds
Starting iteration 6 at 9.5451 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 9.5547 seconds
Got sol from cvxopt at 9.5809 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 10.8506 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 0m12.571s
user 0m7.508s
sys 0m4.259s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/GPSize.py test;
+ python -u pyCAPS/GPSize.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 0m10.112s
user 0m9.537s
sys 0m0.665s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case pyCAPS/GPSize.py passed (as expected)
=================================================
mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/mses
=================================================
+ echo 'pyCAPS/MSES.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/MSES.py test;
+ python -u pyCAPS/MSES.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 2m41.161s
user 2m30.364s
sys 0m7.761s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/Camber.py test;
+ python -u pyCAPS/Camber.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/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 6m39.785s
user 6m11.244s
sys 0m19.074s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/CMConstraint.py test;
+ python -u pyCAPS/CMConstraint.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 4m8.915s
user 3m53.885s
sys 0m10.883s
+ 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
+ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ find /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 50752
-rw-r--r-- 1 jenkins staff 1.2M Apr 27 18:01 ASTRO.D01
-rw-r--r-- 1 jenkins staff 277K Apr 27 18:01 ASTRO.IDX
-rwxr-xr-x 1 jenkins staff 129K Apr 27 18:03 ESPxddm
-rwxr-xr-x 1 jenkins staff 210K Apr 27 18:03 Slugs
-rwxr-xr-x 1 jenkins staff 85K Apr 27 18:03 TestFit
-rwxr-xr-x 1 jenkins staff 1.8M Apr 27 18:01 avl
-rwxr-xr-x 1 jenkins staff 34K Apr 28 10:41 cart3dTest
-rwxr-xr-x 1 jenkins staff 34K Apr 28 10:41 egads2cart
-rwxr-xr-x 1 jenkins staff 70K Apr 27 18:03 egads2cgt
-rwxr-xr-x 1 jenkins staff 416K Apr 27 18:02 friction
-rwxr-xr-x 1 jenkins staff 8.9M Apr 27 18:01 mastros.exe
-rwxr-xr-x 1 jenkins staff 2.2M Apr 27 18:01 mses
-rwxr-xr-x 1 jenkins staff 2.5M Apr 27 18:01 mset
-rwxr-xr-x 1 jenkins staff 34K Apr 28 10:41 phaseUtil
-rw-r--r-- 1 jenkins staff 1.6K Apr 28 13:02 pod.egads
-rw-r--r-- 1 jenkins staff 0B Apr 28 13:02 port7681.jrnl
-rwxr-xr-x 1 jenkins staff 1.2M Apr 27 18:01 pplot
-rwxr-xr-x 1 jenkins staff 1.2M Apr 27 18:01 pxplot
-rwxr-xr-x 1 jenkins staff 68K Apr 28 10:41 sensCSM
-rwxr-xr-x 1 jenkins staff 206K Apr 27 18:03 serveCSM
-rwxr-xr-x 1 jenkins staff 174K Apr 27 18:03 serveESP
-rwxr-xr-x 1 jenkins staff 51K Apr 27 18:03 vCurvature
-rwxr-xr-x 1 jenkins staff 35K Apr 27 18:03 vGeom
-rwxr-xr-x 1 jenkins staff 52K Apr 27 18:03 vTess
-rwxr-xr-x 1 jenkins staff 1.9M Apr 27 18:03 vTesstatic
-rw-r--r-- 1 jenkins staff 195K Apr 28 13:02 wingMultiModel.bdf
-rwxr-xr-x 1 jenkins staff 1.8M Apr 27 18:01 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0a.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 5.416e-07, rmsbest= 6.132e-04, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 2, unclass= 0
Starting pass 3 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m9.479s
user 0m7.659s
sys 0m0.497s
++ set +x
data/Plugs/plugs0a passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0b.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 3.039e-07, rmsbest= 4.036e-02, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 2.814e-07, rmsbest= 1.924e-03, reclass= 1033, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 4.494e-07, rmsbest= 5.920e-04, reclass= 473, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 17, unclass= 0
Starting pass 5 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m6.528s
user 0m7.951s
sys 0m0.087s
++ set +x
data/Plugs/plugs0b passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0c.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m17.616s
user 0m26.356s
sys 0m0.194s
++ set +x
data/Plugs/plugs0c passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0d.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m17.475s
user 0m26.134s
sys 0m0.191s
++ 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] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_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] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_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=beta,buildnode=macys_VM #69'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS