Started by upstream project "ESP_Beta" build number 725
originally caused by:
Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on viggen in workspace /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-06-20T13:25:06.405 -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 2507
Checking out a fresh workspace because /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-06-20T13:25:06.405 -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 871
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [viggen] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [viggen] is in [[viggen]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[DARWIN_ARM64] $ /bin/bash -ex /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jenkins4941950510312134630.sh
+ arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP/ESP_Beta.sh
+ source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export MPLBACKEND=agg
++ MPLBACKEND=agg
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ viggen == \r\e\y\n\o\l\d\s ]]
++ [[ DARWIN_ARM64 == *\.\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
++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64
++ ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ viggen == *\r\e\y\n\o\l\d\s* ]]
++ [[ viggen == *\m\a\c\y\s* ]]
++ [[ viggen == *\v\i\g\g\e\n* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
++++ /opt/homebrew/bin/brew shellenv
+++ eval 'export HOMEBREW_PREFIX="/opt/homebrew";
export HOMEBREW_CELLAR="/opt/homebrew/Cellar";
export HOMEBREW_REPOSITORY="/opt/homebrew";
export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}";
export MANPATH="/opt/homebrew/share/man${MANPATH+:$MANPATH}:";
export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";'
++++ export HOMEBREW_PREFIX=/opt/homebrew
++++ HOMEBREW_PREFIX=/opt/homebrew
++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ export HOMEBREW_REPOSITORY=/opt/homebrew
++++ HOMEBREW_REPOSITORY=/opt/homebrew
++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ export MANPATH=/opt/homebrew/share/man:
++++ MANPATH=/opt/homebrew/share/man:
++++ export INFOPATH=/opt/homebrew/share/info:
++++ INFOPATH=/opt/homebrew/share/info:
+++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]]
+++ . /opt/homebrew/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
+++ export NETCDF_PATH=/opt/homebrew
+++ NETCDF_PATH=/opt/homebrew
++ [[ viggen == *\m\a\c\y\s* ]]
++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/udunits/udunits2.xml
++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib
++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ [[ viggen == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-arm64
++ AFLR_ARCH=MacOSX-arm64
++ 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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ export SEACAS=/Users/jenkins/util/sandialabs/seacas
++ SEACAS=/Users/jenkins/util/sandialabs/seacas
++ [[ viggen == \v\i\g\g\e\n ]]
++ export NETCDFINC=/opt/homebrew/include
++ NETCDFINC=/opt/homebrew/include
++ 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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
+++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ viggen == \m\a\c\y\s* ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-*'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv
+++ ls '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-*' '/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-*'
ls: /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-*: No such file or directory
ls: /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-*: No such file or directory
+++ python-config --includes
++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/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/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/data
+ virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 243ms
creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv)
added seed packages: pip==24.0, setuptools==70.0.0, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/activate
++ '[' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv
++ '[' darwin23 = cygwin ']'
++ '[' darwin23 = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z '' ']'
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install f90nml
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
Using cached numpy-2.0.0-cp311-cp311-macosx_14_0_arm64.whl.metadata (60 kB)
Using cached numpy-2.0.0-cp311-cp311-macosx_14_0_arm64.whl (5.2 MB)
Installing collected packages: numpy
Successfully installed numpy-2.0.0
+ pip_install openmdao
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
Using cached openmdao-3.33.0-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Collecting numpy<2 (from openmdao)
Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl.metadata (114 kB)
Collecting packaging (from openmdao)
Using cached packaging-24.1-py3-none-any.whl.metadata (3.2 kB)
Collecting requests (from openmdao)
Using cached requests-2.32.3-py3-none-any.whl.metadata (4.6 kB)
Collecting scipy (from openmdao)
Using cached scipy-1.13.1-cp311-cp311-macosx_12_0_arm64.whl.metadata (60 kB)
Collecting charset-normalizer<4,>=2 (from requests->openmdao)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_11_0_arm64.whl.metadata (33 kB)
Collecting idna<4,>=2.5 (from requests->openmdao)
Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB)
Collecting urllib3<3,>=1.21.1 (from requests->openmdao)
Using cached urllib3-2.2.2-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
Using cached certifi-2024.6.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl (14.0 MB)
Using cached packaging-24.1-py3-none-any.whl (53 kB)
Using cached requests-2.32.3-py3-none-any.whl (64 kB)
Using cached scipy-1.13.1-cp311-cp311-macosx_12_0_arm64.whl (30.3 MB)
Using cached certifi-2024.6.2-py3-none-any.whl (164 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_11_0_arm64.whl (118 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.2-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, packaging, numpy, networkx, idna, charset-normalizer, certifi, scipy, requests, openmdao
Attempting uninstall: numpy
Found existing installation: numpy 2.0.0
Uninstalling numpy-2.0.0:
Successfully uninstalled numpy-2.0.0
Successfully installed certifi-2024.6.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 numpy-1.26.4 openmdao-3.33.0 packaging-24.1 requests-2.32.3 scipy-1.13.1 urllib3-2.2.2
+ [[ viggen == *\v\i\g\g\e\n* ]]
+ export CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib
+ CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib
+ export CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0
+ CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0
+ GCC_MAJOR=11
+ export 'CVXOPT_BLAS_EXTRA_LINK_ARGS=/opt/homebrew/opt/gcc/lib/gcc/11/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/11/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/11/gcc/aarch64-apple-darwin21/11/libgcc.a'
+ CVXOPT_BLAS_EXTRA_LINK_ARGS='/opt/homebrew/opt/gcc/lib/gcc/11/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/11/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/11/gcc/aarch64-apple-darwin21/11/libgcc.a'
+ pip_install cvxopt
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl (11.1 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.1)
+ pip_install matplotlib
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
Using cached matplotlib-3.9.0-cp311-cp311-macosx_11_0_arm64.whl.metadata (11 kB)
Collecting contourpy>=1.0.1 (from matplotlib)
Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.whl.metadata (5.8 kB)
Collecting cycler>=0.10 (from matplotlib)
Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB)
Collecting fonttools>=4.22.0 (from matplotlib)
Using cached fonttools-4.53.0-cp311-cp311-macosx_11_0_arm64.whl.metadata (162 kB)
Collecting kiwisolver>=1.3.1 (from matplotlib)
Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl.metadata (6.4 kB)
Requirement already satisfied: numpy>=1.23 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4)
Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.1)
Collecting pillow>=8 (from matplotlib)
Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl.metadata (9.2 kB)
Collecting pyparsing>=2.3.1 (from matplotlib)
Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB)
Collecting python-dateutil>=2.7 (from matplotlib)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB)
Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib)
Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB)
Using cached matplotlib-3.9.0-cp311-cp311-macosx_11_0_arm64.whl (7.8 MB)
Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.whl (245 kB)
Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB)
Using cached fonttools-4.53.0-cp311-cp311-macosx_11_0_arm64.whl (2.2 MB)
Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl (66 kB)
Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl (3.4 MB)
Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB)
Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.53.0 kiwisolver-1.4.5 matplotlib-3.9.0 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.1)
Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4)
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset UDUNITS2_XML_PATH
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
+ unset AFLR
+ unset AFLR_ARCH
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
--2024-06-20 13:25:34-- https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14
Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected.
HTTP request sent, awaiting response... 200 OK
Length: 272149040 (260M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’
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900K .......... .......... .......... .......... .......... 0% 351M 8s
950K .......... .......... .......... .......... .......... 0% 22.6M 8s
1000K .......... .......... .......... .......... .......... 0% 42.1M 8s
1050K .......... .......... .......... .......... .......... 0% 41.8M 8s
1100K .......... .......... .......... .......... .......... 0% 28.0M 8s
1150K .......... .......... .......... .......... .......... 0% 31.6M 8s
1200K .......... .......... .......... .......... .......... 0% 22.8M 8s
1250K .......... .......... .......... .......... .......... 0% 47.1M 8s
1300K .......... .......... .......... .......... .......... 0% 30.1M 8s
1350K .......... .......... .......... .......... .......... 0% 24.2M 8s
1400K .......... .......... .......... .......... .......... 0% 48.0M 8s
1450K .......... .......... .......... .......... .......... 0% 28.9M 8s
1500K .......... .......... .......... .......... .......... 0% 24.0M 8s
1550K .......... .......... .......... .......... .......... 0% 43.2M 8s
1600K .......... .......... .......... .......... .......... 0% 23.7M 8s
1650K .......... .......... .......... .......... .......... 0% 30.2M 8s
1700K .......... .......... .......... .......... .......... 0% 29.0M 8s
1750K .......... .......... .......... .......... .......... 0% 35.0M 8s
1800K .......... .......... .......... .......... .......... 0% 29.3M 8s
1850K .......... .......... .......... .......... .......... 0% 22.2M 8s
1900K .......... .......... .......... .......... .......... 0% 36.1M 8s
1950K .......... .......... .......... .......... .......... 0% 21.4M 8s
2000K .......... .......... .......... .......... .......... 0% 17.0M 9s
2050K .......... .......... .......... .......... .......... 0% 23.2M 9s
2100K .......... .......... .......... .......... .......... 0% 29.2M 9s
2150K .......... .......... .......... .......... .......... 0% 37.5M 9s
2200K .......... .......... .......... .......... .......... 0% 25.6M 9s
2250K .......... .......... .......... .......... .......... 0% 16.0M 9s
2300K .......... .......... .......... .......... .......... 0% 425M 9s
2350K .......... .......... .......... .......... .......... 0% 18.2M 9s
2400K .......... .......... .......... .......... .......... 0% 17.8M 9s
2450K .......... .......... .......... .......... .......... 0% 26.2M 9s
2500K .......... .......... .......... .......... .......... 0% 17.0M 9s
2550K .......... .......... .......... .......... .......... 0% 20.9M 9s
2600K .......... .......... .......... .......... .......... 0% 15.8M 9s
2650K .......... .......... .......... .......... .......... 1% 16.6M 9s
2700K .......... .......... .......... .......... .......... 1% 12.4M 10s
2750K .......... .......... .......... .......... .......... 1% 16.5M 10s
2800K .......... .......... .......... .......... .......... 1% 15.2M 10s
2850K .......... .......... .......... .......... .......... 1% 6.55M 10s
2900K .......... .......... .......... .......... .......... 1% 5.27M 11s
2950K .......... .......... .......... .......... .......... 1% 5.22M 12s
3000K .......... .......... .......... .......... .......... 1% 9.07M 12s
3050K .......... .......... .......... .......... .......... 1% 6.36M 12s
3100K .......... .......... .......... .......... .......... 1% 6.11M 13s
3150K .......... .......... .......... .......... .......... 1% 8.13M 13s
3200K .......... .......... .......... .......... .......... 1% 4.19M 14s
3250K .......... .......... .......... .......... .......... 1% 8.88M 14s
3300K .......... .......... .......... .......... .......... 1% 7.43M 14s
3350K .......... .......... .......... .......... .......... 1% 7.12M 15s
3400K .......... .......... .......... .......... .......... 1% 7.12M 15s
3450K .......... .......... .......... .......... .......... 1% 9.97M 15s
3500K .......... .......... .......... .......... .......... 1% 13.5M 15s
3550K .......... .......... .......... .......... .......... 1% 11.6M 15s
3600K .......... .......... .......... .......... .......... 1% 8.58M 15s
3650K .......... .......... .......... .......... .......... 1% 7.47M 16s
3700K .......... .......... .......... .......... .......... 1% 5.91M 16s
3750K .......... .......... .......... .......... .......... 1% 7.94M 16s
3800K .......... .......... .......... .......... .......... 1% 10.2M 16s
3850K .......... .......... .......... .......... .......... 1% 6.65M 17s
3900K .......... .......... .......... .......... .......... 1% 8.71M 17s
3950K .......... .......... .......... .......... .......... 1% 5.93M 17s
4000K .......... .......... .......... .......... .......... 1% 16.1M 17s
4050K .......... .......... .......... .......... .......... 1% 41.3M 17s
4100K .......... .......... .......... .......... .......... 1% 33.7M 17s
4150K .......... .......... .......... .......... .......... 1% 13.3M 17s
4200K .......... .......... .......... .......... .......... 1% 45.8M 17s
4250K .......... .......... .......... .......... .......... 1% 41.8M 17s
4300K .......... .......... .......... .......... .......... 1% 32.4M 17s
4350K .......... .......... .......... .......... .......... 1% 34.7M 16s
4400K .......... .......... .......... .......... .......... 1% 31.8M 16s
4450K .......... .......... .......... .......... .......... 1% 30.7M 16s
4500K .......... .......... .......... .......... .......... 1% 42.5M 16s
4550K .......... .......... .......... .......... .......... 1% 52.5M 16s
4600K .......... .......... .......... .......... .......... 1% 34.4M 16s
4650K .......... .......... .......... .......... .......... 1% 46.8M 16s
4700K .......... .......... .......... .......... .......... 1% 31.9M 16s
4750K .......... .......... .......... .......... .......... 1% 37.7M 16s
4800K .......... .......... .......... .......... .......... 1% 47.3M 15s
4850K .......... .......... .......... .......... .......... 1% 42.6M 15s
4900K .......... .......... .......... .......... .......... 1% 37.0M 15s
4950K .......... .......... .......... .......... .......... 1% 35.3M 15s
5000K .......... .......... .......... .......... .......... 1% 41.2M 15s
5050K .......... .......... .......... .......... .......... 1% 19.5M 15s
5100K .......... .......... .......... .......... .......... 1% 47.0M 15s
5150K .......... .......... .......... .......... .......... 1% 23.5M 15s
5200K .......... .......... .......... .......... .......... 1% 14.5M 15s
5250K .......... .......... .......... .......... .......... 1% 14.7M 15s
5300K .......... .......... .......... .......... .......... 2% 11.2M 15s
5350K .......... .......... .......... .......... .......... 2% 18.1M 15s
5400K .......... .......... .......... .......... .......... 2% 17.2M 15s
5450K .......... .......... .......... .......... .......... 2% 12.6M 15s
5500K .......... .......... .......... .......... .......... 2% 16.5M 15s
5550K .......... .......... .......... .......... .......... 2% 14.1M 15s
5600K .......... .......... .......... .......... .......... 2% 13.8M 15s
5650K .......... .......... .......... .......... .......... 2% 17.1M 15s
5700K .......... .......... .......... .......... .......... 2% 11.5M 15s
5750K .......... .......... .......... .......... .......... 2% 9.87M 15s
5800K .......... .......... .......... .......... .......... 2% 15.8M 15s
5850K .......... .......... .......... .......... .......... 2% 10.3M 15s
5900K .......... .......... .......... .......... .......... 2% 13.2M 15s
5950K .......... .......... .......... .......... .......... 2% 11.1M 15s
6000K .......... .......... .......... .......... .......... 2% 12.4M 15s
6050K .......... .......... .......... .......... .......... 2% 11.1M 16s
6100K .......... .......... .......... .......... .......... 2% 8.34M 16s
6150K .......... .......... .......... .......... .......... 2% 8.01M 16s
6200K .......... .......... .......... .......... .......... 2% 5.09M 16s
6250K .......... .......... .......... .......... .......... 2% 7.78M 16s
6300K .......... .......... .......... .......... .......... 2% 8.74M 16s
6350K .......... .......... .......... .......... .......... 2% 7.45M 16s
6400K .......... .......... .......... .......... .......... 2% 8.00M 17s
6450K .......... .......... .......... .......... .......... 2% 7.48M 17s
6500K .......... .......... .......... .......... .......... 2% 8.45M 17s
6550K .......... .......... .......... .......... .......... 2% 10.0M 17s
6600K .......... .......... .......... .......... .......... 2% 10.1M 17s
6650K .......... .......... .......... .......... .......... 2% 12.6M 17s
6700K .......... .......... .......... .......... .......... 2% 8.65M 17s
6750K .......... .......... .......... .......... .......... 2% 8.60M 17s
6800K .......... .......... .......... .......... .......... 2% 14.3M 17s
6850K .......... .......... .......... .......... .......... 2% 9.57M 17s
6900K .......... .......... .......... .......... .......... 2% 19.0M 17s
6950K .......... .......... .......... .......... .......... 2% 13.0M 17s
7000K .......... .......... .......... .......... .......... 2% 11.8M 17s
7050K .......... .......... .......... .......... .......... 2% 13.4M 17s
7100K .......... .......... .......... .......... .......... 2% 18.0M 17s
7150K .......... .......... .......... .......... .......... 2% 14.6M 17s
7200K .......... .......... .......... .......... .......... 2% 13.5M 17s
7250K .......... .......... .......... .......... .......... 2% 19.6M 17s
7300K .......... .......... .......... .......... .......... 2% 16.8M 17s
7350K .......... .......... .......... .......... .......... 2% 13.0M 17s
7400K .......... .......... .......... .......... .......... 2% 13.2M 17s
7450K .......... .......... .......... .......... .......... 2% 13.7M 17s
7500K .......... .......... .......... .......... .......... 2% 17.3M 17s
7550K .......... .......... .......... .......... .......... 2% 17.4M 17s
7600K .......... .......... .......... .......... .......... 2% 13.8M 17s
7650K .......... .......... .......... .......... .......... 2% 9.26M 17s
7700K .......... .......... .......... .......... .......... 2% 291M 17s
7750K .......... .......... .......... .......... .......... 2% 15.8M 17s
7800K .......... .......... .......... .......... .......... 2% 10.2M 17s
7850K .......... .......... .......... .......... .......... 2% 13.8M 17s
7900K .......... .......... .......... .......... .......... 2% 13.2M 17s
7950K .......... .......... .......... .......... .......... 3% 11.2M 17s
8000K .......... .......... .......... .......... .......... 3% 11.7M 17s
8050K .......... .......... .......... .......... .......... 3% 15.9M 17s
8100K .......... .......... .......... .......... .......... 3% 11.6M 17s
8150K .......... .......... .......... .......... .......... 3% 10.7M 17s
8200K .......... .......... .......... .......... .......... 3% 11.1M 17s
8250K .......... .......... .......... .......... .......... 3% 14.2M 17s
8300K .......... .......... .......... .......... .......... 3% 9.56M 17s
8350K .......... .......... .......... .......... .......... 3% 8.18M 17s
8400K .......... .......... .......... .......... .......... 3% 13.1M 17s
8450K .......... .......... .......... .......... .......... 3% 9.48M 17s
8500K .......... .......... .......... .......... .......... 3% 11.9M 17s
8550K .......... .......... .......... .......... .......... 3% 9.03M 17s
8600K .......... .......... .......... .......... .......... 3% 4.43M 18s
8650K .......... .......... .......... .......... .......... 3% 9.57M 18s
8700K .......... .......... .......... .......... .......... 3% 24.1M 18s
8750K .......... .......... .......... .......... .......... 3% 13.3M 18s
8800K .......... .......... .......... .......... .......... 3% 23.4M 18s
8850K .......... .......... .......... .......... .......... 3% 24.1M 18s
8900K .......... .......... .......... .......... .......... 3% 24.5M 18s
8950K .......... .......... .......... .......... .......... 3% 17.5M 18s
9000K .......... .......... .......... .......... .......... 3% 19.0M 18s
9050K .......... .......... .......... .......... .......... 3% 17.3M 18s
9100K .......... .......... .......... .......... .......... 3% 16.8M 17s
9150K .......... .......... .......... .......... .......... 3% 22.7M 17s
9200K .......... .......... .......... .......... .......... 3% 17.0M 17s
9250K .......... .......... .......... .......... .......... 3% 18.7M 17s
9300K .......... .......... .......... .......... .......... 3% 21.7M 17s
9350K .......... .......... .......... .......... .......... 3% 16.0M 17s
9400K .......... .......... .......... .......... .......... 3% 18.1M 17s
9450K .......... .......... .......... .......... .......... 3% 16.0M 17s
9500K .......... .......... .......... .......... .......... 3% 29.8M 17s
9550K .......... .......... .......... .......... .......... 3% 25.9M 17s
9600K .......... .......... .......... .......... .......... 3% 14.1M 17s
9650K .......... .......... .......... .......... .......... 3% 103M 17s
9700K .......... .......... .......... .......... .......... 3% 17.3M 17s
9750K .......... .......... .......... .......... .......... 3% 17.2M 17s
9800K .......... .......... .......... .......... .......... 3% 22.2M 17s
9850K .......... .......... .......... .......... .......... 3% 16.7M 17s
9900K .......... .......... .......... .......... .......... 3% 17.9M 17s
9950K .......... .......... .......... .......... .......... 3% 13.9M 17s
10000K .......... .......... .......... .......... .......... 3% 16.4M 17s
10050K .......... .......... .......... .......... .......... 3% 17.7M 17s
10100K .......... .......... .......... .......... .......... 3% 12.7M 17s
10150K .......... .......... .......... .......... .......... 3% 15.0M 17s
10200K .......... .......... .......... .......... .......... 3% 14.8M 17s
10250K .......... .......... .......... .......... .......... 3% 14.1M 17s
10300K .......... .......... .......... .......... .......... 3% 15.0M 17s
10350K .......... .......... .......... .......... .......... 3% 11.5M 17s
10400K .......... .......... .......... .......... .......... 3% 18.3M 17s
10450K .......... .......... .......... .......... .......... 3% 22.3M 17s
10500K .......... .......... .......... .......... .......... 3% 101M 17s
10550K .......... .......... .......... .......... .......... 3% 18.8M 17s
10600K .......... .......... .......... .......... .......... 4% 24.0M 17s
10650K .......... .......... .......... .......... .......... 4% 24.1M 17s
10700K .......... .......... .......... .......... .......... 4% 16.0M 17s
10750K .......... .......... .......... .......... .......... 4% 20.0M 17s
10800K .......... .......... .......... .......... .......... 4% 17.7M 17s
10850K .......... .......... .......... .......... .......... 4% 15.4M 17s
10900K .......... .......... .......... .......... .......... 4% 21.0M 17s
10950K .......... .......... .......... .......... .......... 4% 17.6M 17s
11000K .......... .......... .......... .......... .......... 4% 17.2M 17s
11050K .......... .......... .......... .......... .......... 4% 15.2M 17s
11100K .......... .......... .......... .......... .......... 4% 11.9M 17s
11150K .......... .......... .......... .......... .......... 4% 17.3M 17s
11200K .......... .......... .......... .......... .......... 4% 10.9M 17s
11250K .......... .......... .......... .......... .......... 4% 12.5M 17s
11300K .......... .......... .......... .......... .......... 4% 10.3M 17s
11350K .......... .......... .......... .......... .......... 4% 12.1M 17s
11400K .......... .......... .......... .......... .......... 4% 7.43M 17s
11450K .......... .......... .......... .......... .......... 4% 7.22M 17s
11500K .......... .......... .......... .......... .......... 4% 9.94M 17s
11550K .......... .......... .......... .......... .......... 4% 7.23M 17s
11600K .......... .......... .......... .......... .......... 4% 6.30M 17s
11650K .......... .......... .......... .......... .......... 4% 8.10M 17s
11700K .......... .......... .......... .......... .......... 4% 7.27M 17s
11750K .......... .......... .......... .......... .......... 4% 7.48M 17s
11800K .......... .......... .......... .......... .......... 4% 5.55M 17s
11850K .......... .......... .......... .......... .......... 4% 11.0M 17s
11900K .......... .......... .......... .......... .......... 4% 11.7M 17s
11950K .......... .......... .......... .......... .......... 4% 11.3M 17s
12000K .......... .......... .......... .......... .......... 4% 15.2M 17s
12050K .......... .......... .......... .......... .......... 4% 13.3M 17s
12100K .......... .......... .......... .......... .......... 4% 10.2M 17s
12150K .......... .......... .......... .......... .......... 4% 11.4M 18s
12200K .......... .......... .......... .......... .......... 4% 9.90M 18s
12250K .......... .......... .......... .......... .......... 4% 11.0M 18s
12300K .......... .......... .......... .......... .......... 4% 12.5M 18s
12350K .......... .......... .......... .......... .......... 4% 9.08M 18s
12400K .......... .......... .......... .......... .......... 4% 11.7M 18s
12450K .......... .......... .......... .......... .......... 4% 9.32M 18s
12500K .......... .......... .......... .......... .......... 4% 13.0M 18s
12550K .......... .......... .......... .......... .......... 4% 10.2M 18s
12600K .......... .......... .......... .......... .......... 4% 7.85M 18s
12650K .......... .......... .......... .......... .......... 4% 10.8M 18s
12700K .......... .......... .......... .......... .......... 4% 8.78M 18s
12750K .......... .......... .......... .......... .......... 4% 10.2M 18s
12800K .......... .......... .......... .......... .......... 4% 10.9M 18s
12850K .......... .......... .......... .......... .......... 4% 12.4M 18s
12900K .......... .......... .......... .......... .......... 4% 16.8M 18s
12950K .......... .......... .......... .......... .......... 4% 23.5M 18s
13000K .......... .......... .......... .......... .......... 4% 40.7M 18s
13050K .......... .......... .......... .......... .......... 4% 30.8M 18s
13100K .......... .......... .......... .......... .......... 4% 21.0M 18s
13150K .......... .......... .......... .......... .......... 4% 20.4M 18s
13200K .......... .......... .......... .......... .......... 4% 20.8M 18s
13250K .......... .......... .......... .......... .......... 5% 22.1M 18s
13300K .......... .......... .......... .......... .......... 5% 18.0M 18s
13350K .......... .......... .......... .......... .......... 5% 8.53M 18s
13400K .......... .......... .......... .......... .......... 5% 8.23M 18s
13450K .......... .......... .......... .......... .......... 5% 15.5M 18s
13500K .......... .......... .......... .......... .......... 5% 16.5M 18s
13550K .......... .......... .......... .......... .......... 5% 20.4M 18s
13600K .......... .......... .......... .......... .......... 5% 25.1M 18s
13650K .......... .......... .......... .......... .......... 5% 24.8M 18s
13700K .......... .......... .......... .......... .......... 5% 25.5M 17s
13750K .......... .......... .......... .......... .......... 5% 18.1M 17s
13800K .......... .......... .......... .......... .......... 5% 23.7M 17s
13850K .......... .......... .......... .......... .......... 5% 21.7M 17s
13900K .......... .......... .......... .......... .......... 5% 20.9M 17s
13950K .......... .......... .......... .......... .......... 5% 14.0M 17s
14000K .......... .......... .......... .......... .......... 5% 17.6M 17s
14050K .......... .......... .......... .......... .......... 5% 16.3M 17s
14100K .......... .......... .......... .......... .......... 5% 42.4M 17s
14150K .......... .......... .......... .......... .......... 5% 17.0M 17s
14200K .......... .......... .......... .......... .......... 5% 15.5M 17s
14250K .......... .......... .......... .......... .......... 5% 16.1M 17s
14300K .......... .......... .......... .......... .......... 5% 16.9M 17s
14350K .......... .......... .......... .......... .......... 5% 11.2M 17s
14400K .......... .......... .......... .......... .......... 5% 15.6M 17s
14450K .......... .......... .......... .......... .......... 5% 13.2M 17s
14500K .......... .......... .......... .......... .......... 5% 19.5M 17s
14550K .......... .......... .......... .......... .......... 5% 17.5M 17s
14600K .......... .......... .......... .......... .......... 5% 16.4M 17s
14650K .......... .......... .......... .......... .......... 5% 16.2M 17s
14700K .......... .......... .......... .......... .......... 5% 18.0M 17s
14750K .......... .......... .......... .......... .......... 5% 19.8M 17s
14800K .......... .......... .......... .......... .......... 5% 14.8M 17s
14850K .......... .......... .......... .......... .......... 5% 16.3M 17s
14900K .......... .......... .......... .......... .......... 5% 11.0M 17s
14950K .......... .......... .......... .......... .......... 5% 9.12M 17s
15000K .......... .......... .......... .......... .......... 5% 8.84M 17s
15050K .......... .......... .......... .......... .......... 5% 8.26M 17s
15100K .......... .......... .......... .......... .......... 5% 7.86M 17s
15150K .......... .......... .......... .......... .......... 5% 7.65M 17s
15200K .......... .......... .......... .......... .......... 5% 6.84M 17s
15250K .......... .......... .......... .......... .......... 5% 6.53M 17s
15300K .......... .......... .......... .......... .......... 5% 6.70M 18s
15350K .......... .......... .......... .......... .......... 5% 7.26M 18s
15400K .......... .......... .......... .......... .......... 5% 7.14M 18s
15450K .......... .......... .......... .......... .......... 5% 5.99M 18s
15500K .......... .......... .......... .......... .......... 5% 8.05M 18s
15550K .......... .......... .......... .......... .......... 5% 8.99M 18s
15600K .......... .......... .......... .......... .......... 5% 15.0M 18s
15650K .......... .......... .......... .......... .......... 5% 47.2M 18s
15700K .......... .......... .......... .......... .......... 5% 45.8M 18s
15750K .......... .......... .......... .......... .......... 5% 50.3M 18s
15800K .......... .......... .......... .......... .......... 5% 19.8M 18s
15850K .......... .......... .......... .......... .......... 5% 20.2M 18s
15900K .......... .......... .......... .......... .......... 6% 21.8M 18s
15950K .......... .......... .......... .......... .......... 6% 11.7M 18s
16000K .......... .......... .......... .......... .......... 6% 67.9M 18s
16050K .......... .......... .......... .......... .......... 6% 108M 17s
16100K .......... .......... .......... .......... .......... 6% 27.7M 17s
16150K .......... .......... .......... .......... .......... 6% 33.9M 17s
16200K .......... .......... .......... .......... .......... 6% 28.6M 17s
16250K .......... .......... .......... .......... .......... 6% 28.2M 17s
16300K .......... .......... .......... .......... .......... 6% 37.7M 17s
16350K .......... .......... .......... .......... .......... 6% 23.4M 17s
16400K .......... .......... .......... .......... .......... 6% 156M 17s
16450K .......... .......... .......... .......... .......... 6% 25.3M 17s
16500K .......... .......... .......... .......... .......... 6% 12.5M 17s
16550K .......... .......... .......... .......... .......... 6% 24.5M 17s
16600K .......... .......... .......... .......... .......... 6% 9.04M 17s
16650K .......... .......... .......... .......... .......... 6% 30.5M 17s
16700K .......... .......... .......... .......... .......... 6% 29.4M 17s
16750K .......... .......... .......... .......... .......... 6% 26.7M 17s
16800K .......... .......... .......... .......... .......... 6% 38.3M 17s
16850K .......... .......... .......... .......... .......... 6% 31.9M 17s
16900K .......... .......... .......... .......... .......... 6% 27.3M 17s
16950K .......... .......... .......... .......... .......... 6% 36.9M 17s
17000K .......... .......... .......... .......... .......... 6% 34.5M 17s
17050K .......... .......... .......... .......... .......... 6% 38.4M 17s
17100K .......... .......... .......... .......... .......... 6% 20.6M 17s
17150K .......... .......... .......... .......... .......... 6% 30.6M 17s
17200K .......... .......... .......... .......... .......... 6% 15.6M 17s
17250K .......... .......... .......... .......... .......... 6% 28.9M 17s
17300K .......... .......... .......... .......... .......... 6% 17.9M 17s
17350K .......... .......... .......... .......... .......... 6% 62.8M 17s
17400K .......... .......... .......... .......... .......... 6% 410M 17s
17450K .......... .......... .......... .......... .......... 6% 21.2M 17s
17500K .......... .......... .......... .......... .......... 6% 144M 17s
17550K .......... .......... .......... .......... .......... 6% 23.4M 17s
17600K .......... .......... .......... .......... .......... 6% 28.8M 17s
17650K .......... .......... .......... .......... .......... 6% 30.1M 17s
17700K .......... .......... .......... .......... .......... 6% 31.7M 17s
17750K .......... .......... .......... .......... .......... 6% 23.4M 17s
17800K .......... .......... .......... .......... .......... 6% 34.1M 17s
17850K .......... .......... .......... .......... .......... 6% 25.7M 17s
17900K .......... .......... .......... .......... .......... 6% 31.7M 16s
17950K .......... .......... .......... .......... .......... 6% 37.0M 16s
18000K .......... .......... .......... .......... .......... 6% 28.7M 16s
18050K .......... .......... .......... .......... .......... 6% 26.9M 16s
18100K .......... .......... .......... .......... .......... 6% 25.3M 16s
18150K .......... .......... .......... .......... .......... 6% 30.5M 16s
18200K .......... .......... .......... .......... .......... 6% 30.3M 16s
18250K .......... .......... .......... .......... .......... 6% 35.0M 16s
18300K .......... .......... .......... .......... .......... 6% 25.3M 16s
18350K .......... .......... .......... .......... .......... 6% 23.4M 16s
18400K .......... .......... .......... .......... .......... 6% 31.5M 16s
18450K .......... .......... .......... .......... .......... 6% 13.4M 16s
18500K .......... .......... .......... .......... .......... 6% 15.5M 16s
18550K .......... .......... .......... .......... .......... 6% 17.6M 16s
18600K .......... .......... .......... .......... .......... 7% 12.4M 16s
18650K .......... .......... .......... .......... .......... 7% 12.0M 16s
18700K .......... .......... .......... .......... .......... 7% 13.3M 16s
18750K .......... .......... .......... .......... .......... 7% 14.8M 16s
18800K .......... .......... .......... .......... .......... 7% 14.3M 16s
18850K .......... .......... .......... .......... .......... 7% 12.8M 16s
18900K .......... .......... .......... .......... .......... 7% 14.0M 16s
18950K .......... .......... .......... .......... .......... 7% 11.4M 16s
19000K .......... .......... .......... .......... .......... 7% 9.31M 16s
19050K .......... .......... .......... .......... .......... 7% 6.99M 16s
19100K .......... .......... .......... .......... .......... 7% 8.82M 16s
19150K .......... .......... .......... .......... .......... 7% 15.1M 16s
19200K .......... .......... .......... .......... .......... 7% 12.0M 16s
19250K .......... .......... .......... .......... .......... 7% 9.10M 16s
19300K .......... .......... .......... .......... .......... 7% 11.7M 16s
19350K .......... .......... .......... .......... .......... 7% 10.5M 16s
19400K .......... .......... .......... .......... .......... 7% 10.9M 16s
19450K .......... .......... .......... .......... .......... 7% 12.6M 16s
19500K .......... .......... .......... .......... .......... 7% 10.3M 16s
19550K .......... .......... .......... .......... .......... 7% 12.2M 16s
19600K .......... .......... .......... .......... .......... 7% 8.42M 16s
19650K .......... .......... .......... .......... .......... 7% 15.3M 16s
19700K .......... .......... .......... .......... .......... 7% 12.2M 16s
19750K .......... .......... .......... .......... .......... 7% 14.0M 16s
19800K .......... .......... .......... .......... .......... 7% 17.9M 16s
19850K .......... .......... .......... .......... .......... 7% 7.02M 16s
19900K .......... .......... .......... .......... .......... 7% 17.7M 16s
19950K .......... .......... .......... .......... .......... 7% 9.70M 16s
20000K .......... .......... .......... .......... .......... 7% 11.0M 16s
20050K .......... .......... .......... .......... .......... 7% 6.58M 17s
20100K .......... .......... .......... .......... .......... 7% 7.95M 17s
20150K .......... .......... .......... .......... .......... 7% 9.53M 17s
20200K .......... .......... .......... .......... .......... 7% 13.1M 17s
20250K .......... .......... .......... .......... .......... 7% 8.42M 17s
20300K .......... .......... .......... .......... .......... 7% 18.8M 17s
20350K .......... .......... .......... .......... .......... 7% 8.67M 17s
20400K .......... .......... .......... .......... .......... 7% 12.2M 17s
20450K .......... .......... .......... .......... .......... 7% 9.34M 17s
20500K .......... .......... .......... .......... .......... 7% 12.2M 17s
20550K .......... .......... .......... .......... .......... 7% 9.99M 17s
20600K .......... .......... .......... .......... .......... 7% 9.36M 17s
20650K .......... .......... .......... .......... .......... 7% 9.23M 17s
20700K .......... .......... .......... .......... .......... 7% 11.3M 17s
20750K .......... .......... .......... .......... .......... 7% 17.0M 17s
20800K .......... .......... .......... .......... .......... 7% 19.8M 17s
20850K .......... .......... .......... .......... .......... 7% 10.3M 17s
20900K .......... .......... .......... .......... .......... 7% 28.9M 17s
20950K .......... .......... .......... .......... .......... 7% 12.1M 17s
21000K .......... .......... .......... .......... .......... 7% 34.8M 17s
21050K .......... .......... .......... .......... .......... 7% 22.3M 17s
21100K .......... .......... .......... .......... .......... 7% 17.4M 17s
21150K .......... .......... .......... .......... .......... 7% 27.1M 17s
21200K .......... .......... .......... .......... .......... 7% 15.0M 17s
21250K .......... .......... .......... .......... .......... 8% 22.3M 17s
21300K .......... .......... .......... .......... .......... 8% 22.1M 17s
21350K .......... .......... .......... .......... .......... 8% 20.2M 17s
21400K .......... .......... .......... .......... .......... 8% 18.0M 17s
21450K .......... .......... .......... .......... .......... 8% 17.8M 17s
21500K .......... .......... .......... .......... .......... 8% 24.0M 16s
21550K .......... .......... .......... .......... .......... 8% 14.7M 16s
21600K .......... .......... .......... .......... .......... 8% 8.07M 17s
21650K .......... .......... .......... .......... .......... 8% 12.8M 17s
21700K .......... .......... .......... .......... .......... 8% 14.3M 17s
21750K .......... .......... .......... .......... .......... 8% 30.0M 16s
21800K .......... .......... .......... .......... .......... 8% 20.6M 16s
21850K .......... .......... .......... .......... .......... 8% 11.8M 16s
21900K .......... .......... .......... .......... .......... 8% 17.0M 16s
21950K .......... .......... .......... .......... .......... 8% 10.3M 16s
22000K .......... .......... .......... .......... .......... 8% 24.5M 16s
22050K .......... .......... .......... .......... .......... 8% 42.9M 16s
22100K .......... .......... .......... .......... .......... 8% 15.1M 16s
22150K .......... .......... .......... .......... .......... 8% 15.4M 16s
22200K .......... .......... .......... .......... .......... 8% 37.8M 16s
22250K .......... .......... .......... .......... .......... 8% 23.9M 16s
22300K .......... .......... .......... .......... .......... 8% 21.5M 16s
22350K .......... .......... .......... .......... .......... 8% 19.5M 16s
22400K .......... .......... .......... .......... .......... 8% 27.1M 16s
22450K .......... .......... .......... .......... .......... 8% 25.1M 16s
22500K .......... .......... .......... .......... .......... 8% 19.9M 16s
22550K .......... .......... .......... .......... .......... 8% 27.6M 16s
22600K .......... .......... .......... .......... .......... 8% 23.5M 16s
22650K .......... .......... .......... .......... .......... 8% 25.7M 16s
22700K .......... .......... .......... .......... .......... 8% 19.6M 16s
22750K .......... .......... .......... .......... .......... 8% 26.5M 16s
22800K .......... .......... .......... .......... .......... 8% 22.3M 16s
22850K .......... .......... .......... .......... .......... 8% 23.5M 16s
22900K .......... .......... .......... .......... .......... 8% 25.4M 16s
22950K .......... .......... .......... .......... .......... 8% 21.4M 16s
23000K .......... .......... .......... .......... .......... 8% 31.3M 16s
23050K .......... .......... .......... .......... .......... 8% 28.7M 16s
23100K .......... .......... .......... .......... .......... 8% 24.2M 16s
23150K .......... .......... .......... .......... .......... 8% 21.5M 16s
23200K .......... .......... .......... .......... .......... 8% 38.2M 16s
23250K .......... .......... .......... .......... .......... 8% 33.9M 16s
23300K .......... .......... .......... .......... .......... 8% 33.2M 16s
23350K .......... .......... .......... .......... .......... 8% 19.3M 16s
23400K .......... .......... .......... .......... .......... 8% 119M 16s
23450K .......... .......... .......... .......... .......... 8% 40.9M 16s
23500K .......... .......... .......... .......... .......... 8% 91.1M 16s
23550K .......... .......... .......... .......... .......... 8% 31.2M 16s
23600K .......... .......... .......... .......... .......... 8% 17.1M 16s
23650K .......... .......... .......... .......... .......... 8% 448M 16s
23700K .......... .......... .......... .......... .......... 8% 21.7M 16s
23750K .......... .......... .......... .......... .......... 8% 36.5M 16s
23800K .......... .......... .......... .......... .......... 8% 28.9M 16s
23850K .......... .......... .......... .......... .......... 8% 27.3M 16s
23900K .......... .......... .......... .......... .......... 9% 46.9M 16s
23950K .......... .......... .......... .......... .......... 9% 27.5M 16s
24000K .......... .......... .......... .......... .......... 9% 46.0M 16s
24050K .......... .......... .......... .......... .......... 9% 26.1M 16s
24100K .......... .......... .......... .......... .......... 9% 29.4M 16s
24150K .......... .......... .......... .......... .......... 9% 36.5M 16s
24200K .......... .......... .......... .......... .......... 9% 29.7M 16s
24250K .......... .......... .......... .......... .......... 9% 38.5M 16s
24300K .......... .......... .......... .......... .......... 9% 30.8M 16s
24350K .......... .......... .......... .......... .......... 9% 35.5M 16s
24400K .......... .......... .......... .......... .......... 9% 34.2M 16s
24450K .......... .......... .......... .......... .......... 9% 38.6M 16s
24500K .......... .......... .......... .......... .......... 9% 31.7M 16s
24550K .......... .......... .......... .......... .......... 9% 28.7M 15s
24600K .......... .......... .......... .......... .......... 9% 26.4M 15s
24650K .......... .......... .......... .......... .......... 9% 33.3M 15s
24700K .......... .......... .......... .......... .......... 9% 39.7M 15s
24750K .......... .......... .......... .......... .......... 9% 29.0M 15s
24800K .......... .......... .......... .......... .......... 9% 40.4M 15s
24850K .......... .......... .......... .......... .......... 9% 44.8M 15s
24900K .......... .......... .......... .......... .......... 9% 32.9M 15s
24950K .......... .......... .......... .......... .......... 9% 173M 15s
25000K .......... .......... .......... .......... .......... 9% 15.8M 15s
25050K .......... .......... .......... .......... .......... 9% 130M 15s
25100K .......... .......... .......... .......... .......... 9% 277M 15s
25150K .......... .......... .......... .......... .......... 9% 17.6M 15s
25200K .......... .......... .......... .......... .......... 9% 258M 15s
25250K .......... .......... .......... .......... .......... 9% 22.6M 15s
25300K .......... .......... .......... .......... .......... 9% 19.8M 15s
25350K .......... .......... .......... .......... .......... 9% 50.2M 15s
25400K .......... .......... .......... .......... .......... 9% 96.9M 15s
25450K .......... .......... .......... .......... .......... 9% 22.7M 15s
25500K .......... .......... .......... .......... .......... 9% 20.7M 15s
25550K .......... .......... .......... .......... .......... 9% 29.5M 15s
25600K .......... .......... .......... .......... .......... 9% 18.1M 15s
25650K .......... .......... .......... .......... .......... 9% 21.6M 15s
25700K .......... .......... .......... .......... .......... 9% 19.3M 15s
25750K .......... .......... .......... .......... .......... 9% 26.0M 15s
25800K .......... .......... .......... .......... .......... 9% 27.3M 15s
25850K .......... .......... .......... .......... .......... 9% 18.8M 15s
25900K .......... .......... .......... .......... .......... 9% 21.2M 15s
25950K .......... .......... .......... .......... .......... 9% 25.2M 15s
26000K .......... .......... .......... .......... .......... 9% 21.1M 15s
26050K .......... .......... .......... .......... .......... 9% 22.1M 15s
26100K .......... .......... .......... .......... .......... 9% 20.6M 15s
26150K .......... .......... .......... .......... .......... 9% 20.8M 15s
26200K .......... .......... .......... .......... .......... 9% 17.0M 15s
26250K .......... .......... .......... .......... .......... 9% 25.5M 15s
26300K .......... .......... .......... .......... .......... 9% 21.2M 15s
26350K .......... .......... .......... .......... .......... 9% 76.1M 15s
26400K .......... .......... .......... .......... .......... 9% 20.9M 15s
26450K .......... .......... .......... .......... .......... 9% 19.4M 15s
26500K .......... .......... .......... .......... .......... 9% 18.7M 15s
26550K .......... .......... .......... .......... .......... 10% 66.4M 15s
26600K .......... .......... .......... .......... .......... 10% 27.0M 15s
26650K .......... .......... .......... .......... .......... 10% 27.2M 15s
26700K .......... .......... .......... .......... .......... 10% 29.5M 15s
26750K .......... .......... .......... .......... .......... 10% 39.7M 15s
26800K .......... .......... .......... .......... .......... 10% 37.9M 15s
26850K .......... .......... .......... .......... .......... 10% 33.9M 15s
26900K .......... .......... .......... .......... .......... 10% 25.6M 15s
26950K .......... .......... .......... .......... .......... 10% 43.5M 15s
27000K .......... .......... .......... .......... .......... 10% 31.4M 15s
27050K .......... .......... .......... .......... .......... 10% 58.3M 15s
27100K .......... .......... .......... .......... .......... 10% 29.0M 15s
27150K .......... .......... .......... .......... .......... 10% 27.1M 15s
27200K .......... .......... .......... .......... .......... 10% 20.8M 15s
27250K .......... .......... .......... .......... .......... 10% 40.2M 15s
27300K .......... .......... .......... .......... .......... 10% 25.2M 15s
27350K .......... .......... .......... .......... .......... 10% 31.7M 15s
27400K .......... .......... .......... .......... .......... 10% 25.3M 15s
27450K .......... .......... .......... .......... .......... 10% 21.9M 15s
27500K .......... .......... .......... .......... .......... 10% 34.3M 15s
27550K .......... .......... .......... .......... .......... 10% 26.2M 15s
27600K .......... .......... .......... .......... .......... 10% 26.2M 15s
27650K .......... .......... .......... .......... .......... 10% 26.0M 15s
27700K .......... .......... .......... .......... .......... 10% 22.0M 14s
27750K .......... .......... .......... .......... .......... 10% 25.4M 14s
27800K .......... .......... .......... .......... .......... 10% 27.2M 14s
27850K .......... .......... .......... .......... .......... 10% 26.8M 14s
27900K .......... .......... .......... .......... .......... 10% 31.1M 14s
27950K .......... .......... .......... .......... .......... 10% 22.7M 14s
28000K .......... .......... .......... .......... .......... 10% 25.6M 14s
28050K .......... .......... .......... .......... .......... 10% 28.8M 14s
28100K .......... .......... .......... .......... .......... 10% 27.3M 14s
28150K .......... .......... .......... .......... .......... 10% 37.2M 14s
28200K .......... .......... .......... .......... .......... 10% 19.5M 14s
28250K .......... .......... .......... .......... .......... 10% 56.6M 14s
28300K .......... .......... .......... .......... .......... 10% 35.5M 14s
28350K .......... .......... .......... .......... .......... 10% 24.3M 14s
28400K .......... .......... .......... .......... .......... 10% 34.4M 14s
28450K .......... .......... .......... .......... .......... 10% 27.2M 14s
28500K .......... .......... .......... .......... .......... 10% 19.6M 14s
28550K .......... .......... .......... .......... .......... 10% 112M 14s
28600K .......... .......... .......... .......... .......... 10% 24.0M 14s
28650K .......... .......... .......... .......... .......... 10% 22.5M 14s
28700K .......... .......... .......... .......... .......... 10% 139M 14s
28750K .......... .......... .......... .......... .......... 10% 19.1M 14s
28800K .......... .......... .......... .......... .......... 10% 21.9M 14s
28850K .......... .......... .......... .......... .......... 10% 26.8M 14s
28900K .......... .......... .......... .......... .......... 10% 11.6M 14s
28950K .......... .......... .......... .......... .......... 10% 43.5M 14s
29000K .......... .......... .......... .......... .......... 10% 87.8M 14s
29050K .......... .......... .......... .......... .......... 10% 28.2M 14s
29100K .......... .......... .......... .......... .......... 10% 27.6M 14s
29150K .......... .......... .......... .......... .......... 10% 25.3M 14s
29200K .......... .......... .......... .......... .......... 11% 28.5M 14s
29250K .......... .......... .......... .......... .......... 11% 30.0M 14s
29300K .......... .......... .......... .......... .......... 11% 31.9M 14s
29350K .......... .......... .......... .......... .......... 11% 30.6M 14s
29400K .......... .......... .......... .......... .......... 11% 16.0M 14s
29450K .......... .......... .......... .......... .......... 11% 198M 14s
29500K .......... .......... .......... .......... .......... 11% 20.8M 14s
29550K .......... .......... .......... .......... .......... 11% 31.5M 14s
29600K .......... .......... .......... .......... .......... 11% 29.4M 14s
29650K .......... .......... .......... .......... .......... 11% 10.3M 14s
29700K .......... .......... .......... .......... .......... 11% 321M 14s
29750K .......... .......... .......... .......... .......... 11% 21.5M 14s
29800K .......... .......... .......... .......... .......... 11% 22.7M 14s
29850K .......... .......... .......... .......... .......... 11% 11.7M 14s
29900K .......... .......... .......... .......... .......... 11% 16.8M 14s
29950K .......... .......... .......... .......... .......... 11% 13.2M 14s
30000K .......... .......... .......... .......... .......... 11% 14.9M 14s
30050K .......... .......... .......... .......... .......... 11% 21.0M 14s
30100K .......... .......... .......... .......... .......... 11% 12.5M 14s
30150K .......... .......... .......... .......... .......... 11% 23.4M 14s
30200K .......... .......... .......... .......... .......... 11% 14.0M 14s
30250K .......... .......... .......... .......... .......... 11% 14.9M 14s
30300K .......... .......... .......... .......... .......... 11% 12.3M 14s
30350K .......... .......... .......... .......... .......... 11% 9.59M 14s
30400K .......... .......... .......... .......... .......... 11% 9.24M 14s
30450K .......... .......... .......... .......... .......... 11% 6.68M 14s
30500K .......... .......... .......... .......... .......... 11% 10.5M 14s
30550K .......... .......... .......... .......... .......... 11% 9.21M 14s
30600K .......... .......... .......... .......... .......... 11% 8.98M 14s
30650K .......... .......... .......... .......... .......... 11% 12.8M 14s
30700K .......... .......... .......... .......... .......... 11% 9.73M 14s
30750K .......... .......... .......... .......... .......... 11% 11.2M 14s
30800K .......... .......... .......... .......... .......... 11% 11.4M 14s
30850K .......... .......... .......... .......... .......... 11% 9.00M 14s
30900K .......... .......... .......... .......... .......... 11% 6.16M 14s
30950K .......... .......... .......... .......... .......... 11% 6.39M 14s
31000K .......... .......... .......... .......... .......... 11% 12.5M 14s
31050K .......... .......... .......... .......... .......... 11% 13.2M 14s
31100K .......... .......... .......... .......... .......... 11% 14.9M 14s
31150K .......... .......... .......... .......... .......... 11% 15.7M 14s
31200K .......... .......... .......... .......... .......... 11% 18.0M 14s
31250K .......... .......... .......... .......... .......... 11% 23.7M 14s
31300K .......... .......... .......... .......... .......... 11% 25.2M 14s
31350K .......... .......... .......... .......... .......... 11% 16.4M 14s
31400K .......... .......... .......... .......... .......... 11% 20.5M 14s
31450K .......... .......... .......... .......... .......... 11% 17.3M 14s
31500K .......... .......... .......... .......... .......... 11% 21.9M 14s
31550K .......... .......... .......... .......... .......... 11% 25.5M 14s
31600K .......... .......... .......... .......... .......... 11% 17.1M 14s
31650K .......... .......... .......... .......... .......... 11% 28.7M 14s
31700K .......... .......... .......... .......... .......... 11% 17.5M 14s
31750K .......... .......... .......... .......... .......... 11% 20.9M 14s
31800K .......... .......... .......... .......... .......... 11% 37.9M 14s
31850K .......... .......... .......... .......... .......... 12% 27.0M 14s
31900K .......... .......... .......... .......... .......... 12% 64.3M 14s
31950K .......... .......... .......... .......... .......... 12% 24.8M 14s
32000K .......... .......... .......... .......... .......... 12% 19.9M 14s
32050K .......... .......... .......... .......... .......... 12% 397M 14s
32100K .......... .......... .......... .......... .......... 12% 16.1M 14s
32150K .......... .......... .......... .......... .......... 12% 493M 14s
32200K .......... .......... .......... .......... .......... 12% 10.9M 14s
32250K .......... .......... .......... .......... .......... 12% 514M 14s
32300K .......... .......... .......... .......... .......... 12% 17.2M 14s
32350K .......... .......... .......... .......... .......... 12% 16.7M 14s
32400K .......... .......... .......... .......... .......... 12% 19.4M 14s
32450K .......... .......... .......... .......... .......... 12% 21.1M 14s
32500K .......... .......... .......... .......... .......... 12% 18.7M 14s
32550K .......... .......... .......... .......... .......... 12% 16.8M 14s
32600K .......... .......... .......... .......... .......... 12% 15.5M 14s
32650K .......... .......... .......... .......... .......... 12% 17.1M 14s
32700K .......... .......... .......... .......... .......... 12% 19.6M 14s
32750K .......... .......... .......... .......... .......... 12% 16.8M 14s
32800K .......... .......... .......... .......... .......... 12% 21.5M 14s
32850K .......... .......... .......... .......... .......... 12% 15.4M 14s
32900K .......... .......... .......... .......... .......... 12% 22.4M 14s
32950K .......... .......... .......... .......... .......... 12% 19.8M 14s
33000K .......... .......... .......... .......... .......... 12% 17.1M 14s
33050K .......... .......... .......... .......... .......... 12% 31.2M 14s
33100K .......... .......... .......... .......... .......... 12% 32.5M 14s
33150K .......... .......... .......... .......... .......... 12% 42.7M 14s
33200K .......... .......... .......... .......... .......... 12% 38.4M 14s
33250K .......... .......... .......... .......... .......... 12% 48.1M 14s
33300K .......... .......... .......... .......... .......... 12% 48.1M 14s
33350K .......... .......... .......... .......... .......... 12% 24.5M 14s
33400K .......... .......... .......... .......... .......... 12% 425M 14s
33450K .......... .......... .......... .......... .......... 12% 25.5M 14s
33500K .......... .......... .......... .......... .......... 12% 93.7M 14s
33550K .......... .......... .......... .......... .......... 12% 36.0M 14s
33600K .......... .......... .......... .......... .......... 12% 55.8M 14s
33650K .......... .......... .......... .......... .......... 12% 29.4M 14s
33700K .......... .......... .......... .......... .......... 12% 26.6M 14s
33750K .......... .......... .......... .......... .......... 12% 29.2M 14s
33800K .......... .......... .......... .......... .......... 12% 41.9M 14s
33850K .......... .......... .......... .......... .......... 12% 25.3M 14s
33900K .......... .......... .......... .......... .......... 12% 25.1M 14s
33950K .......... .......... .......... .......... .......... 12% 28.6M 14s
34000K .......... .......... .......... .......... .......... 12% 28.0M 14s
34050K .......... .......... .......... .......... .......... 12% 40.8M 14s
34100K .......... .......... .......... .......... .......... 12% 17.3M 14s
34150K .......... .......... .......... .......... .......... 12% 11.7M 14s
34200K .......... .......... .......... .......... .......... 12% 17.9M 14s
34250K .......... .......... .......... .......... .......... 12% 15.5M 14s
34300K .......... .......... .......... .......... .......... 12% 13.2M 14s
34350K .......... .......... .......... .......... .......... 12% 11.8M 14s
34400K .......... .......... .......... .......... .......... 12% 11.1M 14s
34450K .......... .......... .......... .......... .......... 12% 9.19M 14s
34500K .......... .......... .......... .......... .......... 12% 12.5M 14s
34550K .......... .......... .......... .......... .......... 13% 10.3M 14s
34600K .......... .......... .......... .......... .......... 13% 9.34M 14s
34650K .......... .......... .......... .......... .......... 13% 32.0M 14s
34700K .......... .......... .......... .......... .......... 13% 17.9M 14s
34750K .......... .......... .......... .......... .......... 13% 18.0M 14s
34800K .......... .......... .......... .......... .......... 13% 14.6M 14s
34850K .......... .......... .......... .......... .......... 13% 19.8M 14s
34900K .......... .......... .......... .......... .......... 13% 21.1M 14s
34950K .......... .......... .......... .......... .......... 13% 17.3M 14s
35000K .......... .......... .......... .......... .......... 13% 21.9M 14s
35050K .......... .......... .......... .......... .......... 13% 20.5M 14s
35100K .......... .......... .......... .......... .......... 13% 16.1M 14s
35150K .......... .......... .......... .......... .......... 13% 17.2M 14s
35200K .......... .......... .......... .......... .......... 13% 17.3M 14s
35250K .......... .......... .......... .......... .......... 13% 22.0M 14s
35300K .......... .......... .......... .......... .......... 13% 15.8M 14s
35350K .......... .......... .......... .......... .......... 13% 15.6M 14s
35400K .......... .......... .......... .......... .......... 13% 18.9M 14s
35450K .......... .......... .......... .......... .......... 13% 15.6M 14s
35500K .......... .......... .......... .......... .......... 13% 25.0M 14s
35550K .......... .......... .......... .......... .......... 13% 15.4M 14s
35600K .......... .......... .......... .......... .......... 13% 12.2M 14s
35650K .......... .......... .......... .......... .......... 13% 11.3M 14s
35700K .......... .......... .......... .......... .......... 13% 10.0M 14s
35750K .......... .......... .......... .......... .......... 13% 17.6M 14s
35800K .......... .......... .......... .......... .......... 13% 18.2M 14s
35850K .......... .......... .......... .......... .......... 13% 10.5M 14s
35900K .......... .......... .......... .......... .......... 13% 12.1M 14s
35950K .......... .......... .......... .......... .......... 13% 10.9M 14s
36000K .......... .......... .......... .......... .......... 13% 13.6M 14s
36050K .......... .......... .......... .......... .......... 13% 14.9M 14s
36100K .......... .......... .......... .......... .......... 13% 13.9M 14s
36150K .......... .......... .......... .......... .......... 13% 14.9M 14s
36200K .......... .......... .......... .......... .......... 13% 12.3M 14s
36250K .......... .......... .......... .......... .......... 13% 13.5M 14s
36300K .......... .......... .......... .......... .......... 13% 10.7M 14s
36350K .......... .......... .......... .......... .......... 13% 12.5M 14s
36400K .......... .......... .......... .......... .......... 13% 10.3M 14s
36450K .......... .......... .......... .......... .......... 13% 5.88M 14s
36500K .......... .......... .......... .......... .......... 13% 13.9M 14s
36550K .......... .......... .......... .......... .......... 13% 19.2M 14s
36600K .......... .......... .......... .......... .......... 13% 12.3M 14s
36650K .......... .......... .......... .......... .......... 13% 19.6M 14s
36700K .......... .......... .......... .......... .......... 13% 20.2M 14s
36750K .......... .......... .......... .......... .......... 13% 39.2M 14s
36800K .......... .......... .......... .......... .......... 13% 31.0M 14s
36850K .......... .......... .......... .......... .......... 13% 21.9M 14s
36900K .......... .......... .......... .......... .......... 13% 16.3M 14s
36950K .......... .......... .......... .......... .......... 13% 24.5M 14s
37000K .......... .......... .......... .......... .......... 13% 17.2M 14s
37050K .......... .......... .......... .......... .......... 13% 18.5M 14s
37100K .......... .......... .......... .......... .......... 13% 19.2M 14s
37150K .......... .......... .......... .......... .......... 13% 18.8M 14s
37200K .......... .......... .......... .......... .......... 14% 17.9M 14s
37250K .......... .......... .......... .......... .......... 14% 27.6M 14s
37300K .......... .......... .......... .......... .......... 14% 22.2M 14s
37350K .......... .......... .......... .......... .......... 14% 17.2M 14s
37400K .......... .......... .......... .......... .......... 14% 19.8M 14s
37450K .......... .......... .......... .......... .......... 14% 14.1M 14s
37500K .......... .......... .......... .......... .......... 14% 23.6M 14s
37550K .......... .......... .......... .......... .......... 14% 17.3M 13s
37600K .......... .......... .......... .......... .......... 14% 15.3M 13s
37650K .......... .......... .......... .......... .......... 14% 15.7M 13s
37700K .......... .......... .......... .......... .......... 14% 9.00M 14s
37750K .......... .......... .......... .......... .......... 14% 110M 13s
37800K .......... .......... .......... .......... .......... 14% 20.0M 13s
37850K .......... .......... .......... .......... .......... 14% 11.4M 13s
37900K .......... .......... .......... .......... .......... 14% 18.4M 13s
37950K .......... .......... .......... .......... .......... 14% 13.1M 13s
38000K .......... .......... .......... .......... .......... 14% 16.4M 13s
38050K .......... .......... .......... .......... .......... 14% 19.8M 13s
38100K .......... .......... .......... .......... .......... 14% 11.4M 13s
38150K .......... .......... .......... .......... .......... 14% 13.9M 13s
38200K .......... .......... .......... .......... .......... 14% 13.8M 13s
38250K .......... .......... .......... .......... .......... 14% 15.4M 13s
38300K .......... .......... .......... .......... .......... 14% 16.3M 13s
38350K .......... .......... .......... .......... .......... 14% 15.9M 13s
38400K .......... .......... .......... .......... .......... 14% 13.4M 13s
38450K .......... .......... .......... .......... .......... 14% 9.33M 13s
38500K .......... .......... .......... .......... .......... 14% 18.0M 13s
38550K .......... .......... .......... .......... .......... 14% 10.3M 13s
38600K .......... .......... .......... .......... .......... 14% 7.49M 14s
38650K .......... .......... .......... .......... .......... 14% 8.79M 14s
38700K .......... .......... .......... .......... .......... 14% 9.64M 14s
38750K .......... .......... .......... .......... .......... 14% 7.28M 14s
38800K .......... .......... .......... .......... .......... 14% 8.44M 14s
38850K .......... .......... .......... .......... .......... 14% 10.4M 14s
38900K .......... .......... .......... .......... .......... 14% 9.45M 14s
38950K .......... .......... .......... .......... .......... 14% 19.6M 14s
39000K .......... .......... .......... .......... .......... 14% 10.2M 14s
39050K .......... .......... .......... .......... .......... 14% 32.2M 14s
39100K .......... .......... .......... .......... .......... 14% 11.5M 14s
39150K .......... .......... .......... .......... .......... 14% 13.3M 14s
39200K .......... .......... .......... .......... .......... 14% 10.4M 14s
39250K .......... .......... .......... .......... .......... 14% 14.0M 14s
39300K .......... .......... .......... .......... .......... 14% 9.66M 14s
39350K .......... .......... .......... .......... .......... 14% 9.43M 14s
39400K .......... .......... .......... .......... .......... 14% 11.0M 14s
39450K .......... .......... .......... .......... .......... 14% 8.39M 14s
39500K .......... .......... .......... .......... .......... 14% 9.74M 14s
39550K .......... .......... .......... .......... .......... 14% 10.8M 14s
39600K .......... .......... .......... .......... .......... 14% 7.47M 14s
39650K .......... .......... .......... .......... .......... 14% 9.76M 14s
39700K .......... .......... .......... .......... .......... 14% 9.83M 14s
39750K .......... .......... .......... .......... .......... 14% 9.27M 14s
39800K .......... .......... .......... .......... .......... 14% 13.5M 14s
39850K .......... .......... .......... .......... .......... 15% 10.2M 14s
39900K .......... .......... .......... .......... .......... 15% 10.2M 14s
39950K .......... .......... .......... .......... .......... 15% 12.2M 14s
40000K .......... .......... .......... .......... .......... 15% 12.8M 14s
40050K .......... .......... .......... .......... .......... 15% 11.4M 14s
40100K .......... .......... .......... .......... .......... 15% 11.4M 14s
40150K .......... .......... .......... .......... .......... 15% 11.6M 14s
40200K .......... .......... .......... .......... .......... 15% 7.66M 14s
40250K .......... .......... .......... .......... .......... 15% 121M 14s
40300K .......... .......... .......... .......... .......... 15% 11.0M 14s
40350K .......... .......... .......... .......... .......... 15% 13.6M 14s
40400K .......... .......... .......... .......... .......... 15% 10.8M 14s
40450K .......... .......... .......... .......... .......... 15% 11.7M 14s
40500K .......... .......... .......... .......... .......... 15% 12.9M 14s
40550K .......... .......... .......... .......... .......... 15% 13.9M 14s
40600K .......... .......... .......... .......... .......... 15% 14.0M 14s
40650K .......... .......... .......... .......... .......... 15% 16.5M 14s
40700K .......... .......... .......... .......... .......... 15% 13.2M 14s
40750K .......... .......... .......... .......... .......... 15% 11.5M 14s
40800K .......... .......... .......... .......... .......... 15% 12.2M 14s
40850K .......... .......... .......... .......... .......... 15% 14.1M 14s
40900K .......... .......... .......... .......... .......... 15% 13.3M 14s
40950K .......... .......... .......... .......... .......... 15% 12.6M 14s
41000K .......... .......... .......... .......... .......... 15% 15.7M 14s
41050K .......... .......... .......... .......... .......... 15% 12.3M 14s
41100K .......... .......... .......... .......... .......... 15% 7.19M 14s
41150K .......... .......... .......... .......... .......... 15% 5.92M 14s
41200K .......... .......... .......... .......... .......... 15% 6.21M 14s
41250K .......... .......... .......... .......... .......... 15% 8.78M 14s
41300K .......... .......... .......... .......... .......... 15% 9.30M 14s
41350K .......... .......... .......... .......... .......... 15% 10.3M 14s
41400K .......... .......... .......... .......... .......... 15% 40.0M 14s
41450K .......... .......... .......... .......... .......... 15% 7.56M 14s
41500K .......... .......... .......... .......... .......... 15% 54.7M 14s
41550K .......... .......... .......... .......... .......... 15% 18.2M 14s
41600K .......... .......... .......... .......... .......... 15% 10.8M 14s
41650K .......... .......... .......... .......... .......... 15% 16.8M 14s
41700K .......... .......... .......... .......... .......... 15% 12.0M 14s
41750K .......... .......... .......... .......... .......... 15% 18.6M 14s
41800K .......... .......... .......... .......... .......... 15% 11.1M 14s
41850K .......... .......... .......... .......... .......... 15% 14.8M 14s
41900K .......... .......... .......... .......... .......... 15% 13.7M 14s
41950K .......... .......... .......... .......... .......... 15% 11.5M 14s
42000K .......... .......... .......... .......... .......... 15% 14.6M 14s
42050K .......... .......... .......... .......... .......... 15% 14.1M 14s
42100K .......... .......... .......... .......... .......... 15% 11.1M 14s
42150K .......... .......... .......... .......... .......... 15% 30.2M 14s
42200K .......... .......... .......... .......... .......... 15% 21.7M 14s
42250K .......... .......... .......... .......... .......... 15% 23.7M 14s
42300K .......... .......... .......... .......... .......... 15% 24.8M 14s
42350K .......... .......... .......... .......... .......... 15% 15.6M 14s
42400K .......... .......... .......... .......... .......... 15% 25.0M 14s
42450K .......... .......... .......... .......... .......... 15% 17.8M 14s
42500K .......... .......... .......... .......... .......... 16% 13.4M 14s
42550K .......... .......... .......... .......... .......... 16% 9.67M 14s
42600K .......... .......... .......... .......... .......... 16% 13.4M 14s
42650K .......... .......... .......... .......... .......... 16% 11.3M 14s
42700K .......... .......... .......... .......... .......... 16% 10.2M 14s
42750K .......... .......... .......... .......... .......... 16% 12.4M 14s
42800K .......... .......... .......... .......... .......... 16% 10.4M 14s
42850K .......... .......... .......... .......... .......... 16% 8.11M 14s
42900K .......... .......... .......... .......... .......... 16% 10.9M 14s
42950K .......... .......... .......... .......... .......... 16% 8.81M 14s
43000K .......... .......... .......... .......... .......... 16% 52.8M 14s
43050K .......... .......... .......... .......... .......... 16% 19.5M 14s
43100K .......... .......... .......... .......... .......... 16% 18.1M 14s
43150K .......... .......... .......... .......... .......... 16% 16.7M 14s
43200K .......... .......... .......... .......... .......... 16% 15.9M 14s
43250K .......... .......... .......... .......... .......... 16% 18.1M 14s
43300K .......... .......... .......... .......... .......... 16% 15.1M 14s
43350K .......... .......... .......... .......... .......... 16% 15.5M 14s
43400K .......... .......... .......... .......... .......... 16% 20.5M 14s
43450K .......... .......... .......... .......... .......... 16% 16.2M 14s
43500K .......... .......... .......... .......... .......... 16% 19.0M 14s
43550K .......... .......... .......... .......... .......... 16% 17.2M 14s
43600K .......... .......... .......... .......... .......... 16% 16.1M 14s
43650K .......... .......... .......... .......... .......... 16% 17.6M 14s
43700K .......... .......... .......... .......... .......... 16% 16.1M 14s
43750K .......... .......... .......... .......... .......... 16% 17.3M 14s
43800K .......... .......... .......... .......... .......... 16% 20.0M 14s
43850K .......... .......... .......... .......... .......... 16% 24.0M 14s
43900K .......... .......... .......... .......... .......... 16% 18.5M 14s
43950K .......... .......... .......... .......... .......... 16% 17.5M 14s
44000K .......... .......... .......... .......... .......... 16% 14.2M 14s
44050K .......... .......... .......... .......... .......... 16% 42.5M 14s
44100K .......... .......... .......... .......... .......... 16% 7.01M 14s
44150K .......... .......... .......... .......... .......... 16% 201M 14s
44200K .......... .......... .......... .......... .......... 16% 37.3M 14s
44250K .......... .......... .......... .......... .......... 16% 14.9M 14s
44300K .......... .......... .......... .......... .......... 16% 21.4M 14s
44350K .......... .......... .......... .......... .......... 16% 14.8M 14s
44400K .......... .......... .......... .......... .......... 16% 25.7M 14s
44450K .......... .......... .......... .......... .......... 16% 13.9M 14s
44500K .......... .......... .......... .......... .......... 16% 18.6M 14s
44550K .......... .......... .......... .......... .......... 16% 16.8M 14s
44600K .......... .......... .......... .......... .......... 16% 15.9M 14s
44650K .......... .......... .......... .......... .......... 16% 16.8M 14s
44700K .......... .......... .......... .......... .......... 16% 19.5M 14s
44750K .......... .......... .......... .......... .......... 16% 16.3M 14s
44800K .......... .......... .......... .......... .......... 16% 18.9M 14s
44850K .......... .......... .......... .......... .......... 16% 17.9M 14s
44900K .......... .......... .......... .......... .......... 16% 22.0M 14s
44950K .......... .......... .......... .......... .......... 16% 14.1M 14s
45000K .......... .......... .......... .......... .......... 16% 22.3M 14s
45050K .......... .......... .......... .......... .......... 16% 22.3M 14s
45100K .......... .......... .......... .......... .......... 16% 10.2M 14s
45150K .......... .......... .......... .......... .......... 17% 155M 14s
45200K .......... .......... .......... .......... .......... 17% 11.7M 14s
45250K .......... .......... .......... .......... .......... 17% 185M 14s
45300K .......... .......... .......... .......... .......... 17% 17.5M 14s
45350K .......... .......... .......... .......... .......... 17% 28.3M 14s
45400K .......... .......... .......... .......... .......... 17% 22.4M 14s
45450K .......... .......... .......... .......... .......... 17% 15.6M 14s
45500K .......... .......... .......... .......... .......... 17% 15.8M 14s
45550K .......... .......... .......... .......... .......... 17% 16.2M 14s
45600K .......... .......... .......... .......... .......... 17% 11.3M 14s
45650K .......... .......... .......... .......... .......... 17% 12.6M 14s
45700K .......... .......... .......... .......... .......... 17% 13.5M 14s
45750K .......... .......... .......... .......... .......... 17% 13.9M 14s
45800K .......... .......... .......... .......... .......... 17% 9.49M 14s
45850K .......... .......... .......... .......... .......... 17% 14.2M 14s
45900K .......... .......... .......... .......... .......... 17% 12.6M 14s
45950K .......... .......... .......... .......... .......... 17% 13.4M 14s
46000K .......... .......... .......... .......... .......... 17% 15.6M 14s
46050K .......... .......... .......... .......... .......... 17% 12.4M 14s
46100K .......... .......... .......... .......... .......... 17% 9.28M 14s
46150K .......... .......... .......... .......... .......... 17% 13.4M 14s
46200K .......... .......... .......... .......... .......... 17% 12.0M 14s
46250K .......... .......... .......... .......... .......... 17% 11.6M 14s
46300K .......... .......... .......... .......... .......... 17% 9.79M 14s
46350K .......... .......... .......... .......... .......... 17% 48.2M 14s
46400K .......... .......... .......... .......... .......... 17% 18.5M 14s
46450K .......... .......... .......... .......... .......... 17% 16.2M 14s
46500K .......... .......... .......... .......... .......... 17% 18.0M 14s
46550K .......... .......... .......... .......... .......... 17% 18.6M 14s
46600K .......... .......... .......... .......... .......... 17% 17.5M 14s
46650K .......... .......... .......... .......... .......... 17% 25.0M 14s
46700K .......... .......... .......... .......... .......... 17% 20.5M 13s
46750K .......... .......... .......... .......... .......... 17% 23.4M 13s
46800K .......... .......... .......... .......... .......... 17% 25.2M 13s
46850K .......... .......... .......... .......... .......... 17% 19.5M 13s
46900K .......... .......... .......... .......... .......... 17% 17.5M 13s
46950K .......... .......... .......... .......... .......... 17% 23.6M 13s
47000K .......... .......... .......... .......... .......... 17% 23.9M 13s
47050K .......... .......... .......... .......... .......... 17% 22.6M 13s
47100K .......... .......... .......... .......... .......... 17% 21.0M 13s
47150K .......... .......... .......... .......... .......... 17% 22.8M 13s
47200K .......... .......... .......... .......... .......... 17% 27.2M 13s
47250K .......... .......... .......... .......... .......... 17% 23.6M 13s
47300K .......... .......... .......... .......... .......... 17% 63.0M 13s
47350K .......... .......... .......... .......... .......... 17% 45.0M 13s
47400K .......... .......... .......... .......... .......... 17% 16.7M 13s
47450K .......... .......... .......... .......... .......... 17% 164M 13s
47500K .......... .......... .......... .......... .......... 17% 157M 13s
47550K .......... .......... .......... .......... .......... 17% 14.3M 13s
47600K .......... .......... .......... .......... .......... 17% 16.0M 13s
47650K .......... .......... .......... .......... .......... 17% 97.7M 13s
47700K .......... .......... .......... .......... .......... 17% 14.4M 13s
47750K .......... .......... .......... .......... .......... 17% 15.8M 13s
47800K .......... .......... .......... .......... .......... 18% 7.29M 13s
47850K .......... .......... .......... .......... .......... 18% 44.4M 13s
47900K .......... .......... .......... .......... .......... 18% 24.6M 13s
47950K .......... .......... .......... .......... .......... 18% 15.3M 13s
48000K .......... .......... .......... .......... .......... 18% 23.8M 13s
48050K .......... .......... .......... .......... .......... 18% 25.3M 13s
48100K .......... .......... .......... .......... .......... 18% 21.0M 13s
48150K .......... .......... .......... .......... .......... 18% 17.3M 13s
48200K .......... .......... .......... .......... .......... 18% 21.3M 13s
48250K .......... .......... .......... .......... .......... 18% 23.1M 13s
48300K .......... .......... .......... .......... .......... 18% 18.7M 13s
48350K .......... .......... .......... .......... .......... 18% 19.0M 13s
48400K .......... .......... .......... .......... .......... 18% 45.7M 13s
48450K .......... .......... .......... .......... .......... 18% 32.3M 13s
48500K .......... .......... .......... .......... .......... 18% 34.7M 13s
48550K .......... .......... .......... .......... .......... 18% 15.4M 13s
48600K .......... .......... .......... .......... .......... 18% 104M 13s
48650K .......... .......... .......... .......... .......... 18% 40.0M 13s
48700K .......... .......... .......... .......... .......... 18% 33.6M 13s
48750K .......... .......... .......... .......... .......... 18% 24.3M 13s
48800K .......... .......... .......... .......... .......... 18% 14.0M 13s
48850K .......... .......... .......... .......... .......... 18% 138M 13s
48900K .......... .......... .......... .......... .......... 18% 24.8M 13s
48950K .......... .......... .......... .......... .......... 18% 22.3M 13s
49000K .......... .......... .......... .......... .......... 18% 23.7M 13s
49050K .......... .......... .......... .......... .......... 18% 31.9M 13s
49100K .......... .......... .......... .......... .......... 18% 20.8M 13s
49150K .......... .......... .......... .......... .......... 18% 13.0M 13s
49200K .......... .......... .......... .......... .......... 18% 25.7M 13s
49250K .......... .......... .......... .......... .......... 18% 31.6M 13s
49300K .......... .......... .......... .......... .......... 18% 19.9M 13s
49350K .......... .......... .......... .......... .......... 18% 23.7M 13s
49400K .......... .......... .......... .......... .......... 18% 27.7M 13s
49450K .......... .......... .......... .......... .......... 18% 23.4M 13s
49500K .......... .......... .......... .......... .......... 18% 24.7M 13s
49550K .......... .......... .......... .......... .......... 18% 25.6M 13s
49600K .......... .......... .......... .......... .......... 18% 37.2M 13s
49650K .......... .......... .......... .......... .......... 18% 17.5M 13s
49700K .......... .......... .......... .......... .......... 18% 7.43M 13s
49750K .......... .......... .......... .......... .......... 18% 15.9M 13s
49800K .......... .......... .......... .......... .......... 18% 12.1M 13s
49850K .......... .......... .......... .......... .......... 18% 11.6M 13s
49900K .......... .......... .......... .......... .......... 18% 13.8M 13s
49950K .......... .......... .......... .......... .......... 18% 13.6M 13s
50000K .......... .......... .......... .......... .......... 18% 13.4M 13s
50050K .......... .......... .......... .......... .......... 18% 12.7M 13s
50100K .......... .......... .......... .......... .......... 18% 11.3M 13s
50150K .......... .......... .......... .......... .......... 18% 12.6M 13s
50200K .......... .......... .......... .......... .......... 18% 9.19M 13s
50250K .......... .......... .......... .......... .......... 18% 6.85M 13s
50300K .......... .......... .......... .......... .......... 18% 9.57M 13s
50350K .......... .......... .......... .......... .......... 18% 10.8M 13s
50400K .......... .......... .......... .......... .......... 18% 11.6M 13s
50450K .......... .......... .......... .......... .......... 19% 9.01M 13s
50500K .......... .......... .......... .......... .......... 19% 8.57M 13s
50550K .......... .......... .......... .......... .......... 19% 12.4M 13s
50600K .......... .......... .......... .......... .......... 19% 9.06M 13s
50650K .......... .......... .......... .......... .......... 19% 9.06M 13s
50700K .......... .......... .......... .......... .......... 19% 4.70M 13s
50750K .......... .......... .......... .......... .......... 19% 5.67M 13s
50800K .......... .......... .......... .......... .......... 19% 5.57M 13s
50850K .......... .......... .......... .......... .......... 19% 5.91M 13s
50900K .......... .......... .......... .......... .......... 19% 6.21M 13s
50950K .......... .......... .......... .......... .......... 19% 5.36M 13s
51000K .......... .......... .......... .......... .......... 19% 11.0M 13s
51050K .......... .......... .......... .......... .......... 19% 6.26M 13s
51100K .......... .......... .......... .......... .......... 19% 156M 13s
51150K .......... .......... .......... .......... .......... 19% 11.0M 13s
51200K .......... .......... .......... .......... .......... 19% 14.5M 13s
51250K .......... .......... .......... .......... .......... 19% 10.6M 13s
51300K .......... .......... .......... .......... .......... 19% 10.3M 13s
51350K .......... .......... .......... .......... .......... 19% 17.3M 13s
51400K .......... .......... .......... .......... .......... 19% 16.1M 13s
51450K .......... .......... .......... .......... .......... 19% 12.5M 13s
51500K .......... .......... .......... .......... .......... 19% 12.5M 13s
51550K .......... .......... .......... .......... .......... 19% 13.8M 13s
51600K .......... .......... .......... .......... .......... 19% 12.0M 13s
51650K .......... .......... .......... .......... .......... 19% 12.6M 13s
51700K .......... .......... .......... .......... .......... 19% 12.2M 13s
51750K .......... .......... .......... .......... .......... 19% 12.2M 13s
51800K .......... .......... .......... .......... .......... 19% 13.4M 13s
51850K .......... .......... .......... .......... .......... 19% 12.2M 13s
51900K .......... .......... .......... .......... .......... 19% 15.2M 13s
51950K .......... .......... .......... .......... .......... 19% 13.6M 13s
52000K .......... .......... .......... .......... .......... 19% 8.45M 13s
52050K .......... .......... .......... .......... .......... 19% 24.4M 13s
52100K .......... .......... .......... .......... .......... 19% 32.6M 13s
52150K .......... .......... .......... .......... .......... 19% 27.7M 13s
52200K .......... .......... .......... .......... .......... 19% 15.7M 13s
52250K .......... .......... .......... .......... .......... 19% 11.0M 13s
52300K .......... .......... .......... .......... .......... 19% 21.1M 13s
52350K .......... .......... .......... .......... .......... 19% 11.4M 13s
52400K .......... .......... .......... .......... .......... 19% 10.2M 13s
52450K .......... .......... .......... .......... .......... 19% 9.41M 13s
52500K .......... .......... .......... .......... .......... 19% 14.1M 13s
52550K .......... .......... .......... .......... .......... 19% 12.2M 13s
52600K .......... .......... .......... .......... .......... 19% 10.2M 13s
52650K .......... .......... .......... .......... .......... 19% 12.9M 13s
52700K .......... .......... .......... .......... .......... 19% 6.61M 13s
52750K .......... .......... .......... .......... .......... 19% 11.1M 13s
52800K .......... .......... .......... .......... .......... 19% 13.1M 13s
52850K .......... .......... .......... .......... .......... 19% 17.2M 13s
52900K .......... .......... .......... .......... .......... 19% 19.2M 13s
52950K .......... .......... .......... .......... .......... 19% 12.4M 13s
53000K .......... .......... .......... .......... .......... 19% 11.4M 13s
53050K .......... .......... .......... .......... .......... 19% 15.2M 13s
53100K .......... .......... .......... .......... .......... 19% 19.5M 13s
53150K .......... .......... .......... .......... .......... 20% 8.69M 13s
53200K .......... .......... .......... .......... .......... 20% 10.3M 13s
53250K .......... .......... .......... .......... .......... 20% 14.0M 13s
53300K .......... .......... .......... .......... .......... 20% 14.5M 13s
53350K .......... .......... .......... .......... .......... 20% 13.7M 13s
53400K .......... .......... .......... .......... .......... 20% 12.5M 13s
53450K .......... .......... .......... .......... .......... 20% 15.1M 13s
53500K .......... .......... .......... .......... .......... 20% 12.0M 13s
53550K .......... .......... .......... .......... .......... 20% 15.5M 13s
53600K .......... .......... .......... .......... .......... 20% 22.5M 13s
53650K .......... .......... .......... .......... .......... 20% 20.9M 13s
53700K .......... .......... .......... .......... .......... 20% 8.61M 13s
53750K .......... .......... .......... .......... .......... 20% 209M 13s
53800K .......... .......... .......... .......... .......... 20% 17.8M 13s
53850K .......... .......... .......... .......... .......... 20% 12.1M 13s
53900K .......... .......... .......... .......... .......... 20% 30.7M 13s
53950K .......... .......... .......... .......... .......... 20% 17.6M 13s
54000K .......... .......... .......... .......... .......... 20% 23.6M 13s
54050K .......... .......... .......... .......... .......... 20% 28.1M 13s
54100K .......... .......... .......... .......... .......... 20% 16.3M 13s
54150K .......... .......... .......... .......... .......... 20% 25.6M 13s
54200K .......... .......... .......... .......... .......... 20% 17.0M 13s
54250K .......... .......... .......... .......... .......... 20% 24.1M 13s
54300K .......... .......... .......... .......... .......... 20% 23.9M 13s
54350K .......... .......... .......... .......... .......... 20% 20.2M 13s
54400K .......... .......... .......... .......... .......... 20% 27.1M 13s
54450K .......... .......... .......... .......... .......... 20% 17.8M 13s
54500K .......... .......... .......... .......... .......... 20% 22.7M 13s
54550K .......... .......... .......... .......... .......... 20% 24.9M 13s
54600K .......... .......... .......... .......... .......... 20% 19.9M 13s
54650K .......... .......... .......... .......... .......... 20% 31.7M 13s
54700K .......... .......... .......... .......... .......... 20% 18.1M 13s
54750K .......... .......... .......... .......... .......... 20% 11.1M 13s
54800K .......... .......... .......... .......... .......... 20% 425M 13s
54850K .......... .......... .......... .......... .......... 20% 20.2M 13s
54900K .......... .......... .......... .......... .......... 20% 13.4M 13s
54950K .......... .......... .......... .......... .......... 20% 332M 13s
55000K .......... .......... .......... .......... .......... 20% 22.4M 13s
55050K .......... .......... .......... .......... .......... 20% 15.7M 13s
55100K .......... .......... .......... .......... .......... 20% 68.5M 13s
55150K .......... .......... .......... .......... .......... 20% 18.1M 13s
55200K .......... .......... .......... .......... .......... 20% 17.0M 13s
55250K .......... .......... .......... .......... .......... 20% 15.6M 13s
55300K .......... .......... .......... .......... .......... 20% 20.4M 13s
55350K .......... .......... .......... .......... .......... 20% 14.1M 13s
55400K .......... .......... .......... .......... .......... 20% 15.6M 13s
55450K .......... .......... .......... .......... .......... 20% 12.0M 13s
55500K .......... .......... .......... .......... .......... 20% 9.41M 13s
55550K .......... .......... .......... .......... .......... 20% 14.8M 13s
55600K .......... .......... .......... .......... .......... 20% 9.01M 13s
55650K .......... .......... .......... .......... .......... 20% 10.9M 13s
55700K .......... .......... .......... .......... .......... 20% 12.0M 13s
55750K .......... .......... .......... .......... .......... 20% 25.1M 13s
55800K .......... .......... .......... .......... .......... 21% 13.6M 13s
55850K .......... .......... .......... .......... .......... 21% 21.9M 13s
55900K .......... .......... .......... .......... .......... 21% 34.2M 13s
55950K .......... .......... .......... .......... .......... 21% 21.9M 13s
56000K .......... .......... .......... .......... .......... 21% 23.8M 13s
56050K .......... .......... .......... .......... .......... 21% 17.7M 13s
56100K .......... .......... .......... .......... .......... 21% 13.1M 13s
56150K .......... .......... .......... .......... .......... 21% 19.9M 13s
56200K .......... .......... .......... .......... .......... 21% 11.7M 13s
56250K .......... .......... .......... .......... .......... 21% 16.2M 13s
56300K .......... .......... .......... .......... .......... 21% 16.1M 13s
56350K .......... .......... .......... .......... .......... 21% 7.95M 13s
56400K .......... .......... .......... .......... .......... 21% 13.6M 13s
56450K .......... .......... .......... .......... .......... 21% 11.6M 13s
56500K .......... .......... .......... .......... .......... 21% 9.15M 13s
56550K .......... .......... .......... .......... .......... 21% 10.2M 13s
56600K .......... .......... .......... .......... .......... 21% 14.1M 13s
56650K .......... .......... .......... .......... .......... 21% 15.1M 13s
56700K .......... .......... .......... .......... .......... 21% 11.8M 13s
56750K .......... .......... .......... .......... .......... 21% 29.3M 13s
56800K .......... .......... .......... .......... .......... 21% 18.2M 13s
56850K .......... .......... .......... .......... .......... 21% 13.4M 13s
56900K .......... .......... .......... .......... .......... 21% 18.2M 13s
56950K .......... .......... .......... .......... .......... 21% 13.8M 13s
57000K .......... .......... .......... .......... .......... 21% 15.9M 13s
57050K .......... .......... .......... .......... .......... 21% 17.6M 13s
57100K .......... .......... .......... .......... .......... 21% 14.0M 13s
57150K .......... .......... .......... .......... .......... 21% 14.0M 13s
57200K .......... .......... .......... .......... .......... 21% 14.4M 13s
57250K .......... .......... .......... .......... .......... 21% 18.8M 13s
57300K .......... .......... .......... .......... .......... 21% 10.2M 13s
57350K .......... .......... .......... .......... .......... 21% 9.67M 13s
57400K .......... .......... .......... .......... .......... 21% 8.11M 13s
57450K .......... .......... .......... .......... .......... 21% 4.30M 13s
57500K .......... .......... .......... .......... .......... 21% 21.0M 13s
57550K .......... .......... .......... .......... .......... 21% 20.6M 13s
57600K .......... .......... .......... .......... .......... 21% 11.6M 13s
57650K .......... .......... .......... .......... .......... 21% 15.0M 13s
57700K .......... .......... .......... .......... .......... 21% 13.5M 13s
57750K .......... .......... .......... .......... .......... 21% 16.7M 13s
57800K .......... .......... .......... .......... .......... 21% 13.0M 13s
57850K .......... .......... .......... .......... .......... 21% 30.6M 13s
57900K .......... .......... .......... .......... .......... 21% 21.7M 13s
57950K .......... .......... .......... .......... .......... 21% 22.1M 13s
58000K .......... .......... .......... .......... .......... 21% 29.5M 13s
58050K .......... .......... .......... .......... .......... 21% 23.8M 13s
58100K .......... .......... .......... .......... .......... 21% 24.4M 13s
58150K .......... .......... .......... .......... .......... 21% 24.1M 13s
58200K .......... .......... .......... .......... .......... 21% 19.6M 13s
58250K .......... .......... .......... .......... .......... 21% 29.8M 13s
58300K .......... .......... .......... .......... .......... 21% 24.7M 13s
58350K .......... .......... .......... .......... .......... 21% 23.2M 13s
58400K .......... .......... .......... .......... .......... 21% 25.7M 13s
58450K .......... .......... .......... .......... .......... 22% 25.3M 13s
58500K .......... .......... .......... .......... .......... 22% 33.5M 13s
58550K .......... .......... .......... .......... .......... 22% 25.0M 13s
58600K .......... .......... .......... .......... .......... 22% 21.1M 13s
58650K .......... .......... .......... .......... .......... 22% 22.3M 13s
58700K .......... .......... .......... .......... .......... 22% 22.4M 13s
58750K .......... .......... .......... .......... .......... 22% 47.3M 13s
58800K .......... .......... .......... .......... .......... 22% 31.0M 13s
58850K .......... .......... .......... .......... .......... 22% 31.3M 13s
58900K .......... .......... .......... .......... .......... 22% 125M 13s
58950K .......... .......... .......... .......... .......... 22% 25.4M 13s
59000K .......... .......... .......... .......... .......... 22% 14.0M 13s
59050K .......... .......... .......... .......... .......... 22% 537M 13s
59100K .......... .......... .......... .......... .......... 22% 30.8M 13s
59150K .......... .......... .......... .......... .......... 22% 13.2M 13s
59200K .......... .......... .......... .......... .......... 22% 91.1M 13s
59250K .......... .......... .......... .......... .......... 22% 25.6M 13s
59300K .......... .......... .......... .......... .......... 22% 72.0M 13s
59350K .......... .......... .......... .......... .......... 22% 11.2M 13s
59400K .......... .......... .......... .......... .......... 22% 54.0M 13s
59450K .......... .......... .......... .......... .......... 22% 14.1M 13s
59500K .......... .......... .......... .......... .......... 22% 15.8M 13s
59550K .......... .......... .......... .......... .......... 22% 17.7M 13s
59600K .......... .......... .......... .......... .......... 22% 15.2M 13s
59650K .......... .......... .......... .......... .......... 22% 16.0M 13s
59700K .......... .......... .......... .......... .......... 22% 16.0M 13s
59750K .......... .......... .......... .......... .......... 22% 17.2M 13s
59800K .......... .......... .......... .......... .......... 22% 16.6M 13s
59850K .......... .......... .......... .......... .......... 22% 13.4M 13s
59900K .......... .......... .......... .......... .......... 22% 16.3M 13s
59950K .......... .......... .......... .......... .......... 22% 8.03M 13s
60000K .......... .......... .......... .......... .......... 22% 8.24M 13s
60050K .......... .......... .......... .......... .......... 22% 136M 13s
60100K .......... .......... .......... .......... .......... 22% 7.72M 13s
60150K .......... .......... .......... .......... .......... 22% 10.5M 13s
60200K .......... .......... .......... .......... .......... 22% 10.9M 13s
60250K .......... .......... .......... .......... .......... 22% 15.6M 13s
60300K .......... .......... .......... .......... .......... 22% 6.20M 13s
60350K .......... .......... .......... .......... .......... 22% 14.6M 13s
60400K .......... .......... .......... .......... .......... 22% 16.5M 13s
60450K .......... .......... .......... .......... .......... 22% 25.4M 13s
60500K .......... .......... .......... .......... .......... 22% 15.6M 13s
60550K .......... .......... .......... .......... .......... 22% 26.7M 13s
60600K .......... .......... .......... .......... .......... 22% 32.0M 13s
60650K .......... .......... .......... .......... .......... 22% 46.2M 13s
60700K .......... .......... .......... .......... .......... 22% 47.4M 13s
60750K .......... .......... .......... .......... .......... 22% 64.8M 13s
60800K .......... .......... .......... .......... .......... 22% 45.7M 13s
60850K .......... .......... .......... .......... .......... 22% 18.2M 13s
60900K .......... .......... .......... .......... .......... 22% 45.2M 13s
60950K .......... .......... .......... .......... .......... 22% 341M 13s
61000K .......... .......... .......... .......... .......... 22% 31.7M 13s
61050K .......... .......... .......... .......... .......... 22% 448M 13s
61100K .......... .......... .......... .......... .......... 23% 22.0M 13s
61150K .......... .......... .......... .......... .......... 23% 208M 13s
61200K .......... .......... .......... .......... .......... 23% 25.0M 13s
61250K .......... .......... .......... .......... .......... 23% 48.6M 13s
61300K .......... .......... .......... .......... .......... 23% 26.9M 13s
61350K .......... .......... .......... .......... .......... 23% 27.5M 13s
61400K .......... .......... .......... .......... .......... 23% 37.0M 13s
61450K .......... .......... .......... .......... .......... 23% 26.0M 13s
61500K .......... .......... .......... .......... .......... 23% 47.3M 13s
61550K .......... .......... .......... .......... .......... 23% 19.1M 13s
61600K .......... .......... .......... .......... .......... 23% 34.9M 13s
61650K .......... .......... .......... .......... .......... 23% 23.3M 13s
61700K .......... .......... .......... .......... .......... 23% 21.6M 13s
61750K .......... .......... .......... .......... .......... 23% 25.3M 13s
61800K .......... .......... .......... .......... .......... 23% 29.4M 13s
61850K .......... .......... .......... .......... .......... 23% 19.4M 13s
61900K .......... .......... .......... .......... .......... 23% 22.9M 12s
61950K .......... .......... .......... .......... .......... 23% 26.5M 12s
62000K .......... .......... .......... .......... .......... 23% 16.3M 12s
62050K .......... .......... .......... .......... .......... 23% 17.4M 12s
62100K .......... .......... .......... .......... .......... 23% 14.1M 12s
62150K .......... .......... .......... .......... .......... 23% 13.2M 12s
62200K .......... .......... .......... .......... .......... 23% 12.2M 12s
62250K .......... .......... .......... .......... .......... 23% 15.7M 12s
62300K .......... .......... .......... .......... .......... 23% 10.6M 12s
62350K .......... .......... .......... .......... .......... 23% 13.8M 12s
62400K .......... .......... .......... .......... .......... 23% 111M 12s
62450K .......... .......... .......... .......... .......... 23% 15.5M 12s
62500K .......... .......... .......... .......... .......... 23% 27.1M 12s
62550K .......... .......... .......... .......... .......... 23% 18.0M 12s
62600K .......... .......... .......... .......... .......... 23% 23.8M 12s
62650K .......... .......... .......... .......... .......... 23% 23.5M 12s
62700K .......... .......... .......... .......... .......... 23% 16.0M 12s
62750K .......... .......... .......... .......... .......... 23% 13.5M 12s
62800K .......... .......... .......... .......... .......... 23% 22.9M 12s
62850K .......... .......... .......... .......... .......... 23% 13.2M 12s
62900K .......... .......... .......... .......... .......... 23% 14.4M 12s
62950K .......... .......... .......... .......... .......... 23% 15.9M 12s
63000K .......... .......... .......... .......... .......... 23% 16.4M 12s
63050K .......... .......... .......... .......... .......... 23% 16.4M 12s
63100K .......... .......... .......... .......... .......... 23% 13.4M 12s
63150K .......... .......... .......... .......... .......... 23% 10.6M 12s
63200K .......... .......... .......... .......... .......... 23% 11.9M 12s
63250K .......... .......... .......... .......... .......... 23% 9.24M 12s
63300K .......... .......... .......... .......... .......... 23% 8.95M 12s
63350K .......... .......... .......... .......... .......... 23% 8.04M 12s
63400K .......... .......... .......... .......... .......... 23% 11.7M 12s
63450K .......... .......... .......... .......... .......... 23% 12.7M 12s
63500K .......... .......... .......... .......... .......... 23% 13.0M 12s
63550K .......... .......... .......... .......... .......... 23% 14.7M 12s
63600K .......... .......... .......... .......... .......... 23% 13.4M 12s
63650K .......... .......... .......... .......... .......... 23% 12.1M 12s
63700K .......... .......... .......... .......... .......... 23% 18.4M 12s
63750K .......... .......... .......... .......... .......... 24% 42.6M 12s
63800K .......... .......... .......... .......... .......... 24% 46.4M 12s
63850K .......... .......... .......... .......... .......... 24% 37.8M 12s
63900K .......... .......... .......... .......... .......... 24% 20.0M 12s
63950K .......... .......... .......... .......... .......... 24% 161M 12s
64000K .......... .......... .......... .......... .......... 24% 34.2M 12s
64050K .......... .......... .......... .......... .......... 24% 35.4M 12s
64100K .......... .......... .......... .......... .......... 24% 23.9M 12s
64150K .......... .......... .......... .......... .......... 24% 17.2M 12s
64200K .......... .......... .......... .......... .......... 24% 13.2M 12s
64250K .......... .......... .......... .......... .......... 24% 10.3M 12s
64300K .......... .......... .......... .......... .......... 24% 17.1M 12s
64350K .......... .......... .......... .......... .......... 24% 12.9M 12s
64400K .......... .......... .......... .......... .......... 24% 18.6M 12s
64450K .......... .......... .......... .......... .......... 24% 16.3M 12s
64500K .......... .......... .......... .......... .......... 24% 21.0M 12s
64550K .......... .......... .......... .......... .......... 24% 19.0M 12s
64600K .......... .......... .......... .......... .......... 24% 11.7M 12s
64650K .......... .......... .......... .......... .......... 24% 10.5M 12s
64700K .......... .......... .......... .......... .......... 24% 12.1M 12s
64750K .......... .......... .......... .......... .......... 24% 16.5M 12s
64800K .......... .......... .......... .......... .......... 24% 8.60M 12s
64850K .......... .......... .......... .......... .......... 24% 13.3M 12s
64900K .......... .......... .......... .......... .......... 24% 14.2M 12s
64950K .......... .......... .......... .......... .......... 24% 15.0M 12s
65000K .......... .......... .......... .......... .......... 24% 16.4M 12s
65050K .......... .......... .......... .......... .......... 24% 19.4M 12s
65100K .......... .......... .......... .......... .......... 24% 17.0M 12s
65150K .......... .......... .......... .......... .......... 24% 18.3M 12s
65200K .......... .......... .......... .......... .......... 24% 15.5M 12s
65250K .......... .......... .......... .......... .......... 24% 17.5M 12s
65300K .......... .......... .......... .......... .......... 24% 18.2M 12s
65350K .......... .......... .......... .......... .......... 24% 20.0M 12s
65400K .......... .......... .......... .......... .......... 24% 13.9M 12s
65450K .......... .......... .......... .......... .......... 24% 17.5M 12s
65500K .......... .......... .......... .......... .......... 24% 13.8M 12s
65550K .......... .......... .......... .......... .......... 24% 37.6M 12s
65600K .......... .......... .......... .......... .......... 24% 38.3M 12s
65650K .......... .......... .......... .......... .......... 24% 37.5M 12s
65700K .......... .......... .......... .......... .......... 24% 27.4M 12s
65750K .......... .......... .......... .......... .......... 24% 26.4M 12s
65800K .......... .......... .......... .......... .......... 24% 15.4M 12s
65850K .......... .......... .......... .......... .......... 24% 35.3M 12s
65900K .......... .......... .......... .......... .......... 24% 16.5M 12s
65950K .......... .......... .......... .......... .......... 24% 14.2M 12s
66000K .......... .......... .......... .......... .......... 24% 12.5M 12s
66050K .......... .......... .......... .......... .......... 24% 12.2M 12s
66100K .......... .......... .......... .......... .......... 24% 8.90M 12s
66150K .......... .......... .......... .......... .......... 24% 12.6M 12s
66200K .......... .......... .......... .......... .......... 24% 8.97M 12s
66250K .......... .......... .......... .......... .......... 24% 13.7M 12s
66300K .......... .......... .......... .......... .......... 24% 12.3M 12s
66350K .......... .......... .......... .......... .......... 24% 8.10M 12s
66400K .......... .......... .......... .......... .......... 25% 19.8M 12s
66450K .......... .......... .......... .......... .......... 25% 19.4M 12s
66500K .......... .......... .......... .......... .......... 25% 20.4M 12s
66550K .......... .......... .......... .......... .......... 25% 191M 12s
66600K .......... .......... .......... .......... .......... 25% 16.8M 12s
66650K .......... .......... .......... .......... .......... 25% 16.0M 12s
66700K .......... .......... .......... .......... .......... 25% 14.5M 12s
66750K .......... .......... .......... .......... .......... 25% 12.5M 12s
66800K .......... .......... .......... .......... .......... 25% 12.5M 12s
66850K .......... .......... .......... .......... .......... 25% 12.7M 12s
66900K .......... .......... .......... .......... .......... 25% 13.1M 12s
66950K .......... .......... .......... .......... .......... 25% 12.9M 12s
67000K .......... .......... .......... .......... .......... 25% 16.0M 12s
67050K .......... .......... .......... .......... .......... 25% 12.6M 12s
67100K .......... .......... .......... .......... .......... 25% 11.0M 12s
67150K .......... .......... .......... .......... .......... 25% 12.2M 12s
67200K .......... .......... .......... .......... .......... 25% 11.8M 12s
67250K .......... .......... .......... .......... .......... 25% 12.7M 12s
67300K .......... .......... .......... .......... .......... 25% 12.2M 12s
67350K .......... .......... .......... .......... .......... 25% 9.59M 12s
67400K .......... .......... .......... .......... .......... 25% 12.5M 12s
67450K .......... .......... .......... .......... .......... 25% 7.98M 12s
67500K .......... .......... .......... .......... .......... 25% 46.1M 12s
67550K .......... .......... .......... .......... .......... 25% 21.4M 12s
67600K .......... .......... .......... .......... .......... 25% 12.0M 12s
67650K .......... .......... .......... .......... .......... 25% 26.8M 12s
67700K .......... .......... .......... .......... .......... 25% 15.1M 12s
67750K .......... .......... .......... .......... .......... 25% 20.8M 12s
67800K .......... .......... .......... .......... .......... 25% 14.7M 12s
67850K .......... .......... .......... .......... .......... 25% 10.8M 12s
67900K .......... .......... .......... .......... .......... 25% 14.1M 12s
67950K .......... .......... .......... .......... .......... 25% 13.6M 12s
68000K .......... .......... .......... .......... .......... 25% 13.1M 12s
68050K .......... .......... .......... .......... .......... 25% 13.7M 12s
68100K .......... .......... .......... .......... .......... 25% 10.6M 12s
68150K .......... .......... .......... .......... .......... 25% 9.06M 12s
68200K .......... .......... .......... .......... .......... 25% 20.2M 12s
68250K .......... .......... .......... .......... .......... 25% 18.6M 12s
68300K .......... .......... .......... .......... .......... 25% 9.83M 12s
68350K .......... .......... .......... .......... .......... 25% 72.9M 12s
68400K .......... .......... .......... .......... .......... 25% 10.3M 12s
68450K .......... .......... .......... .......... .......... 25% 64.1M 12s
68500K .......... .......... .......... .......... .......... 25% 15.6M 12s
68550K .......... .......... .......... .......... .......... 25% 19.8M 12s
68600K .......... .......... .......... .......... .......... 25% 14.2M 12s
68650K .......... .......... .......... .......... .......... 25% 11.7M 12s
68700K .......... .......... .......... .......... .......... 25% 11.9M 12s
68750K .......... .......... .......... .......... .......... 25% 25.1M 12s
68800K .......... .......... .......... .......... .......... 25% 17.4M 12s
68850K .......... .......... .......... .......... .......... 25% 19.1M 12s
68900K .......... .......... .......... .......... .......... 25% 19.6M 12s
68950K .......... .......... .......... .......... .......... 25% 16.7M 12s
69000K .......... .......... .......... .......... .......... 25% 17.0M 12s
69050K .......... .......... .......... .......... .......... 25% 17.3M 12s
69100K .......... .......... .......... .......... .......... 26% 6.76M 12s
69150K .......... .......... .......... .......... .......... 26% 15.6M 12s
69200K .......... .......... .......... .......... .......... 26% 15.2M 12s
69250K .......... .......... .......... .......... .......... 26% 14.1M 12s
69300K .......... .......... .......... .......... .......... 26% 22.2M 12s
69350K .......... .......... .......... .......... .......... 26% 13.4M 12s
69400K .......... .......... .......... .......... .......... 26% 16.1M 12s
69450K .......... .......... .......... .......... .......... 26% 12.8M 12s
69500K .......... .......... .......... .......... .......... 26% 16.9M 12s
69550K .......... .......... .......... .......... .......... 26% 12.4M 12s
69600K .......... .......... .......... .......... .......... 26% 15.7M 12s
69650K .......... .......... .......... .......... .......... 26% 15.5M 12s
69700K .......... .......... .......... .......... .......... 26% 13.9M 12s
69750K .......... .......... .......... .......... .......... 26% 15.6M 12s
69800K .......... .......... .......... .......... .......... 26% 19.6M 12s
69850K .......... .......... .......... .......... .......... 26% 10.1M 12s
69900K .......... .......... .......... .......... .......... 26% 35.3M 12s
69950K .......... .......... .......... .......... .......... 26% 16.1M 12s
70000K .......... .......... .......... .......... .......... 26% 21.4M 12s
70050K .......... .......... .......... .......... .......... 26% 34.2M 12s
70100K .......... .......... .......... .......... .......... 26% 17.6M 12s
70150K .......... .......... .......... .......... .......... 26% 16.2M 12s
70200K .......... .......... .......... .......... .......... 26% 19.7M 12s
70250K .......... .......... .......... .......... .......... 26% 14.2M 12s
70300K .......... .......... .......... .......... .......... 26% 20.0M 12s
70350K .......... .......... .......... .......... .......... 26% 14.1M 12s
70400K .......... .......... .......... .......... .......... 26% 17.4M 12s
70450K .......... .......... .......... .......... .......... 26% 12.6M 12s
70500K .......... .......... .......... .......... .......... 26% 22.8M 12s
70550K .......... .......... .......... .......... .......... 26% 16.4M 12s
70600K .......... .......... .......... .......... .......... 26% 17.7M 12s
70650K .......... .......... .......... .......... .......... 26% 16.6M 12s
70700K .......... .......... .......... .......... .......... 26% 12.8M 12s
70750K .......... .......... .......... .......... .......... 26% 20.9M 12s
70800K .......... .......... .......... .......... .......... 26% 18.8M 12s
70850K .......... .......... .......... .......... .......... 26% 9.57M 12s
70900K .......... .......... .......... .......... .......... 26% 22.4M 12s
70950K .......... .......... .......... .......... .......... 26% 18.1M 12s
71000K .......... .......... .......... .......... .......... 26% 15.1M 12s
71050K .......... .......... .......... .......... .......... 26% 13.3M 12s
71100K .......... .......... .......... .......... .......... 26% 21.6M 12s
71150K .......... .......... .......... .......... .......... 26% 23.6M 12s
71200K .......... .......... .......... .......... .......... 26% 18.0M 12s
71250K .......... .......... .......... .......... .......... 26% 25.6M 12s
71300K .......... .......... .......... .......... .......... 26% 19.9M 12s
71350K .......... .......... .......... .......... .......... 26% 22.6M 12s
71400K .......... .......... .......... .......... .......... 26% 26.2M 12s
71450K .......... .......... .......... .......... .......... 26% 18.4M 12s
71500K .......... .......... .......... .......... .......... 26% 21.8M 12s
71550K .......... .......... .......... .......... .......... 26% 20.9M 12s
71600K .......... .......... .......... .......... .......... 26% 19.4M 12s
71650K .......... .......... .......... .......... .......... 26% 21.0M 12s
71700K .......... .......... .......... .......... .......... 26% 17.8M 12s
71750K .......... .......... .......... .......... .......... 27% 18.7M 12s
71800K .......... .......... .......... .......... .......... 27% 20.1M 12s
71850K .......... .......... .......... .......... .......... 27% 16.3M 12s
71900K .......... .......... .......... .......... .......... 27% 8.45M 12s
71950K .......... .......... .......... .......... .......... 27% 32.9M 12s
72000K .......... .......... .......... .......... .......... 27% 13.3M 12s
72050K .......... .......... .......... .......... .......... 27% 25.5M 12s
72100K .......... .......... .......... .......... .......... 27% 7.94M 12s
72150K .......... .......... .......... .......... .......... 27% 183M 12s
72200K .......... .......... .......... .......... .......... 27% 11.4M 12s
72250K .......... .......... .......... .......... .......... 27% 18.9M 12s
72300K .......... .......... .......... .......... .......... 27% 23.6M 12s
72350K .......... .......... .......... .......... .......... 27% 15.6M 12s
72400K .......... .......... .......... .......... .......... 27% 21.9M 12s
72450K .......... .......... .......... .......... .......... 27% 17.2M 12s
72500K .......... .......... .......... .......... .......... 27% 20.1M 12s
72550K .......... .......... .......... .......... .......... 27% 17.6M 12s
72600K .......... .......... .......... .......... .......... 27% 16.7M 12s
72650K .......... .......... .......... .......... .......... 27% 17.2M 12s
72700K .......... .......... .......... .......... .......... 27% 13.6M 12s
72750K .......... .......... .......... .......... .......... 27% 16.2M 12s
72800K .......... .......... .......... .......... .......... 27% 12.5M 12s
72850K .......... .......... .......... .......... .......... 27% 15.6M 12s
72900K .......... .......... .......... .......... .......... 27% 19.0M 12s
72950K .......... .......... .......... .......... .......... 27% 17.7M 12s
73000K .......... .......... .......... .......... .......... 27% 16.8M 12s
73050K .......... .......... .......... .......... .......... 27% 127M 12s
73100K .......... .......... .......... .......... .......... 27% 8.61M 12s
73150K .......... .......... .......... .......... .......... 27% 24.5M 12s
73200K .......... .......... .......... .......... .......... 27% 43.8M 12s
73250K .......... .......... .......... .......... .......... 27% 11.3M 12s
73300K .......... .......... .......... .......... .......... 27% 28.4M 12s
73350K .......... .......... .......... .......... .......... 27% 22.5M 12s
73400K .......... .......... .......... .......... .......... 27% 17.1M 12s
73450K .......... .......... .......... .......... .......... 27% 19.9M 12s
73500K .......... .......... .......... .......... .......... 27% 23.3M 12s
73550K .......... .......... .......... .......... .......... 27% 22.2M 12s
73600K .......... .......... .......... .......... .......... 27% 18.6M 12s
73650K .......... .......... .......... .......... .......... 27% 26.8M 12s
73700K .......... .......... .......... .......... .......... 27% 10.6M 12s
73750K .......... .......... .......... .......... .......... 27% 23.8M 12s
73800K .......... .......... .......... .......... .......... 27% 14.0M 12s
73850K .......... .......... .......... .......... .......... 27% 16.9M 12s
73900K .......... .......... .......... .......... .......... 27% 20.9M 12s
73950K .......... .......... .......... .......... .......... 27% 18.1M 12s
74000K .......... .......... .......... .......... .......... 27% 17.5M 12s
74050K .......... .......... .......... .......... .......... 27% 21.3M 12s
74100K .......... .......... .......... .......... .......... 27% 15.1M 12s
74150K .......... .......... .......... .......... .......... 27% 13.2M 12s
74200K .......... .......... .......... .......... .......... 27% 11.5M 12s
74250K .......... .......... .......... .......... .......... 27% 7.86M 12s
74300K .......... .......... .......... .......... .......... 27% 13.6M 12s
74350K .......... .......... .......... .......... .......... 27% 9.53M 12s
74400K .......... .......... .......... .......... .......... 28% 14.7M 12s
74450K .......... .......... .......... .......... .......... 28% 21.2M 12s
74500K .......... .......... .......... .......... .......... 28% 16.6M 12s
74550K .......... .......... .......... .......... .......... 28% 26.3M 12s
74600K .......... .......... .......... .......... .......... 28% 16.3M 12s
74650K .......... .......... .......... .......... .......... 28% 26.6M 12s
74700K .......... .......... .......... .......... .......... 28% 18.7M 12s
74750K .......... .......... .......... .......... .......... 28% 20.2M 12s
74800K .......... .......... .......... .......... .......... 28% 32.4M 12s
74850K .......... .......... .......... .......... .......... 28% 14.1M 12s
74900K .......... .......... .......... .......... .......... 28% 24.6M 12s
74950K .......... .......... .......... .......... .......... 28% 16.7M 12s
75000K .......... .......... .......... .......... .......... 28% 25.7M 12s
75050K .......... .......... .......... .......... .......... 28% 16.6M 12s
75100K .......... .......... .......... .......... .......... 28% 21.9M 12s
75150K .......... .......... .......... .......... .......... 28% 18.8M 12s
75200K .......... .......... .......... .......... .......... 28% 17.4M 12s
75250K .......... .......... .......... .......... .......... 28% 21.7M 12s
75300K .......... .......... .......... .......... .......... 28% 19.6M 12s
75350K .......... .......... .......... .......... .......... 28% 11.4M 12s
75400K .......... .......... .......... .......... .......... 28% 8.30M 12s
75450K .......... .......... .......... .......... .......... 28% 17.3M 12s
75500K .......... .......... .......... .......... .......... 28% 17.3M 12s
75550K .......... .......... .......... .......... .......... 28% 11.3M 12s
75600K .......... .......... .......... .......... .......... 28% 28.2M 12s
75650K .......... .......... .......... .......... .......... 28% 17.3M 12s
75700K .......... .......... .......... .......... .......... 28% 31.6M 12s
75750K .......... .......... .......... .......... .......... 28% 27.2M 12s
75800K .......... .......... .......... .......... .......... 28% 30.9M 12s
75850K .......... .......... .......... .......... .......... 28% 26.5M 12s
75900K .......... .......... .......... .......... .......... 28% 36.2M 12s
75950K .......... .......... .......... .......... .......... 28% 24.1M 12s
76000K .......... .......... .......... .......... .......... 28% 29.8M 12s
76050K .......... .......... .......... .......... .......... 28% 23.9M 12s
76100K .......... .......... .......... .......... .......... 28% 16.5M 12s
76150K .......... .......... .......... .......... .......... 28% 15.5M 12s
76200K .......... .......... .......... .......... .......... 28% 24.3M 12s
76250K .......... .......... .......... .......... .......... 28% 31.5M 12s
76300K .......... .......... .......... .......... .......... 28% 19.3M 12s
76350K .......... .......... .......... .......... .......... 28% 19.4M 12s
76400K .......... .......... .......... .......... .......... 28% 41.1M 12s
76450K .......... .......... .......... .......... .......... 28% 18.6M 12s
76500K .......... .......... .......... .......... .......... 28% 22.8M 12s
76550K .......... .......... .......... .......... .......... 28% 20.0M 12s
76600K .......... .......... .......... .......... .......... 28% 21.7M 12s
76650K .......... .......... .......... .......... .......... 28% 25.5M 12s
76700K .......... .......... .......... .......... .......... 28% 21.9M 12s
76750K .......... .......... .......... .......... .......... 28% 21.9M 12s
76800K .......... .......... .......... .......... .......... 28% 22.2M 12s
76850K .......... .......... .......... .......... .......... 28% 21.7M 12s
76900K .......... .......... .......... .......... .......... 28% 22.6M 12s
76950K .......... .......... .......... .......... .......... 28% 21.9M 12s
77000K .......... .......... .......... .......... .......... 28% 24.2M 12s
77050K .......... .......... .......... .......... .......... 29% 28.9M 12s
77100K .......... .......... .......... .......... .......... 29% 19.9M 11s
77150K .......... .......... .......... .......... .......... 29% 27.6M 11s
77200K .......... .......... .......... .......... .......... 29% 10.3M 11s
77250K .......... .......... .......... .......... .......... 29% 171M 11s
77300K .......... .......... .......... .......... .......... 29% 12.1M 11s
77350K .......... .......... .......... .......... .......... 29% 127M 11s
77400K .......... .......... .......... .......... .......... 29% 17.4M 11s
77450K .......... .......... .......... .......... .......... 29% 14.7M 11s
77500K .......... .......... .......... .......... .......... 29% 18.4M 11s
77550K .......... .......... .......... .......... .......... 29% 19.6M 11s
77600K .......... .......... .......... .......... .......... 29% 21.4M 11s
77650K .......... .......... .......... .......... .......... 29% 21.6M 11s
77700K .......... .......... .......... .......... .......... 29% 10.4M 11s
77750K .......... .......... .......... .......... .......... 29% 14.9M 11s
77800K .......... .......... .......... .......... .......... 29% 11.6M 11s
77850K .......... .......... .......... .......... .......... 29% 8.64M 11s
77900K .......... .......... .......... .......... .......... 29% 14.1M 11s
77950K .......... .......... .......... .......... .......... 29% 10.8M 11s
78000K .......... .......... .......... .......... .......... 29% 9.24M 11s
78050K .......... .......... .......... .......... .......... 29% 7.26M 11s
78100K .......... .......... .......... .......... .......... 29% 5.85M 11s
78150K .......... .......... .......... .......... .......... 29% 18.7M 11s
78200K .......... .......... .......... .......... .......... 29% 7.16M 11s
78250K .......... .......... .......... .......... .......... 29% 12.2M 11s
78300K .......... .......... .......... .......... .......... 29% 13.2M 11s
78350K .......... .......... .......... .......... .......... 29% 10.5M 11s
78400K .......... .......... .......... .......... .......... 29% 12.0M 11s
78450K .......... .......... .......... .......... .......... 29% 10.2M 11s
78500K .......... .......... .......... .......... .......... 29% 11.6M 11s
78550K .......... .......... .......... .......... .......... 29% 11.0M 11s
78600K .......... .......... .......... .......... .......... 29% 10.2M 11s
78650K .......... .......... .......... .......... .......... 29% 6.32M 11s
78700K .......... .......... .......... .......... .......... 29% 16.3M 11s
78750K .......... .......... .......... .......... .......... 29% 11.9M 11s
78800K .......... .......... .......... .......... .......... 29% 12.1M 11s
78850K .......... .......... .......... .......... .......... 29% 11.7M 11s
78900K .......... .......... .......... .......... .......... 29% 11.2M 11s
78950K .......... .......... .......... .......... .......... 29% 9.40M 11s
79000K .......... .......... .......... .......... .......... 29% 11.1M 11s
79050K .......... .......... .......... .......... .......... 29% 13.7M 11s
79100K .......... .......... .......... .......... .......... 29% 9.22M 11s
79150K .......... .......... .......... .......... .......... 29% 10.6M 11s
79200K .......... .......... .......... .......... .......... 29% 16.0M 11s
79250K .......... .......... .......... .......... .......... 29% 16.5M 11s
79300K .......... .......... .......... .......... .......... 29% 26.0M 11s
79350K .......... .......... .......... .......... .......... 29% 14.8M 11s
79400K .......... .......... .......... .......... .......... 29% 20.6M 11s
79450K .......... .......... .......... .......... .......... 29% 13.6M 11s
79500K .......... .......... .......... .......... .......... 29% 23.4M 11s
79550K .......... .......... .......... .......... .......... 29% 17.8M 11s
79600K .......... .......... .......... .......... .......... 29% 22.3M 11s
79650K .......... .......... .......... .......... .......... 29% 29.3M 11s
79700K .......... .......... .......... .......... .......... 30% 14.3M 11s
79750K .......... .......... .......... .......... .......... 30% 25.3M 11s
79800K .......... .......... .......... .......... .......... 30% 18.3M 11s
79850K .......... .......... .......... .......... .......... 30% 19.8M 11s
79900K .......... .......... .......... .......... .......... 30% 18.2M 11s
79950K .......... .......... .......... .......... .......... 30% 14.5M 11s
80000K .......... .......... .......... .......... .......... 30% 19.8M 11s
80050K .......... .......... .......... .......... .......... 30% 19.3M 11s
80100K .......... .......... .......... .......... .......... 30% 18.1M 11s
80150K .......... .......... .......... .......... .......... 30% 17.6M 11s
80200K .......... .......... .......... .......... .......... 30% 19.0M 11s
80250K .......... .......... .......... .......... .......... 30% 23.9M 11s
80300K .......... .......... .......... .......... .......... 30% 26.6M 11s
80350K .......... .......... .......... .......... .......... 30% 24.5M 11s
80400K .......... .......... .......... .......... .......... 30% 9.33M 11s
80450K .......... .......... .......... .......... .......... 30% 142M 11s
80500K .......... .......... .......... .......... .......... 30% 36.2M 11s
80550K .......... .......... .......... .......... .......... 30% 45.9M 11s
80600K .......... .......... .......... .......... .......... 30% 13.4M 11s
80650K .......... .......... .......... .......... .......... 30% 49.5M 11s
80700K .......... .......... .......... .......... .......... 30% 19.4M 11s
80750K .......... .......... .......... .......... .......... 30% 29.9M 11s
80800K .......... .......... .......... .......... .......... 30% 29.9M 11s
80850K .......... .......... .......... .......... .......... 30% 32.3M 11s
80900K .......... .......... .......... .......... .......... 30% 36.9M 11s
80950K .......... .......... .......... .......... .......... 30% 24.9M 11s
81000K .......... .......... .......... .......... .......... 30% 32.6M 11s
81050K .......... .......... .......... .......... .......... 30% 35.0M 11s
81100K .......... .......... .......... .......... .......... 30% 18.1M 11s
81150K .......... .......... .......... .......... .......... 30% 13.1M 11s
81200K .......... .......... .......... .......... .......... 30% 113M 11s
81250K .......... .......... .......... .......... .......... 30% 17.4M 11s
81300K .......... .......... .......... .......... .......... 30% 21.5M 11s
81350K .......... .......... .......... .......... .......... 30% 24.6M 11s
81400K .......... .......... .......... .......... .......... 30% 21.7M 11s
81450K .......... .......... .......... .......... .......... 30% 22.2M 11s
81500K .......... .......... .......... .......... .......... 30% 7.30M 11s
81550K .......... .......... .......... .......... .......... 30% 6.74M 11s
81600K .......... .......... .......... .......... .......... 30% 8.82M 11s
81650K .......... .......... .......... .......... .......... 30% 21.8M 11s
81700K .......... .......... .......... .......... .......... 30% 15.9M 11s
81750K .......... .......... .......... .......... .......... 30% 7.27M 11s
81800K .......... .......... .......... .......... .......... 30% 307M 11s
81850K .......... .......... .......... .......... .......... 30% 12.4M 11s
81900K .......... .......... .......... .......... .......... 30% 14.3M 11s
81950K .......... .......... .......... .......... .......... 30% 11.0M 11s
82000K .......... .......... .......... .......... .......... 30% 76.1M 11s
82050K .......... .......... .......... .......... .......... 30% 11.7M 11s
82100K .......... .......... .......... .......... .......... 30% 10.5M 11s
82150K .......... .......... .......... .......... .......... 30% 17.6M 11s
82200K .......... .......... .......... .......... .......... 30% 12.2M 11s
82250K .......... .......... .......... .......... .......... 30% 15.8M 11s
82300K .......... .......... .......... .......... .......... 30% 13.7M 11s
82350K .......... .......... .......... .......... .......... 31% 13.6M 11s
82400K .......... .......... .......... .......... .......... 31% 13.3M 11s
82450K .......... .......... .......... .......... .......... 31% 15.6M 11s
82500K .......... .......... .......... .......... .......... 31% 16.0M 11s
82550K .......... .......... .......... .......... .......... 31% 13.1M 11s
82600K .......... .......... .......... .......... .......... 31% 10.9M 11s
82650K .......... .......... .......... .......... .......... 31% 48.2M 11s
82700K .......... .......... .......... .......... .......... 31% 14.9M 11s
82750K .......... .......... .......... .......... .......... 31% 8.82M 11s
82800K .......... .......... .......... .......... .......... 31% 16.1M 11s
82850K .......... .......... .......... .......... .......... 31% 11.3M 11s
82900K .......... .......... .......... .......... .......... 31% 12.6M 11s
82950K .......... .......... .......... .......... .......... 31% 12.5M 11s
83000K .......... .......... .......... .......... .......... 31% 17.2M 11s
83050K .......... .......... .......... .......... .......... 31% 16.2M 11s
83100K .......... .......... .......... .......... .......... 31% 10.9M 11s
83150K .......... .......... .......... .......... .......... 31% 17.4M 11s
83200K .......... .......... .......... .......... .......... 31% 12.8M 11s
83250K .......... .......... .......... .......... .......... 31% 13.7M 11s
83300K .......... .......... .......... .......... .......... 31% 14.2M 11s
83350K .......... .......... .......... .......... .......... 31% 11.3M 11s
83400K .......... .......... .......... .......... .......... 31% 16.5M 11s
83450K .......... .......... .......... .......... .......... 31% 15.7M 11s
83500K .......... .......... .......... .......... .......... 31% 19.2M 11s
83550K .......... .......... .......... .......... .......... 31% 21.2M 11s
83600K .......... .......... .......... .......... .......... 31% 16.8M 11s
83650K .......... .......... .......... .......... .......... 31% 19.1M 11s
83700K .......... .......... .......... .......... .......... 31% 17.4M 11s
83750K .......... .......... .......... .......... .......... 31% 24.0M 11s
83800K .......... .......... .......... .......... .......... 31% 16.7M 11s
83850K .......... .......... .......... .......... .......... 31% 15.4M 11s
83900K .......... .......... .......... .......... .......... 31% 23.7M 11s
83950K .......... .......... .......... .......... .......... 31% 22.7M 11s
84000K .......... .......... .......... .......... .......... 31% 54.5M 11s
84050K .......... .......... .......... .......... .......... 31% 17.2M 11s
84100K .......... .......... .......... .......... .......... 31% 41.4M 11s
84150K .......... .......... .......... .......... .......... 31% 24.2M 11s
84200K .......... .......... .......... .......... .......... 31% 440M 11s
84250K .......... .......... .......... .......... .......... 31% 13.6M 11s
84300K .......... .......... .......... .......... .......... 31% 30.3M 11s
84350K .......... .......... .......... .......... .......... 31% 16.7M 11s
84400K .......... .......... .......... .......... .......... 31% 16.3M 11s
84450K .......... .......... .......... .......... .......... 31% 24.4M 11s
84500K .......... .......... .......... .......... .......... 31% 25.8M 11s
84550K .......... .......... .......... .......... .......... 31% 21.3M 11s
84600K .......... .......... .......... .......... .......... 31% 20.2M 11s
84650K .......... .......... .......... .......... .......... 31% 24.0M 11s
84700K .......... .......... .......... .......... .......... 31% 18.3M 11s
84750K .......... .......... .......... .......... .......... 31% 24.7M 11s
84800K .......... .......... .......... .......... .......... 31% 17.2M 11s
84850K .......... .......... .......... .......... .......... 31% 16.1M 11s
84900K .......... .......... .......... .......... .......... 31% 20.6M 11s
84950K .......... .......... .......... .......... .......... 31% 19.1M 11s
85000K .......... .......... .......... .......... .......... 32% 23.8M 11s
85050K .......... .......... .......... .......... .......... 32% 10.3M 11s
85100K .......... .......... .......... .......... .......... 32% 10.4M 11s
85150K .......... .......... .......... .......... .......... 32% 31.6M 11s
85200K .......... .......... .......... .......... .......... 32% 17.2M 11s
85250K .......... .......... .......... .......... .......... 32% 138M 11s
85300K .......... .......... .......... .......... .......... 32% 17.4M 11s
85350K .......... .......... .......... .......... .......... 32% 9.67M 11s
85400K .......... .......... .......... .......... .......... 32% 16.7M 11s
85450K .......... .......... .......... .......... .......... 32% 13.4M 11s
85500K .......... .......... .......... .......... .......... 32% 17.3M 11s
85550K .......... .......... .......... .......... .......... 32% 9.74M 11s
85600K .......... .......... .......... .......... .......... 32% 13.3M 11s
85650K .......... .......... .......... .......... .......... 32% 9.74M 11s
85700K .......... .......... .......... .......... .......... 32% 10.7M 11s
85750K .......... .......... .......... .......... .......... 32% 6.40M 11s
85800K .......... .......... .......... .......... .......... 32% 5.90M 11s
85850K .......... .......... .......... .......... .......... 32% 5.39M 11s
85900K .......... .......... .......... .......... .......... 32% 7.13M 11s
85950K .......... .......... .......... .......... .......... 32% 5.99M 11s
86000K .......... .......... .......... .......... .......... 32% 10.1M 11s
86050K .......... .......... .......... .......... .......... 32% 34.8M 11s
86100K .......... .......... .......... .......... .......... 32% 32.1M 11s
86150K .......... .......... .......... .......... .......... 32% 41.7M 11s
86200K .......... .......... .......... .......... .......... 32% 35.3M 11s
86250K .......... .......... .......... .......... .......... 32% 38.1M 11s
86300K .......... .......... .......... .......... .......... 32% 38.5M 11s
86350K .......... .......... .......... .......... .......... 32% 19.0M 11s
86400K .......... .......... .......... .......... .......... 32% 456M 11s
86450K .......... .......... .......... .......... .......... 32% 42.5M 11s
86500K .......... .......... .......... .......... .......... 32% 61.9M 11s
86550K .......... .......... .......... .......... .......... 32% 25.8M 11s
86600K .......... .......... .......... .......... .......... 32% 29.5M 11s
86650K .......... .......... .......... .......... .......... 32% 19.0M 11s
86700K .......... .......... .......... .......... .......... 32% 39.5M 11s
86750K .......... .......... .......... .......... .......... 32% 22.7M 11s
86800K .......... .......... .......... .......... .......... 32% 22.0M 11s
86850K .......... .......... .......... .......... .......... 32% 28.0M 11s
86900K .......... .......... .......... .......... .......... 32% 27.4M 11s
86950K .......... .......... .......... .......... .......... 32% 21.3M 11s
87000K .......... .......... .......... .......... .......... 32% 25.6M 11s
87050K .......... .......... .......... .......... .......... 32% 29.5M 11s
87100K .......... .......... .......... .......... .......... 32% 22.7M 11s
87150K .......... .......... .......... .......... .......... 32% 32.0M 11s
87200K .......... .......... .......... .......... .......... 32% 24.0M 11s
87250K .......... .......... .......... .......... .......... 32% 27.1M 11s
87300K .......... .......... .......... .......... .......... 32% 29.7M 11s
87350K .......... .......... .......... .......... .......... 32% 25.1M 11s
87400K .......... .......... .......... .......... .......... 32% 22.7M 11s
87450K .......... .......... .......... .......... .......... 32% 14.2M 11s
87500K .......... .......... .......... .......... .......... 32% 17.5M 11s
87550K .......... .......... .......... .......... .......... 32% 15.6M 11s
87600K .......... .......... .......... .......... .......... 32% 10.3M 11s
87650K .......... .......... .......... .......... .......... 32% 11.5M 11s
87700K .......... .......... .......... .......... .......... 33% 10.6M 11s
87750K .......... .......... .......... .......... .......... 33% 14.8M 11s
87800K .......... .......... .......... .......... .......... 33% 19.1M 11s
87850K .......... .......... .......... .......... .......... 33% 12.7M 11s
87900K .......... .......... .......... .......... .......... 33% 17.6M 11s
87950K .......... .......... .......... .......... .......... 33% 10.1M 11s
88000K .......... .......... .......... .......... .......... 33% 8.08M 11s
88050K .......... .......... .......... .......... .......... 33% 10.1M 11s
88100K .......... .......... .......... .......... .......... 33% 14.1M 11s
88150K .......... .......... .......... .......... .......... 33% 13.2M 11s
88200K .......... .......... .......... .......... .......... 33% 13.2M 11s
88250K .......... .......... .......... .......... .......... 33% 15.4M 11s
88300K .......... .......... .......... .......... .......... 33% 16.6M 11s
88350K .......... .......... .......... .......... .......... 33% 11.3M 11s
88400K .......... .......... .......... .......... .......... 33% 16.7M 11s
88450K .......... .......... .......... .......... .......... 33% 12.8M 11s
88500K .......... .......... .......... .......... .......... 33% 16.0M 11s
88550K .......... .......... .......... .......... .......... 33% 20.1M 11s
88600K .......... .......... .......... .......... .......... 33% 27.4M 11s
88650K .......... .......... .......... .......... .......... 33% 23.9M 11s
88700K .......... .......... .......... .......... .......... 33% 14.2M 11s
88750K .......... .......... .......... .......... .......... 33% 531M 11s
88800K .......... .......... .......... .......... .......... 33% 18.5M 11s
88850K .......... .......... .......... .......... .......... 33% 14.4M 11s
88900K .......... .......... .......... .......... .......... 33% 35.1M 11s
88950K .......... .......... .......... .......... .......... 33% 13.3M 11s
89000K .......... .......... .......... .......... .......... 33% 38.2M 11s
89050K .......... .......... .......... .......... .......... 33% 25.7M 11s
89100K .......... .......... .......... .......... .......... 33% 16.8M 11s
89150K .......... .......... .......... .......... .......... 33% 22.5M 11s
89200K .......... .......... .......... .......... .......... 33% 19.0M 11s
89250K .......... .......... .......... .......... .......... 33% 20.3M 11s
89300K .......... .......... .......... .......... .......... 33% 17.4M 11s
89350K .......... .......... .......... .......... .......... 33% 22.5M 11s
89400K .......... .......... .......... .......... .......... 33% 18.5M 11s
89450K .......... .......... .......... .......... .......... 33% 21.3M 11s
89500K .......... .......... .......... .......... .......... 33% 22.5M 11s
89550K .......... .......... .......... .......... .......... 33% 18.3M 11s
89600K .......... .......... .......... .......... .......... 33% 6.96M 11s
89650K .......... .......... .......... .......... .......... 33% 11.0M 11s
89700K .......... .......... .......... .......... .......... 33% 8.31M 11s
89750K .......... .......... .......... .......... .......... 33% 24.5M 11s
89800K .......... .......... .......... .......... .......... 33% 15.5M 11s
89850K .......... .......... .......... .......... .......... 33% 13.2M 11s
89900K .......... .......... .......... .......... .......... 33% 10.3M 11s
89950K .......... .......... .......... .......... .......... 33% 12.9M 11s
90000K .......... .......... .......... .......... .......... 33% 17.3M 11s
90050K .......... .......... .......... .......... .......... 33% 15.3M 11s
90100K .......... .......... .......... .......... .......... 33% 12.2M 11s
90150K .......... .......... .......... .......... .......... 33% 17.5M 11s
90200K .......... .......... .......... .......... .......... 33% 12.7M 11s
90250K .......... .......... .......... .......... .......... 33% 15.7M 11s
90300K .......... .......... .......... .......... .......... 33% 15.9M 11s
90350K .......... .......... .......... .......... .......... 34% 12.2M 11s
90400K .......... .......... .......... .......... .......... 34% 14.7M 11s
90450K .......... .......... .......... .......... .......... 34% 8.21M 11s
90500K .......... .......... .......... .......... .......... 34% 16.6M 11s
90550K .......... .......... .......... .......... .......... 34% 18.3M 11s
90600K .......... .......... .......... .......... .......... 34% 9.30M 11s
90650K .......... .......... .......... .......... .......... 34% 16.8M 11s
90700K .......... .......... .......... .......... .......... 34% 15.1M 11s
90750K .......... .......... .......... .......... .......... 34% 19.5M 11s
90800K .......... .......... .......... .......... .......... 34% 16.6M 11s
90850K .......... .......... .......... .......... .......... 34% 18.0M 11s
90900K .......... .......... .......... .......... .......... 34% 17.4M 11s
90950K .......... .......... .......... .......... .......... 34% 13.3M 11s
91000K .......... .......... .......... .......... .......... 34% 17.1M 11s
91050K .......... .......... .......... .......... .......... 34% 18.7M 11s
91100K .......... .......... .......... .......... .......... 34% 17.1M 11s
91150K .......... .......... .......... .......... .......... 34% 16.6M 11s
91200K .......... .......... .......... .......... .......... 34% 17.4M 11s
91250K .......... .......... .......... .......... .......... 34% 18.3M 11s
91300K .......... .......... .......... .......... .......... 34% 19.1M 11s
91350K .......... .......... .......... .......... .......... 34% 14.8M 11s
91400K .......... .......... .......... .......... .......... 34% 11.7M 11s
91450K .......... .......... .......... .......... .......... 34% 11.9M 11s
91500K .......... .......... .......... .......... .......... 34% 8.80M 11s
91550K .......... .......... .......... .......... .......... 34% 18.9M 11s
91600K .......... .......... .......... .......... .......... 34% 15.7M 11s
91650K .......... .......... .......... .......... .......... 34% 14.6M 11s
91700K .......... .......... .......... .......... .......... 34% 12.3M 11s
91750K .......... .......... .......... .......... .......... 34% 18.2M 11s
91800K .......... .......... .......... .......... .......... 34% 14.9M 11s
91850K .......... .......... .......... .......... .......... 34% 17.5M 11s
91900K .......... .......... .......... .......... .......... 34% 17.4M 11s
91950K .......... .......... .......... .......... .......... 34% 15.3M 11s
92000K .......... .......... .......... .......... .......... 34% 14.2M 11s
92050K .......... .......... .......... .......... .......... 34% 16.1M 11s
92100K .......... .......... .......... .......... .......... 34% 17.3M 11s
92150K .......... .......... .......... .......... .......... 34% 16.2M 11s
92200K .......... .......... .......... .......... .......... 34% 15.7M 11s
92250K .......... .......... .......... .......... .......... 34% 16.2M 11s
92300K .......... .......... .......... .......... .......... 34% 11.2M 11s
92350K .......... .......... .......... .......... .......... 34% 20.1M 11s
92400K .......... .......... .......... .......... .......... 34% 20.2M 11s
92450K .......... .......... .......... .......... .......... 34% 21.0M 11s
92500K .......... .......... .......... .......... .......... 34% 18.6M 11s
92550K .......... .......... .......... .......... .......... 34% 16.9M 11s
92600K .......... .......... .......... .......... .......... 34% 27.2M 11s
92650K .......... .......... .......... .......... .......... 34% 23.2M 11s
92700K .......... .......... .......... .......... .......... 34% 15.7M 11s
92750K .......... .......... .......... .......... .......... 34% 24.6M 11s
92800K .......... .......... .......... .......... .......... 34% 20.6M 11s
92850K .......... .......... .......... .......... .......... 34% 24.0M 11s
92900K .......... .......... .......... .......... .......... 34% 26.4M 11s
92950K .......... .......... .......... .......... .......... 34% 21.0M 11s
93000K .......... .......... .......... .......... .......... 35% 20.9M 11s
93050K .......... .......... .......... .......... .......... 35% 31.1M 11s
93100K .......... .......... .......... .......... .......... 35% 22.4M 11s
93150K .......... .......... .......... .......... .......... 35% 25.3M 11s
93200K .......... .......... .......... .......... .......... 35% 20.4M 11s
93250K .......... .......... .......... .......... .......... 35% 26.7M 11s
93300K .......... .......... .......... .......... .......... 35% 31.5M 11s
93350K .......... .......... .......... .......... .......... 35% 24.2M 11s
93400K .......... .......... .......... .......... .......... 35% 25.5M 11s
93450K .......... .......... .......... .......... .......... 35% 27.5M 11s
93500K .......... .......... .......... .......... .......... 35% 38.4M 11s
93550K .......... .......... .......... .......... .......... 35% 38.1M 11s
93600K .......... .......... .......... .......... .......... 35% 63.8M 10s
93650K .......... .......... .......... .......... .......... 35% 38.6M 10s
93700K .......... .......... .......... .......... .......... 35% 55.6M 10s
93750K .......... .......... .......... .......... .......... 35% 15.8M 10s
93800K .......... .......... .......... .......... .......... 35% 36.5M 10s
93850K .......... .......... .......... .......... .......... 35% 56.7M 10s
93900K .......... .......... .......... .......... .......... 35% 78.9M 10s
93950K .......... .......... .......... .......... .......... 35% 28.5M 10s
94000K .......... .......... .......... .......... .......... 35% 130M 10s
94050K .......... .......... .......... .......... .......... 35% 4.10M 10s
94100K .......... .......... .......... .......... .......... 35% 28.5M 10s
94150K .......... .......... .......... .......... .......... 35% 58.2M 10s
94200K .......... .......... .......... .......... .......... 35% 43.1M 10s
94250K .......... .......... .......... .......... .......... 35% 38.1M 10s
94300K .......... .......... .......... .......... .......... 35% 38.2M 10s
94350K .......... .......... .......... .......... .......... 35% 21.2M 10s
94400K .......... .......... .......... .......... .......... 35% 47.1M 10s
94450K .......... .......... .......... .......... .......... 35% 27.7M 10s
94500K .......... .......... .......... .......... .......... 35% 34.4M 10s
94550K .......... .......... .......... .......... .......... 35% 26.3M 10s
94600K .......... .......... .......... .......... .......... 35% 19.7M 10s
94650K .......... .......... .......... .......... .......... 35% 10.0M 10s
94700K .......... .......... .......... .......... .......... 35% 39.3M 10s
94750K .......... .......... .......... .......... .......... 35% 22.2M 10s
94800K .......... .......... .......... .......... .......... 35% 11.7M 10s
94850K .......... .......... .......... .......... .......... 35% 24.0M 10s
94900K .......... .......... .......... .......... .......... 35% 13.6M 10s
94950K .......... .......... .......... .......... .......... 35% 13.7M 10s
95000K .......... .......... .......... .......... .......... 35% 14.3M 10s
95050K .......... .......... .......... .......... .......... 35% 17.5M 10s
95100K .......... .......... .......... .......... .......... 35% 13.1M 10s
95150K .......... .......... .......... .......... .......... 35% 16.6M 10s
95200K .......... .......... .......... .......... .......... 35% 12.0M 10s
95250K .......... .......... .......... .......... .......... 35% 13.8M 10s
95300K .......... .......... .......... .......... .......... 35% 11.2M 10s
95350K .......... .......... .......... .......... .......... 35% 9.50M 10s
95400K .......... .......... .......... .......... .......... 35% 23.4M 10s
95450K .......... .......... .......... .......... .......... 35% 16.8M 10s
95500K .......... .......... .......... .......... .......... 35% 16.2M 10s
95550K .......... .......... .......... .......... .......... 35% 15.9M 10s
95600K .......... .......... .......... .......... .......... 35% 11.1M 10s
95650K .......... .......... .......... .......... .......... 36% 13.7M 10s
95700K .......... .......... .......... .......... .......... 36% 12.7M 10s
95750K .......... .......... .......... .......... .......... 36% 10.6M 10s
95800K .......... .......... .......... .......... .......... 36% 13.6M 10s
95850K .......... .......... .......... .......... .......... 36% 17.3M 10s
95900K .......... .......... .......... .......... .......... 36% 27.0M 10s
95950K .......... .......... .......... .......... .......... 36% 16.5M 10s
96000K .......... .......... .......... .......... .......... 36% 15.6M 10s
96050K .......... .......... .......... .......... .......... 36% 25.5M 10s
96100K .......... .......... .......... .......... .......... 36% 14.8M 10s
96150K .......... .......... .......... .......... .......... 36% 14.6M 10s
96200K .......... .......... .......... .......... .......... 36% 14.2M 10s
96250K .......... .......... .......... .......... .......... 36% 19.5M 10s
96300K .......... .......... .......... .......... .......... 36% 12.6M 10s
96350K .......... .......... .......... .......... .......... 36% 10.7M 10s
96400K .......... .......... .......... .......... .......... 36% 10.2M 10s
96450K .......... .......... .......... .......... .......... 36% 24.9M 10s
96500K .......... .......... .......... .......... .......... 36% 29.0M 10s
96550K .......... .......... .......... .......... .......... 36% 18.4M 10s
96600K .......... .......... .......... .......... .......... 36% 22.3M 10s
96650K .......... .......... .......... .......... .......... 36% 13.4M 10s
96700K .......... .......... .......... .......... .......... 36% 17.6M 10s
96750K .......... .......... .......... .......... .......... 36% 18.0M 10s
96800K .......... .......... .......... .......... .......... 36% 15.0M 10s
96850K .......... .......... .......... .......... .......... 36% 15.3M 10s
96900K .......... .......... .......... .......... .......... 36% 14.8M 10s
96950K .......... .......... .......... .......... .......... 36% 15.9M 10s
97000K .......... .......... .......... .......... .......... 36% 14.4M 10s
97050K .......... .......... .......... .......... .......... 36% 15.3M 10s
97100K .......... .......... .......... .......... .......... 36% 9.87M 10s
97150K .......... .......... .......... .......... .......... 36% 11.7M 10s
97200K .......... .......... .......... .......... .......... 36% 8.62M 10s
97250K .......... .......... .......... .......... .......... 36% 14.2M 10s
97300K .......... .......... .......... .......... .......... 36% 13.7M 10s
97350K .......... .......... .......... .......... .......... 36% 14.7M 10s
97400K .......... .......... .......... .......... .......... 36% 13.7M 10s
97450K .......... .......... .......... .......... .......... 36% 13.6M 10s
97500K .......... .......... .......... .......... .......... 36% 15.6M 10s
97550K .......... .......... .......... .......... .......... 36% 2.18M 10s
97600K .......... .......... .......... .......... .......... 36% 8.90M 10s
97650K .......... .......... .......... .......... .......... 36% 21.3M 10s
97700K .......... .......... .......... .......... .......... 36% 9.16M 10s
97750K .......... .......... .......... .......... .......... 36% 13.5M 10s
97800K .......... .......... .......... .......... .......... 36% 11.0M 10s
97850K .......... .......... .......... .......... .......... 36% 12.1M 10s
97900K .......... .......... .......... .......... .......... 36% 17.3M 10s
97950K .......... .......... .......... .......... .......... 36% 14.3M 10s
98000K .......... .......... .......... .......... .......... 36% 14.4M 10s
98050K .......... .......... .......... .......... .......... 36% 7.66M 10s
98100K .......... .......... .......... .......... .......... 36% 14.3M 10s
98150K .......... .......... .......... .......... .......... 36% 15.3M 10s
98200K .......... .......... .......... .......... .......... 36% 15.1M 10s
98250K .......... .......... .......... .......... .......... 36% 18.7M 10s
98300K .......... .......... .......... .......... .......... 37% 27.1M 10s
98350K .......... .......... .......... .......... .......... 37% 30.8M 10s
98400K .......... .......... .......... .......... .......... 37% 29.5M 10s
98450K .......... .......... .......... .......... .......... 37% 29.1M 10s
98500K .......... .......... .......... .......... .......... 37% 36.7M 10s
98550K .......... .......... .......... .......... .......... 37% 16.0M 10s
98600K .......... .......... .......... .......... .......... 37% 98.2M 10s
98650K .......... .......... .......... .......... .......... 37% 23.2M 10s
98700K .......... .......... .......... .......... .......... 37% 21.8M 10s
98750K .......... .......... .......... .......... .......... 37% 22.3M 10s
98800K .......... .......... .......... .......... .......... 37% 22.0M 10s
98850K .......... .......... .......... .......... .......... 37% 15.9M 10s
98900K .......... .......... .......... .......... .......... 37% 25.3M 10s
98950K .......... .......... .......... .......... .......... 37% 18.5M 10s
99000K .......... .......... .......... .......... .......... 37% 17.8M 10s
99050K .......... .......... .......... .......... .......... 37% 20.6M 10s
99100K .......... .......... .......... .......... .......... 37% 16.4M 10s
99150K .......... .......... .......... .......... .......... 37% 21.0M 10s
99200K .......... .......... .......... .......... .......... 37% 17.3M 10s
99250K .......... .......... .......... .......... .......... 37% 20.4M 10s
99300K .......... .......... .......... .......... .......... 37% 20.9M 10s
99350K .......... .......... .......... .......... .......... 37% 16.3M 10s
99400K .......... .......... .......... .......... .......... 37% 18.1M 10s
99450K .......... .......... .......... .......... .......... 37% 18.1M 10s
99500K .......... .......... .......... .......... .......... 37% 17.8M 10s
99550K .......... .......... .......... .......... .......... 37% 17.9M 10s
99600K .......... .......... .......... .......... .......... 37% 14.0M 10s
99650K .......... .......... .......... .......... .......... 37% 14.2M 10s
99700K .......... .......... .......... .......... .......... 37% 15.7M 10s
99750K .......... .......... .......... .......... .......... 37% 17.4M 10s
99800K .......... .......... .......... .......... .......... 37% 16.6M 10s
99850K .......... .......... .......... .......... .......... 37% 10.0M 10s
99900K .......... .......... .......... .......... .......... 37% 8.10M 10s
99950K .......... .......... .......... .......... .......... 37% 11.1M 10s
100000K .......... .......... .......... .......... .......... 37% 11.5M 10s
100050K .......... .......... .......... .......... .......... 37% 12.7M 10s
100100K .......... .......... .......... .......... .......... 37% 12.6M 10s
100150K .......... .......... .......... .......... .......... 37% 15.7M 10s
100200K .......... .......... .......... .......... .......... 37% 11.7M 10s
100250K .......... .......... .......... .......... .......... 37% 38.6M 10s
100300K .......... .......... .......... .......... .......... 37% 23.7M 10s
100350K .......... .......... .......... .......... .......... 37% 14.9M 10s
100400K .......... .......... .......... .......... .......... 37% 14.2M 10s
100450K .......... .......... .......... .......... .......... 37% 13.7M 10s
100500K .......... .......... .......... .......... .......... 37% 7.95M 10s
100550K .......... .......... .......... .......... .......... 37% 10.2M 10s
100600K .......... .......... .......... .......... .......... 37% 7.16M 10s
100650K .......... .......... .......... .......... .......... 37% 13.2M 10s
100700K .......... .......... .......... .......... .......... 37% 10.5M 10s
100750K .......... .......... .......... .......... .......... 37% 15.5M 10s
100800K .......... .......... .......... .......... .......... 37% 10.2M 10s
100850K .......... .......... .......... .......... .......... 37% 18.9M 10s
100900K .......... .......... .......... .......... .......... 37% 12.9M 10s
100950K .......... .......... .......... .......... .......... 38% 9.88M 10s
101000K .......... .......... .......... .......... .......... 38% 12.1M 10s
101050K .......... .......... .......... .......... .......... 38% 6.57M 10s
101100K .......... .......... .......... .......... .......... 38% 27.2M 10s
101150K .......... .......... .......... .......... .......... 38% 14.1M 10s
101200K .......... .......... .......... .......... .......... 38% 34.3M 10s
101250K .......... .......... .......... .......... .......... 38% 13.2M 10s
101300K .......... .......... .......... .......... .......... 38% 13.4M 10s
101350K .......... .......... .......... .......... .......... 38% 14.8M 10s
101400K .......... .......... .......... .......... .......... 38% 18.3M 10s
101450K .......... .......... .......... .......... .......... 38% 14.2M 10s
101500K .......... .......... .......... .......... .......... 38% 15.8M 10s
101550K .......... .......... .......... .......... .......... 38% 16.6M 10s
101600K .......... .......... .......... .......... .......... 38% 13.7M 10s
101650K .......... .......... .......... .......... .......... 38% 15.8M 10s
101700K .......... .......... .......... .......... .......... 38% 14.5M 10s
101750K .......... .......... .......... .......... .......... 38% 18.2M 10s
101800K .......... .......... .......... .......... .......... 38% 22.0M 10s
101850K .......... .......... .......... .......... .......... 38% 15.1M 10s
101900K .......... .......... .......... .......... .......... 38% 35.3M 10s
101950K .......... .......... .......... .......... .......... 38% 37.4M 10s
102000K .......... .......... .......... .......... .......... 38% 63.7M 10s
102050K .......... .......... .......... .......... .......... 38% 20.6M 10s
102100K .......... .......... .......... .......... .......... 38% 159M 10s
102150K .......... .......... .......... .......... .......... 38% 162M 10s
102200K .......... .......... .......... .......... .......... 38% 23.1M 10s
102250K .......... .......... .......... .......... .......... 38% 219M 10s
102300K .......... .......... .......... .......... .......... 38% 54.9M 10s
102350K .......... .......... .......... .......... .......... 38% 38.6M 10s
102400K .......... .......... .......... .......... .......... 38% 37.6M 10s
102450K .......... .......... .......... .......... .......... 38% 36.9M 10s
102500K .......... .......... .......... .......... .......... 38% 43.7M 10s
102550K .......... .......... .......... .......... .......... 38% 10.6M 10s
102600K .......... .......... .......... .......... .......... 38% 11.6M 10s
102650K .......... .......... .......... .......... .......... 38% 12.2M 10s
102700K .......... .......... .......... .......... .......... 38% 10.1M 10s
102750K .......... .......... .......... .......... .......... 38% 19.6M 10s
102800K .......... .......... .......... .......... .......... 38% 16.0M 10s
102850K .......... .......... .......... .......... .......... 38% 24.7M 10s
102900K .......... .......... .......... .......... .......... 38% 25.9M 10s
102950K .......... .......... .......... .......... .......... 38% 20.5M 10s
103000K .......... .......... .......... .......... .......... 38% 22.0M 10s
103050K .......... .......... .......... .......... .......... 38% 21.5M 10s
103100K .......... .......... .......... .......... .......... 38% 48.2M 10s
103150K .......... .......... .......... .......... .......... 38% 17.3M 10s
103200K .......... .......... .......... .......... .......... 38% 22.8M 10s
103250K .......... .......... .......... .......... .......... 38% 20.4M 10s
103300K .......... .......... .......... .......... .......... 38% 11.9M 10s
103350K .......... .......... .......... .......... .......... 38% 249M 10s
103400K .......... .......... .......... .......... .......... 38% 20.6M 10s
103450K .......... .......... .......... .......... .......... 38% 23.3M 10s
103500K .......... .......... .......... .......... .......... 38% 11.4M 10s
103550K .......... .......... .......... .......... .......... 38% 19.2M 10s
103600K .......... .......... .......... .......... .......... 38% 25.0M 10s
103650K .......... .......... .......... .......... .......... 39% 22.2M 10s
103700K .......... .......... .......... .......... .......... 39% 21.0M 10s
103750K .......... .......... .......... .......... .......... 39% 21.2M 10s
103800K .......... .......... .......... .......... .......... 39% 20.7M 10s
103850K .......... .......... .......... .......... .......... 39% 25.3M 10s
103900K .......... .......... .......... .......... .......... 39% 23.6M 10s
103950K .......... .......... .......... .......... .......... 39% 15.3M 10s
104000K .......... .......... .......... .......... .......... 39% 14.5M 10s
104050K .......... .......... .......... .......... .......... 39% 18.1M 10s
104100K .......... .......... .......... .......... .......... 39% 13.7M 10s
104150K .......... .......... .......... .......... .......... 39% 15.6M 10s
104200K .......... .......... .......... .......... .......... 39% 14.4M 10s
104250K .......... .......... .......... .......... .......... 39% 13.0M 10s
104300K .......... .......... .......... .......... .......... 39% 14.1M 10s
104350K .......... .......... .......... .......... .......... 39% 11.4M 10s
104400K .......... .......... .......... .......... .......... 39% 10.5M 10s
104450K .......... .......... .......... .......... .......... 39% 7.88M 10s
104500K .......... .......... .......... .......... .......... 39% 11.0M 10s
104550K .......... .......... .......... .......... .......... 39% 17.9M 10s
104600K .......... .......... .......... .......... .......... 39% 8.95M 10s
104650K .......... .......... .......... .......... .......... 39% 10.0M 10s
104700K .......... .......... .......... .......... .......... 39% 7.73M 10s
104750K .......... .......... .......... .......... .......... 39% 11.6M 10s
104800K .......... .......... .......... .......... .......... 39% 10.7M 10s
104850K .......... .......... .......... .......... .......... 39% 7.59M 10s
104900K .......... .......... .......... .......... .......... 39% 10.5M 10s
104950K .......... .......... .......... .......... .......... 39% 9.46M 10s
105000K .......... .......... .......... .......... .......... 39% 10.3M 10s
105050K .......... .......... .......... .......... .......... 39% 12.8M 10s
105100K .......... .......... .......... .......... .......... 39% 53.0M 10s
105150K .......... .......... .......... .......... .......... 39% 6.55M 10s
105200K .......... .......... .......... .......... .......... 39% 49.1M 10s
105250K .......... .......... .......... .......... .......... 39% 13.6M 10s
105300K .......... .......... .......... .......... .......... 39% 13.8M 10s
105350K .......... .......... .......... .......... .......... 39% 18.6M 10s
105400K .......... .......... .......... .......... .......... 39% 10.4M 10s
105450K .......... .......... .......... .......... .......... 39% 7.73M 10s
105500K .......... .......... .......... .......... .......... 39% 9.85M 10s
105550K .......... .......... .......... .......... .......... 39% 7.72M 10s
105600K .......... .......... .......... .......... .......... 39% 8.46M 10s
105650K .......... .......... .......... .......... .......... 39% 8.63M 10s
105700K .......... .......... .......... .......... .......... 39% 8.26M 10s
105750K .......... .......... .......... .......... .......... 39% 18.6M 10s
105800K .......... .......... .......... .......... .......... 39% 21.0M 10s
105850K .......... .......... .......... .......... .......... 39% 33.1M 10s
105900K .......... .......... .......... .......... .......... 39% 23.2M 10s
105950K .......... .......... .......... .......... .......... 39% 23.5M 10s
106000K .......... .......... .......... .......... .......... 39% 13.3M 10s
106050K .......... .......... .......... .......... .......... 39% 23.2M 10s
106100K .......... .......... .......... .......... .......... 39% 22.5M 10s
106150K .......... .......... .......... .......... .......... 39% 41.8M 10s
106200K .......... .......... .......... .......... .......... 39% 21.8M 10s
106250K .......... .......... .......... .......... .......... 39% 22.1M 10s
106300K .......... .......... .......... .......... .......... 40% 23.7M 10s
106350K .......... .......... .......... .......... .......... 40% 15.9M 10s
106400K .......... .......... .......... .......... .......... 40% 11.8M 10s
106450K .......... .......... .......... .......... .......... 40% 13.1M 10s
106500K .......... .......... .......... .......... .......... 40% 18.8M 10s
106550K .......... .......... .......... .......... .......... 40% 22.9M 10s
106600K .......... .......... .......... .......... .......... 40% 28.0M 10s
106650K .......... .......... .......... .......... .......... 40% 15.6M 10s
106700K .......... .......... .......... .......... .......... 40% 373M 10s
106750K .......... .......... .......... .......... .......... 40% 18.8M 10s
106800K .......... .......... .......... .......... .......... 40% 29.8M 10s
106850K .......... .......... .......... .......... .......... 40% 27.1M 10s
106900K .......... .......... .......... .......... .......... 40% 23.1M 10s
106950K .......... .......... .......... .......... .......... 40% 18.7M 10s
107000K .......... .......... .......... .......... .......... 40% 14.4M 10s
107050K .......... .......... .......... .......... .......... 40% 14.0M 10s
107100K .......... .......... .......... .......... .......... 40% 11.0M 10s
107150K .......... .......... .......... .......... .......... 40% 12.2M 10s
107200K .......... .......... .......... .......... .......... 40% 10.4M 10s
107250K .......... .......... .......... .......... .......... 40% 12.8M 10s
107300K .......... .......... .......... .......... .......... 40% 11.9M 10s
107350K .......... .......... .......... .......... .......... 40% 7.52M 10s
107400K .......... .......... .......... .......... .......... 40% 10.3M 10s
107450K .......... .......... .......... .......... .......... 40% 10.0M 10s
107500K .......... .......... .......... .......... .......... 40% 17.0M 10s
107550K .......... .......... .......... .......... .......... 40% 17.1M 10s
107600K .......... .......... .......... .......... .......... 40% 11.4M 10s
107650K .......... .......... .......... .......... .......... 40% 11.8M 10s
107700K .......... .......... .......... .......... .......... 40% 10.4M 10s
107750K .......... .......... .......... .......... .......... 40% 15.2M 10s
107800K .......... .......... .......... .......... .......... 40% 14.2M 10s
107850K .......... .......... .......... .......... .......... 40% 11.8M 10s
107900K .......... .......... .......... .......... .......... 40% 27.4M 10s
107950K .......... .......... .......... .......... .......... 40% 7.09M 10s
108000K .......... .......... .......... .......... .......... 40% 138M 10s
108050K .......... .......... .......... .......... .......... 40% 13.5M 10s
108100K .......... .......... .......... .......... .......... 40% 27.9M 10s
108150K .......... .......... .......... .......... .......... 40% 13.4M 10s
108200K .......... .......... .......... .......... .......... 40% 13.4M 10s
108250K .......... .......... .......... .......... .......... 40% 13.1M 10s
108300K .......... .......... .......... .......... .......... 40% 14.2M 10s
108350K .......... .......... .......... .......... .......... 40% 10.5M 10s
108400K .......... .......... .......... .......... .......... 40% 10.1M 10s
108450K .......... .......... .......... .......... .......... 40% 8.98M 10s
108500K .......... .......... .......... .......... .......... 40% 8.32M 10s
108550K .......... .......... .......... .......... .......... 40% 7.02M 10s
108600K .......... .......... .......... .......... .......... 40% 5.58M 10s
108650K .......... .......... .......... .......... .......... 40% 7.61M 10s
108700K .......... .......... .......... .......... .......... 40% 8.91M 10s
108750K .......... .......... .......... .......... .......... 40% 10.4M 10s
108800K .......... .......... .......... .......... .......... 40% 8.93M 10s
108850K .......... .......... .......... .......... .......... 40% 10.1M 10s
108900K .......... .......... .......... .......... .......... 40% 12.3M 10s
108950K .......... .......... .......... .......... .......... 41% 9.62M 10s
109000K .......... .......... .......... .......... .......... 41% 7.98M 10s
109050K .......... .......... .......... .......... .......... 41% 12.0M 10s
109100K .......... .......... .......... .......... .......... 41% 12.7M 10s
109150K .......... .......... .......... .......... .......... 41% 19.6M 10s
109200K .......... .......... .......... .......... .......... 41% 14.3M 10s
109250K .......... .......... .......... .......... .......... 41% 24.8M 10s
109300K .......... .......... .......... .......... .......... 41% 16.3M 10s
109350K .......... .......... .......... .......... .......... 41% 14.7M 10s
109400K .......... .......... .......... .......... .......... 41% 9.62M 10s
109450K .......... .......... .......... .......... .......... 41% 20.0M 10s
109500K .......... .......... .......... .......... .......... 41% 79.1M 10s
109550K .......... .......... .......... .......... .......... 41% 20.1M 10s
109600K .......... .......... .......... .......... .......... 41% 15.5M 10s
109650K .......... .......... .......... .......... .......... 41% 14.7M 10s
109700K .......... .......... .......... .......... .......... 41% 10.9M 10s
109750K .......... .......... .......... .......... .......... 41% 9.53M 10s
109800K .......... .......... .......... .......... .......... 41% 4.49M 10s
109850K .......... .......... .......... .......... .......... 41% 6.72M 10s
109900K .......... .......... .......... .......... .......... 41% 9.10M 10s
109950K .......... .......... .......... .......... .......... 41% 12.0M 10s
110000K .......... .......... .......... .......... .......... 41% 11.9M 10s
110050K .......... .......... .......... .......... .......... 41% 18.7M 10s
110100K .......... .......... .......... .......... .......... 41% 11.1M 10s
110150K .......... .......... .......... .......... .......... 41% 22.8M 10s
110200K .......... .......... .......... .......... .......... 41% 8.85M 10s
110250K .......... .......... .......... .......... .......... 41% 13.5M 10s
110300K .......... .......... .......... .......... .......... 41% 10.5M 10s
110350K .......... .......... .......... .......... .......... 41% 7.99M 10s
110400K .......... .......... .......... .......... .......... 41% 9.53M 10s
110450K .......... .......... .......... .......... .......... 41% 11.5M 10s
110500K .......... .......... .......... .......... .......... 41% 7.79M 10s
110550K .......... .......... .......... .......... .......... 41% 12.6M 10s
110600K .......... .......... .......... .......... .......... 41% 17.1M 10s
110650K .......... .......... .......... .......... .......... 41% 9.92M 10s
110700K .......... .......... .......... .......... .......... 41% 12.6M 10s
110750K .......... .......... .......... .......... .......... 41% 12.7M 10s
110800K .......... .......... .......... .......... .......... 41% 12.1M 10s
110850K .......... .......... .......... .......... .......... 41% 17.6M 10s
110900K .......... .......... .......... .......... .......... 41% 16.6M 10s
110950K .......... .......... .......... .......... .......... 41% 14.2M 10s
111000K .......... .......... .......... .......... .......... 41% 14.1M 10s
111050K .......... .......... .......... .......... .......... 41% 18.0M 10s
111100K .......... .......... .......... .......... .......... 41% 13.2M 10s
111150K .......... .......... .......... .......... .......... 41% 17.3M 10s
111200K .......... .......... .......... .......... .......... 41% 13.5M 10s
111250K .......... .......... .......... .......... .......... 41% 24.9M 10s
111300K .......... .......... .......... .......... .......... 41% 16.9M 10s
111350K .......... .......... .......... .......... .......... 41% 15.7M 10s
111400K .......... .......... .......... .......... .......... 41% 16.8M 10s
111450K .......... .......... .......... .......... .......... 41% 8.29M 10s
111500K .......... .......... .......... .......... .......... 41% 5.30M 10s
111550K .......... .......... .......... .......... .......... 41% 7.53M 10s
111600K .......... .......... .......... .......... .......... 42% 7.80M 10s
111650K .......... .......... .......... .......... .......... 42% 8.80M 10s
111700K .......... .......... .......... .......... .......... 42% 9.00M 10s
111750K .......... .......... .......... .......... .......... 42% 7.92M 10s
111800K .......... .......... .......... .......... .......... 42% 9.65M 10s
111850K .......... .......... .......... .......... .......... 42% 7.28M 10s
111900K .......... .......... .......... .......... .......... 42% 9.55M 10s
111950K .......... .......... .......... .......... .......... 42% 7.60M 10s
112000K .......... .......... .......... .......... .......... 42% 9.01M 10s
112050K .......... .......... .......... .......... .......... 42% 8.74M 10s
112100K .......... .......... .......... .......... .......... 42% 22.2M 10s
112150K .......... .......... .......... .......... .......... 42% 11.5M 10s
112200K .......... .......... .......... .......... .......... 42% 12.5M 10s
112250K .......... .......... .......... .......... .......... 42% 11.1M 10s
112300K .......... .......... .......... .......... .......... 42% 8.38M 10s
112350K .......... .......... .......... .......... .......... 42% 10.4M 10s
112400K .......... .......... .......... .......... .......... 42% 11.2M 10s
112450K .......... .......... .......... .......... .......... 42% 10.6M 10s
112500K .......... .......... .......... .......... .......... 42% 11.5M 10s
112550K .......... .......... .......... .......... .......... 42% 15.0M 10s
112600K .......... .......... .......... .......... .......... 42% 10.2M 10s
112650K .......... .......... .......... .......... .......... 42% 15.9M 10s
112700K .......... .......... .......... .......... .......... 42% 10.2M 10s
112750K .......... .......... .......... .......... .......... 42% 9.71M 10s
112800K .......... .......... .......... .......... .......... 42% 7.24M 10s
112850K .......... .......... .......... .......... .......... 42% 12.1M 10s
112900K .......... .......... .......... .......... .......... 42% 12.6M 10s
112950K .......... .......... .......... .......... .......... 42% 11.1M 10s
113000K .......... .......... .......... .......... .......... 42% 8.42M 10s
113050K .......... .......... .......... .......... .......... 42% 16.3M 10s
113100K .......... .......... .......... .......... .......... 42% 11.3M 10s
113150K .......... .......... .......... .......... .......... 42% 11.8M 10s
113200K .......... .......... .......... .......... .......... 42% 10.8M 10s
113250K .......... .......... .......... .......... .......... 42% 12.8M 10s
113300K .......... .......... .......... .......... .......... 42% 10.7M 10s
113350K .......... .......... .......... .......... .......... 42% 7.26M 10s
113400K .......... .......... .......... .......... .......... 42% 15.7M 10s
113450K .......... .......... .......... .......... .......... 42% 11.7M 10s
113500K .......... .......... .......... .......... .......... 42% 11.2M 10s
113550K .......... .......... .......... .......... .......... 42% 18.1M 10s
113600K .......... .......... .......... .......... .......... 42% 13.0M 10s
113650K .......... .......... .......... .......... .......... 42% 16.4M 10s
113700K .......... .......... .......... .......... .......... 42% 11.2M 10s
113750K .......... .......... .......... .......... .......... 42% 17.2M 10s
113800K .......... .......... .......... .......... .......... 42% 16.6M 10s
113850K .......... .......... .......... .......... .......... 42% 9.98M 10s
113900K .......... .......... .......... .......... .......... 42% 29.0M 10s
113950K .......... .......... .......... .......... .......... 42% 13.4M 10s
114000K .......... .......... .......... .......... .......... 42% 16.7M 10s
114050K .......... .......... .......... .......... .......... 42% 40.5M 10s
114100K .......... .......... .......... .......... .......... 42% 17.1M 10s
114150K .......... .......... .......... .......... .......... 42% 15.8M 10s
114200K .......... .......... .......... .......... .......... 42% 12.8M 10s
114250K .......... .......... .......... .......... .......... 43% 160M 9s
114300K .......... .......... .......... .......... .......... 43% 19.0M 9s
114350K .......... .......... .......... .......... .......... 43% 24.6M 9s
114400K .......... .......... .......... .......... .......... 43% 22.1M 9s
114450K .......... .......... .......... .......... .......... 43% 19.9M 9s
114500K .......... .......... .......... .......... .......... 43% 23.2M 9s
114550K .......... .......... .......... .......... .......... 43% 28.8M 9s
114600K .......... .......... .......... .......... .......... 43% 17.6M 9s
114650K .......... .......... .......... .......... .......... 43% 29.0M 9s
114700K .......... .......... .......... .......... .......... 43% 12.7M 9s
114750K .......... .......... .......... .......... .......... 43% 23.8M 9s
114800K .......... .......... .......... .......... .......... 43% 19.8M 9s
114850K .......... .......... .......... .......... .......... 43% 14.9M 9s
114900K .......... .......... .......... .......... .......... 43% 17.2M 9s
114950K .......... .......... .......... .......... .......... 43% 9.01M 9s
115000K .......... .......... .......... .......... .......... 43% 20.3M 9s
115050K .......... .......... .......... .......... .......... 43% 16.3M 9s
115100K .......... .......... .......... .......... .......... 43% 10.3M 9s
115150K .......... .......... .......... .......... .......... 43% 13.1M 9s
115200K .......... .......... .......... .......... .......... 43% 12.1M 9s
115250K .......... .......... .......... .......... .......... 43% 13.5M 9s
115300K .......... .......... .......... .......... .......... 43% 11.2M 9s
115350K .......... .......... .......... .......... .......... 43% 10.4M 9s
115400K .......... .......... .......... .......... .......... 43% 7.88M 9s
115450K .......... .......... .......... .......... .......... 43% 8.41M 9s
115500K .......... .......... .......... .......... .......... 43% 10.2M 9s
115550K .......... .......... .......... .......... .......... 43% 19.9M 9s
115600K .......... .......... .......... .......... .......... 43% 12.2M 9s
115650K .......... .......... .......... .......... .......... 43% 42.7M 9s
115700K .......... .......... .......... .......... .......... 43% 15.9M 9s
115750K .......... .......... .......... .......... .......... 43% 17.7M 9s
115800K .......... .......... .......... .......... .......... 43% 16.8M 9s
115850K .......... .......... .......... .......... .......... 43% 31.4M 9s
115900K .......... .......... .......... .......... .......... 43% 19.4M 9s
115950K .......... .......... .......... .......... .......... 43% 15.6M 9s
116000K .......... .......... .......... .......... .......... 43% 35.0M 9s
116050K .......... .......... .......... .......... .......... 43% 28.5M 9s
116100K .......... .......... .......... .......... .......... 43% 17.9M 9s
116150K .......... .......... .......... .......... .......... 43% 21.6M 9s
116200K .......... .......... .......... .......... .......... 43% 18.7M 9s
116250K .......... .......... .......... .......... .......... 43% 16.3M 9s
116300K .......... .......... .......... .......... .......... 43% 19.5M 9s
116350K .......... .......... .......... .......... .......... 43% 19.9M 9s
116400K .......... .......... .......... .......... .......... 43% 18.8M 9s
116450K .......... .......... .......... .......... .......... 43% 12.8M 9s
116500K .......... .......... .......... .......... .......... 43% 20.0M 9s
116550K .......... .......... .......... .......... .......... 43% 17.8M 9s
116600K .......... .......... .......... .......... .......... 43% 15.8M 9s
116650K .......... .......... .......... .......... .......... 43% 15.7M 9s
116700K .......... .......... .......... .......... .......... 43% 14.1M 9s
116750K .......... .......... .......... .......... .......... 43% 24.3M 9s
116800K .......... .......... .......... .......... .......... 43% 16.6M 9s
116850K .......... .......... .......... .......... .......... 43% 19.9M 9s
116900K .......... .......... .......... .......... .......... 44% 26.2M 9s
116950K .......... .......... .......... .......... .......... 44% 45.3M 9s
117000K .......... .......... .......... .......... .......... 44% 74.4M 9s
117050K .......... .......... .......... .......... .......... 44% 48.3M 9s
117100K .......... .......... .......... .......... .......... 44% 75.9M 9s
117150K .......... .......... .......... .......... .......... 44% 22.8M 9s
117200K .......... .......... .......... .......... .......... 44% 131M 9s
117250K .......... .......... .......... .......... .......... 44% 77.6M 9s
117300K .......... .......... .......... .......... .......... 44% 18.5M 9s
117350K .......... .......... .......... .......... .......... 44% 25.1M 9s
117400K .......... .......... .......... .......... .......... 44% 24.8M 9s
117450K .......... .......... .......... .......... .......... 44% 22.4M 9s
117500K .......... .......... .......... .......... .......... 44% 25.5M 9s
117550K .......... .......... .......... .......... .......... 44% 23.2M 9s
117600K .......... .......... .......... .......... .......... 44% 10.7M 9s
117650K .......... .......... .......... .......... .......... 44% 34.5M 9s
117700K .......... .......... .......... .......... .......... 44% 13.0M 9s
117750K .......... .......... .......... .......... .......... 44% 13.0M 9s
117800K .......... .......... .......... .......... .......... 44% 15.1M 9s
117850K .......... .......... .......... .......... .......... 44% 12.9M 9s
117900K .......... .......... .......... .......... .......... 44% 11.6M 9s
117950K .......... .......... .......... .......... .......... 44% 12.3M 9s
118000K .......... .......... .......... .......... .......... 44% 14.4M 9s
118050K .......... .......... .......... .......... .......... 44% 8.49M 9s
118100K .......... .......... .......... .......... .......... 44% 6.39M 9s
118150K .......... .......... .......... .......... .......... 44% 8.99M 9s
118200K .......... .......... .......... .......... .......... 44% 9.05M 9s
118250K .......... .......... .......... .......... .......... 44% 10.6M 9s
118300K .......... .......... .......... .......... .......... 44% 10.3M 9s
118350K .......... .......... .......... .......... .......... 44% 8.17M 9s
118400K .......... .......... .......... .......... .......... 44% 10.6M 9s
118450K .......... .......... .......... .......... .......... 44% 7.77M 9s
118500K .......... .......... .......... .......... .......... 44% 6.84M 9s
118550K .......... .......... .......... .......... .......... 44% 15.4M 9s
118600K .......... .......... .......... .......... .......... 44% 10.7M 9s
118650K .......... .......... .......... .......... .......... 44% 19.9M 9s
118700K .......... .......... .......... .......... .......... 44% 14.4M 9s
118750K .......... .......... .......... .......... .......... 44% 28.8M 9s
118800K .......... .......... .......... .......... .......... 44% 31.5M 9s
118850K .......... .......... .......... .......... .......... 44% 25.1M 9s
118900K .......... .......... .......... .......... .......... 44% 31.3M 9s
118950K .......... .......... .......... .......... .......... 44% 14.4M 9s
119000K .......... .......... .......... .......... .......... 44% 20.0M 9s
119050K .......... .......... .......... .......... .......... 44% 20.8M 9s
119100K .......... .......... .......... .......... .......... 44% 15.5M 9s
119150K .......... .......... .......... .......... .......... 44% 11.9M 9s
119200K .......... .......... .......... .......... .......... 44% 11.6M 9s
119250K .......... .......... .......... .......... .......... 44% 16.5M 9s
119300K .......... .......... .......... .......... .......... 44% 11.4M 9s
119350K .......... .......... .......... .......... .......... 44% 9.36M 9s
119400K .......... .......... .......... .......... .......... 44% 8.03M 9s
119450K .......... .......... .......... .......... .......... 44% 9.08M 9s
119500K .......... .......... .......... .......... .......... 44% 7.55M 9s
119550K .......... .......... .......... .......... .......... 45% 14.0M 9s
119600K .......... .......... .......... .......... .......... 45% 13.4M 9s
119650K .......... .......... .......... .......... .......... 45% 188M 9s
119700K .......... .......... .......... .......... .......... 45% 21.3M 9s
119750K .......... .......... .......... .......... .......... 45% 17.0M 9s
119800K .......... .......... .......... .......... .......... 45% 204M 9s
119850K .......... .......... .......... .......... .......... 45% 19.5M 9s
119900K .......... .......... .......... .......... .......... 45% 25.8M 9s
119950K .......... .......... .......... .......... .......... 45% 20.3M 9s
120000K .......... .......... .......... .......... .......... 45% 27.1M 9s
120050K .......... .......... .......... .......... .......... 45% 25.4M 9s
120100K .......... .......... .......... .......... .......... 45% 21.4M 9s
120150K .......... .......... .......... .......... .......... 45% 23.2M 9s
120200K .......... .......... .......... .......... .......... 45% 20.0M 9s
120250K .......... .......... .......... .......... .......... 45% 24.0M 9s
120300K .......... .......... .......... .......... .......... 45% 21.7M 9s
120350K .......... .......... .......... .......... .......... 45% 20.1M 9s
120400K .......... .......... .......... .......... .......... 45% 31.5M 9s
120450K .......... .......... .......... .......... .......... 45% 18.4M 9s
120500K .......... .......... .......... .......... .......... 45% 5.39M 9s
120550K .......... .......... .......... .......... .......... 45% 30.7M 9s
120600K .......... .......... .......... .......... .......... 45% 6.55M 9s
120650K .......... .......... .......... .......... .......... 45% 13.4M 9s
120700K .......... .......... .......... .......... .......... 45% 11.2M 9s
120750K .......... .......... .......... .......... .......... 45% 12.3M 9s
120800K .......... .......... .......... .......... .......... 45% 11.7M 9s
120850K .......... .......... .......... .......... .......... 45% 12.5M 9s
120900K .......... .......... .......... .......... .......... 45% 11.2M 9s
120950K .......... .......... .......... .......... .......... 45% 11.6M 9s
121000K .......... .......... .......... .......... .......... 45% 10.6M 9s
121050K .......... .......... .......... .......... .......... 45% 15.3M 9s
121100K .......... .......... .......... .......... .......... 45% 5.94M 9s
121150K .......... .......... .......... .......... .......... 45% 10.2M 9s
121200K .......... .......... .......... .......... .......... 45% 8.87M 9s
121250K .......... .......... .......... .......... .......... 45% 10.0M 9s
121300K .......... .......... .......... .......... .......... 45% 8.84M 9s
121350K .......... .......... .......... .......... .......... 45% 6.65M 9s
121400K .......... .......... .......... .......... .......... 45% 11.9M 9s
121450K .......... .......... .......... .......... .......... 45% 5.81M 9s
121500K .......... .......... .......... .......... .......... 45% 14.2M 9s
121550K .......... .......... .......... .......... .......... 45% 14.5M 9s
121600K .......... .......... .......... .......... .......... 45% 13.0M 9s
121650K .......... .......... .......... .......... .......... 45% 14.1M 9s
121700K .......... .......... .......... .......... .......... 45% 13.3M 9s
121750K .......... .......... .......... .......... .......... 45% 14.7M 9s
121800K .......... .......... .......... .......... .......... 45% 11.5M 9s
121850K .......... .......... .......... .......... .......... 45% 11.9M 9s
121900K .......... .......... .......... .......... .......... 45% 9.21M 9s
121950K .......... .......... .......... .......... .......... 45% 16.5M 9s
122000K .......... .......... .......... .......... .......... 45% 18.3M 9s
122050K .......... .......... .......... .......... .......... 45% 21.3M 9s
122100K .......... .......... .......... .......... .......... 45% 19.5M 9s
122150K .......... .......... .......... .......... .......... 45% 17.4M 9s
122200K .......... .......... .......... .......... .......... 45% 12.8M 9s
122250K .......... .......... .......... .......... .......... 46% 34.9M 9s
122300K .......... .......... .......... .......... .......... 46% 23.1M 9s
122350K .......... .......... .......... .......... .......... 46% 21.9M 9s
122400K .......... .......... .......... .......... .......... 46% 11.8M 9s
122450K .......... .......... .......... .......... .......... 46% 31.0M 9s
122500K .......... .......... .......... .......... .......... 46% 16.3M 9s
122550K .......... .......... .......... .......... .......... 46% 16.0M 9s
122600K .......... .......... .......... .......... .......... 46% 13.7M 9s
122650K .......... .......... .......... .......... .......... 46% 13.5M 9s
122700K .......... .......... .......... .......... .......... 46% 11.8M 9s
122750K .......... .......... .......... .......... .......... 46% 14.9M 9s
122800K .......... .......... .......... .......... .......... 46% 16.3M 9s
122850K .......... .......... .......... .......... .......... 46% 10.2M 9s
122900K .......... .......... .......... .......... .......... 46% 15.7M 9s
122950K .......... .......... .......... .......... .......... 46% 7.41M 9s
123000K .......... .......... .......... .......... .......... 46% 6.89M 9s
123050K .......... .......... .......... .......... .......... 46% 4.34M 9s
123100K .......... .......... .......... .......... .......... 46% 11.6M 9s
123150K .......... .......... .......... .......... .......... 46% 19.6M 9s
123200K .......... .......... .......... .......... .......... 46% 10.6M 9s
123250K .......... .......... .......... .......... .......... 46% 37.8M 9s
123300K .......... .......... .......... .......... .......... 46% 18.5M 9s
123350K .......... .......... .......... .......... .......... 46% 15.7M 9s
123400K .......... .......... .......... .......... .......... 46% 19.5M 9s
123450K .......... .......... .......... .......... .......... 46% 18.5M 9s
123500K .......... .......... .......... .......... .......... 46% 17.6M 9s
123550K .......... .......... .......... .......... .......... 46% 31.9M 9s
123600K .......... .......... .......... .......... .......... 46% 26.0M 9s
123650K .......... .......... .......... .......... .......... 46% 21.7M 9s
123700K .......... .......... .......... .......... .......... 46% 12.1M 9s
123750K .......... .......... .......... .......... .......... 46% 20.1M 9s
123800K .......... .......... .......... .......... .......... 46% 19.6M 9s
123850K .......... .......... .......... .......... .......... 46% 13.2M 9s
123900K .......... .......... .......... .......... .......... 46% 14.3M 9s
123950K .......... .......... .......... .......... .......... 46% 28.0M 9s
124000K .......... .......... .......... .......... .......... 46% 15.0M 9s
124050K .......... .......... .......... .......... .......... 46% 13.3M 9s
124100K .......... .......... .......... .......... .......... 46% 12.6M 9s
124150K .......... .......... .......... .......... .......... 46% 10.4M 9s
124200K .......... .......... .......... .......... .......... 46% 29.6M 9s
124250K .......... .......... .......... .......... .......... 46% 13.4M 9s
124300K .......... .......... .......... .......... .......... 46% 19.0M 9s
124350K .......... .......... .......... .......... .......... 46% 19.8M 9s
124400K .......... .......... .......... .......... .......... 46% 34.2M 9s
124450K .......... .......... .......... .......... .......... 46% 23.8M 9s
124500K .......... .......... .......... .......... .......... 46% 23.2M 9s
124550K .......... .......... .......... .......... .......... 46% 3.48M 9s
124600K .......... .......... .......... .......... .......... 46% 25.9M 9s
124650K .......... .......... .......... .......... .......... 46% 26.8M 9s
124700K .......... .......... .......... .......... .......... 46% 22.1M 9s
124750K .......... .......... .......... .......... .......... 46% 36.5M 9s
124800K .......... .......... .......... .......... .......... 46% 28.3M 9s
124850K .......... .......... .......... .......... .......... 46% 34.7M 9s
124900K .......... .......... .......... .......... .......... 47% 72.1M 9s
124950K .......... .......... .......... .......... .......... 47% 48.3M 9s
125000K .......... .......... .......... .......... .......... 47% 17.4M 9s
125050K .......... .......... .......... .......... .......... 47% 384M 9s
125100K .......... .......... .......... .......... .......... 47% 273M 9s
125150K .......... .......... .......... .......... .......... 47% 25.4M 9s
125200K .......... .......... .......... .......... .......... 47% 55.4M 9s
125250K .......... .......... .......... .......... .......... 47% 388M 9s
125300K .......... .......... .......... .......... .......... 47% 18.6M 9s
125350K .......... .......... .......... .......... .......... 47% 50.5M 9s
125400K .......... .......... .......... .......... .......... 47% 22.5M 9s
125450K .......... .......... .......... .......... .......... 47% 11.9M 9s
125500K .......... .......... .......... .......... .......... 47% 20.0M 9s
125550K .......... .......... .......... .......... .......... 47% 21.0M 9s
125600K .......... .......... .......... .......... .......... 47% 13.1M 9s
125650K .......... .......... .......... .......... .......... 47% 21.1M 9s
125700K .......... .......... .......... .......... .......... 47% 13.7M 9s
125750K .......... .......... .......... .......... .......... 47% 15.9M 9s
125800K .......... .......... .......... .......... .......... 47% 12.9M 9s
125850K .......... .......... .......... .......... .......... 47% 13.7M 9s
125900K .......... .......... .......... .......... .......... 47% 12.2M 9s
125950K .......... .......... .......... .......... .......... 47% 11.2M 9s
126000K .......... .......... .......... .......... .......... 47% 5.43M 9s
126050K .......... .......... .......... .......... .......... 47% 8.41M 9s
126100K .......... .......... .......... .......... .......... 47% 10.6M 9s
126150K .......... .......... .......... .......... .......... 47% 9.71M 9s
126200K .......... .......... .......... .......... .......... 47% 7.32M 9s
126250K .......... .......... .......... .......... .......... 47% 7.52M 9s
126300K .......... .......... .......... .......... .......... 47% 7.15M 9s
126350K .......... .......... .......... .......... .......... 47% 16.0M 9s
126400K .......... .......... .......... .......... .......... 47% 10.3M 9s
126450K .......... .......... .......... .......... .......... 47% 9.04M 9s
126500K .......... .......... .......... .......... .......... 47% 10.4M 9s
126550K .......... .......... .......... .......... .......... 47% 10.3M 9s
126600K .......... .......... .......... .......... .......... 47% 11.7M 9s
126650K .......... .......... .......... .......... .......... 47% 16.7M 9s
126700K .......... .......... .......... .......... .......... 47% 13.8M 9s
126750K .......... .......... .......... .......... .......... 47% 14.4M 9s
126800K .......... .......... .......... .......... .......... 47% 15.2M 9s
126850K .......... .......... .......... .......... .......... 47% 16.5M 9s
126900K .......... .......... .......... .......... .......... 47% 15.3M 9s
126950K .......... .......... .......... .......... .......... 47% 13.2M 9s
127000K .......... .......... .......... .......... .......... 47% 15.0M 9s
127050K .......... .......... .......... .......... .......... 47% 15.9M 9s
127100K .......... .......... .......... .......... .......... 47% 16.0M 9s
127150K .......... .......... .......... .......... .......... 47% 16.7M 9s
127200K .......... .......... .......... .......... .......... 47% 21.9M 9s
127250K .......... .......... .......... .......... .......... 47% 10.6M 9s
127300K .......... .......... .......... .......... .......... 47% 32.0M 9s
127350K .......... .......... .......... .......... .......... 47% 76.9M 9s
127400K .......... .......... .......... .......... .......... 47% 13.5M 9s
127450K .......... .......... .......... .......... .......... 47% 20.0M 9s
127500K .......... .......... .......... .......... .......... 47% 22.9M 9s
127550K .......... .......... .......... .......... .......... 48% 11.5M 9s
127600K .......... .......... .......... .......... .......... 48% 19.3M 9s
127650K .......... .......... .......... .......... .......... 48% 11.2M 9s
127700K .......... .......... .......... .......... .......... 48% 12.5M 9s
127750K .......... .......... .......... .......... .......... 48% 12.5M 9s
127800K .......... .......... .......... .......... .......... 48% 6.96M 9s
127850K .......... .......... .......... .......... .......... 48% 8.20M 9s
127900K .......... .......... .......... .......... .......... 48% 8.20M 9s
127950K .......... .......... .......... .......... .......... 48% 7.19M 9s
128000K .......... .......... .......... .......... .......... 48% 6.81M 9s
128050K .......... .......... .......... .......... .......... 48% 16.5M 9s
128100K .......... .......... .......... .......... .......... 48% 11.4M 9s
128150K .......... .......... .......... .......... .......... 48% 14.6M 9s
128200K .......... .......... .......... .......... .......... 48% 14.4M 9s
128250K .......... .......... .......... .......... .......... 48% 16.8M 9s
128300K .......... .......... .......... .......... .......... 48% 15.4M 9s
128350K .......... .......... .......... .......... .......... 48% 13.1M 9s
128400K .......... .......... .......... .......... .......... 48% 16.7M 9s
128450K .......... .......... .......... .......... .......... 48% 16.3M 9s
128500K .......... .......... .......... .......... .......... 48% 15.1M 9s
128550K .......... .......... .......... .......... .......... 48% 18.1M 9s
128600K .......... .......... .......... .......... .......... 48% 13.1M 9s
128650K .......... .......... .......... .......... .......... 48% 18.3M 9s
128700K .......... .......... .......... .......... .......... 48% 10.6M 9s
128750K .......... .......... .......... .......... .......... 48% 10.9M 9s
128800K .......... .......... .......... .......... .......... 48% 10.5M 9s
128850K .......... .......... .......... .......... .......... 48% 13.3M 9s
128900K .......... .......... .......... .......... .......... 48% 10.9M 9s
128950K .......... .......... .......... .......... .......... 48% 17.5M 9s
129000K .......... .......... .......... .......... .......... 48% 25.8M 9s
129050K .......... .......... .......... .......... .......... 48% 15.1M 9s
129100K .......... .......... .......... .......... .......... 48% 36.2M 9s
129150K .......... .......... .......... .......... .......... 48% 11.4M 9s
129200K .......... .......... .......... .......... .......... 48% 23.8M 9s
129250K .......... .......... .......... .......... .......... 48% 14.1M 9s
129300K .......... .......... .......... .......... .......... 48% 13.9M 9s
129350K .......... .......... .......... .......... .......... 48% 14.7M 9s
129400K .......... .......... .......... .......... .......... 48% 17.2M 9s
129450K .......... .......... .......... .......... .......... 48% 14.8M 9s
129500K .......... .......... .......... .......... .......... 48% 15.5M 9s
129550K .......... .......... .......... .......... .......... 48% 11.9M 9s
129600K .......... .......... .......... .......... .......... 48% 8.49M 9s
129650K .......... .......... .......... .......... .......... 48% 8.48M 9s
129700K .......... .......... .......... .......... .......... 48% 7.21M 9s
129750K .......... .......... .......... .......... .......... 48% 10.8M 9s
129800K .......... .......... .......... .......... .......... 48% 9.96M 9s
129850K .......... .......... .......... .......... .......... 48% 5.82M 9s
129900K .......... .......... .......... .......... .......... 48% 13.1M 9s
129950K .......... .......... .......... .......... .......... 48% 8.98M 9s
130000K .......... .......... .......... .......... .......... 48% 38.9M 9s
130050K .......... .......... .......... .......... .......... 48% 18.5M 9s
130100K .......... .......... .......... .......... .......... 48% 17.1M 9s
130150K .......... .......... .......... .......... .......... 48% 16.2M 9s
130200K .......... .......... .......... .......... .......... 49% 8.73M 9s
130250K .......... .......... .......... .......... .......... 49% 9.72M 9s
130300K .......... .......... .......... .......... .......... 49% 10.1M 9s
130350K .......... .......... .......... .......... .......... 49% 8.95M 9s
130400K .......... .......... .......... .......... .......... 49% 12.7M 9s
130450K .......... .......... .......... .......... .......... 49% 16.9M 9s
130500K .......... .......... .......... .......... .......... 49% 23.3M 9s
130550K .......... .......... .......... .......... .......... 49% 39.4M 9s
130600K .......... .......... .......... .......... .......... 49% 23.1M 9s
130650K .......... .......... .......... .......... .......... 49% 21.7M 9s
130700K .......... .......... .......... .......... .......... 49% 21.1M 9s
130750K .......... .......... .......... .......... .......... 49% 23.2M 9s
130800K .......... .......... .......... .......... .......... 49% 18.6M 9s
130850K .......... .......... .......... .......... .......... 49% 25.1M 9s
130900K .......... .......... .......... .......... .......... 49% 21.9M 9s
130950K .......... .......... .......... .......... .......... 49% 19.2M 9s
131000K .......... .......... .......... .......... .......... 49% 27.2M 9s
131050K .......... .......... .......... .......... .......... 49% 24.1M 9s
131100K .......... .......... .......... .......... .......... 49% 27.2M 9s
131150K .......... .......... .......... .......... .......... 49% 25.6M 9s
131200K .......... .......... .......... .......... .......... 49% 17.7M 9s
131250K .......... .......... .......... .......... .......... 49% 24.6M 9s
131300K .......... .......... .......... .......... .......... 49% 24.8M 9s
131350K .......... .......... .......... .......... .......... 49% 20.0M 9s
131400K .......... .......... .......... .......... .......... 49% 13.7M 9s
131450K .......... .......... .......... .......... .......... 49% 12.1M 9s
131500K .......... .......... .......... .......... .......... 49% 10.0M 9s
131550K .......... .......... .......... .......... .......... 49% 16.3M 9s
131600K .......... .......... .......... .......... .......... 49% 6.94M 9s
131650K .......... .......... .......... .......... .......... 49% 44.9M 8s
131700K .......... .......... .......... .......... .......... 49% 7.69M 8s
131750K .......... .......... .......... .......... .......... 49% 14.9M 8s
131800K .......... .......... .......... .......... .......... 49% 12.7M 8s
131850K .......... .......... .......... .......... .......... 49% 12.0M 8s
131900K .......... .......... .......... .......... .......... 49% 13.4M 8s
131950K .......... .......... .......... .......... .......... 49% 11.1M 8s
132000K .......... .......... .......... .......... .......... 49% 11.7M 8s
132050K .......... .......... .......... .......... .......... 49% 12.0M 8s
132100K .......... .......... .......... .......... .......... 49% 12.2M 8s
132150K .......... .......... .......... .......... .......... 49% 14.5M 8s
132200K .......... .......... .......... .......... .......... 49% 20.0M 8s
132250K .......... .......... .......... .......... .......... 49% 25.0M 8s
132300K .......... .......... .......... .......... .......... 49% 16.8M 8s
132350K .......... .......... .......... .......... .......... 49% 35.9M 8s
132400K .......... .......... .......... .......... .......... 49% 12.8M 8s
132450K .......... .......... .......... .......... .......... 49% 29.2M 8s
132500K .......... .......... .......... .......... .......... 49% 17.1M 8s
132550K .......... .......... .......... .......... .......... 49% 16.4M 8s
132600K .......... .......... .......... .......... .......... 49% 16.9M 8s
132650K .......... .......... .......... .......... .......... 49% 4.62M 8s
132700K .......... .......... .......... .......... .......... 49% 20.7M 8s
132750K .......... .......... .......... .......... .......... 49% 26.8M 8s
132800K .......... .......... .......... .......... .......... 49% 21.3M 8s
132850K .......... .......... .......... .......... .......... 50% 14.4M 8s
132900K .......... .......... .......... .......... .......... 50% 21.4M 8s
132950K .......... .......... .......... .......... .......... 50% 12.7M 8s
133000K .......... .......... .......... .......... .......... 50% 19.9M 8s
133050K .......... .......... .......... .......... .......... 50% 17.4M 8s
133100K .......... .......... .......... .......... .......... 50% 13.6M 8s
133150K .......... .......... .......... .......... .......... 50% 11.8M 8s
133200K .......... .......... .......... .......... .......... 50% 9.43M 8s
133250K .......... .......... .......... .......... .......... 50% 9.80M 8s
133300K .......... .......... .......... .......... .......... 50% 14.1M 8s
133350K .......... .......... .......... .......... .......... 50% 11.8M 8s
133400K .......... .......... .......... .......... .......... 50% 11.6M 8s
133450K .......... .......... .......... .......... .......... 50% 11.5M 8s
133500K .......... .......... .......... .......... .......... 50% 12.5M 8s
133550K .......... .......... .......... .......... .......... 50% 8.16M 8s
133600K .......... .......... .......... .......... .......... 50% 8.35M 8s
133650K .......... .......... .......... .......... .......... 50% 40.3M 8s
133700K .......... .......... .......... .......... .......... 50% 18.4M 8s
133750K .......... .......... .......... .......... .......... 50% 17.8M 8s
133800K .......... .......... .......... .......... .......... 50% 6.12M 8s
133850K .......... .......... .......... .......... .......... 50% 8.49M 8s
133900K .......... .......... .......... .......... .......... 50% 10.6M 8s
133950K .......... .......... .......... .......... .......... 50% 9.20M 8s
134000K .......... .......... .......... .......... .......... 50% 7.41M 8s
134050K .......... .......... .......... .......... .......... 50% 10.5M 8s
134100K .......... .......... .......... .......... .......... 50% 7.58M 8s
134150K .......... .......... .......... .......... .......... 50% 11.2M 8s
134200K .......... .......... .......... .......... .......... 50% 8.45M 8s
134250K .......... .......... .......... .......... .......... 50% 9.85M 8s
134300K .......... .......... .......... .......... .......... 50% 10.2M 8s
134350K .......... .......... .......... .......... .......... 50% 7.27M 8s
134400K .......... .......... .......... .......... .......... 50% 10.2M 8s
134450K .......... .......... .......... .......... .......... 50% 9.18M 8s
134500K .......... .......... .......... .......... .......... 50% 21.5M 8s
134550K .......... .......... .......... .......... .......... 50% 15.9M 8s
134600K .......... .......... .......... .......... .......... 50% 10.6M 8s
134650K .......... .......... .......... .......... .......... 50% 18.0M 8s
134700K .......... .......... .......... .......... .......... 50% 13.4M 8s
134750K .......... .......... .......... .......... .......... 50% 20.6M 8s
134800K .......... .......... .......... .......... .......... 50% 15.7M 8s
134850K .......... .......... .......... .......... .......... 50% 15.6M 8s
134900K .......... .......... .......... .......... .......... 50% 16.0M 8s
134950K .......... .......... .......... .......... .......... 50% 13.1M 8s
135000K .......... .......... .......... .......... .......... 50% 15.9M 8s
135050K .......... .......... .......... .......... .......... 50% 23.5M 8s
135100K .......... .......... .......... .......... .......... 50% 13.1M 8s
135150K .......... .......... .......... .......... .......... 50% 18.9M 8s
135200K .......... .......... .......... .......... .......... 50% 14.6M 8s
135250K .......... .......... .......... .......... .......... 50% 17.2M 8s
135300K .......... .......... .......... .......... .......... 50% 18.4M 8s
135350K .......... .......... .......... .......... .......... 50% 19.7M 8s
135400K .......... .......... .......... .......... .......... 50% 26.5M 8s
135450K .......... .......... .......... .......... .......... 50% 40.5M 8s
135500K .......... .......... .......... .......... .......... 51% 122M 8s
135550K .......... .......... .......... .......... .......... 51% 29.9M 8s
135600K .......... .......... .......... .......... .......... 51% 40.4M 8s
135650K .......... .......... .......... .......... .......... 51% 10.4M 8s
135700K .......... .......... .......... .......... .......... 51% 196M 8s
135750K .......... .......... .......... .......... .......... 51% 456M 8s
135800K .......... .......... .......... .......... .......... 51% 25.2M 8s
135850K .......... .......... .......... .......... .......... 51% 356M 8s
135900K .......... .......... .......... .......... .......... 51% 198M 8s
135950K .......... .......... .......... .......... .......... 51% 25.6M 8s
136000K .......... .......... .......... .......... .......... 51% 36.7M 8s
136050K .......... .......... .......... .......... .......... 51% 22.2M 8s
136100K .......... .......... .......... .......... .......... 51% 35.4M 8s
136150K .......... .......... .......... .......... .......... 51% 34.0M 8s
136200K .......... .......... .......... .......... .......... 51% 23.5M 8s
136250K .......... .......... .......... .......... .......... 51% 25.4M 8s
136300K .......... .......... .......... .......... .......... 51% 25.1M 8s
136350K .......... .......... .......... .......... .......... 51% 26.1M 8s
136400K .......... .......... .......... .......... .......... 51% 32.1M 8s
136450K .......... .......... .......... .......... .......... 51% 24.5M 8s
136500K .......... .......... .......... .......... .......... 51% 23.7M 8s
136550K .......... .......... .......... .......... .......... 51% 31.2M 8s
136600K .......... .......... .......... .......... .......... 51% 28.7M 8s
136650K .......... .......... .......... .......... .......... 51% 36.7M 8s
136700K .......... .......... .......... .......... .......... 51% 22.8M 8s
136750K .......... .......... .......... .......... .......... 51% 16.6M 8s
136800K .......... .......... .......... .......... .......... 51% 55.7M 8s
136850K .......... .......... .......... .......... .......... 51% 12.8M 8s
136900K .......... .......... .......... .......... .......... 51% 29.7M 8s
136950K .......... .......... .......... .......... .......... 51% 18.7M 8s
137000K .......... .......... .......... .......... .......... 51% 16.6M 8s
137050K .......... .......... .......... .......... .......... 51% 8.00M 8s
137100K .......... .......... .......... .......... .......... 51% 7.91M 8s
137150K .......... .......... .......... .......... .......... 51% 9.04M 8s
137200K .......... .......... .......... .......... .......... 51% 9.32M 8s
137250K .......... .......... .......... .......... .......... 51% 8.90M 8s
137300K .......... .......... .......... .......... .......... 51% 15.6M 8s
137350K .......... .......... .......... .......... .......... 51% 14.0M 8s
137400K .......... .......... .......... .......... .......... 51% 13.3M 8s
137450K .......... .......... .......... .......... .......... 51% 11.6M 8s
137500K .......... .......... .......... .......... .......... 51% 14.7M 8s
137550K .......... .......... .......... .......... .......... 51% 12.4M 8s
137600K .......... .......... .......... .......... .......... 51% 6.43M 8s
137650K .......... .......... .......... .......... .......... 51% 22.9M 8s
137700K .......... .......... .......... .......... .......... 51% 13.5M 8s
137750K .......... .......... .......... .......... .......... 51% 13.3M 8s
137800K .......... .......... .......... .......... .......... 51% 17.1M 8s
137850K .......... .......... .......... .......... .......... 51% 15.5M 8s
137900K .......... .......... .......... .......... .......... 51% 15.5M 8s
137950K .......... .......... .......... .......... .......... 51% 13.5M 8s
138000K .......... .......... .......... .......... .......... 51% 14.6M 8s
138050K .......... .......... .......... .......... .......... 51% 16.6M 8s
138100K .......... .......... .......... .......... .......... 51% 15.9M 8s
138150K .......... .......... .......... .......... .......... 51% 15.1M 8s
138200K .......... .......... .......... .......... .......... 52% 17.0M 8s
138250K .......... .......... .......... .......... .......... 52% 14.0M 8s
138300K .......... .......... .......... .......... .......... 52% 19.0M 8s
138350K .......... .......... .......... .......... .......... 52% 20.2M 8s
138400K .......... .......... .......... .......... .......... 52% 18.2M 8s
138450K .......... .......... .......... .......... .......... 52% 15.8M 8s
138500K .......... .......... .......... .......... .......... 52% 20.3M 8s
138550K .......... .......... .......... .......... .......... 52% 19.8M 8s
138600K .......... .......... .......... .......... .......... 52% 15.2M 8s
138650K .......... .......... .......... .......... .......... 52% 18.9M 8s
138700K .......... .......... .......... .......... .......... 52% 14.0M 8s
138750K .......... .......... .......... .......... .......... 52% 20.6M 8s
138800K .......... .......... .......... .......... .......... 52% 23.6M 8s
138850K .......... .......... .......... .......... .......... 52% 37.7M 8s
138900K .......... .......... .......... .......... .......... 52% 44.8M 8s
138950K .......... .......... .......... .......... .......... 52% 8.14M 8s
139000K .......... .......... .......... .......... .......... 52% 73.8M 8s
139050K .......... .......... .......... .......... .......... 52% 201M 8s
139100K .......... .......... .......... .......... .......... 52% 28.1M 8s
139150K .......... .......... .......... .......... .......... 52% 15.1M 8s
139200K .......... .......... .......... .......... .......... 52% 38.4M 8s
139250K .......... .......... .......... .......... .......... 52% 32.1M 8s
139300K .......... .......... .......... .......... .......... 52% 22.6M 8s
139350K .......... .......... .......... .......... .......... 52% 17.7M 8s
139400K .......... .......... .......... .......... .......... 52% 18.4M 8s
139450K .......... .......... .......... .......... .......... 52% 19.1M 8s
139500K .......... .......... .......... .......... .......... 52% 12.2M 8s
139550K .......... .......... .......... .......... .......... 52% 17.5M 8s
139600K .......... .......... .......... .......... .......... 52% 18.0M 8s
139650K .......... .......... .......... .......... .......... 52% 16.7M 8s
139700K .......... .......... .......... .......... .......... 52% 13.6M 8s
139750K .......... .......... .......... .......... .......... 52% 18.2M 8s
139800K .......... .......... .......... .......... .......... 52% 10.2M 8s
139850K .......... .......... .......... .......... .......... 52% 14.6M 8s
139900K .......... .......... .......... .......... .......... 52% 17.2M 8s
139950K .......... .......... .......... .......... .......... 52% 21.7M 8s
140000K .......... .......... .......... .......... .......... 52% 50.4M 8s
140050K .......... .......... .......... .......... .......... 52% 28.1M 8s
140100K .......... .......... .......... .......... .......... 52% 24.8M 8s
140150K .......... .......... .......... .......... .......... 52% 31.0M 8s
140200K .......... .......... .......... .......... .......... 52% 24.4M 8s
140250K .......... .......... .......... .......... .......... 52% 26.8M 8s
140300K .......... .......... .......... .......... .......... 52% 19.0M 8s
140350K .......... .......... .......... .......... .......... 52% 29.9M 8s
140400K .......... .......... .......... .......... .......... 52% 32.7M 8s
140450K .......... .......... .......... .......... .......... 52% 17.0M 8s
140500K .......... .......... .......... .......... .......... 52% 20.0M 8s
140550K .......... .......... .......... .......... .......... 52% 18.4M 8s
140600K .......... .......... .......... .......... .......... 52% 12.2M 8s
140650K .......... .......... .......... .......... .......... 52% 12.9M 8s
140700K .......... .......... .......... .......... .......... 52% 18.3M 8s
140750K .......... .......... .......... .......... .......... 52% 19.8M 8s
140800K .......... .......... .......... .......... .......... 52% 22.7M 8s
140850K .......... .......... .......... .......... .......... 53% 15.4M 8s
140900K .......... .......... .......... .......... .......... 53% 17.1M 8s
140950K .......... .......... .......... .......... .......... 53% 17.2M 8s
141000K .......... .......... .......... .......... .......... 53% 23.6M 8s
141050K .......... .......... .......... .......... .......... 53% 17.3M 8s
141100K .......... .......... .......... .......... .......... 53% 17.0M 8s
141150K .......... .......... .......... .......... .......... 53% 23.1M 8s
141200K .......... .......... .......... .......... .......... 53% 16.1M 8s
141250K .......... .......... .......... .......... .......... 53% 14.2M 8s
141300K .......... .......... .......... .......... .......... 53% 12.2M 8s
141350K .......... .......... .......... .......... .......... 53% 16.2M 8s
141400K .......... .......... .......... .......... .......... 53% 18.1M 8s
141450K .......... .......... .......... .......... .......... 53% 13.9M 8s
141500K .......... .......... .......... .......... .......... 53% 15.9M 8s
141550K .......... .......... .......... .......... .......... 53% 20.1M 8s
141600K .......... .......... .......... .......... .......... 53% 15.9M 8s
141650K .......... .......... .......... .......... .......... 53% 18.1M 8s
141700K .......... .......... .......... .......... .......... 53% 17.1M 8s
141750K .......... .......... .......... .......... .......... 53% 16.4M 8s
141800K .......... .......... .......... .......... .......... 53% 20.4M 8s
141850K .......... .......... .......... .......... .......... 53% 12.9M 8s
141900K .......... .......... .......... .......... .......... 53% 22.5M 8s
141950K .......... .......... .......... .......... .......... 53% 18.8M 8s
142000K .......... .......... .......... .......... .......... 53% 25.7M 8s
142050K .......... .......... .......... .......... .......... 53% 8.92M 8s
142100K .......... .......... .......... .......... .......... 53% 311M 8s
142150K .......... .......... .......... .......... .......... 53% 15.4M 8s
142200K .......... .......... .......... .......... .......... 53% 14.6M 8s
142250K .......... .......... .......... .......... .......... 53% 25.7M 8s
142300K .......... .......... .......... .......... .......... 53% 13.9M 8s
142350K .......... .......... .......... .......... .......... 53% 13.7M 8s
142400K .......... .......... .......... .......... .......... 53% 34.5M 8s
142450K .......... .......... .......... .......... .......... 53% 11.9M 8s
142500K .......... .......... .......... .......... .......... 53% 12.5M 8s
142550K .......... .......... .......... .......... .......... 53% 16.4M 8s
142600K .......... .......... .......... .......... .......... 53% 14.2M 8s
142650K .......... .......... .......... .......... .......... 53% 14.0M 8s
142700K .......... .......... .......... .......... .......... 53% 9.26M 8s
142750K .......... .......... .......... .......... .......... 53% 16.7M 8s
142800K .......... .......... .......... .......... .......... 53% 16.5M 8s
142850K .......... .......... .......... .......... .......... 53% 12.0M 8s
142900K .......... .......... .......... .......... .......... 53% 15.2M 8s
142950K .......... .......... .......... .......... .......... 53% 13.3M 8s
143000K .......... .......... .......... .......... .......... 53% 11.5M 8s
143050K .......... .......... .......... .......... .......... 53% 11.7M 8s
143100K .......... .......... .......... .......... .......... 53% 9.88M 8s
143150K .......... .......... .......... .......... .......... 53% 9.57M 8s
143200K .......... .......... .......... .......... .......... 53% 10.9M 8s
143250K .......... .......... .......... .......... .......... 53% 12.5M 8s
143300K .......... .......... .......... .......... .......... 53% 11.2M 8s
143350K .......... .......... .......... .......... .......... 53% 7.15M 8s
143400K .......... .......... .......... .......... .......... 53% 16.0M 8s
143450K .......... .......... .......... .......... .......... 53% 9.46M 8s
143500K .......... .......... .......... .......... .......... 54% 10.2M 8s
143550K .......... .......... .......... .......... .......... 54% 7.76M 8s
143600K .......... .......... .......... .......... .......... 54% 9.12M 8s
143650K .......... .......... .......... .......... .......... 54% 12.0M 8s
143700K .......... .......... .......... .......... .......... 54% 9.60M 8s
143750K .......... .......... .......... .......... .......... 54% 16.5M 8s
143800K .......... .......... .......... .......... .......... 54% 14.5M 8s
143850K .......... .......... .......... .......... .......... 54% 13.9M 8s
143900K .......... .......... .......... .......... .......... 54% 14.9M 8s
143950K .......... .......... .......... .......... .......... 54% 10.5M 8s
144000K .......... .......... .......... .......... .......... 54% 14.8M 8s
144050K .......... .......... .......... .......... .......... 54% 22.2M 8s
144100K .......... .......... .......... .......... .......... 54% 22.7M 8s
144150K .......... .......... .......... .......... .......... 54% 30.3M 8s
144200K .......... .......... .......... .......... .......... 54% 27.4M 8s
144250K .......... .......... .......... .......... .......... 54% 27.5M 8s
144300K .......... .......... .......... .......... .......... 54% 29.1M 8s
144350K .......... .......... .......... .......... .......... 54% 31.6M 8s
144400K .......... .......... .......... .......... .......... 54% 32.5M 8s
144450K .......... .......... .......... .......... .......... 54% 15.9M 8s
144500K .......... .......... .......... .......... .......... 54% 98.0M 8s
144550K .......... .......... .......... .......... .......... 54% 21.0M 8s
144600K .......... .......... .......... .......... .......... 54% 19.3M 8s
144650K .......... .......... .......... .......... .......... 54% 40.1M 8s
144700K .......... .......... .......... .......... .......... 54% 21.1M 8s
144750K .......... .......... .......... .......... .......... 54% 23.4M 8s
144800K .......... .......... .......... .......... .......... 54% 33.8M 8s
144850K .......... .......... .......... .......... .......... 54% 24.1M 8s
144900K .......... .......... .......... .......... .......... 54% 22.5M 8s
144950K .......... .......... .......... .......... .......... 54% 23.1M 8s
145000K .......... .......... .......... .......... .......... 54% 29.8M 8s
145050K .......... .......... .......... .......... .......... 54% 20.0M 8s
145100K .......... .......... .......... .......... .......... 54% 23.2M 8s
145150K .......... .......... .......... .......... .......... 54% 25.8M 8s
145200K .......... .......... .......... .......... .......... 54% 15.7M 8s
145250K .......... .......... .......... .......... .......... 54% 27.3M 8s
145300K .......... .......... .......... .......... .......... 54% 28.5M 8s
145350K .......... .......... .......... .......... .......... 54% 26.9M 8s
145400K .......... .......... .......... .......... .......... 54% 25.3M 8s
145450K .......... .......... .......... .......... .......... 54% 21.3M 8s
145500K .......... .......... .......... .......... .......... 54% 15.4M 8s
145550K .......... .......... .......... .......... .......... 54% 18.8M 8s
145600K .......... .......... .......... .......... .......... 54% 14.5M 8s
145650K .......... .......... .......... .......... .......... 54% 10.4M 8s
145700K .......... .......... .......... .......... .......... 54% 12.2M 8s
145750K .......... .......... .......... .......... .......... 54% 15.2M 8s
145800K .......... .......... .......... .......... .......... 54% 11.9M 8s
145850K .......... .......... .......... .......... .......... 54% 16.0M 8s
145900K .......... .......... .......... .......... .......... 54% 13.2M 8s
145950K .......... .......... .......... .......... .......... 54% 12.7M 8s
146000K .......... .......... .......... .......... .......... 54% 14.5M 8s
146050K .......... .......... .......... .......... .......... 54% 15.9M 8s
146100K .......... .......... .......... .......... .......... 54% 13.1M 8s
146150K .......... .......... .......... .......... .......... 55% 17.4M 8s
146200K .......... .......... .......... .......... .......... 55% 41.7M 8s
146250K .......... .......... .......... .......... .......... 55% 45.6M 8s
146300K .......... .......... .......... .......... .......... 55% 41.9M 8s
146350K .......... .......... .......... .......... .......... 55% 16.7M 8s
146400K .......... .......... .......... .......... .......... 55% 59.7M 8s
146450K .......... .......... .......... .......... .......... 55% 50.1M 8s
146500K .......... .......... .......... .......... .......... 55% 92.0M 8s
146550K .......... .......... .......... .......... .......... 55% 25.3M 8s
146600K .......... .......... .......... .......... .......... 55% 18.0M 8s
146650K .......... .......... .......... .......... .......... 55% 158M 8s
146700K .......... .......... .......... .......... .......... 55% 22.5M 8s
146750K .......... .......... .......... .......... .......... 55% 29.3M 8s
146800K .......... .......... .......... .......... .......... 55% 26.5M 8s
146850K .......... .......... .......... .......... .......... 55% 18.8M 7s
146900K .......... .......... .......... .......... .......... 55% 19.9M 7s
146950K .......... .......... .......... .......... .......... 55% 14.6M 7s
147000K .......... .......... .......... .......... .......... 55% 46.6M 7s
147050K .......... .......... .......... .......... .......... 55% 21.6M 7s
147100K .......... .......... .......... .......... .......... 55% 15.3M 7s
147150K .......... .......... .......... .......... .......... 55% 23.2M 7s
147200K .......... .......... .......... .......... .......... 55% 18.7M 7s
147250K .......... .......... .......... .......... .......... 55% 15.7M 7s
147300K .......... .......... .......... .......... .......... 55% 18.0M 7s
147350K .......... .......... .......... .......... .......... 55% 21.0M 7s
147400K .......... .......... .......... .......... .......... 55% 10.2M 7s
147450K .......... .......... .......... .......... .......... 55% 13.9M 7s
147500K .......... .......... .......... .......... .......... 55% 14.0M 7s
147550K .......... .......... .......... .......... .......... 55% 11.7M 7s
147600K .......... .......... .......... .......... .......... 55% 11.2M 7s
147650K .......... .......... .......... .......... .......... 55% 15.2M 7s
147700K .......... .......... .......... .......... .......... 55% 10.0M 7s
147750K .......... .......... .......... .......... .......... 55% 13.8M 7s
147800K .......... .......... .......... .......... .......... 55% 12.3M 7s
147850K .......... .......... .......... .......... .......... 55% 12.1M 7s
147900K .......... .......... .......... .......... .......... 55% 13.1M 7s
147950K .......... .......... .......... .......... .......... 55% 10.6M 7s
148000K .......... .......... .......... .......... .......... 55% 16.7M 7s
148050K .......... .......... .......... .......... .......... 55% 23.8M 7s
148100K .......... .......... .......... .......... .......... 55% 25.4M 7s
148150K .......... .......... .......... .......... .......... 55% 16.3M 7s
148200K .......... .......... .......... .......... .......... 55% 31.1M 7s
148250K .......... .......... .......... .......... .......... 55% 17.5M 7s
148300K .......... .......... .......... .......... .......... 55% 15.8M 7s
148350K .......... .......... .......... .......... .......... 55% 22.9M 7s
148400K .......... .......... .......... .......... .......... 55% 11.8M 7s
148450K .......... .......... .......... .......... .......... 55% 10.6M 7s
148500K .......... .......... .......... .......... .......... 55% 16.6M 7s
148550K .......... .......... .......... .......... .......... 55% 11.8M 7s
148600K .......... .......... .......... .......... .......... 55% 11.2M 7s
148650K .......... .......... .......... .......... .......... 55% 11.8M 7s
148700K .......... .......... .......... .......... .......... 55% 9.68M 7s
148750K .......... .......... .......... .......... .......... 55% 17.3M 7s
148800K .......... .......... .......... .......... .......... 56% 7.77M 7s
148850K .......... .......... .......... .......... .......... 56% 11.0M 7s
148900K .......... .......... .......... .......... .......... 56% 13.0M 7s
148950K .......... .......... .......... .......... .......... 56% 14.1M 7s
149000K .......... .......... .......... .......... .......... 56% 13.9M 7s
149050K .......... .......... .......... .......... .......... 56% 43.6M 7s
149100K .......... .......... .......... .......... .......... 56% 10.7M 7s
149150K .......... .......... .......... .......... .......... 56% 19.8M 7s
149200K .......... .......... .......... .......... .......... 56% 13.0M 7s
149250K .......... .......... .......... .......... .......... 56% 14.7M 7s
149300K .......... .......... .......... .......... .......... 56% 14.2M 7s
149350K .......... .......... .......... .......... .......... 56% 12.4M 7s
149400K .......... .......... .......... .......... .......... 56% 14.9M 7s
149450K .......... .......... .......... .......... .......... 56% 16.6M 7s
149500K .......... .......... .......... .......... .......... 56% 21.1M 7s
149550K .......... .......... .......... .......... .......... 56% 13.9M 7s
149600K .......... .......... .......... .......... .......... 56% 13.9M 7s
149650K .......... .......... .......... .......... .......... 56% 16.1M 7s
149700K .......... .......... .......... .......... .......... 56% 6.95M 7s
149750K .......... .......... .......... .......... .......... 56% 12.6M 7s
149800K .......... .......... .......... .......... .......... 56% 23.5M 7s
149850K .......... .......... .......... .......... .......... 56% 13.8M 7s
149900K .......... .......... .......... .......... .......... 56% 13.6M 7s
149950K .......... .......... .......... .......... .......... 56% 10.4M 7s
150000K .......... .......... .......... .......... .......... 56% 7.97M 7s
150050K .......... .......... .......... .......... .......... 56% 16.8M 7s
150100K .......... .......... .......... .......... .......... 56% 11.8M 7s
150150K .......... .......... .......... .......... .......... 56% 9.63M 7s
150200K .......... .......... .......... .......... .......... 56% 9.08M 7s
150250K .......... .......... .......... .......... .......... 56% 6.42M 7s
150300K .......... .......... .......... .......... .......... 56% 8.29M 7s
150350K .......... .......... .......... .......... .......... 56% 10.7M 7s
150400K .......... .......... .......... .......... .......... 56% 19.7M 7s
150450K .......... .......... .......... .......... .......... 56% 30.4M 7s
150500K .......... .......... .......... .......... .......... 56% 28.4M 7s
150550K .......... .......... .......... .......... .......... 56% 15.1M 7s
150600K .......... .......... .......... .......... .......... 56% 32.9M 7s
150650K .......... .......... .......... .......... .......... 56% 37.7M 7s
150700K .......... .......... .......... .......... .......... 56% 20.8M 7s
150750K .......... .......... .......... .......... .......... 56% 15.7M 7s
150800K .......... .......... .......... .......... .......... 56% 18.0M 7s
150850K .......... .......... .......... .......... .......... 56% 18.8M 7s
150900K .......... .......... .......... .......... .......... 56% 28.3M 7s
150950K .......... .......... .......... .......... .......... 56% 17.0M 7s
151000K .......... .......... .......... .......... .......... 56% 16.9M 7s
151050K .......... .......... .......... .......... .......... 56% 19.0M 7s
151100K .......... .......... .......... .......... .......... 56% 17.9M 7s
151150K .......... .......... .......... .......... .......... 56% 20.1M 7s
151200K .......... .......... .......... .......... .......... 56% 17.2M 7s
151250K .......... .......... .......... .......... .......... 56% 18.8M 7s
151300K .......... .......... .......... .......... .......... 56% 22.4M 7s
151350K .......... .......... .......... .......... .......... 56% 18.6M 7s
151400K .......... .......... .......... .......... .......... 56% 16.6M 7s
151450K .......... .......... .......... .......... .......... 57% 16.6M 7s
151500K .......... .......... .......... .......... .......... 57% 27.4M 7s
151550K .......... .......... .......... .......... .......... 57% 21.3M 7s
151600K .......... .......... .......... .......... .......... 57% 13.5M 7s
151650K .......... .......... .......... .......... .......... 57% 31.7M 7s
151700K .......... .......... .......... .......... .......... 57% 11.2M 7s
151750K .......... .......... .......... .......... .......... 57% 19.4M 7s
151800K .......... .......... .......... .......... .......... 57% 7.77M 7s
151850K .......... .......... .......... .......... .......... 57% 11.5M 7s
151900K .......... .......... .......... .......... .......... 57% 12.6M 7s
151950K .......... .......... .......... .......... .......... 57% 15.8M 7s
152000K .......... .......... .......... .......... .......... 57% 14.6M 7s
152050K .......... .......... .......... .......... .......... 57% 14.9M 7s
152100K .......... .......... .......... .......... .......... 57% 7.79M 7s
152150K .......... .......... .......... .......... .......... 57% 12.8M 7s
152200K .......... .......... .......... .......... .......... 57% 15.8M 7s
152250K .......... .......... .......... .......... .......... 57% 15.1M 7s
152300K .......... .......... .......... .......... .......... 57% 16.5M 7s
152350K .......... .......... .......... .......... .......... 57% 13.4M 7s
152400K .......... .......... .......... .......... .......... 57% 19.3M 7s
152450K .......... .......... .......... .......... .......... 57% 14.6M 7s
152500K .......... .......... .......... .......... .......... 57% 15.5M 7s
152550K .......... .......... .......... .......... .......... 57% 15.6M 7s
152600K .......... .......... .......... .......... .......... 57% 10.5M 7s
152650K .......... .......... .......... .......... .......... 57% 14.2M 7s
152700K .......... .......... .......... .......... .......... 57% 9.82M 7s
152750K .......... .......... .......... .......... .......... 57% 17.6M 7s
152800K .......... .......... .......... .......... .......... 57% 23.3M 7s
152850K .......... .......... .......... .......... .......... 57% 12.5M 7s
152900K .......... .......... .......... .......... .......... 57% 14.7M 7s
152950K .......... .......... .......... .......... .......... 57% 28.6M 7s
153000K .......... .......... .......... .......... .......... 57% 13.3M 7s
153050K .......... .......... .......... .......... .......... 57% 30.2M 7s
153100K .......... .......... .......... .......... .......... 57% 16.9M 7s
153150K .......... .......... .......... .......... .......... 57% 22.0M 7s
153200K .......... .......... .......... .......... .......... 57% 16.2M 7s
153250K .......... .......... .......... .......... .......... 57% 23.6M 7s
153300K .......... .......... .......... .......... .......... 57% 20.0M 7s
153350K .......... .......... .......... .......... .......... 57% 15.5M 7s
153400K .......... .......... .......... .......... .......... 57% 16.9M 7s
153450K .......... .......... .......... .......... .......... 57% 14.7M 7s
153500K .......... .......... .......... .......... .......... 57% 26.6M 7s
153550K .......... .......... .......... .......... .......... 57% 18.8M 7s
153600K .......... .......... .......... .......... .......... 57% 19.0M 7s
153650K .......... .......... .......... .......... .......... 57% 25.3M 7s
153700K .......... .......... .......... .......... .......... 57% 14.4M 7s
153750K .......... .......... .......... .......... .......... 57% 14.5M 7s
153800K .......... .......... .......... .......... .......... 57% 15.2M 7s
153850K .......... .......... .......... .......... .......... 57% 13.8M 7s
153900K .......... .......... .......... .......... .......... 57% 13.1M 7s
153950K .......... .......... .......... .......... .......... 57% 10.9M 7s
154000K .......... .......... .......... .......... .......... 57% 11.6M 7s
154050K .......... .......... .......... .......... .......... 57% 19.8M 7s
154100K .......... .......... .......... .......... .......... 58% 9.21M 7s
154150K .......... .......... .......... .......... .......... 58% 24.5M 7s
154200K .......... .......... .......... .......... .......... 58% 17.8M 7s
154250K .......... .......... .......... .......... .......... 58% 23.8M 7s
154300K .......... .......... .......... .......... .......... 58% 26.7M 7s
154350K .......... .......... .......... .......... .......... 58% 19.0M 7s
154400K .......... .......... .......... .......... .......... 58% 22.2M 7s
154450K .......... .......... .......... .......... .......... 58% 19.9M 7s
154500K .......... .......... .......... .......... .......... 58% 27.0M 7s
154550K .......... .......... .......... .......... .......... 58% 23.3M 7s
154600K .......... .......... .......... .......... .......... 58% 23.7M 7s
154650K .......... .......... .......... .......... .......... 58% 26.2M 7s
154700K .......... .......... .......... .......... .......... 58% 19.2M 7s
154750K .......... .......... .......... .......... .......... 58% 25.1M 7s
154800K .......... .......... .......... .......... .......... 58% 19.1M 7s
154850K .......... .......... .......... .......... .......... 58% 20.9M 7s
154900K .......... .......... .......... .......... .......... 58% 22.4M 7s
154950K .......... .......... .......... .......... .......... 58% 15.5M 7s
155000K .......... .......... .......... .......... .......... 58% 8.35M 7s
155050K .......... .......... .......... .......... .......... 58% 167M 7s
155100K .......... .......... .......... .......... .......... 58% 15.7M 7s
155150K .......... .......... .......... .......... .......... 58% 13.0M 7s
155200K .......... .......... .......... .......... .......... 58% 12.4M 7s
155250K .......... .......... .......... .......... .......... 58% 13.8M 7s
155300K .......... .......... .......... .......... .......... 58% 12.0M 7s
155350K .......... .......... .......... .......... .......... 58% 12.7M 7s
155400K .......... .......... .......... .......... .......... 58% 15.4M 7s
155450K .......... .......... .......... .......... .......... 58% 11.5M 7s
155500K .......... .......... .......... .......... .......... 58% 8.60M 7s
155550K .......... .......... .......... .......... .......... 58% 20.8M 7s
155600K .......... .......... .......... .......... .......... 58% 9.21M 7s
155650K .......... .......... .......... .......... .......... 58% 12.8M 7s
155700K .......... .......... .......... .......... .......... 58% 10.1M 7s
155750K .......... .......... .......... .......... .......... 58% 11.9M 7s
155800K .......... .......... .......... .......... .......... 58% 9.54M 7s
155850K .......... .......... .......... .......... .......... 58% 10.3M 7s
155900K .......... .......... .......... .......... .......... 58% 17.3M 7s
155950K .......... .......... .......... .......... .......... 58% 15.6M 7s
156000K .......... .......... .......... .......... .......... 58% 17.0M 7s
156050K .......... .......... .......... .......... .......... 58% 11.5M 7s
156100K .......... .......... .......... .......... .......... 58% 7.06M 7s
156150K .......... .......... .......... .......... .......... 58% 16.5M 7s
156200K .......... .......... .......... .......... .......... 58% 11.9M 7s
156250K .......... .......... .......... .......... .......... 58% 24.5M 7s
156300K .......... .......... .......... .......... .......... 58% 27.8M 7s
156350K .......... .......... .......... .......... .......... 58% 28.0M 7s
156400K .......... .......... .......... .......... .......... 58% 27.9M 7s
156450K .......... .......... .......... .......... .......... 58% 36.0M 7s
156500K .......... .......... .......... .......... .......... 58% 31.5M 7s
156550K .......... .......... .......... .......... .......... 58% 37.1M 7s
156600K .......... .......... .......... .......... .......... 58% 17.5M 7s
156650K .......... .......... .......... .......... .......... 58% 189M 7s
156700K .......... .......... .......... .......... .......... 58% 19.6M 7s
156750K .......... .......... .......... .......... .......... 58% 20.2M 7s
156800K .......... .......... .......... .......... .......... 59% 13.5M 7s
156850K .......... .......... .......... .......... .......... 59% 13.3M 7s
156900K .......... .......... .......... .......... .......... 59% 15.4M 7s
156950K .......... .......... .......... .......... .......... 59% 12.9M 7s
157000K .......... .......... .......... .......... .......... 59% 13.0M 7s
157050K .......... .......... .......... .......... .......... 59% 14.0M 7s
157100K .......... .......... .......... .......... .......... 59% 8.62M 7s
157150K .......... .......... .......... .......... .......... 59% 10.7M 7s
157200K .......... .......... .......... .......... .......... 59% 7.72M 7s
157250K .......... .......... .......... .......... .......... 59% 10.8M 7s
157300K .......... .......... .......... .......... .......... 59% 17.9M 7s
157350K .......... .......... .......... .......... .......... 59% 10.4M 7s
157400K .......... .......... .......... .......... .......... 59% 59.8M 7s
157450K .......... .......... .......... .......... .......... 59% 12.3M 7s
157500K .......... .......... .......... .......... .......... 59% 12.7M 7s
157550K .......... .......... .......... .......... .......... 59% 20.8M 7s
157600K .......... .......... .......... .......... .......... 59% 19.5M 7s
157650K .......... .......... .......... .......... .......... 59% 22.4M 7s
157700K .......... .......... .......... .......... .......... 59% 16.7M 7s
157750K .......... .......... .......... .......... .......... 59% 23.1M 7s
157800K .......... .......... .......... .......... .......... 59% 16.1M 7s
157850K .......... .......... .......... .......... .......... 59% 19.2M 7s
157900K .......... .......... .......... .......... .......... 59% 24.1M 7s
157950K .......... .......... .......... .......... .......... 59% 15.3M 7s
158000K .......... .......... .......... .......... .......... 59% 13.7M 7s
158050K .......... .......... .......... .......... .......... 59% 21.2M 7s
158100K .......... .......... .......... .......... .......... 59% 17.3M 7s
158150K .......... .......... .......... .......... .......... 59% 20.4M 7s
158200K .......... .......... .......... .......... .......... 59% 15.6M 7s
158250K .......... .......... .......... .......... .......... 59% 19.2M 7s
158300K .......... .......... .......... .......... .......... 59% 16.1M 7s
158350K .......... .......... .......... .......... .......... 59% 16.8M 7s
158400K .......... .......... .......... .......... .......... 59% 11.2M 7s
158450K .......... .......... .......... .......... .......... 59% 11.4M 7s
158500K .......... .......... .......... .......... .......... 59% 10.5M 7s
158550K .......... .......... .......... .......... .......... 59% 14.6M 7s
158600K .......... .......... .......... .......... .......... 59% 6.62M 7s
158650K .......... .......... .......... .......... .......... 59% 76.2M 7s
158700K .......... .......... .......... .......... .......... 59% 30.1M 7s
158750K .......... .......... .......... .......... .......... 59% 19.1M 7s
158800K .......... .......... .......... .......... .......... 59% 21.1M 7s
158850K .......... .......... .......... .......... .......... 59% 16.3M 7s
158900K .......... .......... .......... .......... .......... 59% 11.1M 7s
158950K .......... .......... .......... .......... .......... 59% 11.2M 7s
159000K .......... .......... .......... .......... .......... 59% 13.2M 7s
159050K .......... .......... .......... .......... .......... 59% 15.7M 7s
159100K .......... .......... .......... .......... .......... 59% 10.9M 7s
159150K .......... .......... .......... .......... .......... 59% 12.6M 7s
159200K .......... .......... .......... .......... .......... 59% 12.8M 7s
159250K .......... .......... .......... .......... .......... 59% 12.8M 7s
159300K .......... .......... .......... .......... .......... 59% 13.0M 7s
159350K .......... .......... .......... .......... .......... 59% 12.3M 7s
159400K .......... .......... .......... .......... .......... 59% 7.96M 7s
159450K .......... .......... .......... .......... .......... 60% 18.0M 7s
159500K .......... .......... .......... .......... .......... 60% 12.7M 7s
159550K .......... .......... .......... .......... .......... 60% 9.98M 7s
159600K .......... .......... .......... .......... .......... 60% 25.3M 7s
159650K .......... .......... .......... .......... .......... 60% 10.6M 7s
159700K .......... .......... .......... .......... .......... 60% 12.5M 7s
159750K .......... .......... .......... .......... .......... 60% 12.3M 7s
159800K .......... .......... .......... .......... .......... 60% 14.3M 7s
159850K .......... .......... .......... .......... .......... 60% 11.1M 7s
159900K .......... .......... .......... .......... .......... 60% 14.7M 7s
159950K .......... .......... .......... .......... .......... 60% 10.8M 7s
160000K .......... .......... .......... .......... .......... 60% 20.0M 7s
160050K .......... .......... .......... .......... .......... 60% 14.2M 7s
160100K .......... .......... .......... .......... .......... 60% 11.8M 7s
160150K .......... .......... .......... .......... .......... 60% 9.77M 7s
160200K .......... .......... .......... .......... .......... 60% 6.52M 7s
160250K .......... .......... .......... .......... .......... 60% 10.9M 7s
160300K .......... .......... .......... .......... .......... 60% 11.6M 7s
160350K .......... .......... .......... .......... .......... 60% 10.8M 7s
160400K .......... .......... .......... .......... .......... 60% 13.1M 7s
160450K .......... .......... .......... .......... .......... 60% 12.4M 7s
160500K .......... .......... .......... .......... .......... 60% 10.4M 7s
160550K .......... .......... .......... .......... .......... 60% 11.3M 7s
160600K .......... .......... .......... .......... .......... 60% 9.28M 7s
160650K .......... .......... .......... .......... .......... 60% 17.7M 7s
160700K .......... .......... .......... .......... .......... 60% 14.3M 7s
160750K .......... .......... .......... .......... .......... 60% 12.3M 7s
160800K .......... .......... .......... .......... .......... 60% 18.6M 7s
160850K .......... .......... .......... .......... .......... 60% 15.1M 7s
160900K .......... .......... .......... .......... .......... 60% 18.2M 7s
160950K .......... .......... .......... .......... .......... 60% 13.7M 7s
161000K .......... .......... .......... .......... .......... 60% 181M 7s
161050K .......... .......... .......... .......... .......... 60% 21.9M 7s
161100K .......... .......... .......... .......... .......... 60% 15.1M 7s
161150K .......... .......... .......... .......... .......... 60% 23.9M 7s
161200K .......... .......... .......... .......... .......... 60% 15.2M 7s
161250K .......... .......... .......... .......... .......... 60% 23.7M 7s
161300K .......... .......... .......... .......... .......... 60% 19.9M 7s
161350K .......... .......... .......... .......... .......... 60% 14.1M 7s
161400K .......... .......... .......... .......... .......... 60% 19.1M 7s
161450K .......... .......... .......... .......... .......... 60% 16.2M 7s
161500K .......... .......... .......... .......... .......... 60% 14.1M 7s
161550K .......... .......... .......... .......... .......... 60% 21.2M 7s
161600K .......... .......... .......... .......... .......... 60% 10.2M 7s
161650K .......... .......... .......... .......... .......... 60% 29.2M 7s
161700K .......... .......... .......... .......... .......... 60% 18.4M 7s
161750K .......... .......... .......... .......... .......... 60% 18.8M 7s
161800K .......... .......... .......... .......... .......... 60% 113M 7s
161850K .......... .......... .......... .......... .......... 60% 15.5M 7s
161900K .......... .......... .......... .......... .......... 60% 7.33M 7s
161950K .......... .......... .......... .......... .......... 60% 80.6M 7s
162000K .......... .......... .......... .......... .......... 60% 128M 7s
162050K .......... .......... .......... .......... .......... 60% 23.9M 7s
162100K .......... .......... .......... .......... .......... 61% 14.5M 7s
162150K .......... .......... .......... .......... .......... 61% 9.00M 7s
162200K .......... .......... .......... .......... .......... 61% 20.7M 7s
162250K .......... .......... .......... .......... .......... 61% 14.2M 7s
162300K .......... .......... .......... .......... .......... 61% 13.5M 7s
162350K .......... .......... .......... .......... .......... 61% 14.2M 7s
162400K .......... .......... .......... .......... .......... 61% 14.4M 7s
162450K .......... .......... .......... .......... .......... 61% 13.0M 7s
162500K .......... .......... .......... .......... .......... 61% 14.9M 7s
162550K .......... .......... .......... .......... .......... 61% 16.1M 7s
162600K .......... .......... .......... .......... .......... 61% 10.6M 7s
162650K .......... .......... .......... .......... .......... 61% 12.1M 7s
162700K .......... .......... .......... .......... .......... 61% 14.6M 7s
162750K .......... .......... .......... .......... .......... 61% 12.1M 7s
162800K .......... .......... .......... .......... .......... 61% 18.6M 7s
162850K .......... .......... .......... .......... .......... 61% 11.7M 7s
162900K .......... .......... .......... .......... .......... 61% 11.2M 7s
162950K .......... .......... .......... .......... .......... 61% 13.1M 7s
163000K .......... .......... .......... .......... .......... 61% 11.6M 7s
163050K .......... .......... .......... .......... .......... 61% 17.6M 7s
163100K .......... .......... .......... .......... .......... 61% 18.3M 7s
163150K .......... .......... .......... .......... .......... 61% 20.9M 6s
163200K .......... .......... .......... .......... .......... 61% 13.8M 6s
163250K .......... .......... .......... .......... .......... 61% 16.5M 6s
163300K .......... .......... .......... .......... .......... 61% 22.0M 6s
163350K .......... .......... .......... .......... .......... 61% 8.31M 6s
163400K .......... .......... .......... .......... .......... 61% 18.3M 6s
163450K .......... .......... .......... .......... .......... 61% 12.5M 6s
163500K .......... .......... .......... .......... .......... 61% 12.1M 6s
163550K .......... .......... .......... .......... .......... 61% 13.0M 6s
163600K .......... .......... .......... .......... .......... 61% 18.3M 6s
163650K .......... .......... .......... .......... .......... 61% 20.8M 6s
163700K .......... .......... .......... .......... .......... 61% 9.59M 6s
163750K .......... .......... .......... .......... .......... 61% 8.74M 6s
163800K .......... .......... .......... .......... .......... 61% 8.37M 6s
163850K .......... .......... .......... .......... .......... 61% 5.23M 6s
163900K .......... .......... .......... .......... .......... 61% 5.49M 6s
163950K .......... .......... .......... .......... .......... 61% 6.27M 6s
164000K .......... .......... .......... .......... .......... 61% 8.04M 6s
164050K .......... .......... .......... .......... .......... 61% 7.09M 6s
164100K .......... .......... .......... .......... .......... 61% 9.77M 6s
164150K .......... .......... .......... .......... .......... 61% 13.7M 6s
164200K .......... .......... .......... .......... .......... 61% 9.44M 6s
164250K .......... .......... .......... .......... .......... 61% 14.5M 6s
164300K .......... .......... .......... .......... .......... 61% 13.9M 6s
164350K .......... .......... .......... .......... .......... 61% 10.2M 6s
164400K .......... .......... .......... .......... .......... 61% 17.1M 6s
164450K .......... .......... .......... .......... .......... 61% 12.7M 6s
164500K .......... .......... .......... .......... .......... 61% 11.4M 6s
164550K .......... .......... .......... .......... .......... 61% 17.5M 6s
164600K .......... .......... .......... .......... .......... 61% 14.2M 6s
164650K .......... .......... .......... .......... .......... 61% 15.9M 6s
164700K .......... .......... .......... .......... .......... 61% 10.6M 6s
164750K .......... .......... .......... .......... .......... 62% 28.9M 6s
164800K .......... .......... .......... .......... .......... 62% 26.9M 6s
164850K .......... .......... .......... .......... .......... 62% 15.3M 6s
164900K .......... .......... .......... .......... .......... 62% 15.2M 6s
164950K .......... .......... .......... .......... .......... 62% 8.39M 6s
165000K .......... .......... .......... .......... .......... 62% 9.31M 6s
165050K .......... .......... .......... .......... .......... 62% 10.6M 6s
165100K .......... .......... .......... .......... .......... 62% 9.95M 6s
165150K .......... .......... .......... .......... .......... 62% 8.84M 6s
165200K .......... .......... .......... .......... .......... 62% 12.7M 6s
165250K .......... .......... .......... .......... .......... 62% 11.8M 6s
165300K .......... .......... .......... .......... .......... 62% 10.0M 6s
165350K .......... .......... .......... .......... .......... 62% 9.27M 6s
165400K .......... .......... .......... .......... .......... 62% 10.8M 6s
165450K .......... .......... .......... .......... .......... 62% 9.34M 6s
165500K .......... .......... .......... .......... .......... 62% 8.73M 6s
165550K .......... .......... .......... .......... .......... 62% 10.7M 6s
165600K .......... .......... .......... .......... .......... 62% 20.4M 6s
165650K .......... .......... .......... .......... .......... 62% 15.5M 6s
165700K .......... .......... .......... .......... .......... 62% 13.8M 6s
165750K .......... .......... .......... .......... .......... 62% 13.1M 6s
165800K .......... .......... .......... .......... .......... 62% 12.7M 6s
165850K .......... .......... .......... .......... .......... 62% 15.8M 6s
165900K .......... .......... .......... .......... .......... 62% 22.3M 6s
165950K .......... .......... .......... .......... .......... 62% 15.2M 6s
166000K .......... .......... .......... .......... .......... 62% 14.3M 6s
166050K .......... .......... .......... .......... .......... 62% 20.6M 6s
166100K .......... .......... .......... .......... .......... 62% 15.3M 6s
166150K .......... .......... .......... .......... .......... 62% 18.1M 6s
166200K .......... .......... .......... .......... .......... 62% 16.6M 6s
166250K .......... .......... .......... .......... .......... 62% 19.8M 6s
166300K .......... .......... .......... .......... .......... 62% 13.5M 6s
166350K .......... .......... .......... .......... .......... 62% 23.4M 6s
166400K .......... .......... .......... .......... .......... 62% 24.5M 6s
166450K .......... .......... .......... .......... .......... 62% 21.8M 6s
166500K .......... .......... .......... .......... .......... 62% 16.7M 6s
166550K .......... .......... .......... .......... .......... 62% 21.3M 6s
166600K .......... .......... .......... .......... .......... 62% 17.2M 6s
166650K .......... .......... .......... .......... .......... 62% 23.9M 6s
166700K .......... .......... .......... .......... .......... 62% 21.8M 6s
166750K .......... .......... .......... .......... .......... 62% 20.3M 6s
166800K .......... .......... .......... .......... .......... 62% 25.3M 6s
166850K .......... .......... .......... .......... .......... 62% 17.4M 6s
166900K .......... .......... .......... .......... .......... 62% 24.9M 6s
166950K .......... .......... .......... .......... .......... 62% 17.3M 6s
167000K .......... .......... .......... .......... .......... 62% 11.8M 6s
167050K .......... .......... .......... .......... .......... 62% 8.17M 6s
167100K .......... .......... .......... .......... .......... 62% 7.41M 6s
167150K .......... .......... .......... .......... .......... 62% 11.0M 6s
167200K .......... .......... .......... .......... .......... 62% 14.5M 6s
167250K .......... .......... .......... .......... .......... 62% 16.5M 6s
167300K .......... .......... .......... .......... .......... 62% 11.8M 6s
167350K .......... .......... .......... .......... .......... 62% 11.2M 6s
167400K .......... .......... .......... .......... .......... 63% 7.06M 6s
167450K .......... .......... .......... .......... .......... 63% 7.54M 6s
167500K .......... .......... .......... .......... .......... 63% 18.7M 6s
167550K .......... .......... .......... .......... .......... 63% 12.7M 6s
167600K .......... .......... .......... .......... .......... 63% 11.0M 6s
167650K .......... .......... .......... .......... .......... 63% 12.8M 6s
167700K .......... .......... .......... .......... .......... 63% 10.8M 6s
167750K .......... .......... .......... .......... .......... 63% 14.2M 6s
167800K .......... .......... .......... .......... .......... 63% 13.9M 6s
167850K .......... .......... .......... .......... .......... 63% 11.6M 6s
167900K .......... .......... .......... .......... .......... 63% 14.6M 6s
167950K .......... .......... .......... .......... .......... 63% 16.5M 6s
168000K .......... .......... .......... .......... .......... 63% 19.9M 6s
168050K .......... .......... .......... .......... .......... 63% 30.9M 6s
168100K .......... .......... .......... .......... .......... 63% 14.0M 6s
168150K .......... .......... .......... .......... .......... 63% 21.8M 6s
168200K .......... .......... .......... .......... .......... 63% 14.5M 6s
168250K .......... .......... .......... .......... .......... 63% 34.3M 6s
168300K .......... .......... .......... .......... .......... 63% 11.2M 6s
168350K .......... .......... .......... .......... .......... 63% 8.38M 6s
168400K .......... .......... .......... .......... .......... 63% 10.0M 6s
168450K .......... .......... .......... .......... .......... 63% 7.53M 6s
168500K .......... .......... .......... .......... .......... 63% 7.50M 6s
168550K .......... .......... .......... .......... .......... 63% 5.28M 6s
168600K .......... .......... .......... .......... .......... 63% 6.26M 6s
168650K .......... .......... .......... .......... .......... 63% 8.18M 6s
168700K .......... .......... .......... .......... .......... 63% 8.91M 6s
168750K .......... .......... .......... .......... .......... 63% 5.53M 6s
168800K .......... .......... .......... .......... .......... 63% 26.7M 6s
168850K .......... .......... .......... .......... .......... 63% 9.85M 6s
168900K .......... .......... .......... .......... .......... 63% 15.0M 6s
168950K .......... .......... .......... .......... .......... 63% 13.3M 6s
169000K .......... .......... .......... .......... .......... 63% 13.7M 6s
169050K .......... .......... .......... .......... .......... 63% 15.7M 6s
169100K .......... .......... .......... .......... .......... 63% 14.6M 6s
169150K .......... .......... .......... .......... .......... 63% 17.3M 6s
169200K .......... .......... .......... .......... .......... 63% 15.6M 6s
169250K .......... .......... .......... .......... .......... 63% 14.3M 6s
169300K .......... .......... .......... .......... .......... 63% 15.4M 6s
169350K .......... .......... .......... .......... .......... 63% 14.5M 6s
169400K .......... .......... .......... .......... .......... 63% 15.2M 6s
169450K .......... .......... .......... .......... .......... 63% 12.4M 6s
169500K .......... .......... .......... .......... .......... 63% 7.54M 6s
169550K .......... .......... .......... .......... .......... 63% 12.0M 6s
169600K .......... .......... .......... .......... .......... 63% 8.40M 6s
169650K .......... .......... .......... .......... .......... 63% 6.49M 6s
169700K .......... .......... .......... .......... .......... 63% 155M 6s
169750K .......... .......... .......... .......... .......... 63% 10.7M 6s
169800K .......... .......... .......... .......... .......... 63% 8.44M 6s
169850K .......... .......... .......... .......... .......... 63% 13.4M 6s
169900K .......... .......... .......... .......... .......... 63% 11.4M 6s
169950K .......... .......... .......... .......... .......... 63% 8.71M 6s
170000K .......... .......... .......... .......... .......... 63% 10.8M 6s
170050K .......... .......... .......... .......... .......... 64% 7.86M 6s
170100K .......... .......... .......... .......... .......... 64% 21.1M 6s
170150K .......... .......... .......... .......... .......... 64% 15.6M 6s
170200K .......... .......... .......... .......... .......... 64% 9.15M 6s
170250K .......... .......... .......... .......... .......... 64% 6.17M 6s
170300K .......... .......... .......... .......... .......... 64% 12.5M 6s
170350K .......... .......... .......... .......... .......... 64% 8.11M 6s
170400K .......... .......... .......... .......... .......... 64% 6.18M 6s
170450K .......... .......... .......... .......... .......... 64% 7.21M 6s
170500K .......... .......... .......... .......... .......... 64% 7.83M 6s
170550K .......... .......... .......... .......... .......... 64% 5.31M 6s
170600K .......... .......... .......... .......... .......... 64% 20.8M 6s
170650K .......... .......... .......... .......... .......... 64% 11.7M 6s
170700K .......... .......... .......... .......... .......... 64% 7.64M 6s
170750K .......... .......... .......... .......... .......... 64% 9.01M 6s
170800K .......... .......... .......... .......... .......... 64% 11.3M 6s
170850K .......... .......... .......... .......... .......... 64% 9.84M 6s
170900K .......... .......... .......... .......... .......... 64% 13.1M 6s
170950K .......... .......... .......... .......... .......... 64% 11.2M 6s
171000K .......... .......... .......... .......... .......... 64% 11.6M 6s
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171100K .......... .......... .......... .......... .......... 64% 9.45M 6s
171150K .......... .......... .......... .......... .......... 64% 12.2M 6s
171200K .......... .......... .......... .......... .......... 64% 7.15M 6s
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171300K .......... .......... .......... .......... .......... 64% 10.4M 6s
171350K .......... .......... .......... .......... .......... 64% 11.2M 6s
171400K .......... .......... .......... .......... .......... 64% 21.2M 6s
171450K .......... .......... .......... .......... .......... 64% 14.5M 6s
171500K .......... .......... .......... .......... .......... 64% 19.9M 6s
171550K .......... .......... .......... .......... .......... 64% 13.4M 6s
171600K .......... .......... .......... .......... .......... 64% 11.6M 6s
171650K .......... .......... .......... .......... .......... 64% 14.8M 6s
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171800K .......... .......... .......... .......... .......... 64% 13.9M 6s
171850K .......... .......... .......... .......... .......... 64% 17.0M 6s
171900K .......... .......... .......... .......... .......... 64% 20.0M 6s
171950K .......... .......... .......... .......... .......... 64% 21.3M 6s
172000K .......... .......... .......... .......... .......... 64% 7.33M 6s
172050K .......... .......... .......... .......... .......... 64% 153M 6s
172100K .......... .......... .......... .......... .......... 64% 21.6M 6s
172150K .......... .......... .......... .......... .......... 64% 14.7M 6s
172200K .......... .......... .......... .......... .......... 64% 22.3M 6s
172250K .......... .......... .......... .......... .......... 64% 21.6M 6s
172300K .......... .......... .......... .......... .......... 64% 17.1M 6s
172350K .......... .......... .......... .......... .......... 64% 15.5M 6s
172400K .......... .......... .......... .......... .......... 64% 11.7M 6s
172450K .......... .......... .......... .......... .......... 64% 20.6M 6s
172500K .......... .......... .......... .......... .......... 64% 15.3M 6s
172550K .......... .......... .......... .......... .......... 64% 16.6M 6s
172600K .......... .......... .......... .......... .......... 64% 15.1M 6s
172650K .......... .......... .......... .......... .......... 64% 8.50M 6s
172700K .......... .......... .......... .......... .......... 64% 5.48M 6s
172750K .......... .......... .......... .......... .......... 65% 6.85M 6s
172800K .......... .......... .......... .......... .......... 65% 5.70M 6s
172850K .......... .......... .......... .......... .......... 65% 6.14M 6s
172900K .......... .......... .......... .......... .......... 65% 3.92M 6s
172950K .......... .......... .......... .......... .......... 65% 7.18M 6s
173000K .......... .......... .......... .......... .......... 65% 16.3M 6s
173050K .......... .......... .......... .......... .......... 65% 11.0M 6s
173100K .......... .......... .......... .......... .......... 65% 9.36M 6s
173150K .......... .......... .......... .......... .......... 65% 15.4M 6s
173200K .......... .......... .......... .......... .......... 65% 7.17M 6s
173250K .......... .......... .......... .......... .......... 65% 13.6M 6s
173300K .......... .......... .......... .......... .......... 65% 9.17M 6s
173350K .......... .......... .......... .......... .......... 65% 7.54M 6s
173400K .......... .......... .......... .......... .......... 65% 8.24M 6s
173450K .......... .......... .......... .......... .......... 65% 6.99M 6s
173500K .......... .......... .......... .......... .......... 65% 7.24M 6s
173550K .......... .......... .......... .......... .......... 65% 8.90M 6s
173600K .......... .......... .......... .......... .......... 65% 14.5M 6s
173650K .......... .......... .......... .......... .......... 65% 16.3M 6s
173700K .......... .......... .......... .......... .......... 65% 18.9M 6s
173750K .......... .......... .......... .......... .......... 65% 19.1M 6s
173800K .......... .......... .......... .......... .......... 65% 23.9M 6s
173850K .......... .......... .......... .......... .......... 65% 23.6M 6s
173900K .......... .......... .......... .......... .......... 65% 17.4M 6s
173950K .......... .......... .......... .......... .......... 65% 38.4M 6s
174000K .......... .......... .......... .......... .......... 65% 14.5M 6s
174050K .......... .......... .......... .......... .......... 65% 48.3M 6s
174100K .......... .......... .......... .......... .......... 65% 15.3M 6s
174150K .......... .......... .......... .......... .......... 65% 24.1M 6s
174200K .......... .......... .......... .......... .......... 65% 16.4M 6s
174250K .......... .......... .......... .......... .......... 65% 16.2M 6s
174300K .......... .......... .......... .......... .......... 65% 22.0M 6s
174350K .......... .......... .......... .......... .......... 65% 12.7M 6s
174400K .......... .......... .......... .......... .......... 65% 18.5M 6s
174450K .......... .......... .......... .......... .......... 65% 16.6M 6s
174500K .......... .......... .......... .......... .......... 65% 19.8M 6s
174550K .......... .......... .......... .......... .......... 65% 20.2M 6s
174600K .......... .......... .......... .......... .......... 65% 16.2M 6s
174650K .......... .......... .......... .......... .......... 65% 22.9M 6s
174700K .......... .......... .......... .......... .......... 65% 17.4M 6s
174750K .......... .......... .......... .......... .......... 65% 20.9M 6s
174800K .......... .......... .......... .......... .......... 65% 16.8M 6s
174850K .......... .......... .......... .......... .......... 65% 20.3M 6s
174900K .......... .......... .......... .......... .......... 65% 29.5M 6s
174950K .......... .......... .......... .......... .......... 65% 30.9M 6s
175000K .......... .......... .......... .......... .......... 65% 19.2M 6s
175050K .......... .......... .......... .......... .......... 65% 84.9M 6s
175100K .......... .......... .......... .......... .......... 65% 43.9M 6s
175150K .......... .......... .......... .......... .......... 65% 25.3M 6s
175200K .......... .......... .......... .......... .......... 65% 400M 6s
175250K .......... .......... .......... .......... .......... 65% 29.0M 6s
175300K .......... .......... .......... .......... .......... 65% 27.9M 6s
175350K .......... .......... .......... .......... .......... 65% 21.4M 6s
175400K .......... .......... .......... .......... .......... 66% 79.1M 6s
175450K .......... .......... .......... .......... .......... 66% 20.1M 6s
175500K .......... .......... .......... .......... .......... 66% 14.5M 6s
175550K .......... .......... .......... .......... .......... 66% 28.7M 6s
175600K .......... .......... .......... .......... .......... 66% 12.7M 6s
175650K .......... .......... .......... .......... .......... 66% 15.7M 6s
175700K .......... .......... .......... .......... .......... 66% 12.9M 6s
175750K .......... .......... .......... .......... .......... 66% 15.7M 6s
175800K .......... .......... .......... .......... .......... 66% 15.1M 6s
175850K .......... .......... .......... .......... .......... 66% 12.4M 6s
175900K .......... .......... .......... .......... .......... 66% 11.4M 6s
175950K .......... .......... .......... .......... .......... 66% 14.4M 6s
176000K .......... .......... .......... .......... .......... 66% 10.1M 6s
176050K .......... .......... .......... .......... .......... 66% 15.4M 6s
176100K .......... .......... .......... .......... .......... 66% 11.0M 6s
176150K .......... .......... .......... .......... .......... 66% 14.5M 6s
176200K .......... .......... .......... .......... .......... 66% 8.88M 6s
176250K .......... .......... .......... .......... .......... 66% 37.2M 6s
176300K .......... .......... .......... .......... .......... 66% 15.3M 6s
176350K .......... .......... .......... .......... .......... 66% 19.5M 6s
176400K .......... .......... .......... .......... .......... 66% 16.5M 6s
176450K .......... .......... .......... .......... .......... 66% 18.5M 6s
176500K .......... .......... .......... .......... .......... 66% 16.5M 6s
176550K .......... .......... .......... .......... .......... 66% 20.1M 6s
176600K .......... .......... .......... .......... .......... 66% 22.4M 6s
176650K .......... .......... .......... .......... .......... 66% 17.5M 6s
176700K .......... .......... .......... .......... .......... 66% 13.7M 6s
176750K .......... .......... .......... .......... .......... 66% 11.5M 6s
176800K .......... .......... .......... .......... .......... 66% 16.2M 6s
176850K .......... .......... .......... .......... .......... 66% 18.3M 6s
176900K .......... .......... .......... .......... .......... 66% 16.4M 6s
176950K .......... .......... .......... .......... .......... 66% 15.0M 6s
177000K .......... .......... .......... .......... .......... 66% 22.4M 6s
177050K .......... .......... .......... .......... .......... 66% 16.4M 6s
177100K .......... .......... .......... .......... .......... 66% 15.2M 6s
177150K .......... .......... .......... .......... .......... 66% 18.7M 6s
177200K .......... .......... .......... .......... .......... 66% 16.5M 6s
177250K .......... .......... .......... .......... .......... 66% 16.5M 6s
177300K .......... .......... .......... .......... .......... 66% 18.9M 6s
177350K .......... .......... .......... .......... .......... 66% 22.3M 6s
177400K .......... .......... .......... .......... .......... 66% 22.3M 6s
177450K .......... .......... .......... .......... .......... 66% 22.4M 6s
177500K .......... .......... .......... .......... .......... 66% 34.3M 6s
177550K .......... .......... .......... .......... .......... 66% 36.6M 6s
177600K .......... .......... .......... .......... .......... 66% 11.6M 6s
177650K .......... .......... .......... .......... .......... 66% 31.7M 6s
177700K .......... .......... .......... .......... .......... 66% 36.6M 6s
177750K .......... .......... .......... .......... .......... 66% 15.5M 6s
177800K .......... .......... .......... .......... .......... 66% 194M 6s
177850K .......... .......... .......... .......... .......... 66% 11.0M 6s
177900K .......... .......... .......... .......... .......... 66% 11.7M 6s
177950K .......... .......... .......... .......... .......... 66% 30.6M 6s
178000K .......... .......... .......... .......... .......... 66% 19.5M 6s
178050K .......... .......... .......... .......... .......... 67% 16.9M 6s
178100K .......... .......... .......... .......... .......... 67% 18.0M 6s
178150K .......... .......... .......... .......... .......... 67% 15.2M 6s
178200K .......... .......... .......... .......... .......... 67% 11.6M 6s
178250K .......... .......... .......... .......... .......... 67% 10.9M 6s
178300K .......... .......... .......... .......... .......... 67% 7.78M 6s
178350K .......... .......... .......... .......... .......... 67% 6.87M 6s
178400K .......... .......... .......... .......... .......... 67% 8.65M 6s
178450K .......... .......... .......... .......... .......... 67% 8.82M 6s
178500K .......... .......... .......... .......... .......... 67% 11.2M 6s
178550K .......... .......... .......... .......... .......... 67% 10.5M 6s
178600K .......... .......... .......... .......... .......... 67% 16.2M 6s
178650K .......... .......... .......... .......... .......... 67% 15.9M 6s
178700K .......... .......... .......... .......... .......... 67% 15.1M 6s
178750K .......... .......... .......... .......... .......... 67% 36.1M 6s
178800K .......... .......... .......... .......... .......... 67% 19.4M 6s
178850K .......... .......... .......... .......... .......... 67% 22.6M 6s
178900K .......... .......... .......... .......... .......... 67% 20.7M 6s
178950K .......... .......... .......... .......... .......... 67% 24.7M 6s
179000K .......... .......... .......... .......... .......... 67% 15.0M 6s
179050K .......... .......... .......... .......... .......... 67% 14.6M 6s
179100K .......... .......... .......... .......... .......... 67% 13.4M 6s
179150K .......... .......... .......... .......... .......... 67% 13.8M 6s
179200K .......... .......... .......... .......... .......... 67% 8.28M 6s
179250K .......... .......... .......... .......... .......... 67% 18.0M 6s
179300K .......... .......... .......... .......... .......... 67% 15.1M 6s
179350K .......... .......... .......... .......... .......... 67% 11.8M 6s
179400K .......... .......... .......... .......... .......... 67% 7.14M 6s
179450K .......... .......... .......... .......... .......... 67% 9.90M 6s
179500K .......... .......... .......... .......... .......... 67% 10.3M 6s
179550K .......... .......... .......... .......... .......... 67% 12.2M 6s
179600K .......... .......... .......... .......... .......... 67% 9.32M 6s
179650K .......... .......... .......... .......... .......... 67% 11.1M 6s
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179750K .......... .......... .......... .......... .......... 67% 9.93M 6s
179800K .......... .......... .......... .......... .......... 67% 11.7M 6s
179850K .......... .......... .......... .......... .......... 67% 14.2M 6s
179900K .......... .......... .......... .......... .......... 67% 43.7M 6s
179950K .......... .......... .......... .......... .......... 67% 16.8M 6s
180000K .......... .......... .......... .......... .......... 67% 12.5M 6s
180050K .......... .......... .......... .......... .......... 67% 12.6M 6s
180100K .......... .......... .......... .......... .......... 67% 9.56M 6s
180150K .......... .......... .......... .......... .......... 67% 10.6M 6s
180200K .......... .......... .......... .......... .......... 67% 8.91M 6s
180250K .......... .......... .......... .......... .......... 67% 9.42M 6s
180300K .......... .......... .......... .......... .......... 67% 11.2M 6s
180350K .......... .......... .......... .......... .......... 67% 15.5M 6s
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180450K .......... .......... .......... .......... .......... 67% 16.2M 6s
180500K .......... .......... .......... .......... .......... 67% 18.3M 6s
180550K .......... .......... .......... .......... .......... 67% 19.8M 6s
180600K .......... .......... .......... .......... .......... 67% 15.8M 5s
180650K .......... .......... .......... .......... .......... 67% 17.9M 5s
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180750K .......... .......... .......... .......... .......... 68% 17.8M 5s
180800K .......... .......... .......... .......... .......... 68% 15.1M 5s
180850K .......... .......... .......... .......... .......... 68% 7.07M 5s
180900K .......... .......... .......... .......... .......... 68% 8.46M 5s
180950K .......... .......... .......... .......... .......... 68% 22.0M 5s
181000K .......... .......... .......... .......... .......... 68% 16.9M 5s
181050K .......... .......... .......... .......... .......... 68% 17.2M 5s
181100K .......... .......... .......... .......... .......... 68% 11.4M 5s
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181200K .......... .......... .......... .......... .......... 68% 12.7M 5s
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181400K .......... .......... .......... .......... .......... 68% 17.3M 5s
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181500K .......... .......... .......... .......... .......... 68% 17.6M 5s
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181600K .......... .......... .......... .......... .......... 68% 12.9M 5s
181650K .......... .......... .......... .......... .......... 68% 15.6M 5s
181700K .......... .......... .......... .......... .......... 68% 27.1M 5s
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181800K .......... .......... .......... .......... .......... 68% 23.5M 5s
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181900K .......... .......... .......... .......... .......... 68% 47.9M 5s
181950K .......... .......... .......... .......... .......... 68% 24.7M 5s
182000K .......... .......... .......... .......... .......... 68% 15.9M 5s
182050K .......... .......... .......... .......... .......... 68% 25.3M 5s
182100K .......... .......... .......... .......... .......... 68% 17.9M 5s
182150K .......... .......... .......... .......... .......... 68% 28.5M 5s
182200K .......... .......... .......... .......... .......... 68% 21.2M 5s
182250K .......... .......... .......... .......... .......... 68% 29.8M 5s
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182350K .......... .......... .......... .......... .......... 68% 25.2M 5s
182400K .......... .......... .......... .......... .......... 68% 25.3M 5s
182450K .......... .......... .......... .......... .......... 68% 21.1M 5s
182500K .......... .......... .......... .......... .......... 68% 23.1M 5s
182550K .......... .......... .......... .......... .......... 68% 24.3M 5s
182600K .......... .......... .......... .......... .......... 68% 20.3M 5s
182650K .......... .......... .......... .......... .......... 68% 26.2M 5s
182700K .......... .......... .......... .......... .......... 68% 14.5M 5s
182750K .......... .......... .......... .......... .......... 68% 23.1M 5s
182800K .......... .......... .......... .......... .......... 68% 14.9M 5s
182850K .......... .......... .......... .......... .......... 68% 12.1M 5s
182900K .......... .......... .......... .......... .......... 68% 14.9M 5s
182950K .......... .......... .......... .......... .......... 68% 15.5M 5s
183000K .......... .......... .......... .......... .......... 68% 34.8M 5s
183050K .......... .......... .......... .......... .......... 68% 54.0M 5s
183100K .......... .......... .......... .......... .......... 68% 32.5M 5s
183150K .......... .......... .......... .......... .......... 68% 15.4M 5s
183200K .......... .......... .......... .......... .......... 68% 174M 5s
183250K .......... .......... .......... .......... .......... 68% 180M 5s
183300K .......... .......... .......... .......... .......... 68% 27.3M 5s
183350K .......... .......... .......... .......... .......... 69% 29.4M 5s
183400K .......... .......... .......... .......... .......... 69% 71.7M 5s
183450K .......... .......... .......... .......... .......... 69% 29.3M 5s
183500K .......... .......... .......... .......... .......... 69% 34.0M 5s
183550K .......... .......... .......... .......... .......... 69% 34.3M 5s
183600K .......... .......... .......... .......... .......... 69% 30.0M 5s
183650K .......... .......... .......... .......... .......... 69% 19.7M 5s
183700K .......... .......... .......... .......... .......... 69% 31.3M 5s
183750K .......... .......... .......... .......... .......... 69% 16.6M 5s
183800K .......... .......... .......... .......... .......... 69% 17.9M 5s
183850K .......... .......... .......... .......... .......... 69% 24.5M 5s
183900K .......... .......... .......... .......... .......... 69% 15.8M 5s
183950K .......... .......... .......... .......... .......... 69% 15.0M 5s
184000K .......... .......... .......... .......... .......... 69% 19.2M 5s
184050K .......... .......... .......... .......... .......... 69% 17.3M 5s
184100K .......... .......... .......... .......... .......... 69% 16.0M 5s
184150K .......... .......... .......... .......... .......... 69% 18.9M 5s
184200K .......... .......... .......... .......... .......... 69% 14.6M 5s
184250K .......... .......... .......... .......... .......... 69% 20.9M 5s
184300K .......... .......... .......... .......... .......... 69% 16.4M 5s
184350K .......... .......... .......... .......... .......... 69% 17.5M 5s
184400K .......... .......... .......... .......... .......... 69% 15.2M 5s
184450K .......... .......... .......... .......... .......... 69% 15.3M 5s
184500K .......... .......... .......... .......... .......... 69% 17.9M 5s
184550K .......... .......... .......... .......... .......... 69% 15.7M 5s
184600K .......... .......... .......... .......... .......... 69% 13.2M 5s
184650K .......... .......... .......... .......... .......... 69% 31.9M 5s
184700K .......... .......... .......... .......... .......... 69% 36.0M 5s
184750K .......... .......... .......... .......... .......... 69% 30.3M 5s
184800K .......... .......... .......... .......... .......... 69% 59.5M 5s
184850K .......... .......... .......... .......... .......... 69% 34.6M 5s
184900K .......... .......... .......... .......... .......... 69% 24.8M 5s
184950K .......... .......... .......... .......... .......... 69% 14.9M 5s
185000K .......... .......... .......... .......... .......... 69% 19.6M 5s
185050K .......... .......... .......... .......... .......... 69% 69.2M 5s
185100K .......... .......... .......... .......... .......... 69% 17.8M 5s
185150K .......... .......... .......... .......... .......... 69% 20.1M 5s
185200K .......... .......... .......... .......... .......... 69% 18.4M 5s
185250K .......... .......... .......... .......... .......... 69% 18.0M 5s
185300K .......... .......... .......... .......... .......... 69% 27.0M 5s
185350K .......... .......... .......... .......... .......... 69% 18.8M 5s
185400K .......... .......... .......... .......... .......... 69% 25.9M 5s
185450K .......... .......... .......... .......... .......... 69% 18.0M 5s
185500K .......... .......... .......... .......... .......... 69% 18.0M 5s
185550K .......... .......... .......... .......... .......... 69% 19.3M 5s
185600K .......... .......... .......... .......... .......... 69% 16.5M 5s
185650K .......... .......... .......... .......... .......... 69% 21.7M 5s
185700K .......... .......... .......... .......... .......... 69% 15.4M 5s
185750K .......... .......... .......... .......... .......... 69% 19.1M 5s
185800K .......... .......... .......... .......... .......... 69% 23.3M 5s
185850K .......... .......... .......... .......... .......... 69% 15.6M 5s
185900K .......... .......... .......... .......... .......... 69% 20.9M 5s
185950K .......... .......... .......... .......... .......... 69% 17.4M 5s
186000K .......... .......... .......... .......... .......... 70% 20.3M 5s
186050K .......... .......... .......... .......... .......... 70% 15.3M 5s
186100K .......... .......... .......... .......... .......... 70% 19.0M 5s
186150K .......... .......... .......... .......... .......... 70% 14.8M 5s
186200K .......... .......... .......... .......... .......... 70% 13.6M 5s
186250K .......... .......... .......... .......... .......... 70% 10.1M 5s
186300K .......... .......... .......... .......... .......... 70% 12.3M 5s
186350K .......... .......... .......... .......... .......... 70% 7.47M 5s
186400K .......... .......... .......... .......... .......... 70% 10.6M 5s
186450K .......... .......... .......... .......... .......... 70% 11.7M 5s
186500K .......... .......... .......... .......... .......... 70% 10.2M 5s
186550K .......... .......... .......... .......... .......... 70% 17.6M 5s
186600K .......... .......... .......... .......... .......... 70% 14.7M 5s
186650K .......... .......... .......... .......... .......... 70% 16.6M 5s
186700K .......... .......... .......... .......... .......... 70% 13.4M 5s
186750K .......... .......... .......... .......... .......... 70% 14.8M 5s
186800K .......... .......... .......... .......... .......... 70% 13.2M 5s
186850K .......... .......... .......... .......... .......... 70% 13.1M 5s
186900K .......... .......... .......... .......... .......... 70% 9.49M 5s
186950K .......... .......... .......... .......... .......... 70% 13.3M 5s
187000K .......... .......... .......... .......... .......... 70% 12.2M 5s
187050K .......... .......... .......... .......... .......... 70% 15.7M 5s
187100K .......... .......... .......... .......... .......... 70% 12.5M 5s
187150K .......... .......... .......... .......... .......... 70% 14.2M 5s
187200K .......... .......... .......... .......... .......... 70% 11.0M 5s
187250K .......... .......... .......... .......... .......... 70% 11.6M 5s
187300K .......... .......... .......... .......... .......... 70% 17.3M 5s
187350K .......... .......... .......... .......... .......... 70% 12.6M 5s
187400K .......... .......... .......... .......... .......... 70% 9.40M 5s
187450K .......... .......... .......... .......... .......... 70% 9.80M 5s
187500K .......... .......... .......... .......... .......... 70% 12.3M 5s
187550K .......... .......... .......... .......... .......... 70% 13.3M 5s
187600K .......... .......... .......... .......... .......... 70% 9.78M 5s
187650K .......... .......... .......... .......... .......... 70% 28.8M 5s
187700K .......... .......... .......... .......... .......... 70% 12.7M 5s
187750K .......... .......... .......... .......... .......... 70% 14.5M 5s
187800K .......... .......... .......... .......... .......... 70% 15.6M 5s
187850K .......... .......... .......... .......... .......... 70% 4.77M 5s
187900K .......... .......... .......... .......... .......... 70% 11.4M 5s
187950K .......... .......... .......... .......... .......... 70% 13.7M 5s
188000K .......... .......... .......... .......... .......... 70% 14.8M 5s
188050K .......... .......... .......... .......... .......... 70% 16.4M 5s
188100K .......... .......... .......... .......... .......... 70% 14.0M 5s
188150K .......... .......... .......... .......... .......... 70% 14.9M 5s
188200K .......... .......... .......... .......... .......... 70% 10.1M 5s
188250K .......... .......... .......... .......... .......... 70% 11.7M 5s
188300K .......... .......... .......... .......... .......... 70% 9.84M 5s
188350K .......... .......... .......... .......... .......... 70% 10.3M 5s
188400K .......... .......... .......... .......... .......... 70% 8.34M 5s
188450K .......... .......... .......... .......... .......... 70% 21.3M 5s
188500K .......... .......... .......... .......... .......... 70% 21.3M 5s
188550K .......... .......... .......... .......... .......... 70% 22.1M 5s
188600K .......... .......... .......... .......... .......... 70% 25.2M 5s
188650K .......... .......... .......... .......... .......... 71% 60.7M 5s
188700K .......... .......... .......... .......... .......... 71% 15.0M 5s
188750K .......... .......... .......... .......... .......... 71% 12.7M 5s
188800K .......... .......... .......... .......... .......... 71% 35.1M 5s
188850K .......... .......... .......... .......... .......... 71% 13.4M 5s
188900K .......... .......... .......... .......... .......... 71% 17.2M 5s
188950K .......... .......... .......... .......... .......... 71% 10.3M 5s
189000K .......... .......... .......... .......... .......... 71% 16.0M 5s
189050K .......... .......... .......... .......... .......... 71% 14.9M 5s
189100K .......... .......... .......... .......... .......... 71% 16.4M 5s
189150K .......... .......... .......... .......... .......... 71% 19.8M 5s
189200K .......... .......... .......... .......... .......... 71% 14.6M 5s
189250K .......... .......... .......... .......... .......... 71% 17.0M 5s
189300K .......... .......... .......... .......... .......... 71% 18.4M 5s
189350K .......... .......... .......... .......... .......... 71% 14.3M 5s
189400K .......... .......... .......... .......... .......... 71% 16.5M 5s
189450K .......... .......... .......... .......... .......... 71% 13.6M 5s
189500K .......... .......... .......... .......... .......... 71% 18.1M 5s
189550K .......... .......... .......... .......... .......... 71% 14.6M 5s
189600K .......... .......... .......... .......... .......... 71% 13.7M 5s
189650K .......... .......... .......... .......... .......... 71% 23.1M 5s
189700K .......... .......... .......... .......... .......... 71% 9.77M 5s
189750K .......... .......... .......... .......... .......... 71% 136M 5s
189800K .......... .......... .......... .......... .......... 71% 18.6M 5s
189850K .......... .......... .......... .......... .......... 71% 8.73M 5s
189900K .......... .......... .......... .......... .......... 71% 156M 5s
189950K .......... .......... .......... .......... .......... 71% 15.1M 5s
190000K .......... .......... .......... .......... .......... 71% 29.6M 5s
190050K .......... .......... .......... .......... .......... 71% 15.6M 5s
190100K .......... .......... .......... .......... .......... 71% 19.2M 5s
190150K .......... .......... .......... .......... .......... 71% 12.4M 5s
190200K .......... .......... .......... .......... .......... 71% 17.3M 5s
190250K .......... .......... .......... .......... .......... 71% 14.8M 5s
190300K .......... .......... .......... .......... .......... 71% 15.8M 5s
190350K .......... .......... .......... .......... .......... 71% 13.2M 5s
190400K .......... .......... .......... .......... .......... 71% 9.59M 5s
190450K .......... .......... .......... .......... .......... 71% 16.5M 5s
190500K .......... .......... .......... .......... .......... 71% 17.0M 5s
190550K .......... .......... .......... .......... .......... 71% 14.4M 5s
190600K .......... .......... .......... .......... .......... 71% 15.5M 5s
190650K .......... .......... .......... .......... .......... 71% 17.9M 5s
190700K .......... .......... .......... .......... .......... 71% 15.6M 5s
190750K .......... .......... .......... .......... .......... 71% 17.9M 5s
190800K .......... .......... .......... .......... .......... 71% 15.0M 5s
190850K .......... .......... .......... .......... .......... 71% 15.4M 5s
190900K .......... .......... .......... .......... .......... 71% 12.4M 5s
190950K .......... .......... .......... .......... .......... 71% 8.19M 5s
191000K .......... .......... .......... .......... .......... 71% 10.0M 5s
191050K .......... .......... .......... .......... .......... 71% 9.89M 5s
191100K .......... .......... .......... .......... .......... 71% 15.5M 5s
191150K .......... .......... .......... .......... .......... 71% 15.2M 5s
191200K .......... .......... .......... .......... .......... 71% 9.93M 5s
191250K .......... .......... .......... .......... .......... 71% 11.6M 5s
191300K .......... .......... .......... .......... .......... 71% 13.5M 5s
191350K .......... .......... .......... .......... .......... 72% 9.83M 5s
191400K .......... .......... .......... .......... .......... 72% 13.0M 5s
191450K .......... .......... .......... .......... .......... 72% 11.1M 5s
191500K .......... .......... .......... .......... .......... 72% 13.4M 5s
191550K .......... .......... .......... .......... .......... 72% 14.2M 5s
191600K .......... .......... .......... .......... .......... 72% 9.99M 5s
191650K .......... .......... .......... .......... .......... 72% 14.9M 5s
191700K .......... .......... .......... .......... .......... 72% 15.4M 5s
191750K .......... .......... .......... .......... .......... 72% 19.4M 5s
191800K .......... .......... .......... .......... .......... 72% 17.0M 5s
191850K .......... .......... .......... .......... .......... 72% 8.95M 5s
191900K .......... .......... .......... .......... .......... 72% 15.9M 5s
191950K .......... .......... .......... .......... .......... 72% 9.02M 5s
192000K .......... .......... .......... .......... .......... 72% 12.6M 5s
192050K .......... .......... .......... .......... .......... 72% 36.4M 5s
192100K .......... .......... .......... .......... .......... 72% 12.3M 5s
192150K .......... .......... .......... .......... .......... 72% 18.5M 5s
192200K .......... .......... .......... .......... .......... 72% 17.1M 5s
192250K .......... .......... .......... .......... .......... 72% 23.1M 5s
192300K .......... .......... .......... .......... .......... 72% 18.5M 5s
192350K .......... .......... .......... .......... .......... 72% 17.1M 5s
192400K .......... .......... .......... .......... .......... 72% 24.8M 5s
192450K .......... .......... .......... .......... .......... 72% 14.1M 5s
192500K .......... .......... .......... .......... .......... 72% 22.3M 5s
192550K .......... .......... .......... .......... .......... 72% 22.9M 5s
192600K .......... .......... .......... .......... .......... 72% 16.4M 5s
192650K .......... .......... .......... .......... .......... 72% 23.8M 5s
192700K .......... .......... .......... .......... .......... 72% 17.7M 5s
192750K .......... .......... .......... .......... .......... 72% 11.3M 5s
192800K .......... .......... .......... .......... .......... 72% 10.8M 5s
192850K .......... .......... .......... .......... .......... 72% 15.4M 5s
192900K .......... .......... .......... .......... .......... 72% 11.8M 5s
192950K .......... .......... .......... .......... .......... 72% 12.5M 5s
193000K .......... .......... .......... .......... .......... 72% 25.0M 5s
193050K .......... .......... .......... .......... .......... 72% 18.8M 5s
193100K .......... .......... .......... .......... .......... 72% 11.2M 5s
193150K .......... .......... .......... .......... .......... 72% 41.6M 5s
193200K .......... .......... .......... .......... .......... 72% 15.1M 5s
193250K .......... .......... .......... .......... .......... 72% 18.2M 5s
193300K .......... .......... .......... .......... .......... 72% 17.9M 5s
193350K .......... .......... .......... .......... .......... 72% 22.3M 5s
193400K .......... .......... .......... .......... .......... 72% 13.9M 5s
193450K .......... .......... .......... .......... .......... 72% 10.5M 5s
193500K .......... .......... .......... .......... .......... 72% 12.2M 5s
193550K .......... .......... .......... .......... .......... 72% 11.5M 5s
193600K .......... .......... .......... .......... .......... 72% 12.7M 5s
193650K .......... .......... .......... .......... .......... 72% 13.3M 5s
193700K .......... .......... .......... .......... .......... 72% 12.1M 5s
193750K .......... .......... .......... .......... .......... 72% 10.9M 5s
193800K .......... .......... .......... .......... .......... 72% 11.7M 5s
193850K .......... .......... .......... .......... .......... 72% 7.35M 5s
193900K .......... .......... .......... .......... .......... 72% 18.9M 5s
193950K .......... .......... .......... .......... .......... 72% 8.67M 5s
194000K .......... .......... .......... .......... .......... 73% 16.4M 5s
194050K .......... .......... .......... .......... .......... 73% 25.4M 5s
194100K .......... .......... .......... .......... .......... 73% 12.2M 5s
194150K .......... .......... .......... .......... .......... 73% 11.7M 5s
194200K .......... .......... .......... .......... .......... 73% 17.0M 5s
194250K .......... .......... .......... .......... .......... 73% 13.0M 5s
194300K .......... .......... .......... .......... .......... 73% 17.2M 5s
194350K .......... .......... .......... .......... .......... 73% 15.8M 5s
194400K .......... .......... .......... .......... .......... 73% 15.9M 5s
194450K .......... .......... .......... .......... .......... 73% 14.0M 5s
194500K .......... .......... .......... .......... .......... 73% 18.9M 5s
194550K .......... .......... .......... .......... .......... 73% 11.1M 5s
194600K .......... .......... .......... .......... .......... 73% 12.7M 5s
194650K .......... .......... .......... .......... .......... 73% 14.5M 5s
194700K .......... .......... .......... .......... .......... 73% 11.6M 5s
194750K .......... .......... .......... .......... .......... 73% 13.1M 5s
194800K .......... .......... .......... .......... .......... 73% 26.7M 5s
194850K .......... .......... .......... .......... .......... 73% 22.1M 5s
194900K .......... .......... .......... .......... .......... 73% 11.2M 5s
194950K .......... .......... .......... .......... .......... 73% 28.3M 5s
195000K .......... .......... .......... .......... .......... 73% 38.3M 5s
195050K .......... .......... .......... .......... .......... 73% 32.6M 5s
195100K .......... .......... .......... .......... .......... 73% 16.3M 5s
195150K .......... .......... .......... .......... .......... 73% 76.2M 5s
195200K .......... .......... .......... .......... .......... 73% 18.6M 5s
195250K .......... .......... .......... .......... .......... 73% 12.5M 5s
195300K .......... .......... .......... .......... .......... 73% 24.0M 5s
195350K .......... .......... .......... .......... .......... 73% 19.3M 5s
195400K .......... .......... .......... .......... .......... 73% 18.2M 5s
195450K .......... .......... .......... .......... .......... 73% 17.2M 5s
195500K .......... .......... .......... .......... .......... 73% 20.2M 5s
195550K .......... .......... .......... .......... .......... 73% 19.4M 5s
195600K .......... .......... .......... .......... .......... 73% 9.38M 5s
195650K .......... .......... .......... .......... .......... 73% 23.4M 5s
195700K .......... .......... .......... .......... .......... 73% 9.96M 5s
195750K .......... .......... .......... .......... .......... 73% 10.4M 5s
195800K .......... .......... .......... .......... .......... 73% 9.03M 5s
195850K .......... .......... .......... .......... .......... 73% 8.03M 5s
195900K .......... .......... .......... .......... .......... 73% 13.7M 5s
195950K .......... .......... .......... .......... .......... 73% 12.1M 4s
196000K .......... .......... .......... .......... .......... 73% 12.8M 4s
196050K .......... .......... .......... .......... .......... 73% 12.7M 4s
196100K .......... .......... .......... .......... .......... 73% 13.1M 4s
196150K .......... .......... .......... .......... .......... 73% 13.1M 4s
196200K .......... .......... .......... .......... .......... 73% 10.3M 4s
196250K .......... .......... .......... .......... .......... 73% 6.24M 4s
196300K .......... .......... .......... .......... .......... 73% 33.7M 4s
196350K .......... .......... .......... .......... .......... 73% 11.5M 4s
196400K .......... .......... .......... .......... .......... 73% 11.4M 4s
196450K .......... .......... .......... .......... .......... 73% 22.3M 4s
196500K .......... .......... .......... .......... .......... 73% 19.4M 4s
196550K .......... .......... .......... .......... .......... 73% 13.8M 4s
196600K .......... .......... .......... .......... .......... 73% 18.6M 4s
196650K .......... .......... .......... .......... .......... 74% 16.3M 4s
196700K .......... .......... .......... .......... .......... 74% 11.3M 4s
196750K .......... .......... .......... .......... .......... 74% 16.7M 4s
196800K .......... .......... .......... .......... .......... 74% 17.9M 4s
196850K .......... .......... .......... .......... .......... 74% 13.8M 4s
196900K .......... .......... .......... .......... .......... 74% 16.7M 4s
196950K .......... .......... .......... .......... .......... 74% 14.4M 4s
197000K .......... .......... .......... .......... .......... 74% 20.0M 4s
197050K .......... .......... .......... .......... .......... 74% 14.4M 4s
197100K .......... .......... .......... .......... .......... 74% 14.1M 4s
197150K .......... .......... .......... .......... .......... 74% 19.6M 4s
197200K .......... .......... .......... .......... .......... 74% 15.5M 4s
197250K .......... .......... .......... .......... .......... 74% 26.2M 4s
197300K .......... .......... .......... .......... .......... 74% 19.5M 4s
197350K .......... .......... .......... .......... .......... 74% 18.2M 4s
197400K .......... .......... .......... .......... .......... 74% 22.3M 4s
197450K .......... .......... .......... .......... .......... 74% 17.4M 4s
197500K .......... .......... .......... .......... .......... 74% 17.8M 4s
197550K .......... .......... .......... .......... .......... 74% 9.15M 4s
197600K .......... .......... .......... .......... .......... 74% 15.0M 4s
197650K .......... .......... .......... .......... .......... 74% 6.75M 4s
197700K .......... .......... .......... .......... .......... 74% 13.8M 4s
197750K .......... .......... .......... .......... .......... 74% 15.8M 4s
197800K .......... .......... .......... .......... .......... 74% 13.3M 4s
197850K .......... .......... .......... .......... .......... 74% 11.3M 4s
197900K .......... .......... .......... .......... .......... 74% 17.4M 4s
197950K .......... .......... .......... .......... .......... 74% 9.04M 4s
198000K .......... .......... .......... .......... .......... 74% 9.99M 4s
198050K .......... .......... .......... .......... .......... 74% 8.93M 4s
198100K .......... .......... .......... .......... .......... 74% 8.60M 4s
198150K .......... .......... .......... .......... .......... 74% 9.40M 4s
198200K .......... .......... .......... .......... .......... 74% 7.71M 4s
198250K .......... .......... .......... .......... .......... 74% 9.87M 4s
198300K .......... .......... .......... .......... .......... 74% 17.5M 4s
198350K .......... .......... .......... .......... .......... 74% 34.1M 4s
198400K .......... .......... .......... .......... .......... 74% 28.1M 4s
198450K .......... .......... .......... .......... .......... 74% 13.4M 4s
198500K .......... .......... .......... .......... .......... 74% 22.1M 4s
198550K .......... .......... .......... .......... .......... 74% 22.8M 4s
198600K .......... .......... .......... .......... .......... 74% 9.24M 4s
198650K .......... .......... .......... .......... .......... 74% 181M 4s
198700K .......... .......... .......... .......... .......... 74% 18.7M 4s
198750K .......... .......... .......... .......... .......... 74% 26.9M 4s
198800K .......... .......... .......... .......... .......... 74% 19.4M 4s
198850K .......... .......... .......... .......... .......... 74% 21.2M 4s
198900K .......... .......... .......... .......... .......... 74% 22.8M 4s
198950K .......... .......... .......... .......... .......... 74% 19.0M 4s
199000K .......... .......... .......... .......... .......... 74% 17.2M 4s
199050K .......... .......... .......... .......... .......... 74% 13.3M 4s
199100K .......... .......... .......... .......... .......... 74% 17.5M 4s
199150K .......... .......... .......... .......... .......... 74% 15.4M 4s
199200K .......... .......... .......... .......... .......... 74% 12.5M 4s
199250K .......... .......... .......... .......... .......... 74% 15.7M 4s
199300K .......... .......... .......... .......... .......... 75% 12.9M 4s
199350K .......... .......... .......... .......... .......... 75% 14.2M 4s
199400K .......... .......... .......... .......... .......... 75% 13.4M 4s
199450K .......... .......... .......... .......... .......... 75% 11.8M 4s
199500K .......... .......... .......... .......... .......... 75% 16.6M 4s
199550K .......... .......... .......... .......... .......... 75% 20.7M 4s
199600K .......... .......... .......... .......... .......... 75% 15.6M 4s
199650K .......... .......... .......... .......... .......... 75% 10.7M 4s
199700K .......... .......... .......... .......... .......... 75% 4.62M 4s
199750K .......... .......... .......... .......... .......... 75% 13.3M 4s
199800K .......... .......... .......... .......... .......... 75% 14.7M 4s
199850K .......... .......... .......... .......... .......... 75% 11.1M 4s
199900K .......... .......... .......... .......... .......... 75% 14.1M 4s
199950K .......... .......... .......... .......... .......... 75% 20.0M 4s
200000K .......... .......... .......... .......... .......... 75% 14.7M 4s
200050K .......... .......... .......... .......... .......... 75% 21.2M 4s
200100K .......... .......... .......... .......... .......... 75% 18.6M 4s
200150K .......... .......... .......... .......... .......... 75% 14.6M 4s
200200K .......... .......... .......... .......... .......... 75% 17.8M 4s
200250K .......... .......... .......... .......... .......... 75% 21.1M 4s
200300K .......... .......... .......... .......... .......... 75% 22.3M 4s
200350K .......... .......... .......... .......... .......... 75% 24.9M 4s
200400K .......... .......... .......... .......... .......... 75% 38.2M 4s
200450K .......... .......... .......... .......... .......... 75% 36.7M 4s
200500K .......... .......... .......... .......... .......... 75% 17.9M 4s
200550K .......... .......... .......... .......... .......... 75% 182M 4s
200600K .......... .......... .......... .......... .......... 75% 167M 4s
200650K .......... .......... .......... .......... .......... 75% 132M 4s
200700K .......... .......... .......... .......... .......... 75% 22.4M 4s
200750K .......... .......... .......... .......... .......... 75% 177M 4s
200800K .......... .......... .......... .......... .......... 75% 25.1M 4s
200850K .......... .......... .......... .......... .......... 75% 132M 4s
200900K .......... .......... .......... .......... .......... 75% 25.8M 4s
200950K .......... .......... .......... .......... .......... 75% 17.2M 4s
201000K .......... .......... .......... .......... .......... 75% 29.9M 4s
201050K .......... .......... .......... .......... .......... 75% 17.1M 4s
201100K .......... .......... .......... .......... .......... 75% 23.6M 4s
201150K .......... .......... .......... .......... .......... 75% 16.5M 4s
201200K .......... .......... .......... .......... .......... 75% 22.6M 4s
201250K .......... .......... .......... .......... .......... 75% 18.6M 4s
201300K .......... .......... .......... .......... .......... 75% 22.1M 4s
201350K .......... .......... .......... .......... .......... 75% 19.3M 4s
201400K .......... .......... .......... .......... .......... 75% 20.0M 4s
201450K .......... .......... .......... .......... .......... 75% 19.9M 4s
201500K .......... .......... .......... .......... .......... 75% 18.1M 4s
201550K .......... .......... .......... .......... .......... 75% 14.3M 4s
201600K .......... .......... .......... .......... .......... 75% 16.1M 4s
201650K .......... .......... .......... .......... .......... 75% 24.5M 4s
201700K .......... .......... .......... .......... .......... 75% 9.07M 4s
201750K .......... .......... .......... .......... .......... 75% 23.3M 4s
201800K .......... .......... .......... .......... .......... 75% 28.9M 4s
201850K .......... .......... .......... .......... .......... 75% 13.0M 4s
201900K .......... .......... .......... .......... .......... 75% 156M 4s
201950K .......... .......... .......... .......... .......... 76% 8.35M 4s
202000K .......... .......... .......... .......... .......... 76% 162M 4s
202050K .......... .......... .......... .......... .......... 76% 83.6M 4s
202100K .......... .......... .......... .......... .......... 76% 15.1M 4s
202150K .......... .......... .......... .......... .......... 76% 8.51M 4s
202200K .......... .......... .......... .......... .......... 76% 13.2M 4s
202250K .......... .......... .......... .......... .......... 76% 21.5M 4s
202300K .......... .......... .......... .......... .......... 76% 15.2M 4s
202350K .......... .......... .......... .......... .......... 76% 11.5M 4s
202400K .......... .......... .......... .......... .......... 76% 14.8M 4s
202450K .......... .......... .......... .......... .......... 76% 12.2M 4s
202500K .......... .......... .......... .......... .......... 76% 14.6M 4s
202550K .......... .......... .......... .......... .......... 76% 11.2M 4s
202600K .......... .......... .......... .......... .......... 76% 10.8M 4s
202650K .......... .......... .......... .......... .......... 76% 11.2M 4s
202700K .......... .......... .......... .......... .......... 76% 11.7M 4s
202750K .......... .......... .......... .......... .......... 76% 26.9M 4s
202800K .......... .......... .......... .......... .......... 76% 18.9M 4s
202850K .......... .......... .......... .......... .......... 76% 37.4M 4s
202900K .......... .......... .......... .......... .......... 76% 16.2M 4s
202950K .......... .......... .......... .......... .......... 76% 8.11M 4s
203000K .......... .......... .......... .......... .......... 76% 19.4M 4s
203050K .......... .......... .......... .......... .......... 76% 16.5M 4s
203100K .......... .......... .......... .......... .......... 76% 15.2M 4s
203150K .......... .......... .......... .......... .......... 76% 16.0M 4s
203200K .......... .......... .......... .......... .......... 76% 14.1M 4s
203250K .......... .......... .......... .......... .......... 76% 16.4M 4s
203300K .......... .......... .......... .......... .......... 76% 20.0M 4s
203350K .......... .......... .......... .......... .......... 76% 11.9M 4s
203400K .......... .......... .......... .......... .......... 76% 13.9M 4s
203450K .......... .......... .......... .......... .......... 76% 10.7M 4s
203500K .......... .......... .......... .......... .......... 76% 27.0M 4s
203550K .......... .......... .......... .......... .......... 76% 25.5M 4s
203600K .......... .......... .......... .......... .......... 76% 10.2M 4s
203650K .......... .......... .......... .......... .......... 76% 7.82M 4s
203700K .......... .......... .......... .......... .......... 76% 10.0M 4s
203750K .......... .......... .......... .......... .......... 76% 9.55M 4s
203800K .......... .......... .......... .......... .......... 76% 13.0M 4s
203850K .......... .......... .......... .......... .......... 76% 10.1M 4s
203900K .......... .......... .......... .......... .......... 76% 9.30M 4s
203950K .......... .......... .......... .......... .......... 76% 7.57M 4s
204000K .......... .......... .......... .......... .......... 76% 9.00M 4s
204050K .......... .......... .......... .......... .......... 76% 8.17M 4s
204100K .......... .......... .......... .......... .......... 76% 8.00M 4s
204150K .......... .......... .......... .......... .......... 76% 17.3M 4s
204200K .......... .......... .......... .......... .......... 76% 11.6M 4s
204250K .......... .......... .......... .......... .......... 76% 14.3M 4s
204300K .......... .......... .......... .......... .......... 76% 9.59M 4s
204350K .......... .......... .......... .......... .......... 76% 11.5M 4s
204400K .......... .......... .......... .......... .......... 76% 18.2M 4s
204450K .......... .......... .......... .......... .......... 76% 6.96M 4s
204500K .......... .......... .......... .......... .......... 76% 6.89M 4s
204550K .......... .......... .......... .......... .......... 76% 3.26M 4s
204600K .......... .......... .......... .......... .......... 77% 12.2M 4s
204650K .......... .......... .......... .......... .......... 77% 14.7M 4s
204700K .......... .......... .......... .......... .......... 77% 32.0M 4s
204750K .......... .......... .......... .......... .......... 77% 12.0M 4s
204800K .......... .......... .......... .......... .......... 77% 10.3M 4s
204850K .......... .......... .......... .......... .......... 77% 4.33M 4s
204900K .......... .......... .......... .......... .......... 77% 4.46M 4s
204950K .......... .......... .......... .......... .......... 77% 4.66M 4s
205000K .......... .......... .......... .......... .......... 77% 6.05M 4s
205050K .......... .......... .......... .......... .......... 77% 5.77M 4s
205100K .......... .......... .......... .......... .......... 77% 5.62M 4s
205150K .......... .......... .......... .......... .......... 77% 5.88M 4s
205200K .......... .......... .......... .......... .......... 77% 13.6M 4s
205250K .......... .......... .......... .......... .......... 77% 31.7M 4s
205300K .......... .......... .......... .......... .......... 77% 30.0M 4s
205350K .......... .......... .......... .......... .......... 77% 18.6M 4s
205400K .......... .......... .......... .......... .......... 77% 28.2M 4s
205450K .......... .......... .......... .......... .......... 77% 17.4M 4s
205500K .......... .......... .......... .......... .......... 77% 17.4M 4s
205550K .......... .......... .......... .......... .......... 77% 18.8M 4s
205600K .......... .......... .......... .......... .......... 77% 19.2M 4s
205650K .......... .......... .......... .......... .......... 77% 15.5M 4s
205700K .......... .......... .......... .......... .......... 77% 11.3M 4s
205750K .......... .......... .......... .......... .......... 77% 14.4M 4s
205800K .......... .......... .......... .......... .......... 77% 9.47M 4s
205850K .......... .......... .......... .......... .......... 77% 6.91M 4s
205900K .......... .......... .......... .......... .......... 77% 7.65M 4s
205950K .......... .......... .......... .......... .......... 77% 6.29M 4s
206000K .......... .......... .......... .......... .......... 77% 6.07M 4s
206050K .......... .......... .......... .......... .......... 77% 5.41M 4s
206100K .......... .......... .......... .......... .......... 77% 4.99M 4s
206150K .......... .......... .......... .......... .......... 77% 20.7M 4s
206200K .......... .......... .......... .......... .......... 77% 7.92M 4s
206250K .......... .......... .......... .......... .......... 77% 30.6M 4s
206300K .......... .......... .......... .......... .......... 77% 10.1M 4s
206350K .......... .......... .......... .......... .......... 77% 11.6M 4s
206400K .......... .......... .......... .......... .......... 77% 9.94M 4s
206450K .......... .......... .......... .......... .......... 77% 5.69M 4s
206500K .......... .......... .......... .......... .......... 77% 9.13M 4s
206550K .......... .......... .......... .......... .......... 77% 11.3M 4s
206600K .......... .......... .......... .......... .......... 77% 10.4M 4s
206650K .......... .......... .......... .......... .......... 77% 3.75M 4s
206700K .......... .......... .......... .......... .......... 77% 11.6M 4s
206750K .......... .......... .......... .......... .......... 77% 8.86M 4s
206800K .......... .......... .......... .......... .......... 77% 9.15M 4s
206850K .......... .......... .......... .......... .......... 77% 8.56M 4s
206900K .......... .......... .......... .......... .......... 77% 18.2M 4s
206950K .......... .......... .......... .......... .......... 77% 13.8M 4s
207000K .......... .......... .......... .......... .......... 77% 79.0M 4s
207050K .......... .......... .......... .......... .......... 77% 18.7M 4s
207100K .......... .......... .......... .......... .......... 77% 97.7M 4s
207150K .......... .......... .......... .......... .......... 77% 15.5M 4s
207200K .......... .......... .......... .......... .......... 77% 13.4M 4s
207250K .......... .......... .......... .......... .......... 77% 31.7M 4s
207300K .......... .......... .......... .......... .......... 78% 15.2M 4s
207350K .......... .......... .......... .......... .......... 78% 15.1M 4s
207400K .......... .......... .......... .......... .......... 78% 15.7M 4s
207450K .......... .......... .......... .......... .......... 78% 11.7M 4s
207500K .......... .......... .......... .......... .......... 78% 10.9M 4s
207550K .......... .......... .......... .......... .......... 78% 11.9M 4s
207600K .......... .......... .......... .......... .......... 78% 7.93M 4s
207650K .......... .......... .......... .......... .......... 78% 5.51M 4s
207700K .......... .......... .......... .......... .......... 78% 6.99M 4s
207750K .......... .......... .......... .......... .......... 78% 8.39M 4s
207800K .......... .......... .......... .......... .......... 78% 5.92M 4s
207850K .......... .......... .......... .......... .......... 78% 7.00M 4s
207900K .......... .......... .......... .......... .......... 78% 7.57M 4s
207950K .......... .......... .......... .......... .......... 78% 11.5M 4s
208000K .......... .......... .......... .......... .......... 78% 160M 4s
208050K .......... .......... .......... .......... .......... 78% 40.6M 4s
208100K .......... .......... .......... .......... .......... 78% 18.9M 4s
208150K .......... .......... .......... .......... .......... 78% 15.5M 4s
208200K .......... .......... .......... .......... .......... 78% 13.1M 4s
208250K .......... .......... .......... .......... .......... 78% 6.87M 4s
208300K .......... .......... .......... .......... .......... 78% 10.2M 4s
208350K .......... .......... .......... .......... .......... 78% 6.78M 4s
208400K .......... .......... .......... .......... .......... 78% 8.26M 4s
208450K .......... .......... .......... .......... .......... 78% 6.28M 4s
208500K .......... .......... .......... .......... .......... 78% 7.48M 4s
208550K .......... .......... .......... .......... .......... 78% 13.3M 4s
208600K .......... .......... .......... .......... .......... 78% 30.0M 4s
208650K .......... .......... .......... .......... .......... 78% 21.9M 4s
208700K .......... .......... .......... .......... .......... 78% 24.2M 4s
208750K .......... .......... .......... .......... .......... 78% 27.1M 4s
208800K .......... .......... .......... .......... .......... 78% 23.0M 4s
208850K .......... .......... .......... .......... .......... 78% 18.6M 4s
208900K .......... .......... .......... .......... .......... 78% 24.6M 4s
208950K .......... .......... .......... .......... .......... 78% 18.0M 4s
209000K .......... .......... .......... .......... .......... 78% 23.1M 4s
209050K .......... .......... .......... .......... .......... 78% 16.6M 4s
209100K .......... .......... .......... .......... .......... 78% 18.0M 4s
209150K .......... .......... .......... .......... .......... 78% 15.7M 4s
209200K .......... .......... .......... .......... .......... 78% 17.3M 4s
209250K .......... .......... .......... .......... .......... 78% 22.3M 4s
209300K .......... .......... .......... .......... .......... 78% 18.0M 4s
209350K .......... .......... .......... .......... .......... 78% 17.7M 4s
209400K .......... .......... .......... .......... .......... 78% 22.8M 4s
209450K .......... .......... .......... .......... .......... 78% 16.1M 4s
209500K .......... .......... .......... .......... .......... 78% 18.6M 4s
209550K .......... .......... .......... .......... .......... 78% 21.3M 4s
209600K .......... .......... .......... .......... .......... 78% 19.5M 4s
209650K .......... .......... .......... .......... .......... 78% 17.0M 4s
209700K .......... .......... .......... .......... .......... 78% 22.1M 4s
209750K .......... .......... .......... .......... .......... 78% 19.8M 4s
209800K .......... .......... .......... .......... .......... 78% 14.7M 4s
209850K .......... .......... .......... .......... .......... 78% 9.07M 4s
209900K .......... .......... .......... .......... .......... 78% 11.3M 4s
209950K .......... .......... .......... .......... .......... 79% 7.62M 4s
210000K .......... .......... .......... .......... .......... 79% 14.4M 4s
210050K .......... .......... .......... .......... .......... 79% 9.41M 4s
210100K .......... .......... .......... .......... .......... 79% 8.91M 4s
210150K .......... .......... .......... .......... .......... 79% 9.90M 4s
210200K .......... .......... .......... .......... .......... 79% 11.9M 4s
210250K .......... .......... .......... .......... .......... 79% 11.7M 4s
210300K .......... .......... .......... .......... .......... 79% 11.6M 4s
210350K .......... .......... .......... .......... .......... 79% 11.4M 4s
210400K .......... .......... .......... .......... .......... 79% 9.99M 4s
210450K .......... .......... .......... .......... .......... 79% 10.7M 4s
210500K .......... .......... .......... .......... .......... 79% 10.7M 4s
210550K .......... .......... .......... .......... .......... 79% 14.1M 4s
210600K .......... .......... .......... .......... .......... 79% 16.2M 4s
210650K .......... .......... .......... .......... .......... 79% 17.1M 4s
210700K .......... .......... .......... .......... .......... 79% 16.2M 4s
210750K .......... .......... .......... .......... .......... 79% 10.2M 4s
210800K .......... .......... .......... .......... .......... 79% 9.88M 4s
210850K .......... .......... .......... .......... .......... 79% 7.09M 4s
210900K .......... .......... .......... .......... .......... 79% 6.40M 4s
210950K .......... .......... .......... .......... .......... 79% 7.42M 4s
211000K .......... .......... .......... .......... .......... 79% 10.1M 4s
211050K .......... .......... .......... .......... .......... 79% 9.34M 4s
211100K .......... .......... .......... .......... .......... 79% 7.81M 4s
211150K .......... .......... .......... .......... .......... 79% 9.16M 4s
211200K .......... .......... .......... .......... .......... 79% 9.36M 4s
211250K .......... .......... .......... .......... .......... 79% 8.88M 4s
211300K .......... .......... .......... .......... .......... 79% 9.80M 4s
211350K .......... .......... .......... .......... .......... 79% 11.8M 4s
211400K .......... .......... .......... .......... .......... 79% 23.8M 4s
211450K .......... .......... .......... .......... .......... 79% 16.2M 4s
211500K .......... .......... .......... .......... .......... 79% 24.1M 4s
211550K .......... .......... .......... .......... .......... 79% 15.9M 4s
211600K .......... .......... .......... .......... .......... 79% 10.8M 4s
211650K .......... .......... .......... .......... .......... 79% 12.5M 4s
211700K .......... .......... .......... .......... .......... 79% 11.4M 4s
211750K .......... .......... .......... .......... .......... 79% 11.0M 4s
211800K .......... .......... .......... .......... .......... 79% 12.4M 4s
211850K .......... .......... .......... .......... .......... 79% 13.7M 4s
211900K .......... .......... .......... .......... .......... 79% 22.0M 4s
211950K .......... .......... .......... .......... .......... 79% 26.8M 4s
212000K .......... .......... .......... .......... .......... 79% 42.8M 4s
212050K .......... .......... .......... .......... .......... 79% 53.7M 4s
212100K .......... .......... .......... .......... .......... 79% 21.0M 4s
212150K .......... .......... .......... .......... .......... 79% 66.6M 4s
212200K .......... .......... .......... .......... .......... 79% 42.7M 3s
212250K .......... .......... .......... .......... .......... 79% 55.9M 3s
212300K .......... .......... .......... .......... .......... 79% 32.0M 3s
212350K .......... .......... .......... .......... .......... 79% 28.7M 3s
212400K .......... .......... .......... .......... .......... 79% 20.5M 3s
212450K .......... .......... .......... .......... .......... 79% 23.1M 3s
212500K .......... .......... .......... .......... .......... 79% 15.7M 3s
212550K .......... .......... .......... .......... .......... 79% 16.5M 3s
212600K .......... .......... .......... .......... .......... 80% 18.9M 3s
212650K .......... .......... .......... .......... .......... 80% 20.1M 3s
212700K .......... .......... .......... .......... .......... 80% 14.9M 3s
212750K .......... .......... .......... .......... .......... 80% 10.6M 3s
212800K .......... .......... .......... .......... .......... 80% 14.3M 3s
212850K .......... .......... .......... .......... .......... 80% 6.63M 3s
212900K .......... .......... .......... .......... .......... 80% 7.51M 3s
212950K .......... .......... .......... .......... .......... 80% 7.05M 3s
213000K .......... .......... .......... .......... .......... 80% 7.51M 3s
213050K .......... .......... .......... .......... .......... 80% 6.76M 3s
213100K .......... .......... .......... .......... .......... 80% 5.24M 3s
213150K .......... .......... .......... .......... .......... 80% 6.61M 3s
213200K .......... .......... .......... .......... .......... 80% 7.47M 3s
213250K .......... .......... .......... .......... .......... 80% 10.0M 3s
213300K .......... .......... .......... .......... .......... 80% 11.2M 3s
213350K .......... .......... .......... .......... .......... 80% 6.04M 3s
213400K .......... .......... .......... .......... .......... 80% 7.99M 3s
213450K .......... .......... .......... .......... .......... 80% 7.71M 3s
213500K .......... .......... .......... .......... .......... 80% 8.04M 3s
213550K .......... .......... .......... .......... .......... 80% 8.30M 3s
213600K .......... .......... .......... .......... .......... 80% 8.48M 3s
213650K .......... .......... .......... .......... .......... 80% 7.39M 3s
213700K .......... .......... .......... .......... .......... 80% 7.35M 3s
213750K .......... .......... .......... .......... .......... 80% 9.12M 3s
213800K .......... .......... .......... .......... .......... 80% 9.09M 3s
213850K .......... .......... .......... .......... .......... 80% 12.1M 3s
213900K .......... .......... .......... .......... .......... 80% 10.5M 3s
213950K .......... .......... .......... .......... .......... 80% 8.26M 3s
214000K .......... .......... .......... .......... .......... 80% 13.0M 3s
214050K .......... .......... .......... .......... .......... 80% 8.77M 3s
214100K .......... .......... .......... .......... .......... 80% 12.9M 3s
214150K .......... .......... .......... .......... .......... 80% 12.5M 3s
214200K .......... .......... .......... .......... .......... 80% 8.48M 3s
214250K .......... .......... .......... .......... .......... 80% 9.77M 3s
214300K .......... .......... .......... .......... .......... 80% 11.2M 3s
214350K .......... .......... .......... .......... .......... 80% 10.2M 3s
214400K .......... .......... .......... .......... .......... 80% 16.3M 3s
214450K .......... .......... .......... .......... .......... 80% 5.90M 3s
214500K .......... .......... .......... .......... .......... 80% 9.34M 3s
214550K .......... .......... .......... .......... .......... 80% 10.7M 3s
214600K .......... .......... .......... .......... .......... 80% 8.23M 3s
214650K .......... .......... .......... .......... .......... 80% 6.59M 3s
214700K .......... .......... .......... .......... .......... 80% 5.15M 3s
214750K .......... .......... .......... .......... .......... 80% 5.69M 3s
214800K .......... .......... .......... .......... .......... 80% 8.04M 3s
214850K .......... .......... .......... .......... .......... 80% 5.50M 3s
214900K .......... .......... .......... .......... .......... 80% 6.22M 3s
214950K .......... .......... .......... .......... .......... 80% 6.65M 3s
215000K .......... .......... .......... .......... .......... 80% 5.41M 3s
215050K .......... .......... .......... .......... .......... 80% 5.36M 3s
215100K .......... .......... .......... .......... .......... 80% 6.59M 3s
215150K .......... .......... .......... .......... .......... 80% 8.39M 3s
215200K .......... .......... .......... .......... .......... 80% 5.60M 3s
215250K .......... .......... .......... .......... .......... 81% 5.20M 3s
215300K .......... .......... .......... .......... .......... 81% 6.83M 3s
215350K .......... .......... .......... .......... .......... 81% 12.8M 3s
215400K .......... .......... .......... .......... .......... 81% 16.7M 3s
215450K .......... .......... .......... .......... .......... 81% 11.3M 3s
215500K .......... .......... .......... .......... .......... 81% 14.5M 3s
215550K .......... .......... .......... .......... .......... 81% 12.3M 3s
215600K .......... .......... .......... .......... .......... 81% 3.77M 3s
215650K .......... .......... .......... .......... .......... 81% 10.6M 3s
215700K .......... .......... .......... .......... .......... 81% 9.06M 3s
215750K .......... .......... .......... .......... .......... 81% 12.9M 3s
215800K .......... .......... .......... .......... .......... 81% 10.0M 3s
215850K .......... .......... .......... .......... .......... 81% 29.7M 3s
215900K .......... .......... .......... .......... .......... 81% 95.0M 3s
215950K .......... .......... .......... .......... .......... 81% 29.2M 3s
216000K .......... .......... .......... .......... .......... 81% 28.6M 3s
216050K .......... .......... .......... .......... .......... 81% 30.2M 3s
216100K .......... .......... .......... .......... .......... 81% 27.4M 3s
216150K .......... .......... .......... .......... .......... 81% 37.2M 3s
216200K .......... .......... .......... .......... .......... 81% 32.6M 3s
216250K .......... .......... .......... .......... .......... 81% 24.4M 3s
216300K .......... .......... .......... .......... .......... 81% 50.8M 3s
216350K .......... .......... .......... .......... .......... 81% 32.5M 3s
216400K .......... .......... .......... .......... .......... 81% 30.0M 3s
216450K .......... .......... .......... .......... .......... 81% 24.0M 3s
216500K .......... .......... .......... .......... .......... 81% 40.1M 3s
216550K .......... .......... .......... .......... .......... 81% 18.3M 3s
216600K .......... .......... .......... .......... .......... 81% 31.3M 3s
216650K .......... .......... .......... .......... .......... 81% 17.1M 3s
216700K .......... .......... .......... .......... .......... 81% 12.5M 3s
216750K .......... .......... .......... .......... .......... 81% 10.9M 3s
216800K .......... .......... .......... .......... .......... 81% 13.4M 3s
216850K .......... .......... .......... .......... .......... 81% 9.02M 3s
216900K .......... .......... .......... .......... .......... 81% 10.8M 3s
216950K .......... .......... .......... .......... .......... 81% 9.79M 3s
217000K .......... .......... .......... .......... .......... 81% 10.8M 3s
217050K .......... .......... .......... .......... .......... 81% 11.9M 3s
217100K .......... .......... .......... .......... .......... 81% 22.1M 3s
217150K .......... .......... .......... .......... .......... 81% 50.1M 3s
217200K .......... .......... .......... .......... .......... 81% 27.0M 3s
217250K .......... .......... .......... .......... .......... 81% 27.8M 3s
217300K .......... .......... .......... .......... .......... 81% 37.2M 3s
217350K .......... .......... .......... .......... .......... 81% 20.7M 3s
217400K .......... .......... .......... .......... .......... 81% 30.7M 3s
217450K .......... .......... .......... .......... .......... 81% 17.7M 3s
217500K .......... .......... .......... .......... .......... 81% 21.4M 3s
217550K .......... .......... .......... .......... .......... 81% 22.6M 3s
217600K .......... .......... .......... .......... .......... 81% 10.8M 3s
217650K .......... .......... .......... .......... .......... 81% 17.2M 3s
217700K .......... .......... .......... .......... .......... 81% 13.5M 3s
217750K .......... .......... .......... .......... .......... 81% 18.3M 3s
217800K .......... .......... .......... .......... .......... 81% 16.0M 3s
217850K .......... .......... .......... .......... .......... 81% 14.7M 3s
217900K .......... .......... .......... .......... .......... 82% 8.47M 3s
217950K .......... .......... .......... .......... .......... 82% 8.14M 3s
218000K .......... .......... .......... .......... .......... 82% 14.5M 3s
218050K .......... .......... .......... .......... .......... 82% 9.97M 3s
218100K .......... .......... .......... .......... .......... 82% 10.6M 3s
218150K .......... .......... .......... .......... .......... 82% 9.90M 3s
218200K .......... .......... .......... .......... .......... 82% 9.75M 3s
218250K .......... .......... .......... .......... .......... 82% 12.7M 3s
218300K .......... .......... .......... .......... .......... 82% 9.14M 3s
218350K .......... .......... .......... .......... .......... 82% 7.91M 3s
218400K .......... .......... .......... .......... .......... 82% 9.91M 3s
218450K .......... .......... .......... .......... .......... 82% 12.4M 3s
218500K .......... .......... .......... .......... .......... 82% 10.9M 3s
218550K .......... .......... .......... .......... .......... 82% 22.5M 3s
218600K .......... .......... .......... .......... .......... 82% 15.9M 3s
218650K .......... .......... .......... .......... .......... 82% 23.9M 3s
218700K .......... .......... .......... .......... .......... 82% 9.73M 3s
218750K .......... .......... .......... .......... .......... 82% 21.1M 3s
218800K .......... .......... .......... .......... .......... 82% 55.5M 3s
218850K .......... .......... .......... .......... .......... 82% 15.0M 3s
218900K .......... .......... .......... .......... .......... 82% 20.7M 3s
218950K .......... .......... .......... .......... .......... 82% 25.4M 3s
219000K .......... .......... .......... .......... .......... 82% 11.1M 3s
219050K .......... .......... .......... .......... .......... 82% 10.7M 3s
219100K .......... .......... .......... .......... .......... 82% 54.1M 3s
219150K .......... .......... .......... .......... .......... 82% 21.1M 3s
219200K .......... .......... .......... .......... .......... 82% 13.2M 3s
219250K .......... .......... .......... .......... .......... 82% 14.7M 3s
219300K .......... .......... .......... .......... .......... 82% 17.9M 3s
219350K .......... .......... .......... .......... .......... 82% 12.7M 3s
219400K .......... .......... .......... .......... .......... 82% 15.9M 3s
219450K .......... .......... .......... .......... .......... 82% 7.71M 3s
219500K .......... .......... .......... .......... .......... 82% 10.5M 3s
219550K .......... .......... .......... .......... .......... 82% 9.18M 3s
219600K .......... .......... .......... .......... .......... 82% 6.68M 3s
219650K .......... .......... .......... .......... .......... 82% 7.18M 3s
219700K .......... .......... .......... .......... .......... 82% 5.49M 3s
219750K .......... .......... .......... .......... .......... 82% 7.52M 3s
219800K .......... .......... .......... .......... .......... 82% 5.31M 3s
219850K .......... .......... .......... .......... .......... 82% 8.58M 3s
219900K .......... .......... .......... .......... .......... 82% 6.45M 3s
219950K .......... .......... .......... .......... .......... 82% 7.06M 3s
220000K .......... .......... .......... .......... .......... 82% 6.30M 3s
220050K .......... .......... .......... .......... .......... 82% 6.55M 3s
220100K .......... .......... .......... .......... .......... 82% 17.5M 3s
220150K .......... .......... .......... .......... .......... 82% 21.1M 3s
220200K .......... .......... .......... .......... .......... 82% 19.2M 3s
220250K .......... .......... .......... .......... .......... 82% 53.0M 3s
220300K .......... .......... .......... .......... .......... 82% 22.5M 3s
220350K .......... .......... .......... .......... .......... 82% 21.2M 3s
220400K .......... .......... .......... .......... .......... 82% 37.5M 3s
220450K .......... .......... .......... .......... .......... 82% 25.1M 3s
220500K .......... .......... .......... .......... .......... 82% 26.8M 3s
220550K .......... .......... .......... .......... .......... 83% 27.1M 3s
220600K .......... .......... .......... .......... .......... 83% 22.3M 3s
220650K .......... .......... .......... .......... .......... 83% 32.3M 3s
220700K .......... .......... .......... .......... .......... 83% 18.8M 3s
220750K .......... .......... .......... .......... .......... 83% 25.8M 3s
220800K .......... .......... .......... .......... .......... 83% 35.2M 3s
220850K .......... .......... .......... .......... .......... 83% 23.4M 3s
220900K .......... .......... .......... .......... .......... 83% 23.2M 3s
220950K .......... .......... .......... .......... .......... 83% 23.6M 3s
221000K .......... .......... .......... .......... .......... 83% 28.4M 3s
221050K .......... .......... .......... .......... .......... 83% 22.9M 3s
221100K .......... .......... .......... .......... .......... 83% 11.7M 3s
221150K .......... .......... .......... .......... .......... 83% 30.3M 3s
221200K .......... .......... .......... .......... .......... 83% 8.45M 3s
221250K .......... .......... .......... .......... .......... 83% 24.0M 3s
221300K .......... .......... .......... .......... .......... 83% 25.2M 3s
221350K .......... .......... .......... .......... .......... 83% 14.2M 3s
221400K .......... .......... .......... .......... .......... 83% 20.4M 3s
221450K .......... .......... .......... .......... .......... 83% 13.0M 3s
221500K .......... .......... .......... .......... .......... 83% 19.9M 3s
221550K .......... .......... .......... .......... .......... 83% 19.9M 3s
221600K .......... .......... .......... .......... .......... 83% 15.9M 3s
221650K .......... .......... .......... .......... .......... 83% 21.1M 3s
221700K .......... .......... .......... .......... .......... 83% 17.2M 3s
221750K .......... .......... .......... .......... .......... 83% 16.8M 3s
221800K .......... .......... .......... .......... .......... 83% 35.5M 3s
221850K .......... .......... .......... .......... .......... 83% 13.1M 3s
221900K .......... .......... .......... .......... .......... 83% 30.6M 3s
221950K .......... .......... .......... .......... .......... 83% 8.91M 3s
222000K .......... .......... .......... .......... .......... 83% 175M 3s
222050K .......... .......... .......... .......... .......... 83% 26.3M 3s
222100K .......... .......... .......... .......... .......... 83% 10.5M 3s
222150K .......... .......... .......... .......... .......... 83% 130M 3s
222200K .......... .......... .......... .......... .......... 83% 23.1M 3s
222250K .......... .......... .......... .......... .......... 83% 20.5M 3s
222300K .......... .......... .......... .......... .......... 83% 17.5M 3s
222350K .......... .......... .......... .......... .......... 83% 15.0M 3s
222400K .......... .......... .......... .......... .......... 83% 11.6M 3s
222450K .......... .......... .......... .......... .......... 83% 25.4M 3s
222500K .......... .......... .......... .......... .......... 83% 20.1M 3s
222550K .......... .......... .......... .......... .......... 83% 10.0M 3s
222600K .......... .......... .......... .......... .......... 83% 15.5M 3s
222650K .......... .......... .......... .......... .......... 83% 8.83M 3s
222700K .......... .......... .......... .......... .......... 83% 7.20M 3s
222750K .......... .......... .......... .......... .......... 83% 8.46M 3s
222800K .......... .......... .......... .......... .......... 83% 8.51M 3s
222850K .......... .......... .......... .......... .......... 83% 6.25M 3s
222900K .......... .......... .......... .......... .......... 83% 7.16M 3s
222950K .......... .......... .......... .......... .......... 83% 6.21M 3s
223000K .......... .......... .......... .......... .......... 83% 12.9M 3s
223050K .......... .......... .......... .......... .......... 83% 10.8M 3s
223100K .......... .......... .......... .......... .......... 83% 10.5M 3s
223150K .......... .......... .......... .......... .......... 83% 13.4M 3s
223200K .......... .......... .......... .......... .......... 84% 10.8M 3s
223250K .......... .......... .......... .......... .......... 84% 15.1M 3s
223300K .......... .......... .......... .......... .......... 84% 15.3M 3s
223350K .......... .......... .......... .......... .......... 84% 14.2M 3s
223400K .......... .......... .......... .......... .......... 84% 12.3M 3s
223450K .......... .......... .......... .......... .......... 84% 14.8M 3s
223500K .......... .......... .......... .......... .......... 84% 16.5M 3s
223550K .......... .......... .......... .......... .......... 84% 19.1M 3s
223600K .......... .......... .......... .......... .......... 84% 12.5M 3s
223650K .......... .......... .......... .......... .......... 84% 11.2M 3s
223700K .......... .......... .......... .......... .......... 84% 6.88M 3s
223750K .......... .......... .......... .......... .......... 84% 11.0M 3s
223800K .......... .......... .......... .......... .......... 84% 5.18M 3s
223850K .......... .......... .......... .......... .......... 84% 11.0M 3s
223900K .......... .......... .......... .......... .......... 84% 10.3M 3s
223950K .......... .......... .......... .......... .......... 84% 7.84M 3s
224000K .......... .......... .......... .......... .......... 84% 8.79M 3s
224050K .......... .......... .......... .......... .......... 84% 7.49M 3s
224100K .......... .......... .......... .......... .......... 84% 6.84M 3s
224150K .......... .......... .......... .......... .......... 84% 7.97M 3s
224200K .......... .......... .......... .......... .......... 84% 6.32M 3s
224250K .......... .......... .......... .......... .......... 84% 6.77M 3s
224300K .......... .......... .......... .......... .......... 84% 5.89M 3s
224350K .......... .......... .......... .......... .......... 84% 5.49M 3s
224400K .......... .......... .......... .......... .......... 84% 9.70M 3s
224450K .......... .......... .......... .......... .......... 84% 4.82M 3s
224500K .......... .......... .......... .......... .......... 84% 5.94M 3s
224550K .......... .......... .......... .......... .......... 84% 6.47M 3s
224600K .......... .......... .......... .......... .......... 84% 5.46M 3s
224650K .......... .......... .......... .......... .......... 84% 6.45M 3s
224700K .......... .......... .......... .......... .......... 84% 5.05M 3s
224750K .......... .......... .......... .......... .......... 84% 6.55M 3s
224800K .......... .......... .......... .......... .......... 84% 13.7M 3s
224850K .......... .......... .......... .......... .......... 84% 30.8M 3s
224900K .......... .......... .......... .......... .......... 84% 32.3M 3s
224950K .......... .......... .......... .......... .......... 84% 30.6M 3s
225000K .......... .......... .......... .......... .......... 84% 30.6M 3s
225050K .......... .......... .......... .......... .......... 84% 30.9M 3s
225100K .......... .......... .......... .......... .......... 84% 25.5M 3s
225150K .......... .......... .......... .......... .......... 84% 25.6M 3s
225200K .......... .......... .......... .......... .......... 84% 22.3M 3s
225250K .......... .......... .......... .......... .......... 84% 25.4M 3s
225300K .......... .......... .......... .......... .......... 84% 10.1M 3s
225350K .......... .......... .......... .......... .......... 84% 277M 3s
225400K .......... .......... .......... .......... .......... 84% 42.9M 3s
225450K .......... .......... .......... .......... .......... 84% 14.3M 3s
225500K .......... .......... .......... .......... .......... 84% 43.8M 3s
225550K .......... .......... .......... .......... .......... 84% 20.9M 3s
225600K .......... .......... .......... .......... .......... 84% 19.6M 3s
225650K .......... .......... .......... .......... .......... 84% 21.1M 3s
225700K .......... .......... .......... .......... .......... 84% 17.1M 3s
225750K .......... .......... .......... .......... .......... 84% 19.1M 3s
225800K .......... .......... .......... .......... .......... 84% 19.8M 3s
225850K .......... .......... .......... .......... .......... 84% 18.7M 3s
225900K .......... .......... .......... .......... .......... 85% 19.9M 3s
225950K .......... .......... .......... .......... .......... 85% 17.0M 3s
226000K .......... .......... .......... .......... .......... 85% 15.6M 3s
226050K .......... .......... .......... .......... .......... 85% 20.4M 3s
226100K .......... .......... .......... .......... .......... 85% 15.3M 3s
226150K .......... .......... .......... .......... .......... 85% 13.3M 3s
226200K .......... .......... .......... .......... .......... 85% 12.1M 3s
226250K .......... .......... .......... .......... .......... 85% 15.8M 3s
226300K .......... .......... .......... .......... .......... 85% 28.2M 3s
226350K .......... .......... .......... .......... .......... 85% 20.1M 3s
226400K .......... .......... .......... .......... .......... 85% 21.5M 3s
226450K .......... .......... .......... .......... .......... 85% 18.9M 3s
226500K .......... .......... .......... .......... .......... 85% 21.9M 3s
226550K .......... .......... .......... .......... .......... 85% 24.2M 3s
226600K .......... .......... .......... .......... .......... 85% 17.3M 3s
226650K .......... .......... .......... .......... .......... 85% 19.9M 3s
226700K .......... .......... .......... .......... .......... 85% 9.86M 3s
226750K .......... .......... .......... .......... .......... 85% 29.3M 3s
226800K .......... .......... .......... .......... .......... 85% 13.9M 3s
226850K .......... .......... .......... .......... .......... 85% 31.5M 3s
226900K .......... .......... .......... .......... .......... 85% 21.3M 3s
226950K .......... .......... .......... .......... .......... 85% 14.5M 3s
227000K .......... .......... .......... .......... .......... 85% 16.9M 3s
227050K .......... .......... .......... .......... .......... 85% 17.0M 3s
227100K .......... .......... .......... .......... .......... 85% 12.2M 3s
227150K .......... .......... .......... .......... .......... 85% 16.0M 3s
227200K .......... .......... .......... .......... .......... 85% 9.37M 3s
227250K .......... .......... .......... .......... .......... 85% 14.4M 3s
227300K .......... .......... .......... .......... .......... 85% 14.9M 3s
227350K .......... .......... .......... .......... .......... 85% 11.0M 3s
227400K .......... .......... .......... .......... .......... 85% 8.73M 3s
227450K .......... .......... .......... .......... .......... 85% 9.97M 3s
227500K .......... .......... .......... .......... .......... 85% 17.8M 3s
227550K .......... .......... .......... .......... .......... 85% 20.7M 3s
227600K .......... .......... .......... .......... .......... 85% 23.3M 3s
227650K .......... .......... .......... .......... .......... 85% 18.6M 3s
227700K .......... .......... .......... .......... .......... 85% 12.7M 3s
227750K .......... .......... .......... .......... .......... 85% 80.8M 3s
227800K .......... .......... .......... .......... .......... 85% 20.6M 3s
227850K .......... .......... .......... .......... .......... 85% 15.6M 3s
227900K .......... .......... .......... .......... .......... 85% 13.4M 3s
227950K .......... .......... .......... .......... .......... 85% 22.0M 3s
228000K .......... .......... .......... .......... .......... 85% 25.2M 3s
228050K .......... .......... .......... .......... .......... 85% 18.1M 3s
228100K .......... .......... .......... .......... .......... 85% 15.9M 2s
228150K .......... .......... .......... .......... .......... 85% 15.3M 2s
228200K .......... .......... .......... .......... .......... 85% 14.5M 2s
228250K .......... .......... .......... .......... .......... 85% 13.1M 2s
228300K .......... .......... .......... .......... .......... 85% 18.0M 2s
228350K .......... .......... .......... .......... .......... 85% 14.0M 2s
228400K .......... .......... .......... .......... .......... 85% 17.5M 2s
228450K .......... .......... .......... .......... .......... 85% 11.8M 2s
228500K .......... .......... .......... .......... .......... 85% 12.1M 2s
228550K .......... .......... .......... .......... .......... 86% 14.1M 2s
228600K .......... .......... .......... .......... .......... 86% 11.4M 2s
228650K .......... .......... .......... .......... .......... 86% 17.3M 2s
228700K .......... .......... .......... .......... .......... 86% 23.5M 2s
228750K .......... .......... .......... .......... .......... 86% 25.3M 2s
228800K .......... .......... .......... .......... .......... 86% 27.4M 2s
228850K .......... .......... .......... .......... .......... 86% 21.1M 2s
228900K .......... .......... .......... .......... .......... 86% 25.2M 2s
228950K .......... .......... .......... .......... .......... 86% 22.3M 2s
229000K .......... .......... .......... .......... .......... 86% 25.4M 2s
229050K .......... .......... .......... .......... .......... 86% 23.5M 2s
229100K .......... .......... .......... .......... .......... 86% 24.9M 2s
229150K .......... .......... .......... .......... .......... 86% 25.4M 2s
229200K .......... .......... .......... .......... .......... 86% 22.4M 2s
229250K .......... .......... .......... .......... .......... 86% 26.5M 2s
229300K .......... .......... .......... .......... .......... 86% 21.9M 2s
229350K .......... .......... .......... .......... .......... 86% 18.3M 2s
229400K .......... .......... .......... .......... .......... 86% 25.8M 2s
229450K .......... .......... .......... .......... .......... 86% 16.4M 2s
229500K .......... .......... .......... .......... .......... 86% 24.6M 2s
229550K .......... .......... .......... .......... .......... 86% 25.8M 2s
229600K .......... .......... .......... .......... .......... 86% 22.2M 2s
229650K .......... .......... .......... .......... .......... 86% 23.4M 2s
229700K .......... .......... .......... .......... .......... 86% 15.1M 2s
229750K .......... .......... .......... .......... .......... 86% 28.6M 2s
229800K .......... .......... .......... .......... .......... 86% 18.9M 2s
229850K .......... .......... .......... .......... .......... 86% 10.4M 2s
229900K .......... .......... .......... .......... .......... 86% 49.3M 2s
229950K .......... .......... .......... .......... .......... 86% 17.9M 2s
230000K .......... .......... .......... .......... .......... 86% 19.2M 2s
230050K .......... .......... .......... .......... .......... 86% 15.5M 2s
230100K .......... .......... .......... .......... .......... 86% 19.2M 2s
230150K .......... .......... .......... .......... .......... 86% 11.2M 2s
230200K .......... .......... .......... .......... .......... 86% 18.0M 2s
230250K .......... .......... .......... .......... .......... 86% 15.2M 2s
230300K .......... .......... .......... .......... .......... 86% 12.1M 2s
230350K .......... .......... .......... .......... .......... 86% 9.94M 2s
230400K .......... .......... .......... .......... .......... 86% 12.0M 2s
230450K .......... .......... .......... .......... .......... 86% 10.6M 2s
230500K .......... .......... .......... .......... .......... 86% 12.5M 2s
230550K .......... .......... .......... .......... .......... 86% 12.2M 2s
230600K .......... .......... .......... .......... .......... 86% 10.3M 2s
230650K .......... .......... .......... .......... .......... 86% 11.5M 2s
230700K .......... .......... .......... .......... .......... 86% 18.4M 2s
230750K .......... .......... .......... .......... .......... 86% 28.0M 2s
230800K .......... .......... .......... .......... .......... 86% 28.6M 2s
230850K .......... .......... .......... .......... .......... 86% 16.4M 2s
230900K .......... .......... .......... .......... .......... 86% 97.9M 2s
230950K .......... .......... .......... .......... .......... 86% 19.1M 2s
231000K .......... .......... .......... .......... .......... 86% 13.6M 2s
231050K .......... .......... .......... .......... .......... 86% 31.8M 2s
231100K .......... .......... .......... .......... .......... 86% 15.7M 2s
231150K .......... .......... .......... .......... .......... 86% 18.5M 2s
231200K .......... .......... .......... .......... .......... 87% 16.7M 2s
231250K .......... .......... .......... .......... .......... 87% 18.7M 2s
231300K .......... .......... .......... .......... .......... 87% 20.5M 2s
231350K .......... .......... .......... .......... .......... 87% 15.3M 2s
231400K .......... .......... .......... .......... .......... 87% 14.3M 2s
231450K .......... .......... .......... .......... .......... 87% 15.2M 2s
231500K .......... .......... .......... .......... .......... 87% 19.0M 2s
231550K .......... .......... .......... .......... .......... 87% 17.3M 2s
231600K .......... .......... .......... .......... .......... 87% 13.8M 2s
231650K .......... .......... .......... .......... .......... 87% 19.7M 2s
231700K .......... .......... .......... .......... .......... 87% 11.5M 2s
231750K .......... .......... .......... .......... .......... 87% 135M 2s
231800K .......... .......... .......... .......... .......... 87% 22.1M 2s
231850K .......... .......... .......... .......... .......... 87% 13.7M 2s
231900K .......... .......... .......... .......... .......... 87% 41.6M 2s
231950K .......... .......... .......... .......... .......... 87% 12.7M 2s
232000K .......... .......... .......... .......... .......... 87% 21.8M 2s
232050K .......... .......... .......... .......... .......... 87% 16.3M 2s
232100K .......... .......... .......... .......... .......... 87% 13.1M 2s
232150K .......... .......... .......... .......... .......... 87% 13.8M 2s
232200K .......... .......... .......... .......... .......... 87% 13.4M 2s
232250K .......... .......... .......... .......... .......... 87% 15.0M 2s
232300K .......... .......... .......... .......... .......... 87% 15.7M 2s
232350K .......... .......... .......... .......... .......... 87% 11.9M 2s
232400K .......... .......... .......... .......... .......... 87% 10.2M 2s
232450K .......... .......... .......... .......... .......... 87% 16.9M 2s
232500K .......... .......... .......... .......... .......... 87% 14.2M 2s
232550K .......... .......... .......... .......... .......... 87% 10.2M 2s
232600K .......... .......... .......... .......... .......... 87% 8.75M 2s
232650K .......... .......... .......... .......... .......... 87% 13.3M 2s
232700K .......... .......... .......... .......... .......... 87% 11.4M 2s
232750K .......... .......... .......... .......... .......... 87% 13.6M 2s
232800K .......... .......... .......... .......... .......... 87% 11.5M 2s
232850K .......... .......... .......... .......... .......... 87% 12.4M 2s
232900K .......... .......... .......... .......... .......... 87% 17.2M 2s
232950K .......... .......... .......... .......... .......... 87% 12.9M 2s
233000K .......... .......... .......... .......... .......... 87% 15.9M 2s
233050K .......... .......... .......... .......... .......... 87% 18.9M 2s
233100K .......... .......... .......... .......... .......... 87% 13.7M 2s
233150K .......... .......... .......... .......... .......... 87% 17.8M 2s
233200K .......... .......... .......... .......... .......... 87% 15.4M 2s
233250K .......... .......... .......... .......... .......... 87% 14.7M 2s
233300K .......... .......... .......... .......... .......... 87% 16.6M 2s
233350K .......... .......... .......... .......... .......... 87% 26.1M 2s
233400K .......... .......... .......... .......... .......... 87% 47.3M 2s
233450K .......... .......... .......... .......... .......... 87% 15.1M 2s
233500K .......... .......... .......... .......... .......... 87% 404M 2s
233550K .......... .......... .......... .......... .......... 87% 88.3M 2s
233600K .......... .......... .......... .......... .......... 87% 44.7M 2s
233650K .......... .......... .......... .......... .......... 87% 32.2M 2s
233700K .......... .......... .......... .......... .......... 87% 61.8M 2s
233750K .......... .......... .......... .......... .......... 87% 9.67M 2s
233800K .......... .......... .......... .......... .......... 87% 18.8M 2s
233850K .......... .......... .......... .......... .......... 88% 11.5M 2s
233900K .......... .......... .......... .......... .......... 88% 17.2M 2s
233950K .......... .......... .......... .......... .......... 88% 12.4M 2s
234000K .......... .......... .......... .......... .......... 88% 13.1M 2s
234050K .......... .......... .......... .......... .......... 88% 13.5M 2s
234100K .......... .......... .......... .......... .......... 88% 14.1M 2s
234150K .......... .......... .......... .......... .......... 88% 13.4M 2s
234200K .......... .......... .......... .......... .......... 88% 11.4M 2s
234250K .......... .......... .......... .......... .......... 88% 14.0M 2s
234300K .......... .......... .......... .......... .......... 88% 10.2M 2s
234350K .......... .......... .......... .......... .......... 88% 7.46M 2s
234400K .......... .......... .......... .......... .......... 88% 9.76M 2s
234450K .......... .......... .......... .......... .......... 88% 8.76M 2s
234500K .......... .......... .......... .......... .......... 88% 11.0M 2s
234550K .......... .......... .......... .......... .......... 88% 10.4M 2s
234600K .......... .......... .......... .......... .......... 88% 8.63M 2s
234650K .......... .......... .......... .......... .......... 88% 9.47M 2s
234700K .......... .......... .......... .......... .......... 88% 15.4M 2s
234750K .......... .......... .......... .......... .......... 88% 12.4M 2s
234800K .......... .......... .......... .......... .......... 88% 11.4M 2s
234850K .......... .......... .......... .......... .......... 88% 21.6M 2s
234900K .......... .......... .......... .......... .......... 88% 14.1M 2s
234950K .......... .......... .......... .......... .......... 88% 10.6M 2s
235000K .......... .......... .......... .......... .......... 88% 15.2M 2s
235050K .......... .......... .......... .......... .......... 88% 10.0M 2s
235100K .......... .......... .......... .......... .......... 88% 16.2M 2s
235150K .......... .......... .......... .......... .......... 88% 13.5M 2s
235200K .......... .......... .......... .......... .......... 88% 11.9M 2s
235250K .......... .......... .......... .......... .......... 88% 17.1M 2s
235300K .......... .......... .......... .......... .......... 88% 15.0M 2s
235350K .......... .......... .......... .......... .......... 88% 11.4M 2s
235400K .......... .......... .......... .......... .......... 88% 14.2M 2s
235450K .......... .......... .......... .......... .......... 88% 11.6M 2s
235500K .......... .......... .......... .......... .......... 88% 12.2M 2s
235550K .......... .......... .......... .......... .......... 88% 14.8M 2s
235600K .......... .......... .......... .......... .......... 88% 11.9M 2s
235650K .......... .......... .......... .......... .......... 88% 14.7M 2s
235700K .......... .......... .......... .......... .......... 88% 17.4M 2s
235750K .......... .......... .......... .......... .......... 88% 28.7M 2s
235800K .......... .......... .......... .......... .......... 88% 28.4M 2s
235850K .......... .......... .......... .......... .......... 88% 33.9M 2s
235900K .......... .......... .......... .......... .......... 88% 24.6M 2s
235950K .......... .......... .......... .......... .......... 88% 18.3M 2s
236000K .......... .......... .......... .......... .......... 88% 162M 2s
236050K .......... .......... .......... .......... .......... 88% 20.9M 2s
236100K .......... .......... .......... .......... .......... 88% 22.6M 2s
236150K .......... .......... .......... .......... .......... 88% 6.37M 2s
236200K .......... .......... .......... .......... .......... 88% 344M 2s
236250K .......... .......... .......... .......... .......... 88% 16.5M 2s
236300K .......... .......... .......... .......... .......... 88% 11.0M 2s
236350K .......... .......... .......... .......... .......... 88% 9.79M 2s
236400K .......... .......... .......... .......... .......... 88% 8.41M 2s
236450K .......... .......... .......... .......... .......... 88% 9.46M 2s
236500K .......... .......... .......... .......... .......... 89% 12.7M 2s
236550K .......... .......... .......... .......... .......... 89% 12.4M 2s
236600K .......... .......... .......... .......... .......... 89% 13.4M 2s
236650K .......... .......... .......... .......... .......... 89% 11.1M 2s
236700K .......... .......... .......... .......... .......... 89% 11.3M 2s
236750K .......... .......... .......... .......... .......... 89% 11.5M 2s
236800K .......... .......... .......... .......... .......... 89% 13.1M 2s
236850K .......... .......... .......... .......... .......... 89% 10.2M 2s
236900K .......... .......... .......... .......... .......... 89% 8.37M 2s
236950K .......... .......... .......... .......... .......... 89% 6.50M 2s
237000K .......... .......... .......... .......... .......... 89% 8.06M 2s
237050K .......... .......... .......... .......... .......... 89% 8.54M 2s
237100K .......... .......... .......... .......... .......... 89% 6.55M 2s
237150K .......... .......... .......... .......... .......... 89% 8.09M 2s
237200K .......... .......... .......... .......... .......... 89% 7.31M 2s
237250K .......... .......... .......... .......... .......... 89% 23.7M 2s
237300K .......... .......... .......... .......... .......... 89% 34.5M 2s
237350K .......... .......... .......... .......... .......... 89% 21.1M 2s
237400K .......... .......... .......... .......... .......... 89% 55.5M 2s
237450K .......... .......... .......... .......... .......... 89% 30.9M 2s
237500K .......... .......... .......... .......... .......... 89% 18.8M 2s
237550K .......... .......... .......... .......... .......... 89% 51.4M 2s
237600K .......... .......... .......... .......... .......... 89% 23.6M 2s
237650K .......... .......... .......... .......... .......... 89% 15.1M 2s
237700K .......... .......... .......... .......... .......... 89% 21.0M 2s
237750K .......... .......... .......... .......... .......... 89% 21.2M 2s
237800K .......... .......... .......... .......... .......... 89% 13.9M 2s
237850K .......... .......... .......... .......... .......... 89% 12.4M 2s
237900K .......... .......... .......... .......... .......... 89% 13.3M 2s
237950K .......... .......... .......... .......... .......... 89% 11.7M 2s
238000K .......... .......... .......... .......... .......... 89% 11.1M 2s
238050K .......... .......... .......... .......... .......... 89% 10.3M 2s
238100K .......... .......... .......... .......... .......... 89% 8.89M 2s
238150K .......... .......... .......... .......... .......... 89% 15.2M 2s
238200K .......... .......... .......... .......... .......... 89% 11.7M 2s
238250K .......... .......... .......... .......... .......... 89% 9.90M 2s
238300K .......... .......... .......... .......... .......... 89% 12.3M 2s
238350K .......... .......... .......... .......... .......... 89% 8.02M 2s
238400K .......... .......... .......... .......... .......... 89% 8.76M 2s
238450K .......... .......... .......... .......... .......... 89% 7.08M 2s
238500K .......... .......... .......... .......... .......... 89% 8.68M 2s
238550K .......... .......... .......... .......... .......... 89% 9.24M 2s
238600K .......... .......... .......... .......... .......... 89% 7.36M 2s
238650K .......... .......... .......... .......... .......... 89% 10.7M 2s
238700K .......... .......... .......... .......... .......... 89% 7.02M 2s
238750K .......... .......... .......... .......... .......... 89% 14.5M 2s
238800K .......... .......... .......... .......... .......... 89% 11.7M 2s
238850K .......... .......... .......... .......... .......... 89% 9.72M 2s
238900K .......... .......... .......... .......... .......... 89% 13.0M 2s
238950K .......... .......... .......... .......... .......... 89% 10.2M 2s
239000K .......... .......... .......... .......... .......... 89% 10.5M 2s
239050K .......... .......... .......... .......... .......... 89% 9.60M 2s
239100K .......... .......... .......... .......... .......... 89% 7.38M 2s
239150K .......... .......... .......... .......... .......... 90% 9.23M 2s
239200K .......... .......... .......... .......... .......... 90% 9.63M 2s
239250K .......... .......... .......... .......... .......... 90% 9.80M 2s
239300K .......... .......... .......... .......... .......... 90% 10.0M 2s
239350K .......... .......... .......... .......... .......... 90% 8.60M 2s
239400K .......... .......... .......... .......... .......... 90% 11.2M 2s
239450K .......... .......... .......... .......... .......... 90% 6.70M 2s
239500K .......... .......... .......... .......... .......... 90% 5.01M 2s
239550K .......... .......... .......... .......... .......... 90% 6.05M 2s
239600K .......... .......... .......... .......... .......... 90% 5.48M 2s
239650K .......... .......... .......... .......... .......... 90% 6.67M 2s
239700K .......... .......... .......... .......... .......... 90% 6.30M 2s
239750K .......... .......... .......... .......... .......... 90% 6.79M 2s
239800K .......... .......... .......... .......... .......... 90% 7.77M 2s
239850K .......... .......... .......... .......... .......... 90% 4.86M 2s
239900K .......... .......... .......... .......... .......... 90% 8.97M 2s
239950K .......... .......... .......... .......... .......... 90% 8.08M 2s
240000K .......... .......... .......... .......... .......... 90% 8.88M 2s
240050K .......... .......... .......... .......... .......... 90% 12.1M 2s
240100K .......... .......... .......... .......... .......... 90% 9.80M 2s
240150K .......... .......... .......... .......... .......... 90% 11.1M 2s
240200K .......... .......... .......... .......... .......... 90% 10.6M 2s
240250K .......... .......... .......... .......... .......... 90% 14.7M 2s
240300K .......... .......... .......... .......... .......... 90% 13.2M 2s
240350K .......... .......... .......... .......... .......... 90% 10.5M 2s
240400K .......... .......... .......... .......... .......... 90% 12.3M 2s
240450K .......... .......... .......... .......... .......... 90% 10.3M 2s
240500K .......... .......... .......... .......... .......... 90% 12.1M 2s
240550K .......... .......... .......... .......... .......... 90% 13.6M 2s
240600K .......... .......... .......... .......... .......... 90% 9.48M 2s
240650K .......... .......... .......... .......... .......... 90% 10.6M 2s
240700K .......... .......... .......... .......... .......... 90% 8.23M 2s
240750K .......... .......... .......... .......... .......... 90% 9.55M 2s
240800K .......... .......... .......... .......... .......... 90% 11.3M 2s
240850K .......... .......... .......... .......... .......... 90% 7.39M 2s
240900K .......... .......... .......... .......... .......... 90% 10.8M 2s
240950K .......... .......... .......... .......... .......... 90% 7.52M 2s
241000K .......... .......... .......... .......... .......... 90% 15.8M 2s
241050K .......... .......... .......... .......... .......... 90% 12.7M 2s
241100K .......... .......... .......... .......... .......... 90% 17.1M 2s
241150K .......... .......... .......... .......... .......... 90% 10.4M 2s
241200K .......... .......... .......... .......... .......... 90% 12.1M 2s
241250K .......... .......... .......... .......... .......... 90% 15.5M 2s
241300K .......... .......... .......... .......... .......... 90% 14.0M 2s
241350K .......... .......... .......... .......... .......... 90% 11.0M 2s
241400K .......... .......... .......... .......... .......... 90% 11.9M 2s
241450K .......... .......... .......... .......... .......... 90% 12.1M 2s
241500K .......... .......... .......... .......... .......... 90% 16.2M 2s
241550K .......... .......... .......... .......... .......... 90% 11.5M 2s
241600K .......... .......... .......... .......... .......... 90% 14.3M 2s
241650K .......... .......... .......... .......... .......... 90% 11.2M 2s
241700K .......... .......... .......... .......... .......... 90% 11.7M 2s
241750K .......... .......... .......... .......... .......... 90% 16.6M 2s
241800K .......... .......... .......... .......... .......... 90% 15.8M 2s
241850K .......... .......... .......... .......... .......... 91% 12.8M 2s
241900K .......... .......... .......... .......... .......... 91% 13.3M 2s
241950K .......... .......... .......... .......... .......... 91% 9.52M 2s
242000K .......... .......... .......... .......... .......... 91% 14.7M 2s
242050K .......... .......... .......... .......... .......... 91% 9.86M 2s
242100K .......... .......... .......... .......... .......... 91% 9.56M 2s
242150K .......... .......... .......... .......... .......... 91% 9.24M 2s
242200K .......... .......... .......... .......... .......... 91% 9.80M 2s
242250K .......... .......... .......... .......... .......... 91% 11.3M 2s
242300K .......... .......... .......... .......... .......... 91% 9.71M 2s
242350K .......... .......... .......... .......... .......... 91% 9.07M 2s
242400K .......... .......... .......... .......... .......... 91% 9.44M 2s
242450K .......... .......... .......... .......... .......... 91% 8.87M 2s
242500K .......... .......... .......... .......... .......... 91% 14.6M 2s
242550K .......... .......... .......... .......... .......... 91% 27.0M 2s
242600K .......... .......... .......... .......... .......... 91% 9.04M 2s
242650K .......... .......... .......... .......... .......... 91% 160M 2s
242700K .......... .......... .......... .......... .......... 91% 12.6M 2s
242750K .......... .......... .......... .......... .......... 91% 17.6M 2s
242800K .......... .......... .......... .......... .......... 91% 11.1M 2s
242850K .......... .......... .......... .......... .......... 91% 11.5M 2s
242900K .......... .......... .......... .......... .......... 91% 11.7M 2s
242950K .......... .......... .......... .......... .......... 91% 10.2M 2s
243000K .......... .......... .......... .......... .......... 91% 10.5M 2s
243050K .......... .......... .......... .......... .......... 91% 10.1M 2s
243100K .......... .......... .......... .......... .......... 91% 7.67M 2s
243150K .......... .......... .......... .......... .......... 91% 6.43M 2s
243200K .......... .......... .......... .......... .......... 91% 7.26M 2s
243250K .......... .......... .......... .......... .......... 91% 8.52M 2s
243300K .......... .......... .......... .......... .......... 91% 14.1M 2s
243350K .......... .......... .......... .......... .......... 91% 21.9M 1s
243400K .......... .......... .......... .......... .......... 91% 33.2M 1s
243450K .......... .......... .......... .......... .......... 91% 24.8M 1s
243500K .......... .......... .......... .......... .......... 91% 30.4M 1s
243550K .......... .......... .......... .......... .......... 91% 24.3M 1s
243600K .......... .......... .......... .......... .......... 91% 17.1M 1s
243650K .......... .......... .......... .......... .......... 91% 15.8M 1s
243700K .......... .......... .......... .......... .......... 91% 13.3M 1s
243750K .......... .......... .......... .......... .......... 91% 15.1M 1s
243800K .......... .......... .......... .......... .......... 91% 17.9M 1s
243850K .......... .......... .......... .......... .......... 91% 12.2M 1s
243900K .......... .......... .......... .......... .......... 91% 14.6M 1s
243950K .......... .......... .......... .......... .......... 91% 13.9M 1s
244000K .......... .......... .......... .......... .......... 91% 12.9M 1s
244050K .......... .......... .......... .......... .......... 91% 11.7M 1s
244100K .......... .......... .......... .......... .......... 91% 9.44M 1s
244150K .......... .......... .......... .......... .......... 91% 9.88M 1s
244200K .......... .......... .......... .......... .......... 91% 6.91M 1s
244250K .......... .......... .......... .......... .......... 91% 8.38M 1s
244300K .......... .......... .......... .......... .......... 91% 6.98M 1s
244350K .......... .......... .......... .......... .......... 91% 1.44M 1s
244400K .......... .......... .......... .......... .......... 91% 7.37M 1s
244450K .......... .......... .......... .......... .......... 91% 5.55M 1s
244500K .......... .......... .......... .......... .......... 92% 6.76M 1s
244550K .......... .......... .......... .......... .......... 92% 6.87M 1s
244600K .......... .......... .......... .......... .......... 92% 10.2M 1s
244650K .......... .......... .......... .......... .......... 92% 10.9M 1s
244700K .......... .......... .......... .......... .......... 92% 10.4M 1s
244750K .......... .......... .......... .......... .......... 92% 9.15M 1s
244800K .......... .......... .......... .......... .......... 92% 12.3M 1s
244850K .......... .......... .......... .......... .......... 92% 7.30M 1s
244900K .......... .......... .......... .......... .......... 92% 10.4M 1s
244950K .......... .......... .......... .......... .......... 92% 7.64M 1s
245000K .......... .......... .......... .......... .......... 92% 9.45M 1s
245050K .......... .......... .......... .......... .......... 92% 7.50M 1s
245100K .......... .......... .......... .......... .......... 92% 8.17M 1s
245150K .......... .......... .......... .......... .......... 92% 4.06M 1s
245200K .......... .......... .......... .......... .......... 92% 93.7M 1s
245250K .......... .......... .......... .......... .......... 92% 6.45M 1s
245300K .......... .......... .......... .......... .......... 92% 7.22M 1s
245350K .......... .......... .......... .......... .......... 92% 9.20M 1s
245400K .......... .......... .......... .......... .......... 92% 6.84M 1s
245450K .......... .......... .......... .......... .......... 92% 5.61M 1s
245500K .......... .......... .......... .......... .......... 92% 5.59M 1s
245550K .......... .......... .......... .......... .......... 92% 6.86M 1s
245600K .......... .......... .......... .......... .......... 92% 5.79M 1s
245650K .......... .......... .......... .......... .......... 92% 18.7M 1s
245700K .......... .......... .......... .......... .......... 92% 22.5M 1s
245750K .......... .......... .......... .......... .......... 92% 23.0M 1s
245800K .......... .......... .......... .......... .......... 92% 22.2M 1s
245850K .......... .......... .......... .......... .......... 92% 12.9M 1s
245900K .......... .......... .......... .......... .......... 92% 18.4M 1s
245950K .......... .......... .......... .......... .......... 92% 16.2M 1s
246000K .......... .......... .......... .......... .......... 92% 10.7M 1s
246050K .......... .......... .......... .......... .......... 92% 8.07M 1s
246100K .......... .......... .......... .......... .......... 92% 8.97M 1s
246150K .......... .......... .......... .......... .......... 92% 14.0M 1s
246200K .......... .......... .......... .......... .......... 92% 11.1M 1s
246250K .......... .......... .......... .......... .......... 92% 12.6M 1s
246300K .......... .......... .......... .......... .......... 92% 11.6M 1s
246350K .......... .......... .......... .......... .......... 92% 11.2M 1s
246400K .......... .......... .......... .......... .......... 92% 8.47M 1s
246450K .......... .......... .......... .......... .......... 92% 7.90M 1s
246500K .......... .......... .......... .......... .......... 92% 6.88M 1s
246550K .......... .......... .......... .......... .......... 92% 9.63M 1s
246600K .......... .......... .......... .......... .......... 92% 6.73M 1s
246650K .......... .......... .......... .......... .......... 92% 9.20M 1s
246700K .......... .......... .......... .......... .......... 92% 8.35M 1s
246750K .......... .......... .......... .......... .......... 92% 19.1M 1s
246800K .......... .......... .......... .......... .......... 92% 15.5M 1s
246850K .......... .......... .......... .......... .......... 92% 14.5M 1s
246900K .......... .......... .......... .......... .......... 92% 21.5M 1s
246950K .......... .......... .......... .......... .......... 92% 14.2M 1s
247000K .......... .......... .......... .......... .......... 92% 23.7M 1s
247050K .......... .......... .......... .......... .......... 92% 16.1M 1s
247100K .......... .......... .......... .......... .......... 92% 21.4M 1s
247150K .......... .......... .......... .......... .......... 93% 18.1M 1s
247200K .......... .......... .......... .......... .......... 93% 13.5M 1s
247250K .......... .......... .......... .......... .......... 93% 14.1M 1s
247300K .......... .......... .......... .......... .......... 93% 21.7M 1s
247350K .......... .......... .......... .......... .......... 93% 14.5M 1s
247400K .......... .......... .......... .......... .......... 93% 18.0M 1s
247450K .......... .......... .......... .......... .......... 93% 12.9M 1s
247500K .......... .......... .......... .......... .......... 93% 207M 1s
247550K .......... .......... .......... .......... .......... 93% 13.3M 1s
247600K .......... .......... .......... .......... .......... 93% 34.7M 1s
247650K .......... .......... .......... .......... .......... 93% 27.2M 1s
247700K .......... .......... .......... .......... .......... 93% 20.5M 1s
247750K .......... .......... .......... .......... .......... 93% 26.4M 1s
247800K .......... .......... .......... .......... .......... 93% 23.4M 1s
247850K .......... .......... .......... .......... .......... 93% 20.1M 1s
247900K .......... .......... .......... .......... .......... 93% 26.9M 1s
247950K .......... .......... .......... .......... .......... 93% 20.3M 1s
248000K .......... .......... .......... .......... .......... 93% 24.9M 1s
248050K .......... .......... .......... .......... .......... 93% 36.1M 1s
248100K .......... .......... .......... .......... .......... 93% 17.7M 1s
248150K .......... .......... .......... .......... .......... 93% 37.5M 1s
248200K .......... .......... .......... .......... .......... 93% 21.0M 1s
248250K .......... .......... .......... .......... .......... 93% 33.8M 1s
248300K .......... .......... .......... .......... .......... 93% 19.1M 1s
248350K .......... .......... .......... .......... .......... 93% 27.2M 1s
248400K .......... .......... .......... .......... .......... 93% 23.5M 1s
248450K .......... .......... .......... .......... .......... 93% 21.7M 1s
248500K .......... .......... .......... .......... .......... 93% 31.4M 1s
248550K .......... .......... .......... .......... .......... 93% 28.6M 1s
248600K .......... .......... .......... .......... .......... 93% 12.6M 1s
248650K .......... .......... .......... .......... .......... 93% 214M 1s
248700K .......... .......... .......... .......... .......... 93% 22.4M 1s
248750K .......... .......... .......... .......... .......... 93% 21.6M 1s
248800K .......... .......... .......... .......... .......... 93% 88.9M 1s
248850K .......... .......... .......... .......... .......... 93% 23.4M 1s
248900K .......... .......... .......... .......... .......... 93% 25.3M 1s
248950K .......... .......... .......... .......... .......... 93% 16.9M 1s
249000K .......... .......... .......... .......... .......... 93% 14.9M 1s
249050K .......... .......... .......... .......... .......... 93% 24.8M 1s
249100K .......... .......... .......... .......... .......... 93% 10.6M 1s
249150K .......... .......... .......... .......... .......... 93% 21.1M 1s
249200K .......... .......... .......... .......... .......... 93% 9.89M 1s
249250K .......... .......... .......... .......... .......... 93% 10.6M 1s
249300K .......... .......... .......... .......... .......... 93% 7.68M 1s
249350K .......... .......... .......... .......... .......... 93% 8.90M 1s
249400K .......... .......... .......... .......... .......... 93% 10.1M 1s
249450K .......... .......... .......... .......... .......... 93% 10.2M 1s
249500K .......... .......... .......... .......... .......... 93% 11.8M 1s
249550K .......... .......... .......... .......... .......... 93% 10.9M 1s
249600K .......... .......... .......... .......... .......... 93% 10.2M 1s
249650K .......... .......... .......... .......... .......... 93% 11.9M 1s
249700K .......... .......... .......... .......... .......... 93% 7.20M 1s
249750K .......... .......... .......... .......... .......... 93% 8.10M 1s
249800K .......... .......... .......... .......... .......... 94% 8.41M 1s
249850K .......... .......... .......... .......... .......... 94% 9.73M 1s
249900K .......... .......... .......... .......... .......... 94% 13.6M 1s
249950K .......... .......... .......... .......... .......... 94% 10.1M 1s
250000K .......... .......... .......... .......... .......... 94% 10.4M 1s
250050K .......... .......... .......... .......... .......... 94% 5.63M 1s
250100K .......... .......... .......... .......... .......... 94% 6.33M 1s
250150K .......... .......... .......... .......... .......... 94% 6.02M 1s
250200K .......... .......... .......... .......... .......... 94% 7.54M 1s
250250K .......... .......... .......... .......... .......... 94% 11.1M 1s
250300K .......... .......... .......... .......... .......... 94% 10.8M 1s
250350K .......... .......... .......... .......... .......... 94% 8.83M 1s
250400K .......... .......... .......... .......... .......... 94% 9.97M 1s
250450K .......... .......... .......... .......... .......... 94% 8.35M 1s
250500K .......... .......... .......... .......... .......... 94% 11.6M 1s
250550K .......... .......... .......... .......... .......... 94% 11.2M 1s
250600K .......... .......... .......... .......... .......... 94% 28.0M 1s
250650K .......... .......... .......... .......... .......... 94% 10.7M 1s
250700K .......... .......... .......... .......... .......... 94% 26.6M 1s
250750K .......... .......... .......... .......... .......... 94% 13.8M 1s
250800K .......... .......... .......... .......... .......... 94% 13.4M 1s
250850K .......... .......... .......... .......... .......... 94% 10.7M 1s
250900K .......... .......... .......... .......... .......... 94% 12.2M 1s
250950K .......... .......... .......... .......... .......... 94% 11.6M 1s
251000K .......... .......... .......... .......... .......... 94% 11.6M 1s
251050K .......... .......... .......... .......... .......... 94% 13.2M 1s
251100K .......... .......... .......... .......... .......... 94% 10.8M 1s
251150K .......... .......... .......... .......... .......... 94% 12.8M 1s
251200K .......... .......... .......... .......... .......... 94% 9.47M 1s
251250K .......... .......... .......... .......... .......... 94% 13.0M 1s
251300K .......... .......... .......... .......... .......... 94% 12.9M 1s
251350K .......... .......... .......... .......... .......... 94% 11.2M 1s
251400K .......... .......... .......... .......... .......... 94% 15.2M 1s
251450K .......... .......... .......... .......... .......... 94% 13.6M 1s
251500K .......... .......... .......... .......... .......... 94% 17.0M 1s
251550K .......... .......... .......... .......... .......... 94% 15.9M 1s
251600K .......... .......... .......... .......... .......... 94% 9.10M 1s
251650K .......... .......... .......... .......... .......... 94% 16.9M 1s
251700K .......... .......... .......... .......... .......... 94% 10.1M 1s
251750K .......... .......... .......... .......... .......... 94% 9.68M 1s
251800K .......... .......... .......... .......... .......... 94% 13.5M 1s
251850K .......... .......... .......... .......... .......... 94% 18.3M 1s
251900K .......... .......... .......... .......... .......... 94% 16.4M 1s
251950K .......... .......... .......... .......... .......... 94% 14.4M 1s
252000K .......... .......... .......... .......... .......... 94% 16.6M 1s
252050K .......... .......... .......... .......... .......... 94% 22.8M 1s
252100K .......... .......... .......... .......... .......... 94% 13.2M 1s
252150K .......... .......... .......... .......... .......... 94% 25.5M 1s
252200K .......... .......... .......... .......... .......... 94% 12.1M 1s
252250K .......... .......... .......... .......... .......... 94% 11.5M 1s
252300K .......... .......... .......... .......... .......... 94% 17.3M 1s
252350K .......... .......... .......... .......... .......... 94% 18.1M 1s
252400K .......... .......... .......... .......... .......... 94% 19.5M 1s
252450K .......... .......... .......... .......... .......... 95% 144M 1s
252500K .......... .......... .......... .......... .......... 95% 17.3M 1s
252550K .......... .......... .......... .......... .......... 95% 141M 1s
252600K .......... .......... .......... .......... .......... 95% 21.8M 1s
252650K .......... .......... .......... .......... .......... 95% 18.6M 1s
252700K .......... .......... .......... .......... .......... 95% 27.1M 1s
252750K .......... .......... .......... .......... .......... 95% 22.6M 1s
252800K .......... .......... .......... .......... .......... 95% 18.1M 1s
252850K .......... .......... .......... .......... .......... 95% 20.2M 1s
252900K .......... .......... .......... .......... .......... 95% 17.2M 1s
252950K .......... .......... .......... .......... .......... 95% 18.0M 1s
253000K .......... .......... .......... .......... .......... 95% 17.5M 1s
253050K .......... .......... .......... .......... .......... 95% 17.2M 1s
253100K .......... .......... .......... .......... .......... 95% 15.9M 1s
253150K .......... .......... .......... .......... .......... 95% 17.6M 1s
253200K .......... .......... .......... .......... .......... 95% 12.0M 1s
253250K .......... .......... .......... .......... .......... 95% 17.0M 1s
253300K .......... .......... .......... .......... .......... 95% 14.6M 1s
253350K .......... .......... .......... .......... .......... 95% 12.7M 1s
253400K .......... .......... .......... .......... .......... 95% 17.6M 1s
253450K .......... .......... .......... .......... .......... 95% 10.4M 1s
253500K .......... .......... .......... .......... .......... 95% 8.21M 1s
253550K .......... .......... .......... .......... .......... 95% 16.6M 1s
253600K .......... .......... .......... .......... .......... 95% 13.3M 1s
253650K .......... .......... .......... .......... .......... 95% 13.5M 1s
253700K .......... .......... .......... .......... .......... 95% 13.0M 1s
253750K .......... .......... .......... .......... .......... 95% 25.3M 1s
253800K .......... .......... .......... .......... .......... 95% 25.2M 1s
253850K .......... .......... .......... .......... .......... 95% 26.4M 1s
253900K .......... .......... .......... .......... .......... 95% 14.8M 1s
253950K .......... .......... .......... .......... .......... 95% 25.2M 1s
254000K .......... .......... .......... .......... .......... 95% 15.0M 1s
254050K .......... .......... .......... .......... .......... 95% 18.9M 1s
254100K .......... .......... .......... .......... .......... 95% 21.0M 1s
254150K .......... .......... .......... .......... .......... 95% 21.1M 1s
254200K .......... .......... .......... .......... .......... 95% 17.8M 1s
254250K .......... .......... .......... .......... .......... 95% 18.5M 1s
254300K .......... .......... .......... .......... .......... 95% 15.0M 1s
254350K .......... .......... .......... .......... .......... 95% 31.8M 1s
254400K .......... .......... .......... .......... .......... 95% 22.2M 1s
254450K .......... .......... .......... .......... .......... 95% 15.9M 1s
254500K .......... .......... .......... .......... .......... 95% 19.2M 1s
254550K .......... .......... .......... .......... .......... 95% 17.2M 1s
254600K .......... .......... .......... .......... .......... 95% 11.4M 1s
254650K .......... .......... .......... .......... .......... 95% 14.2M 1s
254700K .......... .......... .......... .......... .......... 95% 10.9M 1s
254750K .......... .......... .......... .......... .......... 95% 15.2M 1s
254800K .......... .......... .......... .......... .......... 95% 12.5M 1s
254850K .......... .......... .......... .......... .......... 95% 16.2M 1s
254900K .......... .......... .......... .......... .......... 95% 11.9M 1s
254950K .......... .......... .......... .......... .......... 95% 11.2M 1s
255000K .......... .......... .......... .......... .......... 95% 15.0M 1s
255050K .......... .......... .......... .......... .......... 95% 30.8M 1s
255100K .......... .......... .......... .......... .......... 96% 29.3M 1s
255150K .......... .......... .......... .......... .......... 96% 31.8M 1s
255200K .......... .......... .......... .......... .......... 96% 22.5M 1s
255250K .......... .......... .......... .......... .......... 96% 83.0M 1s
255300K .......... .......... .......... .......... .......... 96% 23.7M 1s
255350K .......... .......... .......... .......... .......... 96% 16.4M 1s
255400K .......... .......... .......... .......... .......... 96% 488M 1s
255450K .......... .......... .......... .......... .......... 96% 16.5M 1s
255500K .......... .......... .......... .......... .......... 96% 18.0M 1s
255550K .......... .......... .......... .......... .......... 96% 15.3M 1s
255600K .......... .......... .......... .......... .......... 96% 6.29M 1s
255650K .......... .......... .......... .......... .......... 96% 13.3M 1s
255700K .......... .......... .......... .......... .......... 96% 14.3M 1s
255750K .......... .......... .......... .......... .......... 96% 18.1M 1s
255800K .......... .......... .......... .......... .......... 96% 16.2M 1s
255850K .......... .......... .......... .......... .......... 96% 10.4M 1s
255900K .......... .......... .......... .......... .......... 96% 11.9M 1s
255950K .......... .......... .......... .......... .......... 96% 13.8M 1s
256000K .......... .......... .......... .......... .......... 96% 12.5M 1s
256050K .......... .......... .......... .......... .......... 96% 15.8M 1s
256100K .......... .......... .......... .......... .......... 96% 12.6M 1s
256150K .......... .......... .......... .......... .......... 96% 16.1M 1s
256200K .......... .......... .......... .......... .......... 96% 11.8M 1s
256250K .......... .......... .......... .......... .......... 96% 14.7M 1s
256300K .......... .......... .......... .......... .......... 96% 14.3M 1s
256350K .......... .......... .......... .......... .......... 96% 13.7M 1s
256400K .......... .......... .......... .......... .......... 96% 15.9M 1s
256450K .......... .......... .......... .......... .......... 96% 14.3M 1s
256500K .......... .......... .......... .......... .......... 96% 15.2M 1s
256550K .......... .......... .......... .......... .......... 96% 16.2M 1s
256600K .......... .......... .......... .......... .......... 96% 14.1M 1s
256650K .......... .......... .......... .......... .......... 96% 11.8M 1s
256700K .......... .......... .......... .......... .......... 96% 7.65M 1s
256750K .......... .......... .......... .......... .......... 96% 8.38M 1s
256800K .......... .......... .......... .......... .......... 96% 10.3M 1s
256850K .......... .......... .......... .......... .......... 96% 7.82M 1s
256900K .......... .......... .......... .......... .......... 96% 9.47M 1s
256950K .......... .......... .......... .......... .......... 96% 6.18M 1s
257000K .......... .......... .......... .......... .......... 96% 9.07M 1s
257050K .......... .......... .......... .......... .......... 96% 28.2M 1s
257100K .......... .......... .......... .......... .......... 96% 31.7M 1s
257150K .......... .......... .......... .......... .......... 96% 31.0M 1s
257200K .......... .......... .......... .......... .......... 96% 27.8M 1s
257250K .......... .......... .......... .......... .......... 96% 12.0M 1s
257300K .......... .......... .......... .......... .......... 96% 18.3M 1s
257350K .......... .......... .......... .......... .......... 96% 44.2M 1s
257400K .......... .......... .......... .......... .......... 96% 37.5M 1s
257450K .......... .......... .......... .......... .......... 96% 14.2M 1s
257500K .......... .......... .......... .......... .......... 96% 11.6M 1s
257550K .......... .......... .......... .......... .......... 96% 13.7M 1s
257600K .......... .......... .......... .......... .......... 96% 11.3M 1s
257650K .......... .......... .......... .......... .......... 96% 11.7M 1s
257700K .......... .......... .......... .......... .......... 96% 12.8M 1s
257750K .......... .......... .......... .......... .......... 97% 9.97M 1s
257800K .......... .......... .......... .......... .......... 97% 12.9M 1s
257850K .......... .......... .......... .......... .......... 97% 10.5M 1s
257900K .......... .......... .......... .......... .......... 97% 12.8M 1s
257950K .......... .......... .......... .......... .......... 97% 15.8M 1s
258000K .......... .......... .......... .......... .......... 97% 30.1M 1s
258050K .......... .......... .......... .......... .......... 97% 27.6M 1s
258100K .......... .......... .......... .......... .......... 97% 29.5M 1s
258150K .......... .......... .......... .......... .......... 97% 27.2M 1s
258200K .......... .......... .......... .......... .......... 97% 27.3M 1s
258250K .......... .......... .......... .......... .......... 97% 35.1M 1s
258300K .......... .......... .......... .......... .......... 97% 18.6M 1s
258350K .......... .......... .......... .......... .......... 97% 228M 0s
258400K .......... .......... .......... .......... .......... 97% 26.7M 0s
258450K .......... .......... .......... .......... .......... 97% 22.8M 0s
258500K .......... .......... .......... .......... .......... 97% 18.5M 0s
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2024-06-20 13:25:52 (14.5 MB/s) - ‘ESPbeta.tgz’ saved [272149040/272149040]
+ tar -xf ESPbeta.tgz
+ rm -rf EngSketchPad/data/Slugs
+ python --version
Python 3.11.9
+ [[ '' == *\.\i\f\o\r\t ]]
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/config/
+ ./makeEnv
ESP runtime AutoConfigurator
CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.7.0 with contents:
bin
include
lib
share
Info: Python exec /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python found!
Info: Python header /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11/Python.h found!
Info: Python library /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/libpython3.11.dylib found!
ESP_ARCH = DARWIN_ARM64
ESP_ROOT = /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad
EFCOMP = gfortran
CARCH = DARWIN_ARM64
CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.7.0
CASARCH = .
CASREV = 7.7
PYTHONINC= /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
PYTHONLIB= -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
+ source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN_ARM64
++ ESP_ARCH=DARWIN_ARM64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad
++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.7
++ CASREV=7.7
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ PYTHONINC=/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=MacOSX-arm64
++ AFLR_ARCH=MacOSX-arm64
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=
++ CAPS_GLYPH=
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/ESP/ESP.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/ESP/ESP.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/wvClient/wv.html'
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src
+ make
(cd EGADS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64
cp -p ../include/DARWIN_ARM64 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads_dot.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads_dot.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.inc
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.inc
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/emp.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/emp.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/prm.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/prm.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.inc
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.inc
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsss.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsss.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTris.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTris.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/always_inline.h
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsGeom.cpp -o ./egadsGeom.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsHLevel.cpp -o ./egadsHLevel.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsTopo.cpp -o ./egadsTopo.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsCopy.cpp -o ./egadsCopy.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsSpline.cpp -o ./egadsSpline.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsIO.cpp -o ./egadsIO.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsSkinning.cpp -o ./egadsSkinning.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsTessSens.cpp -o ./egadsTessSens.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsBase.c -o ./egadsBase.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTess.c -o ./egadsTess.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTris.c -o ./egadsTris.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsFit.c -o ./egadsFit.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmCfit.c -o ./prmCfit.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmGrid.c -o ./prmGrid.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmUV.c -o ./prmUV.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsExport.c -o ./egadsExport.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include ../util/emp.c \
-o ./emp.o
clang++ -g -target arm64-apple-darwin -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \
../util/evaluate.c -o ./evaluate.o
clang++ -g -target arm64-apple-darwin -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \
../util/rational.c -o ./rational.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../util \
../util/regQuads.c -o ./regQuads.o
clang++ -g -target arm64-apple-darwin -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1
SurrealD1_test_suite Complete!
clang++ -g -target arm64-apple-darwin -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
./SurrealD4
SurrealD4_test_suite Complete!
clang++ -g -target arm64-apple-darwin -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
./SurrealS1
SurrealS1_test_suite Complete!
clang++ -g -target arm64-apple-darwin -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
./SurrealS4
SurrealS4_test_suite Complete!
/Library/Developer/CommandLineTools/usr/bin/make -C ../util
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 uvmap/main/uvmap.c -Iuvmap \
-o ./uvmap.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 egadsUVmap.c -Iuvmap \
-o ./egadsUVmap.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a
clang -g -target arm64-apple-darwin -o ./uvmap.exe ./uvmap.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -luvmap -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib
(cd .; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o \
egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -lc++ \
-install_name '@rpath/libegads.dylib' \
-compatibility_version 7.7 \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a
cp /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a
(cd .; \
ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \
evaluate.o rational.o regQuads.o; )
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsBase.c -o ./fgadsBase.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsMemory.c -o ./fgadsMemory.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsAttrs.c -o ./fgadsAttrs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTess.c -o ./fgadsTess.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsHLevel.c -o ./fgadsHLevel.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsGeom.c -o ./fgadsGeom.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libfgads.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libfgads.a
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libemp.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libemp.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libemp.a emp.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libemp.a
*** EGADS Build Complete! ***
(cd EGADS/lite; make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteBase.c -o ./liteBase.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteMemory.c -o ./liteMemory.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteGeom.c -o ./liteGeom.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteTopo.c -o ./liteTopo.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteAttrs.c -o ./liteAttrs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteImport.c -o ./liteImport.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteString.c -o ./liteString.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsTess.c -o ./liteTess.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsTris.c -o ./liteTris.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src \
../src/egadsQuads.c -o ./liteQuads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
-I../util ../src/egadsTessInp.c -o ./liteTessInp.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 ../src/egadsRobust.c \
-o ./egadsRobust.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DDARWIN_ARM64 -I../include ../util/emp.c \
-o ./emp.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../util/evaluate.c -o ./evaLite.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE ../util/rational.c \
-o ./ratLite.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I../util \
../util/regQuads.c -o ./liteRegQuads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsEffect.c -o ./liteEffect.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib
(cd .; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib \
liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \
egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \
liteEffect.o liteUVmap.o \
-install_name '@rpath/libegadslite.dylib' \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
liteUVmap.o ; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a
(cd wvServer; make)
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict map.cpp -o ./map.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include base64-decode.c -o ./base64-decode.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include handshake.c -o ./handshake.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include client-handshake.c -o ./client-handshake.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include md5.c -o ./md5.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include parsers.c -o ./parsers.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include extension.c -o ./extension.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include sha-1.c -o ./sha-1.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include server.c -o ./server.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include wv.c -o ./wv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include browserMessage.c -o ./browserMessage.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include fwv.c -o ./fwv.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
./fwv.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -o ./servertest.o
clang++ -g -target arm64-apple-darwin -o ./server ./servertest.o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a \
-lpthread -lz -lm
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib
(cd .; clang++ -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib \
base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \
-install_name '@rpath/libwsserver.dylib' \
-compatibility_version 7.7 \
-current_version 1.0.25 )
(cd EGADS/examples; make -f egads2cart.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include egads2cart.c \
-o ./egads2cart.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
(cd EGADS/examples; make -f vCurvature.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/vCurvature ./vCurvature.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd EGADS/examples; make -f vGeom.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include vGeom.c -o ./vGeom.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/vGeom ./vGeom.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd EGADS/examples; make -f vTess.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include vTess.c -o ./vTess.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include ../util/retessFaces.c \
-o ./retessFaces.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet \
-lpthread -lz -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd OpenCSM; make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udp.c -o ./udp.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib
clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib ./OpenCSM.o ./udp.o ./tim.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/serveESP ./serveESP.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bezier.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bezier.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/biconvex.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/biconvex.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/box.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/box.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/box.so ./udpBox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bspline.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bspline.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/catmull.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/catmull.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/compare.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/compare.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/compare.so ./udfCompare.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createBEM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createBEM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createPoly.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createPoly.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/csm.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/csm.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/csm.so ./udpCsm.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/deform.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/deform.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/deform.so ./udfDeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/droop.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/droop.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/droop.so ./udfDroop.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/editAttr.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/editAttr.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ellipse.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ellipse.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flend.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flend.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flend.so ./udfFlend.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/freeform.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/freeform.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ganged.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ganged.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/guide.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/guide.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/guide.so ./udfGuide.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hex.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hex.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hex.so ./udpHex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/import.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/import.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/import.so ./udpImport.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/kulfan.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/kulfan.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/linalg.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/linalg.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mechanism.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mechanism.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca.so ./udpNaca.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nacelle.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nacelle.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nuscale.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nuscale.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/offset.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/offset.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/offset.so ./udfOffset.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parsec.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parsec.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pod.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pod.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pod.so ./udpPod.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/poly.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/poly.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/poly.so ./udpPoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBbox.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBbox.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBrep.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBrep.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printEgo.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printEgo.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/prop.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/prop.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/prop.so ./udpProp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/radwaf.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/radwaf.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sample.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sample.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sample.so ./udpSample.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sew.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sew.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sew.so ./udpSew.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/shadow.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/shadow.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slices.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slices.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slices.so ./udfSlices.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stag.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stag.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stag.so ./udpStag.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stiffener.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stiffener.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/supell.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/supell.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/supell.so ./udpSupell.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester1.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester1.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester2.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester2.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vsp3.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vsp3.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/waffle.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/waffle.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfWarp.c -o ./udfWarp.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/warp.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/warp.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/warp.so ./udfWarp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/PDT2.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/PDT2.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca456.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca456.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm -static-libgfortran -static-libgcc -Wl,-w
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ereped.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ereped.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ereped.so ./timEreped.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mitten.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mitten.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mitten.so ./timMitten.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plotter.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plotter.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plugs.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slugs.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/common.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/common.h
cp -p common.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/common.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udp.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udp.h
cp -p udp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udp.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/esp.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/esp.h
cp -p esp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/esp.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/tim.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/tim.h
cp -p tim.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/tim.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egg.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egg.h
cp -p egg.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egg.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c
(cd Slugs; make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. Fitter.c \
-o ./Fitter.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. RedBlackTree.c \
-o ./RedBlackTree.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. Tessellate.c \
-o ./Tessellate.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
./Tessellate.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads \
-lpthread -lz -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads \
-lpthread -lz -lm
(cd CAPS; make)
/bin/cp Cart3D/M1_CLANG/libc3dio.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/M1_CLANG/libCart3D.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/DARWIN_ARM64/avl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/avl
/bin/cp Executables/DARWIN_ARM64/pplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/pplot
/bin/cp Executables/DARWIN_ARM64/pxplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/pxplot
/bin/cp Executables/DARWIN_ARM64/xfoil /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/xfoil
/bin/cp Executables/DARWIN_ARM64/mastros.exe /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/DARWIN_ARM64/ASTRO.D01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/DARWIN_ARM64/ASTRO.IDX /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/DARWIN_ARM64/mses /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/mses
/bin/cp Executables/DARWIN_ARM64/mset /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/mset
/bin/cp udunits/include/*.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include
/bin/cp udunits/DARWIN_ARM64/libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib
/bin/ln -sf libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libudunits2.dylib
/bin/cp Libraries/DARWIN_ARM64/aflr2AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/DARWIN_ARM64/aflr3AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/DARWIN_ARM64/aflr4AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/aflr4AIM.so
(cd CAPS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/caps.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/caps.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimUtil.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimUtil.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimMesh.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimMesh.h
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../include \
-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include \
-I/usr/include/udunits2 aimTransferUtil.c \
-o ./aimTransferUtil.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../include \
aimMesh.c -o ./aimMesh.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a
ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
./aimTransferUtil.o
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \
-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib
(cd .; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
-install_name '@rpath/libcaps.dylib' \
-compatibility_version 1.0.25 \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include testingAIM.c \
-o ./testingAIM.o
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so
rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include testingWriter.c \
-o ./testingWriter.o
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so
rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include phaseUtil.c \
-o ./phaseUtil.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
(cd ../CAPSexamples; make)
(make -C cCAPS -f aeroelastic_SU2.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -g -target arm64-apple-darwin -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f avlTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include avlTest.c -o ./avlTest.o
clang -g -target arm64-apple-darwin -o ./avlTest ./avlTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f awaveTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
clang -g -target arm64-apple-darwin -o ./awaveTest ./awaveTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f frictionTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
clang -g -target arm64-apple-darwin -o ./frictionTest ./frictionTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f fun3d.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
clang -g -target arm64-apple-darwin -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
clang -g -target arm64-apple-darwin -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
clang -g -target arm64-apple-darwin -o ./aeroelasticTest ./aeroelasticTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f hsm.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include hsmTest.c -o ./hsmTest.o
clang -g -target arm64-apple-darwin -o ./hsmTest ./hsmTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o
clang -g -target arm64-apple-darwin -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o
clang -g -target arm64-apple-darwin -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o
clang -g -target arm64-apple-darwin -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f interferenceTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include interferenceTest.c \
-o ./interferenceTest.o
clang -g -target arm64-apple-darwin -o ./interferenceTest ./interferenceTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f msesTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include msesTest.c -o ./msesTest.o
clang -g -target arm64-apple-darwin -o ./msesTest ./msesTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f mystran.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include mystranTest.c -o ./mystranTest.o
clang -g -target arm64-apple-darwin -o ./mystranTest ./mystranTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f pointwiseTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
clang -g -target arm64-apple-darwin -o ./pointwiseTest ./pointwiseTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(cd CAPS/aim; make)
/Library/Developer/CommandLineTools/usr/bin/make -C utils
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libutils.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranCards.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libutils.a
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils
cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/cardUtils.h
cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmUtils.h
/Library/Developer/CommandLineTools/usr/bin/make -C abaqus
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \
abaqusAIM.c -o ./abaqusAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \
abaqusUtils.c -o ./abaqusUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \
-I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -ldl -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
/Library/Developer/CommandLineTools/usr/bin/make -C aflr2
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C aflr3
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C aflr4
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C astros
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils astrosAIM.c \
-o ./astrosAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils astrosUtils.c \
-o ./astrosUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils astrosCards.c \
-o ./astrosCards.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C avl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_CPOML.o ./avlRead_DERMATB.o ./avlRead_DERMATM.o ./avlRead_DERMATS.o ./avlRead_ELE.o ./avlRead_HINGE.o ./avlRead_STRP.o ./avlRead_SURF.o ./avlRead_TOT.o ./avlRead_VM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C awave
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils awaveAIM.c \
-o ./awaveAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cart3d
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/libCart3D -I./xddm \
cart3dAIM.c -o ./cart3dAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/c3dio \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/libCart3D -I./xddm \
writeTrix.c -o ./writeTrix.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/c3dio \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/libCart3D \
surfTrix.c -o ./surfTrix.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -pedantic -I./xddm -I. \
`xml2-config --cflags` ./xddm/xddm.c \
-o ./xddm.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include bodyTess.c -o ./bodyTess.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \
./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/ \
-lc3dio -lCart3D -ldl -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include cart3dTest.c \
-o ./cart3dTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/cart3dTest ./cart3dTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I./xddm \
-I. `xml2-config --cflags` ESPxddm.c -o ./ESPxddm.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \
./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/ -lc3dio -lCart3D \
-lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cbaero
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
clang -g -target arm64-apple-darwin -bundle cbaeroAIM.o -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C cgt
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include egads2cgt.c \
-o ./egads2cgt.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include aflr4egads.c \
-o ./aflr4egads.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C custom
make[2]: Nothing to be done for `default'.
/Library/Developer/CommandLineTools/usr/bin/make -C delaundo
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils delaundoAIM.c \
-o ./delaundoAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C egadsTess
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils egadsTessAIM.c \
-o ./egadsTessAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C friction
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -Wno-format -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils frictionAIM.c \
-o ./frictionAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/friction ./friction.o -static-libgfortran -static-libgcc -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C fun3d
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
-I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
fun3dUtils.c -o ./fun3dUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \
-I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o
Building FUN3D with Python
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
./fun3dNamelist.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
/Library/Developer/CommandLineTools/usr/bin/make -C hsm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils hsmAIM.c \
-o src/hsmAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils hsmUtils.c \
-o src/hsmUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils hsmAdj.c \
-o src/hsmAdj.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -Wno-comment rcm/rcm.cpp -DREVISION=7.7 \
-o src/rcm.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict rcm/genrcmi.cpp -DREVISION=7.7 \
-o src/genrcmi.o
/Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o
/Library/Developer/CommandLineTools/usr/bin/make -C src cross.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o
/Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o
/Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o
/Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libhsm.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so \
src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
src/rcm.o src/genrcmi.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C interference
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include interferenceAIM.c \
-o ./interferenceAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. cloudFns.c \
-o ./cloudFns.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so \
./interferenceAIM.o ./cloudFns.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C masstran
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils masstranAIM.cpp \
-o ./masstranAIM.o
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C meshWriter
/Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include bstlWriter.c \
-o ./bstlWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include bvtkWriter.c \
-o ./bvtkWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include exodusWriter.cpp \
-o ./exodusWriter.o
clang++ -g -target arm64-apple-darwin -bundle -std=c++11 -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/exodusWriter.so ./exodusWriter.o \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C fastWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include fastWriter.c \
-o ./fastWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include libmeshbWriter.c \
-o ./libmeshbWriter.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C stlWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include stlWriter.c \
-o ./stlWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C su2Writer
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include su2Writer.c \
-o ./su2Writer.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include tecplotWriter.c \
-o ./tecplotWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include ugridWriter.c \
-o ./ugridWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include vtkWriter.c \
-o ./vtkWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mses
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mystran
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils mystranAIM.c \
-o ./mystranAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils mystranUtils.c \
-o ./mystranUtils.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C nastran
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils nastranAIM.c \
-o ./nastranAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C plato
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include platoAIM.c \
-o ./platoAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/platoAIM.so ./platoAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C pointwise
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils pointwiseAIM.c \
-o ./pointwiseAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils hashElement.c \
-o ./hashElement.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -lpthread
/Library/Developer/CommandLineTools/usr/bin/make -C refine
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
-o ./refineAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 \
-I../meshWriter/libmeshbWriter/libMeshb/sources \
../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSD
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSDAIM.c \
-o ./sierraSDAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sierraSDAIM.so ./sierraSDAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSM
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSMAIM.c \
-o ./sierraSMAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sierraSMAIM.so ./sierraSMAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C skeleton
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils skeletonAIM.c \
-o ./skeletonAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C spinnaker
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include \
-I../meshWriter/exodusWriter \
-I../meshWriter/libmeshbWriter \
-I../utils -I/Users/jenkins/util/sandialabs/seacas/include \
-I/opt/homebrew/include \
spinnakerAIM.c \
-o ./spinnakerAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 \
-I../meshWriter/libmeshbWriter/libMeshb/sources \
../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/spinnakerAIM.so ./spinnakerAIM.o ./libmeshb7.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C su2
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
-o ./su2AIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils su2Utils.c \
-o ./su2Utils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils su2_4_Cardinal.c \
-o ./su2_4_Cardinal.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils su2_5_Raven.c \
-o ./su2_5_Raven.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils su2_6_Falcon.c \
-o ./su2_6_Falcon.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils su2_7_Blackbird.c \
-o ./su2_7_Blackbird.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils su2_801_Harrier.c \
-o ./su2_801_Harrier.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tacs
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils tacsAIM.c \
-o ./tacsAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C tetgen
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils tetgenAIM.cpp \
-o ./tetgenAIM.o
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
./tetgen_Interface.o ./tetgen.o \
./predicates.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tsfoil
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \
tsfoilAIM.c -o ./tsfoilAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C unitTest
make[2]: Nothing to be done for `all'.
/Library/Developer/CommandLineTools/usr/bin/make -C xfoil
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \
xfoilAIM.c -o ./xfoilAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C zaero
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
(cd OpenCSM; make -f serveESP.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/capsMode.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flowchart.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/viewer.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/viewer.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/viewer.so ./timViewer.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pyscript.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pyscript.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
*** Build Completed! ***
+ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin
++ uname -a
+ [[ Darwin VIGGEN.MIT.EDU 23.3.0 Darwin Kernel Version 23.3.0: Wed Dec 20 21:30:27 PST 2023; root:xnu-10002.81.5~7/RELEASE_ARM64_T8103 arm64 == *\D\a\r\w\i\n* ]]
+ sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
==> serveESP completed successfully with no verification data
real 0m0.618s
user 0m0.064s
sys 0m0.018s
+ set +x
=============================================
ESP verification case 01 passed (as expected)
=============================================
+ expectSuccess 02 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.213s
user 0m0.208s
sys 0m0.037s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.7.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m1.546s
user 0m2.063s
sys 0m0.517s
+ set +x
=============================================
ESP verification case 03 passed (as expected)
=============================================
+ expectSuccess 04 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.288s
user 0m0.304s
sys 0m0.026s
+ set +x
=============================================
ESP verification case 04 passed (as expected)
=============================================
+ expectSuccess 05 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.333s
user 0m0.454s
sys 0m0.062s
+ set +x
=============================================
ESP verification case 05 passed (as expected)
=============================================
+ expectSuccess 06 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.7.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.315s
user 0m0.441s
sys 0m0.024s
+ set +x
=============================================
ESP verification case 06 passed (as expected)
=============================================
+ expectSuccess 07 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.7.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m2.530s
user 0m3.535s
sys 0m0.415s
+ set +x
=============================================
ESP verification case 07 passed (as expected)
=============================================
+ expectSuccess 08 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/CAPS/verify_7.7.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data
real 0m16.832s
user 0m27.272s
sys 0m1.406s
+ set +x
=============================================
ESP verification case 08 passed (as expected)
=============================================
+ expectSuccess 09 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/verify_7.7.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.301s
user 0m0.372s
sys 0m0.017s
+ set +x
=============================================
ESP verification case 09 passed (as expected)
=============================================
+ expectSuccess 10 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data
real 0m24.196s
user 0m47.174s
sys 0m14.566s
+ set +x
=============================================
ESP verification case 10 passed (as expected)
=============================================
+ expectSuccess 11 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: could not find mapping for iedge=10
WARNING:: could not find mapping for iedge=14
WARNING:: could not find mapping for iedge=7
WARNING:: could not find mapping for iedge=11
==> serveESP completed successfully with 5 warnings and no verification data
real 0m0.227s
user 0m0.166s
sys 0m0.019s
+ set +x
=============================================
ESP verification case 11 passed (as expected)
=============================================
+ expectSuccess 12 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.499s
user 0m0.582s
sys 0m0.012s
+ set +x
=============================================
ESP verification case 12 passed (as expected)
=============================================
+ expectSuccess 13 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.102s
user 0m0.113s
sys 0m0.008s
+ set +x
=============================================
ESP verification case 13 passed (as expected)
=============================================
+ expectSuccess 14 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data
real 0m0.364s
user 0m0.333s
sys 0m0.017s
+ set +x
=============================================
ESP verification case 14 passed (as expected)
=============================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 1.240s
OK
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m3.775s
user 0m5.709s
sys 0m0.139s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 10.020s
OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.014 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4285 6326
AFLR2 GG : Nodes, Faces = 6135 10026
AFLR2 GG : Nodes, Faces = 7878 13512
AFLR2 GG : Nodes, Faces = 9485 16726
AFLR2 GG : Nodes, Faces = 10981 19718
AFLR2 GG : Nodes, Faces = 12372 22500
AFLR2 GG : Nodes, Faces = 13686 25128
AFLR2 GG : Nodes, Faces = 14908 27572
AFLR2 GG : Nodes, Faces = 16063 29882
AFLR2 GG : Nodes, Faces = 17170 32096
AFLR2 GG : Nodes, Faces = 18222 34200
AFLR2 GG : Nodes, Faces = 19208 36172
AFLR2 GG : Nodes, Faces = 20165 38086
AFLR2 GG : Nodes, Faces = 21087 39930
AFLR2 GG : Nodes, Faces = 21975 41706
AFLR2 GG : Nodes, Faces = 22803 43362
AFLR2 GG : Nodes, Faces = 23582 44920
AFLR2 GG : Nodes, Faces = 24330 46416
AFLR2 GG : Nodes, Faces = 25041 47838
AFLR2 GG : Nodes, Faces = 25723 49202
AFLR2 GG : Nodes, Faces = 26365 50486
AFLR2 GG : Nodes, Faces = 26993 51742
AFLR2 GG : Nodes, Faces = 27556 52868
AFLR2 GG : Nodes, Faces = 28054 53864
AFLR2 GG : Nodes, Faces = 28487 54730
AFLR2 GG : Nodes, Faces = 28847 55450
AFLR2 GG : Nodes, Faces = 29118 55992
AFLR2 GG : Nodes, Faces = 29355 56466
AFLR2 GG : Nodes, Faces = 29553 56862
AFLR2 GG : Nodes, Faces = 29735 57226
AFLR2 GG : Nodes, Faces = 29878 57512
AFLR2 GG : Nodes, Faces = 29969 57694
AFLR2 GG : Nodes, Faces = 30009 57774
AFLR2 GG : Nodes, Faces = 30018 57792
AFLR2 GG : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.039 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.003 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
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 = 0.014 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2224 2224
AFLR2 GG : Nodes, Faces = 4120 6016
AFLR2 GG : Nodes, Faces = 5820 9416
AFLR2 GG : Nodes, Faces = 7322 12420
AFLR2 GG : Nodes, Faces = 8613 15002
AFLR2 GG : Nodes, Faces = 9793 17362
AFLR2 GG : Nodes, Faces = 10847 19470
AFLR2 GG : Nodes, Faces = 11828 21432
AFLR2 GG : Nodes, Faces = 12749 23274
AFLR2 GG : Nodes, Faces = 13580 24936
AFLR2 GG : Nodes, Faces = 14355 26486
AFLR2 GG : Nodes, Faces = 15088 27952
AFLR2 GG : Nodes, Faces = 15774 29324
AFLR2 GG : Nodes, Faces = 16420 30616
AFLR2 GG : Nodes, Faces = 17013 31802
AFLR2 GG : Nodes, Faces = 17571 32918
AFLR2 GG : Nodes, Faces = 18089 33954
AFLR2 GG : Nodes, Faces = 18573 34922
AFLR2 GG : Nodes, Faces = 19005 35786
AFLR2 GG : Nodes, Faces = 19413 36602
AFLR2 GG : Nodes, Faces = 19779 37334
AFLR2 GG : Nodes, Faces = 20116 38008
AFLR2 GG : Nodes, Faces = 20443 38662
AFLR2 GG : Nodes, Faces = 20756 39288
AFLR2 GG : Nodes, Faces = 21054 39884
AFLR2 GG : Nodes, Faces = 21344 40464
AFLR2 GG : Nodes, Faces = 21621 41018
AFLR2 GG : Nodes, Faces = 21885 41546
AFLR2 GG : Nodes, Faces = 22137 42050
AFLR2 GG : Nodes, Faces = 22387 42550
AFLR2 GG : Nodes, Faces = 22603 42982
AFLR2 GG : Nodes, Faces = 22772 43320
AFLR2 GG : Nodes, Faces = 22912 43600
AFLR2 GG : Nodes, Faces = 23039 43854
AFLR2 GG : Nodes, Faces = 23142 44060
AFLR2 GG : Nodes, Faces = 23205 44186
AFLR2 GG : Nodes, Faces = 23240 44256
AFLR2 GG : Nodes, Faces = 23257 44290
AFLR2 GG : Nodes, Faces = 23269 44314
AFLR2 GG : Nodes, Faces = 23273 44322
AFLR2 : CPU Time = 0.038 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23273 44322
AFLR2 : CPU Time = 0.003 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23273
Number of elements = 46546
Number of tris = 44322
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.014 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4285 6326
AFLR2 GG : Nodes, Faces = 6135 10026
AFLR2 GG : Nodes, Faces = 7878 13512
AFLR2 GG : Nodes, Faces = 9485 16726
AFLR2 GG : Nodes, Faces = 10981 19718
AFLR2 GG : Nodes, Faces = 12372 22500
AFLR2 GG : Nodes, Faces = 13686 25128
AFLR2 GG : Nodes, Faces = 14908 27572
AFLR2 GG : Nodes, Faces = 16063 29882
AFLR2 GG : Nodes, Faces = 17170 32096
AFLR2 GG : Nodes, Faces = 18222 34200
AFLR2 GG : Nodes, Faces = 19208 36172
AFLR2 GG : Nodes, Faces = 20165 38086
AFLR2 GG : Nodes, Faces = 21087 39930
AFLR2 GG : Nodes, Faces = 21975 41706
AFLR2 GG : Nodes, Faces = 22803 43362
AFLR2 GG : Nodes, Faces = 23582 44920
AFLR2 GG : Nodes, Faces = 24330 46416
AFLR2 GG : Nodes, Faces = 25041 47838
AFLR2 GG : Nodes, Faces = 25723 49202
AFLR2 GG : Nodes, Faces = 26365 50486
AFLR2 GG : Nodes, Faces = 26993 51742
AFLR2 GG : Nodes, Faces = 27556 52868
AFLR2 GG : Nodes, Faces = 28054 53864
AFLR2 GG : Nodes, Faces = 28487 54730
AFLR2 GG : Nodes, Faces = 28847 55450
AFLR2 GG : Nodes, Faces = 29118 55992
AFLR2 GG : Nodes, Faces = 29355 56466
AFLR2 GG : Nodes, Faces = 29553 56862
AFLR2 GG : Nodes, Faces = 29735 57226
AFLR2 GG : Nodes, Faces = 29878 57512
AFLR2 GG : Nodes, Faces = 29969 57694
AFLR2 GG : Nodes, Faces = 30009 57774
AFLR2 GG : Nodes, Faces = 30018 57792
AFLR2 GG : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.039 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.003 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.015 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2224 2224
AFLR2 GG : Nodes, Faces = 4120 6016
AFLR2 GG : Nodes, Faces = 5820 9416
AFLR2 GG : Nodes, Faces = 7322 12420
AFLR2 GG : Nodes, Faces = 8613 15002
AFLR2 GG : Nodes, Faces = 9793 17362
AFLR2 GG : Nodes, Faces = 10847 19470
AFLR2 GG : Nodes, Faces = 11828 21432
AFLR2 GG : Nodes, Faces = 12749 23274
AFLR2 GG : Nodes, Faces = 13580 24936
AFLR2 GG : Nodes, Faces = 14355 26486
AFLR2 GG : Nodes, Faces = 15088 27952
AFLR2 GG : Nodes, Faces = 15774 29324
AFLR2 GG : Nodes, Faces = 16420 30616
AFLR2 GG : Nodes, Faces = 17013 31802
AFLR2 GG : Nodes, Faces = 17571 32918
AFLR2 GG : Nodes, Faces = 18089 33954
AFLR2 GG : Nodes, Faces = 18573 34922
AFLR2 GG : Nodes, Faces = 19005 35786
AFLR2 GG : Nodes, Faces = 19413 36602
AFLR2 GG : Nodes, Faces = 19779 37334
AFLR2 GG : Nodes, Faces = 20116 38008
AFLR2 GG : Nodes, Faces = 20443 38662
AFLR2 GG : Nodes, Faces = 20756 39288
AFLR2 GG : Nodes, Faces = 21054 39884
AFLR2 GG : Nodes, Faces = 21344 40464
AFLR2 GG : Nodes, Faces = 21621 41018
AFLR2 GG : Nodes, Faces = 21885 41546
AFLR2 GG : Nodes, Faces = 22137 42050
AFLR2 GG : Nodes, Faces = 22387 42550
AFLR2 GG : Nodes, Faces = 22603 42982
AFLR2 GG : Nodes, Faces = 22772 43320
AFLR2 GG : Nodes, Faces = 22912 43600
AFLR2 GG : Nodes, Faces = 23039 43854
AFLR2 GG : Nodes, Faces = 23142 44060
AFLR2 GG : Nodes, Faces = 23205 44186
AFLR2 GG : Nodes, Faces = 23240 44256
AFLR2 GG : Nodes, Faces = 23257 44290
AFLR2 GG : Nodes, Faces = 23269 44314
AFLR2 GG : Nodes, Faces = 23273 44322
AFLR2 : CPU Time = 0.038 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23273 44322
AFLR2 : CPU Time = 0.003 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23273
Number of elements = 46546
Number of tris = 44322
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.014 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4285 6326
AFLR2 GG : Nodes, Faces = 6135 10026
AFLR2 GG : Nodes, Faces = 7878 13512
AFLR2 GG : Nodes, Faces = 9485 16726
AFLR2 GG : Nodes, Faces = 10981 19718
AFLR2 GG : Nodes, Faces = 12372 22500
AFLR2 GG : Nodes, Faces = 13686 25128
AFLR2 GG : Nodes, Faces = 14908 27572
AFLR2 GG : Nodes, Faces = 16063 29882
AFLR2 GG : Nodes, Faces = 17170 32096
AFLR2 GG : Nodes, Faces = 18222 34200
AFLR2 GG : Nodes, Faces = 19208 36172
AFLR2 GG : Nodes, Faces = 20165 38086
AFLR2 GG : Nodes, Faces = 21087 39930
AFLR2 GG : Nodes, Faces = 21975 41706
AFLR2 GG : Nodes, Faces = 22803 43362
AFLR2 GG : Nodes, Faces = 23582 44920
AFLR2 GG : Nodes, Faces = 24330 46416
AFLR2 GG : Nodes, Faces = 25041 47838
AFLR2 GG : Nodes, Faces = 25723 49202
AFLR2 GG : Nodes, Faces = 26365 50486
AFLR2 GG : Nodes, Faces = 26993 51742
AFLR2 GG : Nodes, Faces = 27556 52868
AFLR2 GG : Nodes, Faces = 28054 53864
AFLR2 GG : Nodes, Faces = 28487 54730
AFLR2 GG : Nodes, Faces = 28847 55450
AFLR2 GG : Nodes, Faces = 29118 55992
AFLR2 GG : Nodes, Faces = 29355 56466
AFLR2 GG : Nodes, Faces = 29553 56862
AFLR2 GG : Nodes, Faces = 29735 57226
AFLR2 GG : Nodes, Faces = 29878 57512
AFLR2 GG : Nodes, Faces = 29969 57694
AFLR2 GG : Nodes, Faces = 30009 57774
AFLR2 GG : Nodes, Faces = 30018 57792
AFLR2 GG : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.039 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.003 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 160 272
AFLR2 GG : Nodes, Faces = 172 296
AFLR2 GG : Nodes, Faces = 182 316
AFLR2 GG : Nodes, Faces = 188 328
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 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 = 0.004 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.001 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Writing exodus file ....
Exodus expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Block: 'Block1_tri', blk_id 1, num_entries 9066
Sideset: 'Airfoil', set_id 1, num_entries 198
Sideset: 'InFlow', set_id 2, num_entries 24
Sideset: 'OutFlow', set_id 3, num_entries 24
Sideset: 'TunnelWall', set_id 4, num_entries 98
Finished writing Exodus file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.006 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 = 0.003 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 exodus file ....
Exodus expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Block: 'Block1_tri', blk_id 1, num_entries 386
Block: 'Block2_quad', blk_id 2, num_entries 3690
Sideset: 'Airfoil', set_id 1, num_entries 198
Sideset: 'InFlow', set_id 2, num_entries 24
Sideset: 'OutFlow', set_id 3, num_entries 24
Sideset: 'TunnelWall', set_id 4, num_entries 98
Finished writing Exodus 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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.006 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 = 0.003 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:62194)
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1198
Number of elements = 6307
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4975
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 6226
Number of elements = 34532
Number of triangles = 4438
Number of quadrilatarals = 0
Number of tetrahedrals = 30094
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 13688
Number of elements = 76798
Number of triangles = 8142
Number of quadrilatarals = 0
Number of tetrahedrals = 68656
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 41861
Number of elements = 237846
Number of triangles = 19888
Number of quadrilatarals = 0
Number of tetrahedrals = 217958
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 4371
Number of elements = 24249
Number of triangles = 3010
Number of quadrilatarals = 0
Number of tetrahedrals = 21239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 11025
Number of elements = 60915
Number of triangles = 8632
Number of quadrilatarals = 0
Number of tetrahedrals = 52283
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 10795
Number of elements = 60547
Number of triangles = 6366
Number of quadrilatarals = 0
Number of tetrahedrals = 54181
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 89164
Number of elements = 501194
Number of triangles = 51808
Number of quadrilatarals = 0
Number of tetrahedrals = 449386
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:62194)
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16607
Number of elements = 94482
Number of triangles = 7926
Number of quadrilatarals = 0
Number of tetrahedrals = 86556
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2585
Number of elements = 13784
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3615
Number of elements = 19589
Number of triangles = 3392
Number of quadrilatarals = 0
Number of tetrahedrals = 16197
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5438
Number of elements = 30214
Number of triangles = 3654
Number of quadrilatarals = 0
Number of tetrahedrals = 26560
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4697
Number of elements = 26013
Number of triangles = 3324
Number of quadrilatarals = 0
Number of tetrahedrals = 22689
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5467
Number of elements = 30346
Number of triangles = 3754
Number of quadrilatarals = 0
Number of tetrahedrals = 26592
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2273
Number of elements = 12220
Number of triangles = 2222
Number of quadrilatarals = 0
Number of tetrahedrals = 9998
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2405
Number of elements = 12664
Number of triangles = 2666
Number of quadrilatarals = 0
Number of tetrahedrals = 9998
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3357
Number of elements = 18188
Number of triangles = 3110
Number of quadrilatarals = 0
Number of tetrahedrals = 15078
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3622
Number of elements = 19080
Number of triangles = 4002
Number of quadrilatarals = 0
Number of tetrahedrals = 15078
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4425
Number of elements = 24045
Number of triangles = 4000
Number of quadrilatarals = 0
Number of tetrahedrals = 20045
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4822
Number of elements = 25381
Number of triangles = 5336
Number of quadrilatarals = 0
Number of tetrahedrals = 20045
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 4):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 2 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 4):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 4):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 4):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5483
Number of elements = 29853
Number of triangles = 4890
Number of quadrilatarals = 0
Number of tetrahedrals = 24963
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6012
Number of elements = 31633
Number of triangles = 6670
Number of quadrilatarals = 0
Number of tetrahedrals = 24963
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1190
Number of elements = 6252
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4918
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6555
Number of elements = 35742
Number of triangles = 5780
Number of quadrilatarals = 0
Number of tetrahedrals = 29962
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7216
Number of elements = 37966
Number of triangles = 8004
Number of quadrilatarals = 0
Number of tetrahedrals = 29962
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 6):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 2 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 6):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 6):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 6):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 6):
Number of nodes = 1190
Number of elements = 6252
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4918
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 6):
Number of nodes = 1204
Number of elements = 6333
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4999
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7634
Number of elements = 41677
Number of triangles = 6670
Number of quadrilatarals = 0
Number of tetrahedrals = 35007
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8427
Number of elements = 44345
Number of triangles = 9338
Number of quadrilatarals = 0
Number of tetrahedrals = 35007
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 1190
Number of elements = 6252
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4918
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 1204
Number of elements = 6333
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4999
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 1211
Number of elements = 6379
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5045
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 19879
Number of elements = 110275
Number of triangles = 15558
Number of quadrilatarals = 0
Number of tetrahedrals = 94717
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 22822
Number of elements = 120055
Number of triangles = 25338
Number of quadrilatarals = 0
Number of tetrahedrals = 94717
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 19):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 2 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 19):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 19):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 19):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 19):
Number of nodes = 1190
Number of elements = 6252
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4918
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 19):
Number of nodes = 1204
Number of elements = 6333
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4999
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 19):
Number of nodes = 1211
Number of elements = 6379
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5045
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 8 (of 19):
Number of nodes = 1220
Number of elements = 6413
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5077
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 9 (of 19):
Number of nodes = 1214
Number of elements = 6396
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5060
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 10 (of 19):
Number of nodes = 1192
Number of elements = 6262
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4930
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 11 (of 19):
Number of nodes = 1201
Number of elements = 6326
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4994
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 12 (of 19):
Number of nodes = 1206
Number of elements = 6356
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5022
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 13 (of 19):
Number of nodes = 1187
Number of elements = 6236
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4904
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 14 (of 19):
Number of nodes = 1197
Number of elements = 6293
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 15 (of 19):
Number of nodes = 1180
Number of elements = 6202
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4870
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 16 (of 19):
Number of nodes = 1197
Number of elements = 6289
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4957
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 17 (of 19):
Number of nodes = 1208
Number of elements = 6351
Number of triangles = 1334
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 18 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 18 (of 19):
Number of nodes = 1193
Number of elements = 6277
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4945
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 19 (of 19):
Number of nodes = 1200
Number of elements = 6309
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4975
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8499
Number of elements = 47040
Number of triangles = 6258
Number of quadrilatarals = 0
Number of tetrahedrals = 40782
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8631
Number of elements = 47484
Number of triangles = 6702
Number of quadrilatarals = 0
Number of tetrahedrals = 40782
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 7444
Number of elements = 41254
Number of triangles = 5370
Number of quadrilatarals = 0
Number of tetrahedrals = 35884
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1187
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
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9625
Number of elements = 53328
Number of triangles = 7146
Number of quadrilatarals = 0
Number of tetrahedrals = 46182
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9899
Number of elements = 54216
Number of triangles = 8034
Number of quadrilatarals = 0
Number of tetrahedrals = 46182
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7485
Number of elements = 41497
Number of triangles = 5370
Number of quadrilatarals = 0
Number of tetrahedrals = 36127
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1212
Number of elements = 6385
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5053
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1202
Number of elements = 6334
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5002
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9302
Number of elements = 51451
Number of triangles = 6968
Number of quadrilatarals = 0
Number of tetrahedrals = 44483
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9522
Number of elements = 52179
Number of triangles = 7696
Number of quadrilatarals = 0
Number of tetrahedrals = 44483
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7466
Number of elements = 41416
Number of triangles = 5368
Number of quadrilatarals = 0
Number of tetrahedrals = 36048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1187
Number of elements = 6230
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4898
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 869
Number of elements = 4533
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3537
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8956
Number of elements = 49469
Number of triangles = 6784
Number of quadrilatarals = 0
Number of tetrahedrals = 42685
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9139
Number of elements = 50065
Number of triangles = 7380
Number of quadrilatarals = 0
Number of tetrahedrals = 42685
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7430
Number of elements = 41197
Number of triangles = 5360
Number of quadrilatarals = 0
Number of tetrahedrals = 35837
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1187
Number of elements = 6230
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4898
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 522
Number of elements = 2638
Number of triangles = 688
Number of quadrilatarals = 0
Number of tetrahedrals = 1950
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8638
Number of elements = 47663
Number of triangles = 6598
Number of quadrilatarals = 0
Number of tetrahedrals = 41065
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8777
Number of elements = 48099
Number of triangles = 7034
Number of quadrilatarals = 0
Number of tetrahedrals = 41065
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7402
Number of elements = 41032
Number of triangles = 5352
Number of quadrilatarals = 0
Number of tetrahedrals = 35680
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 848
Number of elements = 4402
Number of triangles = 994
Number of quadrilatarals = 0
Number of tetrahedrals = 3408
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2665
Number of triangles = 688
Number of quadrilatarals = 0
Number of tetrahedrals = 1977
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9771
Number of elements = 54406
Number of triangles = 6748
Number of quadrilatarals = 0
Number of tetrahedrals = 47658
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10261
Number of elements = 56170
Number of triangles = 8512
Number of quadrilatarals = 0
Number of tetrahedrals = 47658
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7355
Number of elements = 40784
Number of triangles = 5334
Number of quadrilatarals = 0
Number of tetrahedrals = 35450
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 2663
Number of elements = 14238
Number of triangles = 2794
Number of quadrilatarals = 0
Number of tetrahedrals = 11444
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 243
Number of elements = 1148
Number of triangles = 384
Number of quadrilatarals = 0
Number of tetrahedrals = 764
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1510
Number of elements = 7821
Number of triangles = 1986
Number of quadrilatarals = 0
Number of tetrahedrals = 5835
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1574
Number of elements = 7945
Number of triangles = 2110
Number of quadrilatarals = 0
Number of tetrahedrals = 5835
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1170
Number of elements = 6155
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4847
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 360
Number of elements = 1630
Number of triangles = 718
Number of quadrilatarals = 0
Number of tetrahedrals = 912
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 44
Number of elements = 160
Number of triangles = 84
Number of quadrilatarals = 0
Number of tetrahedrals = 76
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5096
Number of elements = 27903
Number of triangles = 4076
Number of quadrilatarals = 0
Number of tetrahedrals = 23827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5242
Number of elements = 28455
Number of triangles = 4628
Number of quadrilatarals = 0
Number of tetrahedrals = 23827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 4905
Number of elements = 26939
Number of triangles = 4044
Number of quadrilatarals = 0
Number of tetrahedrals = 22895
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 337
Number of elements = 1516
Number of triangles = 584
Number of quadrilatarals = 0
Number of tetrahedrals = 932
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 33115
Number of elements = 191815
Number of triangles = 8476
Number of quadrilatarals = 0
Number of tetrahedrals = 183339
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 36459
Number of elements = 205159
Number of triangles = 21820
Number of quadrilatarals = 0
Number of tetrahedrals = 183339
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 28820
Number of elements = 163772
Number of triangles = 15148
Number of quadrilatarals = 0
Number of tetrahedrals = 148624
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1416
Number of elements = 7524
Number of triangles = 1456
Number of quadrilatarals = 0
Number of tetrahedrals = 6068
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 4240
Number of elements = 23511
Number of triangles = 2950
Number of quadrilatarals = 0
Number of tetrahedrals = 20561
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 720
Number of elements = 3724
Number of triangles = 842
Number of quadrilatarals = 0
Number of tetrahedrals = 2882
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1263
Number of elements = 6628
Number of triangles = 1424
Number of quadrilatarals = 0
Number of tetrahedrals = 5204
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16667
Number of elements = 94472
Number of triangles = 8798
Number of quadrilatarals = 0
Number of tetrahedrals = 85674
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18591
Number of elements = 101848
Number of triangles = 16174
Number of quadrilatarals = 0
Number of tetrahedrals = 85674
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 12023
Number of elements = 67478
Number of triangles = 7138
Number of quadrilatarals = 0
Number of tetrahedrals = 60340
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 6568
Number of elements = 34370
Number of triangles = 9036
Number of quadrilatarals = 0
Number of tetrahedrals = 25334
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 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2838
Number of elements = 12404
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 6952
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2494
Number of elements = 10977
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6425
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 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2838
Number of elements = 12404
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 6952
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 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2494
Number of elements = 10977
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6425
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 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2838
Number of elements = 12404
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 6952
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 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2494
Number of elements = 10977
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6425
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 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2838
Number of elements = 12404
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 6952
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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 6952
Sideset: 'Farfield', set_id 1, num_entries 12
Sideset: 'Wing1', set_id 2, num_entries 5440
Finished writing Exodus file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2494
Number of elements = 10977
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6425
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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 6425
Sideset: 'Farfield', set_id 1, num_entries 12
Sideset: 'Wing1', set_id 2, num_entries 4540
Finished writing Exodus file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4972
Number of elements = 27531
Number of triangles = 3460
Number of quadrilatarals = 0
Number of tetrahedrals = 24071
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6395
Number of elements = 35692
Number of triangles = 4048
Number of quadrilatarals = 0
Number of tetrahedrals = 31644
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 60123
Number of elements = 350900
Number of triangles = 12928
Number of quadrilatarals = 0
Number of tetrahedrals = 337972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59547
Number of elements = 346940
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 334512
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 60123
Number of elements = 350400
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 337972
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:62194)
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:62194)
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:62194)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
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:62194)
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:62194)
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:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
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:62194)
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:62194)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
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:62194)
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 exodus file ....
Block: 'Farfield_tri', blk_id 1, num_entries 1332
Block: 'Wing1_tri', blk_id 2, num_entries 73442
Sideset: 'Farfield', set_id 1, num_entries 1332
Sideset: 'Wing1', set_id 2, num_entries 73442
Finished writing Exodus 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 exodus file ....
Block: 'Farfield_tri', blk_id 1, num_entries 300
Block: 'Wing1_tri', blk_id 2, num_entries 32990
Sideset: 'Farfield', set_id 1, num_entries 300
Sideset: 'Wing1', set_id 2, num_entries 32990
Finished writing Exodus file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_regions (test_aflr4.TestAFLR4.test_regions) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: box
2: cut
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing exodus file ....
Block: 'box_tri', blk_id 1, num_entries 9130
Block: 'cut_tri', blk_id 2, num_entries 1288
Sideset: 'box', set_id 1, num_entries 9130
Sideset: 'cut', set_id 2, num_entries 1288
Finished writing Exodus 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_structures (test_aflr4.TestAFLR4.test_structures) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Ribs
2: Skin
3: Spar1
4: Rib_Root
5: Spar2
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing exodus file ....
Block: 'Ribs_tri', blk_id 1, num_entries 722
Block: 'Skin_tri', blk_id 2, num_entries 16906
Block: 'Spar1_tri', blk_id 3, num_entries 422
Block: 'Rib_Root_tri', blk_id 4, num_entries 292
Block: 'Spar2_tri', blk_id 5, num_entries 166
Sideset: 'Rib_Root', set_id 1, num_entries 292
Sideset: 'Ribs', set_id 2, num_entries 722
Sideset: 'Skin', set_id 3, num_entries 16906
Sideset: 'Spar1', set_id 4, num_entries 422
Sideset: 'Spar2', set_id 5, num_entries 166
Sideset: 'Skin_Top', set_id 6, num_entries 8553
Finished writing Exodus 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_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
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
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
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
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) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 28.284271 -nDiv 9 -maxR 7 -mesh2d > autoInputs.out
Executing: ./aero.csh > aero.out
ok
test_outputs (test_cart3d.TestCart3D.test_outputs) ... ok
test_reenter (test_cart3d.TestCart3D.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Getting CFD functional.......
Number of design variables - 1
Objective name - Drag
Done getting CFD functional
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out
Executing: ./aero.csh > aero.out
Executing: ./aero.csh > aero.out
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.307131 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out
Executing: ./aero.csh > aero.out
ok
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - Mach
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 3
Objective name - C_A
Objective name - C_N
Objective name - C_Y
Done getting CFD functional
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:09) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:10) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:13) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(13:31:13) Linearizing cut-cells
(13:31:13) ... done
o Number of simultaneous xsensit jobs: 1
(13:31:13) Computing gradients
(13:31:21) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:22) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:23) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 3
Objective name - C_D
Objective name - C_L
Objective name - C_S
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:23) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:25) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:25) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:27) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(13:31:27) Linearizing cut-cells
(13:31:27) ... done
o Number of simultaneous xsensit jobs: 1
(13:31:27) Computing gradients
(13:31:36) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:36) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:37) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_l
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:38) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:39) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:39) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:40) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(13:31:40) Linearizing cut-cells
(13:31:40) ... done
o Number of simultaneous xsensit jobs: 1
(13:31:40) Computing gradients
(13:31:44) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:45) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:46) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_m
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:46) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:47) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:48) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:49) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(13:31:49) Linearizing cut-cells
(13:31:49) ... done
o Number of simultaneous xsensit jobs: 1
(13:31:49) Computing gradients
(13:31:53) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:54) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:55) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_n
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:55) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:56) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:31:57) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:31:58) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(13:31:58) Linearizing cut-cells
(13:31:58) ... done
o Number of simultaneous xsensit jobs: 1
(13:31:58) Computing gradients
(13:32:02) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:03) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:04) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_M_x
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:04) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:05) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:06) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:07) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(13:32:07) Linearizing cut-cells
(13:32:07) ... done
o Number of simultaneous xsensit jobs: 1
(13:32:07) Computing gradients
(13:32:11) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:11) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:12) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_M_y
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:13) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:14) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:15) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:15) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(13:32:16) Linearizing cut-cells
(13:32:16) ... done
o Number of simultaneous xsensit jobs: 1
(13:32:16) Computing gradients
(13:32:20) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:20) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:21) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_M_z
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:22) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:23) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:23) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:24) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(13:32:24) Linearizing cut-cells
(13:32:24) ... done
o Number of simultaneous xsensit jobs: 1
(13:32:24) Computing gradients
(13:32:28) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:29) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:30) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - Mach
Design Variable name - area
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 3
Objective name - C_A
Objective name - C_N
Objective name - C_Y
Done getting CFD functional
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:31) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:32) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:33) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:35) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 2
o Number of simultaneous cutter jobs: 2
(13:32:35) Linearizing cut-cells
(13:32:37) ... done
o Number of simultaneous xsensit jobs: 2
(13:32:37) Computing gradients
Adjusted OMP_NUM_THREADS to 1 for xsensit
(13:32:45) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(13:32:46) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(13:32:47) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_Output_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Wing1, index = 1
Name = trailingEdge, index = 2
Writing FAST file ....
Finished writing FAST file
Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
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
17C003000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
17C003000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 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
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
17C003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
17C003000 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
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
17C003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
17C003000 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
17C003000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
17C003000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 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:62194)
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:62194)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
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:62194)
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:62194)
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:62194)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62194)
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:62194)
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:62194)
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:62194)
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:62194)
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:62194)
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 exodus file ....
Block: 'Farfield_tri', blk_id 1, num_entries 48
Block: 'Wing1_tri', blk_id 2, num_entries 19110
Sideset: 'Farfield', set_id 1, num_entries 48
Sideset: 'Wing1', set_id 2, num_entries 19110
Finished writing Exodus 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 exodus file ....
Block: 'Farfield_tri', blk_id 1, num_entries 12
Block: 'Wing1_tri', blk_id 2, num_entries 14282
Sideset: 'Farfield', set_id 1, num_entries 12
Sideset: 'Wing1', set_id 2, num_entries 14282
Finished writing Exodus 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 = 7800
Number of elements = 15596
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
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 - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.105111
Creating surface mesh ...
Surface mesh seconds: 0.016493
Recovering boundaries...
Boundary recovery seconds: 0.085066
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.028038
Recovering Delaunayness...
Delaunay recovery seconds: 0.040689
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 1.27827
Smoothing vertices...
Mesh smoothing seconds: 1.04899
Improving mesh...
Mesh improvement seconds: 0.027667
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.005786
Total running seconds: 2.63644
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
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 = 7800
Number of elements = 15596
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
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 - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.09856
Creating surface mesh ...
Surface mesh seconds: 0.014385
Recovering boundaries...
Boundary recovery seconds: 0.085552
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.023245
Recovering Delaunayness...
Delaunay recovery seconds: 0.037924
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 1.26963
Smoothing vertices...
Mesh smoothing seconds: 1.19848
Improving mesh...
Mesh improvement seconds: 0.027212
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.006032
Total running seconds: 2.76135
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok
test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 - 5097, elements - 10182
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 - 5097, elements - 10182
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 - 14248, elements - 28484
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 = 4048
Number of elements = 8092
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8092
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 = 6217
Combined Number of elements = 12425
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12424
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 = 3908
Number of elements = 7812
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7812
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 = 6077
Combined Number of elements = 12145
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12144
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 = 4048
Number of elements = 8092
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8092
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 = 6217
Combined Number of elements = 12425
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12424
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 = 4048
Number of elements = 8092
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8092
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 = 6217
Combined Number of elements = 12425
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12424
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 = 3908
Number of elements = 7812
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7812
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 = 6077
Combined Number of elements = 12145
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12144
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 = 3908
Number of elements = 7812
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7812
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 = 6077
Combined Number of elements = 12145
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12144
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 exodus file ....
Block: 'Block1_tri', blk_id 1, num_entries 396
Sideset: 'Airfoil', set_id 1, num_entries 18
Sideset: 'InFlow', set_id 2, num_entries 9
Sideset: 'OutFlow', set_id 3, num_entries 9
Sideset: 'TunnelWall', set_id 4, num_entries 18
Finished writing Exodus 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 exodus file ....
Block: 'Block1_tri', blk_id 1, num_entries 719
Sideset: 'Airfoil', set_id 1, num_entries 17
Sideset: 'InFlow', set_id 2, num_entries 4
Sideset: 'OutFlow', set_id 3, num_entries 18
Sideset: 'TunnelWall', set_id 4, num_entries 22
Finished writing Exodus 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 exodus file ....
Block: 'Block1_tri', blk_id 1, num_entries 1200
Sideset: 'Airfoil', set_id 1, num_entries 20
Sideset: 'InFlow', set_id 2, num_entries 4
Sideset: 'OutFlow', set_id 3, num_entries 36
Sideset: 'TunnelWall', set_id 4, num_entries 40
Finished writing Exodus 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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1579
Number of elements = 8634
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7394
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2600
Number of elements = 13872
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11114
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1039
Number of elements = 5509
Number of triangles = 998
Number of quadrilatarals = 0
Number of tetrahedrals = 4511
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 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 15766
Number of elements = 90668
Number of triangles = 4632
Number of quadrilatarals = 0
Number of tetrahedrals = 86036
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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 86036
Sideset: 'Farfield', set_id 1, num_entries 36
Sideset: 'Wing1', set_id 2, num_entries 4596
Finished writing Exodus 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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 98795
Sideset: 'Farfield', set_id 1, num_entries 144
Sideset: 'Wing1', set_id 2, num_entries 4086
Finished writing Exodus 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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 163296
Sideset: 'Farfield', set_id 1, num_entries 576
Sideset: 'Wing1', set_id 2, num_entries 5666
Finished writing Exodus file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1579
Number of elements = 8634
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7394
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_inputs (test_refine.TestREFINE.test_inputs) ... ok
test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 432
Number of elements = 2132
Number of triangles = 644
Number of quadrilatarals = 0
Number of tetrahedrals = 1488
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 935
Number of elements = 5010
Number of triangles = 758
Number of quadrilatarals = 0
Number of tetrahedrals = 4252
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 3 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 8 Faces
EGADS : Body 0 has 15 Edges
EGADS : Body 0 has 8 Loops
EGADS : Body 0 has 9 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 8 Faces
EGADS : Body 1 has 15 Edges
EGADS : Body 1 has 8 Loops
EGADS : Body 1 has 9 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 2 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 2 Loops
EGADS : Body 2 has 2 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 4 5
EGADS : 2 Yes 0 0 1 1 1 1 3 4 6
EGADS : 3 Yes 0 0 1 1 1 1 2 4 7
EGADS : 4 Yes 0 0 1 1 1 1 2 3
EGADS : 5 Yes 0 0 1 1 1 1 6 7 8
EGADS : 6 Yes 0 0 1 1 1 2 5 7 8
EGADS : 7 Yes 0 0 1 1 1 3 5 6 8
EGADS : 8 Yes 0 0 1 1 1 5 6 7
EGADS : 9 Yes 1 0 1 0 10 10 11 12 13
EGADS : 10 Yes 1 0 1 0 10 9 11 12 14
EGADS : 11 Yes 1 0 1 0 10 9 10 12 15
EGADS : 12 Yes 1 0 1 0 10 9 10 11
EGADS : 13 Yes 1 0 1 0 10 9 14 15 16
EGADS : 14 Yes 1 0 1 0 10 10 13 15 16
EGADS : 15 Yes 1 0 1 0 10 11 13 14 16
EGADS : 16 Yes 1 0 1 0 10 13 14 15
EGADS : 17 Yes 2 0 1 NA NA 18
EGADS : 18 Yes 2 0 1 NA NA 17
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 4 -3 -2
EGADS : 2 3 7 -6 -5
EGADS : 3 6 9 -1 -8
EGADS : 4 -4 -9 -7
EGADS : 5 -10 2 11 -12
EGADS : 6 -11 5 13 -14
EGADS : 7 -13 8 10 -15
EGADS : 8 12 14 15
EGADS : 9 16 19 -18 -17
EGADS : 10 18 22 -21 -20
EGADS : 11 21 24 -16 -23
EGADS : 12 -19 -24 -22
EGADS : 13 -25 17 26 -27
EGADS : 14 -26 20 28 -29
EGADS : 15 -28 23 25 -30
EGADS : 16 27 29 30
EGADS : 17 -31 -32 33 34
EGADS : 18 -35 -34 36 32
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 4 -3 -2
EGADS : 2 Yes 3 7 -6 -5
EGADS : 3 Yes 6 9 -1 -8
EGADS : 4 Yes -4 -9 -7
EGADS : 5 Yes -10 2 11 -12
EGADS : 6 Yes -11 5 13 -14
EGADS : 7 Yes -13 8 10 -15
EGADS : 8 Yes 12 14 15
EGADS : 9 Yes 16 19 -18 -17
EGADS : 10 Yes 18 22 -21 -20
EGADS : 11 Yes 21 24 -16 -23
EGADS : 12 Yes -19 -24 -22
EGADS : 13 Yes -25 17 26 -27
EGADS : 14 Yes -26 20 28 -29
EGADS : 15 Yes -28 23 25 -30
EGADS : 16 Yes 27 29 30
EGADS : 17 Yes -31 -32 33 34
EGADS : 18 Yes -35 -34 36 32
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 5
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 4
EGADS : 5 0 Yes 3 5 1 2 6
EGADS : 6 0 Yes 5 6 1 2 3
EGADS : 7 0 Yes 4 6 1 2 4
EGADS : 8 0 Yes 5 1 1 3 7
EGADS : 9 0 Yes 6 2 1 3 4
EGADS : 10 0 Yes 1 7 1 5 7
EGADS : 11 0 Yes 3 8 1 5 6
EGADS : 12 0 Yes 7 8 1 5 8
EGADS : 13 0 Yes 5 9 1 6 7
EGADS : 14 0 Yes 8 9 1 6 8
EGADS : 15 0 Yes 9 7 1 7 8
EGADS : 16 1 Yes 10 11 1 9 11
EGADS : 17 1 Yes 10 12 1 9 13
EGADS : 18 1 Yes 12 13 1 9 10
EGADS : 19 1 Yes 11 13 1 9 12
EGADS : 20 1 Yes 12 14 1 10 14
EGADS : 21 1 Yes 14 15 1 10 11
EGADS : 22 1 Yes 13 15 1 10 12
EGADS : 23 1 Yes 14 10 1 11 15
EGADS : 24 1 Yes 15 11 1 11 12
EGADS : 25 1 Yes 10 16 1 13 15
EGADS : 26 1 Yes 12 17 1 13 14
EGADS : 27 1 Yes 16 17 1 13 16
EGADS : 28 1 Yes 14 18 1 14 15
EGADS : 29 1 Yes 17 18 1 14 16
EGADS : 30 1 Yes 18 16 1 15 16
EGADS : 31 2 DEGEN 19 19 - 17
EGADS : 32 2 Yes 20 19 NA 17 18
EGADS : 33 2 DEGEN 20 20 - 17
EGADS : 34 2 Yes 20 19 NA 17 18
EGADS : 35 2 DEGEN 19 19 - 18
EGADS : 36 2 DEGEN 20 20 - 18
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 3.77246052 0 0.00459131419
EGADS : 2 Yes 5.90487498 7.07106781 0
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 4.0824829 7.07106781 0.123425948
EGADS : 5 Yes 3.77001182 0 0
EGADS : 6 Yes 5.90282524 7.07106781 0
EGADS : 7 Yes 5.90487498 0 0
EGADS : 8 Yes 4.0824829 0 0.123425948
EGADS : 9 Yes 5.90282524 0 0
EGADS : 10 Yes 11.5089842 0 0.00183652568
EGADS : 11 Yes 12.36195 2.82842712 0
EGADS : 12 Yes 10 0 0
EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791
EGADS : 14 Yes 11.5080047 0 0
EGADS : 15 Yes 12.3611301 2.82842712 0
EGADS : 16 Yes 12.36195 0 0
EGADS : 17 Yes 11.6329932 0 0.0493703791
EGADS : 18 Yes 12.3611301 0 0
EGADS : 19 Yes 0 0 80
EGADS : 20 Yes 0 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 160
AFLR4 : Min Bounding Box Length = 160
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 0.890888
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 15.6122
AFLR4 : Abs Min Surf Spacing = 0.00222722
AFLR4 : Min Surf Spacing = 0.00445444
AFLR4 : Max Surf Spacing = 0.0890888
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 STD
AFLR4 : 12 CAD geometry 0 STD
AFLR4 : 13 CAD geometry 0 STD
AFLR4 : 14 CAD geometry 0 STD
AFLR4 : 15 CAD geometry 0 STD
AFLR4 : 16 CAD geometry 0 STD
AFLR4 : 17 CAD geometry 0 FARFIELD
AFLR4 : 18 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 12428
AFLR43 : Nodes = 6220
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 23.3.0 arm64
AFLR3 : Compile Date 02/08/24 @ 04:22PM
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 = 0.007 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 25026
AFLR3 IG : Nodes, Elements = 4984 34312
AFLR3 IG : Nodes, Elements = 6227 43517
AFLR3 IG : Nodes, Elements = 6227 43439
AFLR3 IG : Nodes, Elements = 6227 43476
AFLR3 IG : Nodes, Elements = 6227 43444
AFLR3 IG : Nodes, Elements = 6220 26114
AFLR3 IG : Nodes, Elements = 6220 26132
AFLR3 IG : Nodes, Elements = 6220 21569
AFLR3 IG : Nodes, Elements = 6220 19193
AFLR3 : CPU Time = 0.084 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6220 19193
AFLR3 GG : Nodes, Elements = 9101 28053
AFLR3 GG : Nodes, Elements = 9101 39640
AFLR3 GG : Nodes, Elements = 9101 36690
AFLR3 GG : Nodes, Elements = 9101 35155
AFLR3 GG : Nodes, Elements = 11687 43216
AFLR3 GG : Nodes, Elements = 11687 54497
AFLR3 GG : Nodes, Elements = 11687 51170
AFLR3 GG : Nodes, Elements = 11687 50185
AFLR3 GG : Nodes, Elements = 14519 58970
AFLR3 GG : Nodes, Elements = 14519 71103
AFLR3 GG : Nodes, Elements = 14519 67722
AFLR3 GG : Nodes, Elements = 14519 66894
AFLR3 GG : Nodes, Elements = 17597 76360
AFLR3 GG : Nodes, Elements = 17597 89686
AFLR3 GG : Nodes, Elements = 17597 86040
AFLR3 GG : Nodes, Elements = 17597 85134
AFLR3 GG : Nodes, Elements = 20802 94942
AFLR3 GG : Nodes, Elements = 20802 108532
AFLR3 GG : Nodes, Elements = 20802 104847
AFLR3 GG : Nodes, Elements = 20802 104019
AFLR3 GG : Nodes, Elements = 24174 114290
AFLR3 GG : Nodes, Elements = 24174 128631
AFLR3 GG : Nodes, Elements = 24174 124801
AFLR3 GG : Nodes, Elements = 24174 123982
AFLR3 GG : Nodes, Elements = 27742 134809
AFLR3 GG : Nodes, Elements = 27742 150037
AFLR3 GG : Nodes, Elements = 27742 145948
AFLR3 GG : Nodes, Elements = 27742 145081
AFLR3 GG : Nodes, Elements = 31383 156143
AFLR3 GG : Nodes, Elements = 31383 171588
AFLR3 GG : Nodes, Elements = 31383 167421
AFLR3 GG : Nodes, Elements = 31383 166536
AFLR3 GG : Nodes, Elements = 35115 177837
AFLR3 GG : Nodes, Elements = 35115 193748
AFLR3 GG : Nodes, Elements = 35115 189548
AFLR3 GG : Nodes, Elements = 35115 188723
AFLR3 GG : Nodes, Elements = 38948 200319
AFLR3 GG : Nodes, Elements = 38948 216342
AFLR3 GG : Nodes, Elements = 38948 212298
AFLR3 GG : Nodes, Elements = 38948 211481
AFLR3 GG : Nodes, Elements = 42740 222940
AFLR3 GG : Nodes, Elements = 42740 239184
AFLR3 GG : Nodes, Elements = 42740 234883
AFLR3 GG : Nodes, Elements = 42740 234060
AFLR3 GG : Nodes, Elements = 46416 245151
AFLR3 GG : Nodes, Elements = 46416 260680
AFLR3 GG : Nodes, Elements = 46416 256642
AFLR3 GG : Nodes, Elements = 46416 255866
AFLR3 GG : Nodes, Elements = 50035 266777
AFLR3 GG : Nodes, Elements = 50035 281993
AFLR3 GG : Nodes, Elements = 50035 278055
AFLR3 GG : Nodes, Elements = 50035 277383
AFLR3 GG : Nodes, Elements = 53591 288088
AFLR3 GG : Nodes, Elements = 53591 303095
AFLR3 GG : Nodes, Elements = 53591 299307
AFLR3 GG : Nodes, Elements = 53591 298569
AFLR3 GG : Nodes, Elements = 57005 308827
AFLR3 GG : Nodes, Elements = 57005 323244
AFLR3 GG : Nodes, Elements = 57005 319601
AFLR3 GG : Nodes, Elements = 57005 318957
AFLR3 GG : Nodes, Elements = 60293 328832
AFLR3 GG : Nodes, Elements = 60293 342689
AFLR3 GG : Nodes, Elements = 60293 339197
AFLR3 GG : Nodes, Elements = 60293 338647
AFLR3 GG : Nodes, Elements = 63359 347851
AFLR3 GG : Nodes, Elements = 63359 360783
AFLR3 GG : Nodes, Elements = 63359 357437
AFLR3 GG : Nodes, Elements = 63359 356932
AFLR3 GG : Nodes, Elements = 66259 365641
AFLR3 GG : Nodes, Elements = 66259 377775
AFLR3 GG : Nodes, Elements = 66259 374741
AFLR3 GG : Nodes, Elements = 66259 374315
AFLR3 GG : Nodes, Elements = 68879 382177
AFLR3 GG : Nodes, Elements = 68879 393099
AFLR3 GG : Nodes, Elements = 68879 390371
AFLR3 GG : Nodes, Elements = 68879 390020
AFLR3 GG : Nodes, Elements = 71152 396844
AFLR3 GG : Nodes, Elements = 71152 406357
AFLR3 GG : Nodes, Elements = 71152 403836
AFLR3 GG : Nodes, Elements = 71152 403561
AFLR3 GG : Nodes, Elements = 73068 409315
AFLR3 GG : Nodes, Elements = 73068 417362
AFLR3 GG : Nodes, Elements = 73068 415318
AFLR3 GG : Nodes, Elements = 73068 415069
AFLR3 GG : Nodes, Elements = 74529 419454
AFLR3 GG : Nodes, Elements = 74529 425587
AFLR3 GG : Nodes, Elements = 74529 423928
AFLR3 GG : Nodes, Elements = 74529 423776
AFLR3 GG : Nodes, Elements = 75631 427084
AFLR3 GG : Nodes, Elements = 75631 431714
AFLR3 GG : Nodes, Elements = 75631 430512
AFLR3 GG : Nodes, Elements = 75631 430423
AFLR3 GG : Nodes, Elements = 76419 432787
AFLR3 GG : Nodes, Elements = 76419 436211
AFLR3 GG : Nodes, Elements = 76419 435175
AFLR3 GG : Nodes, Elements = 76419 435106
AFLR3 GG : Nodes, Elements = 76934 436651
AFLR3 GG : Nodes, Elements = 76934 438851
AFLR3 GG : Nodes, Elements = 76934 438238
AFLR3 GG : Nodes, Elements = 76934 438198
AFLR3 GG : Nodes, Elements = 77241 439119
AFLR3 GG : Nodes, Elements = 77241 440474
AFLR3 GG : Nodes, Elements = 77241 440052
AFLR3 GG : Nodes, Elements = 77241 440022
AFLR3 GG : Nodes, Elements = 77416 440547
AFLR3 GG : Nodes, Elements = 77416 441274
AFLR3 GG : Nodes, Elements = 77416 441066
AFLR3 GG : Nodes, Elements = 77416 441056
AFLR3 GG : Nodes, Elements = 77509 441335
AFLR3 GG : Nodes, Elements = 77509 441739
AFLR3 GG : Nodes, Elements = 77509 441625
AFLR3 GG : Nodes, Elements = 77509 441612
AFLR3 GG : Nodes, Elements = 77549 441732
AFLR3 GG : Nodes, Elements = 77549 441904
AFLR3 GG : Nodes, Elements = 77549 441849
AFLR3 GG : Nodes, Elements = 77549 441848
AFLR3 GG : Nodes, Elements = 77559 441878
AFLR3 GG : Nodes, Elements = 77559 441913
AFLR3 GG : Nodes, Elements = 77559 441902
AFLR3 GG : Nodes, Elements = 77564 441917
AFLR3 GG : Nodes, Elements = 77564 441932
AFLR3 GG : Nodes, Elements = 77564 441928
AFLR3 GG : Nodes, Elements = 77565 441931
AFLR3 GG : Nodes, Elements = 77565 441938
AFLR3 GG : Nodes, Elements = 77565 441933
AFLR3 GG : Nodes, Elements = 77595 442023
AFLR3 GG : Nodes, Elements = 77595 442128
AFLR3 GG : Nodes, Elements = 77595 442098
AFLR3 GG : Nodes, Elements = 77595 442094
AFLR3 GG : Nodes, Elements = 77599 442106
AFLR3 GG : Nodes, Elements = 77599 442119
AFLR3 GG : Nodes, Elements = 77599 442116
AFLR3 GG : Nodes, Elements = 77599 442115
AFLR3 GG : Nodes, Elements = 77600 442118
AFLR3 GG : Nodes, Elements = 77600 442125
AFLR3 GG : Nodes, Elements = 77600 442121
AFLR3 : CPU Time = 2.694 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 77600 442121
AFLR3 QI : Nodes, Elements = 76105 433678
AFLR3 QI : Nodes, Elements = 75842 432198
AFLR3 QI : Nodes, Elements = 75829 432123
AFLR3 QI : Nodes, Elements = 75827 432113
AFLR3 QI : Nodes, Elements = 75826 432107
AFLR3 QI : Nodes, Elements = 75826 436049
AFLR3 QI : Nodes, Elements = 75826 431912
AFLR3 QI : Nodes, Elements = 75826 431430
AFLR3 QI : Nodes, Elements = 75826 431831
AFLR3 QI : Nodes, Elements = 75826 431146
AFLR3 QI : Nodes, Elements = 75826 430921
AFLR3 QI : Nodes, Elements = 75826 431306
AFLR3 QI : Nodes, Elements = 75826 430921
AFLR3 QI : Nodes, Elements = 75826 430900
AFLR3 QI : Nodes, Elements = 75826 431192
AFLR3 QI : Nodes, Elements = 75826 430885
AFLR3 QI : Nodes, Elements = 75826 430832
AFLR3 QI : Nodes, Elements = 75826 431117
AFLR3 QI : Nodes, Elements = 75826 430836
AFLR3 QI : Nodes, Elements = 75826 430821
AFLR3 QI : Nodes, Elements = 75831 430843
AFLR3 QI : Nodes, Elements = 75831 431136
AFLR3 QI : Nodes, Elements = 75831 430863
AFLR3 QI : Nodes, Elements = 75831 430845
AFLR3 QI : Nodes, Elements = 75831 431106
AFLR3 QI : Nodes, Elements = 75831 430850
AFLR3 QI : Nodes, Elements = 75831 430821
AFLR3 : CPU Time = 0.869 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 75831 430821
AFLR3 QRG: Nodes, Elements = 75839 430867
AFLR3 QRG: Nodes, Elements = 75842 430887
AFLR3 QRG: Nodes, Elements = 75841 430884
AFLR3 QRG: Nodes, Elements = 75841 430883
AFLR3 QRG: Nodes, Elements = 75848 430923
AFLR3 QRG: Nodes, Elements = 75847 430916
AFLR3 : CPU Time = 0.035 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 430916
UG3 : Min, Max Ang = 1.198 173.5
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 54
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 430916
UG3 : Min Vol = 6.52e-10
UG3 : Average Vol = 4.92
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 = 430916
UG3 : Min, Max Q = 0.073 1
UG3 : Average Q = 0.892
UG3 : No. Q< 0.1 = 27
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 3.911 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 430916
UG3 : Min, Max Ang = 1.198 173.5
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 54
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 430916
UG3 : Min Vol = 6.52e-10
UG3 : Average Vol = 4.92
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 = 430916
UG3 : Min, Max Q = 0.189 1
UG3 : Average Q = 0.85
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
Number of nodes = 75847
Number of elements = 443344
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 430916
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 75847
Number of elements = 443344
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 430916
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 75847
Number of elements = 443344
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 430916
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 1
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
ok
test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 75847
Number of elements = 443344
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 430916
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:62194)
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)
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
17C003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
17C003000 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 = 298
Number of elements = 592
Number of triangle elements = 592
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 = 489
Number of elements = 974
Number of triangle elements = 974
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4197
Total number of elements = 8374
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 - 298, elements - 592
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 - 489, elements - 974
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 - 298, elements - 592
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 - 489, elements - 974
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 - 4197, elements - 8374
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 = 173
Number of elements = 342
Number of triangle elements = 342
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 = 2320
Total number of elements = 4604
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 - 173, elements - 342
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 - 173, elements - 342
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 = 443
Number of elements = 882
Number of triangle elements = 882
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 = 965
Total number of elements = 1926
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 443, elements - 882
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 - 443, elements - 882
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 - 9583, elements - 19158
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 - 9583, elements - 19158
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 - 9583, elements - 19158
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 - 9583, elements - 19158
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 - 9583, elements - 19158
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 - 7151, elements - 14294
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 = 9583
Number of elements = 19158
Number of triangle elements = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9583
Total number of elements = 19158
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
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 exodus file ....
Block: 'region_1_tet', blk_id 1, num_entries 104182
Sideset: 'Farfield', set_id 1, num_entries 48
Sideset: 'Wing1', set_id 2, num_entries 19110
Finished writing Exodus 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 - 9583, elements - 19158
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 exodus file ....
Block: 'region_1_tet', blk_id 1, num_entries 69273
Sideset: 'Farfield', set_id 1, num_entries 48
Sideset: 'Wing1', set_id 2, num_entries 19110
Finished writing Exodus 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, 98963.803823, 69822.813293, 6179.981375, 19723.152208, 370546.335525]
ok
----------------------------------------------------------------------
Ran 146 tests in 434.829s
OK (skipped=10)
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
(make -C cCAPS -f avlTest.make)
make[1]: `avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[1]: `awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[1]: `frictionTest' is up to date.
(make -C cCAPS -f fun3d.make)
make[1]: Nothing to be done for `fun3d'.
(make -C cCAPS -f hsm.make)
make[1]: `hsm' is up to date.
(make -C cCAPS -f interferenceTest.make)
make[1]: `interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[1]: `msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[1]: `mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[1]: `pointwiseTest' is up to date.
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests
All tests pass!
=================================================
=================================================
(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)
=================================================
Using python : /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 0.0006119078685800925
CYtot -6.292592518559147e-15
CZtot -0.3012861394881712
Cltot -4.783069014642483e-14
Cmtot -0.1945055953448147
Cntot -2.338890054396671e-15
Cl'tot -4.786422456048383e-14
Cn'tot -1.50377318550154e-15
CLtot 0.3012509314146395
CDtot 0.00464635348821979
CDvis 0.0
CLff 0.3009503023516151
CYff -7.7198870803959e-15
CDind 0.00464635348821979
CDff 0.004968969500894849
e 0.9669902146155998
StripForces
Wing cl = [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407]
Wing cd = [-0.004234137763148, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946456, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372442, -0.004494543653152, -0.00423413776453]
real 0m0.579s
user 0m0.582s
sys 0m0.201s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = [1.05475230551148, 1.36488869373725, 1.56607214272246, 2.03059709357768, 1.9727108312095, 1.87307153172323, 1.76050475760053]
Cd = [0.0131991208831308, 0.0166540240605859, 0.0200551482562657, 0.0458671341873005, 0.0754256009397268, 0.0994469174479059, 0.127479430989221]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.49604411072842, 0.461377732041756, 0.442376568202227, 0.361251636144409, 0.276104140854608, 0.214381239321802, 0.132988264746433]
real 0m2.217s
user 0m2.350s
sys 0m0.087s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = 0.3783791085548177
Cd = 0.007775858417209677
Cm = 0.005262636995835036
real 0m3.570s
user 0m2.585s
sys 0m0.132s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 0m0.372s
user 0m0.460s
sys 0m0.068s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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.
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG
Cl = 0.933407
Cd = 0.000284
Cd Wave = 0.0
Cm = -0.203436
Cp _Critcal = -1.303869
real 0m0.405s
user 0m0.500s
sys 0m0.070s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 0m0.479s
user 0m0.619s
sys 0m0.170s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 0m4.339s
user 0m9.834s
sys 0m4.421s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u aflr2_PyTest.py -outLevel=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 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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.000 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 = 0.010 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 = 0.005 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 0m0.446s
user 0m0.659s
sys 0m0.199s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 150214
Number of elements = 450024
Number of triangles = 14380
Number of quadrilatarals = 0
Number of tetrahedrals = 214592
Number of pyramids = 425
Number of prisms = 220627
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m8.970s
user 0m7.845s
sys 0m0.296s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 = 258
Number of elements = 512
Number of triangle elements = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3130
Total number of elements = 6248
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 - 3130, elements - 6248
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.014402
Creating surface mesh ...
Surface mesh seconds: 0.002017
Recovering boundaries...
Boundary recovery seconds: 0.047967
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.002852
Suppressing Steiner points ...
Steiner suppression seconds: 5e-06
Recovering Delaunayness...
Delaunay recovery seconds: 0.006181
Refining mesh...
4177 insertions, added 2159 points, 136953 tetrahedra in queue.
1390 insertions, added 372 points, 139199 tetrahedra in queue.
1853 insertions, added 454 points, 136118 tetrahedra in queue.
2470 insertions, added 521 points, 118263 tetrahedra in queue.
3293 insertions, added 464 points, 66933 tetrahedra in queue.
4389 insertions, added 406 points, 1337 tetrahedra in queue.
5851 insertions, added 599 points, 33 tetrahedra in queue.
Refinement seconds: 0.416859
Smoothing vertices...
Mesh smoothing seconds: 0.223498
Improving mesh...
Mesh improvement seconds: 0.006965
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000783
Total running seconds: 0.72169
Statistics:
Input points: 3130
Input facets: 6248
Input segments: 9372
Input holes: 2
Input regions: 0
Mesh points: 8156
Mesh tetrahedra: 40155
Mesh faces: 83435
Mesh faces on exterior boundary: 6250
Mesh faces on input facets: 6250
Mesh edges on input segments: 9373
Steiner points on input segments: 1
Steiner points inside domain: 5025
Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.
Writing Tecplot file ....
Finished writing Tecplot file
real 0m1.486s
user 0m1.740s
sys 0m0.135s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.001 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 = 0.022 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 = 0.008 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| 6.2868e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 6.5332e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 6.4629e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 6.4904e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 6.4615e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 6.4049e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 6.4123e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 6.4179e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 6.4243e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 6.4281e-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 0m1.769s
user 0m1.662s
sys 0m0.531s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
./execute_PyTestRegression.sh: line 198: ulimit: stack size: cannot modify limit: Operation not permitted
=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u cart3d_PyTest.py -outLevel=0
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 3.796888
Tessellating body 1 with MaxEdge = 0.094922 Sag = 0.003797 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9 > autoInputs.out
Executing: ./aero.csh > aero.out
C_A 0.023693377
C_Y -0.0012129282
C_N 0.065395002
C_D 0.025961197
C_S -0.0012129282
C_L 0.064528278
C_l 0.0510971
C_m 0.000248187
C_n -0.017525
C_M_x 0.0504544
C_M_y 0.000248187
C_M_z -0.0192976
real 0m10.572s
user 0m18.054s
sys 0m0.606s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 0m0.709s
user 0m0.695s
sys 0m0.165s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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
real 0m0.774s
user 0m0.830s
sys 0m0.233s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 3.428666259749
Mass 5383.006027806
Centroid [1.222256036872, 0.1634981473779, -4.647736192456e-11]
CG [1.222256036872, 0.1634981473779, -4.647907951721e-11]
Ixx 22133.97306031
Iyy 23448.30046704
Izz 1389.213122564
Ixy 164.2055275655
Ixz -7.485782319314e-06
Iyz 1.710545499156e-06
I [22133.97306031, 23448.30046704, 1389.213122564, 164.2055275655, -7.485782319314e-06, 1.710545499156e-06]
II [[22133.97306031, -164.2055275655, 7.485782319314e-06], [-164.2055275655, 23448.30046704, -1.710545499156e-06], [7.485782319314e-06, -1.710545499156e-06, 1389.213122564]]
real 0m3.874s
user 0m5.282s
sys 0m7.780s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 0m0.504s
user 0m0.658s
sys 0m0.059s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u ../corsairlite/qp.py -outLevel=0
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 0m6.778s
user 0m1.596s
sys 0m0.192s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
awave
Mystran
=================================================
All tests pass!
=================================================
=================================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64
+ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/test/plugs
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/test/plugs
+ find /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/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 46360
-rw-r--r-- 1 jenkins staff 1.2M Jun 20 13:27 ASTRO.D01
-rw-r--r-- 1 jenkins staff 277K Jun 20 13:27 ASTRO.IDX
-rwxr-xr-x 1 jenkins staff 130K Jun 20 13:27 ESPxddm
-rwxr-xr-x 1 jenkins staff 212K Jun 20 13:27 Slugs
-rwxr-xr-x 1 jenkins staff 86K Jun 20 13:27 TestFit
-rwxr-xr-x 1 jenkins staff 1.6M Jun 20 13:27 avl
-rwxr-xr-x 1 jenkins staff 35K Jun 20 13:27 cart3dTest
-rwxr-xr-x 1 jenkins staff 34K Jun 20 13:26 egads2cart
-rwxr-xr-x 1 jenkins staff 70K Jun 20 13:27 egads2cgt
-rwxr-xr-x 1 jenkins staff 345K Jun 20 13:27 friction
-rwxr-xr-x 1 jenkins staff 10M Jun 20 13:27 mastros.exe
-rwxr-xr-x 1 jenkins staff 749K Jun 20 13:27 mses
-rwxr-xr-x 1 jenkins staff 1.4M Jun 20 13:27 mset
-rwxr-xr-x 1 jenkins staff 34K Jun 20 13:27 phaseUtil
-rw-r--r-- 1 jenkins staff 1.6K Jun 20 13:28 pod.egads
-rw-r--r-- 1 jenkins staff 0B Jun 20 13:28 port7681.jrnl
-rwxr-xr-x 1 jenkins staff 1.2M Jun 20 13:27 pplot
-rwxr-xr-x 1 jenkins staff 1.1M Jun 20 13:27 pxplot
-rwxr-xr-x 1 jenkins staff 68K Jun 20 13:27 sensCSM
-rwxr-xr-x 1 jenkins staff 192K Jun 20 13:27 serveCSM
-rwxr-xr-x 1 jenkins staff 175K Jun 20 13:27 serveESP
-rwxr-xr-x 1 jenkins staff 52K Jun 20 13:26 vCurvature
-rwxr-xr-x 1 jenkins staff 51K Jun 20 13:26 vGeom
-rwxr-xr-x 1 jenkins staff 36K Jun 20 13:26 vTess
-rwxr-xr-x 1 jenkins staff 1.7M Jun 20 13:26 vTesstatic
-rw-r--r-- 1 jenkins staff 195K Jun 20 13:28 wingMultiModel.bdf
-rwxr-xr-x 1 jenkins staff 1.7M Jun 20 13:27 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/verify_7.7.0/plugs0a.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 5.416e-07, rmsbest= 6.132e-04, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 2, unclass= 0
Starting pass 3 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m5.480s
user 0m4.971s
sys 0m0.315s
++ set +x
data/Plugs/plugs0a passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/verify_7.7.0/plugs0b.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 3.039e-07, rmsbest= 4.036e-02, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 2.814e-07, rmsbest= 1.924e-03, reclass= 1033, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 4.494e-07, rmsbest= 5.920e-04, reclass= 473, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 17, unclass= 0
Starting pass 5 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m4.382s
user 0m5.207s
sys 0m0.084s
++ set +x
data/Plugs/plugs0b passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/verify_7.7.0/plugs0c.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m13.184s
user 0m20.569s
sys 0m0.111s
++ set +x
data/Plugs/plugs0c passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/verify_7.7.0/plugs0d.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m13.018s
user 0m20.438s
sys 0m0.071s
++ set +x
data/Plugs/plugs0d passed (as expected)
--------------------------------------------------------------------------------------------------
[Execution node] check if [viggen] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Beta/CASREV=7.7,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #725'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS