Started by upstream project "ESP_Beta" build number 731
originally caused by:
 Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on macys in workspace /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-06-24T23:09:07.174 -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 2508

Checking out a fresh workspace because /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-06-24T23:09:07.174 -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 872

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [macys] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[DARWIN64] $ /bin/bash -ex /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/jenkins4641616548449217004.sh
+ bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/ESP_Beta.sh
+ source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export MPLBACKEND=agg
++ MPLBACKEND=agg
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ macys == \r\e\y\n\o\l\d\s ]]
++ [[ DARWIN64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64
++ ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ macys == *\r\e\y\n\o\l\d\s* ]]
++ [[ macys == *\m\a\c\y\s* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
+++ export PATH=/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export pwid_LICENSE=5053@acdl.mit.edu
+++ pwid_LICENSE=5053@acdl.mit.edu
++ [[ macys == *\m\a\c\y\s* ]]
++ export PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys == \m\a\c\y\s ]]
++ echo 'data/fighter4.csm;          ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ echo 'data/fighter4.csm;          ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ echo 'data/fighter4.csm;          ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ 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/DARWIN64/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/udunits/udunits2.xml
++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/ipp/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/ipp/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ [[ macys == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys == \m\a\c\y\s ]]
++ export SEACAS=/Users/jenkins/util/sandialabs/seacas
++ SEACAS=/Users/jenkins/util/sandialabs/seacas
++ [[ macys == \v\i\g\g\e\n ]]
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
+++ 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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ 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/DARWIN64/ESP/DARWIN64/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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ macys == \m\a\c\y\s* ]]
++ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/intercept-*'
++ [[ macys == \m\a\c\y\s ]]
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python-config
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/virtualenv
+++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/analyze-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/analyze-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/analyze-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/intercept-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/intercept-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/intercept-cc
+++ 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/DARWIN64/ESP/DARWIN64/bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB=-L/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'
++ [[ macys == \m\a\c\y\s ]]
++ 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
++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/data
+ virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 568ms
  creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
  seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv)
    added seed packages: pip==24.0, setuptools==70.0.0, wheel==0.43.0
  activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/activate
++ '[' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv
++ '[' darwin22 = cygwin ']'
++ '[' darwin22 = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z '' ']'
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
Collecting pip
  Using cached pip-24.1-py3-none-any.whl.metadata (3.6 kB)
Using cached pip-24.1-py3-none-any.whl (1.8 MB)
Installing collected packages: pip
  Attempting uninstall: pip
    Found existing installation: pip 24.0
    Uninstalling pip-24.0:
      Successfully uninstalled pip-24.0
Successfully installed pip-24.1
+ pip_install f90nml
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
  Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
  Using cached numpy-2.0.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB)
Using cached numpy-2.0.0-cp311-cp311-macosx_10_9_x86_64.whl (21.2 MB)
Installing collected packages: numpy
Successfully installed numpy-2.0.0
+ pip_install openmdao
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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_10_9_x86_64.whl.metadata (61 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-1.14.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB)
Collecting charset-normalizer<4,>=2 (from requests->openmdao)
  Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (33 kB)
Collecting idna<4,>=2.5 (from requests->openmdao)
  Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB)
Collecting urllib3<3,>=1.21.1 (from requests->openmdao)
  Using cached urllib3-2.2.2-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_10_9_x86_64.whl (20.6 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-1.14.0-cp311-cp311-macosx_10_9_x86_64.whl (39.1 MB)
Using cached certifi-2024.6.2-py3-none-any.whl (164 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl (121 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.2-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-1.14.0 urllib3-2.2.2
+ [[ macys == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
  Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl (13.8 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
  Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.1)
+ pip_install matplotlib
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
  Using cached matplotlib-3.9.0-cp311-cp311-macosx_10_12_x86_64.whl.metadata (11 kB)
Collecting contourpy>=1.0.1 (from matplotlib)
  Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.whl.metadata (5.8 kB)
Collecting cycler>=0.10 (from matplotlib)
  Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB)
Collecting fonttools>=4.22.0 (from matplotlib)
  Using cached fonttools-4.53.0-cp311-cp311-macosx_10_9_universal2.whl.metadata (162 kB)
Collecting kiwisolver>=1.3.1 (from matplotlib)
  Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl.metadata (6.4 kB)
Requirement already satisfied: numpy>=1.23 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4)
Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.1)
Collecting pillow>=8 (from matplotlib)
  Using cached pillow-10.3.0-cp311-cp311-macosx_10_10_x86_64.whl.metadata (9.2 kB)
Collecting pyparsing>=2.3.1 (from matplotlib)
  Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB)
Collecting python-dateutil>=2.7 (from matplotlib)
  Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB)
Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib)
  Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB)
Using cached matplotlib-3.9.0-cp311-cp311-macosx_10_12_x86_64.whl (7.9 MB)
Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.whl (262 kB)
Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB)
Using cached fonttools-4.53.0-cp311-cp311-macosx_10_9_universal2.whl (2.8 MB)
Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl (68 kB)
Using cached pillow-10.3.0-cp311-cp311-macosx_10_10_x86_64.whl (3.5 MB)
Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB)
Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.53.0 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/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.14.0)
Requirement already satisfied: numpy<2.3,>=1.23.5 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
--2024-06-24 23:10:04--  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: 272179604 (260M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’

     0K .......... .......... .......... .......... ..........  0% 79.3M 3s
    50K .......... .......... .......... .......... ..........  0% 4.71M 29s
   100K .......... .......... .......... .......... ..........  0% 53.3M 21s
   150K .......... .......... .......... .......... ..........  0% 62.0M 17s
   200K .......... .......... .......... .......... ..........  0% 13.0M 17s
   250K .......... .......... .......... .......... ..........  0% 6.05M 22s
   300K .......... .......... .......... .......... ..........  0% 15.9M 21s
   350K .......... .......... .......... .......... ..........  0% 18.7M 20s
   400K .......... .......... .......... .......... ..........  0% 17.5M 19s
   450K .......... .......... .......... .......... ..........  0% 6.65M 21s
   500K .......... .......... .......... .......... ..........  0% 14.1M 21s
   550K .......... .......... .......... .......... ..........  0% 4.58M 24s
   600K .......... .......... .......... .......... ..........  0% 17.5M 23s
   650K .......... .......... .......... .......... ..........  0% 27.6M 22s
   700K .......... .......... .......... .......... ..........  0% 17.5M 22s
   750K .......... .......... .......... .......... ..........  0% 4.82M 24s
   800K .......... .......... .......... .......... ..........  0% 7.45M 24s
   850K .......... .......... .......... .......... ..........  0% 8.50M 25s
   900K .......... .......... .......... .......... ..........  0% 14.9M 24s
   950K .......... .......... .......... .......... ..........  0% 6.11M 25s
  1000K .......... .......... .......... .......... ..........  0% 13.0M 25s
  1050K .......... .......... .......... .......... ..........  0% 27.6M 24s
  1100K .......... .......... .......... .......... ..........  0% 3.96M 26s
  1150K .......... .......... .......... .......... ..........  0% 4.09M 28s
  1200K .......... .......... .......... .......... ..........  0% 3.94M 29s
  1250K .......... .......... .......... .......... ..........  0% 3.09M 31s
  1300K .......... .......... .......... .......... ..........  0% 9.40M 31s
  1350K .......... .......... .......... .......... ..........  0% 1.13M 38s
  1400K .......... .......... .......... .......... ..........  0% 57.1M 37s
  1450K .......... .......... .......... .......... ..........  0% 50.0M 36s
  1500K .......... .......... .......... .......... ..........  0% 76.5M 35s
  1550K .......... .......... .......... .......... ..........  0% 25.2M 34s
  1600K .......... .......... .......... .......... ..........  0% 6.41M 34s
  1650K .......... .......... .......... .......... ..........  0% 8.87M 34s
  1700K .......... .......... .......... .......... ..........  0% 6.15M 34s
  1750K .......... .......... .......... .......... ..........  0% 10.0M 34s
  1800K .......... .......... .......... .......... ..........  0% 7.02M 34s
  1850K .......... .......... .......... .......... ..........  0% 6.61M 34s
  1900K .......... .......... .......... .......... ..........  0% 5.88M 34s
  1950K .......... .......... .......... .......... ..........  0% 6.55M 35s
  2000K .......... .......... .......... .......... ..........  0% 5.19M 35s
  2050K .......... .......... .......... .......... ..........  0% 5.81M 35s
  2100K .......... .......... .......... .......... ..........  0% 4.34M 36s
  2150K .......... .......... .......... .......... ..........  0% 4.09M 36s
  2200K .......... .......... .......... .......... ..........  0% 11.1M 36s
  2250K .......... .......... .......... .......... ..........  0% 16.5M 36s
  2300K .......... .......... .......... .......... ..........  0% 21.3M 35s
  2350K .......... .......... .......... .......... ..........  0% 13.7M 35s
  2400K .......... .......... .......... .......... ..........  0% 22.4M 34s
  2450K .......... .......... .......... .......... ..........  0% 8.46M 34s
  2500K .......... .......... .......... .......... ..........  0% 16.2M 34s
  2550K .......... .......... .......... .......... ..........  0% 11.6M 34s
  2600K .......... .......... .......... .......... ..........  0% 8.67M 34s
  2650K .......... .......... .......... .......... ..........  1% 9.53M 33s
  2700K .......... .......... .......... .......... ..........  1% 5.19M 34s
  2750K .......... .......... .......... .......... ..........  1% 7.86M 34s
  2800K .......... .......... .......... .......... ..........  1% 9.35M 34s
  2850K .......... .......... .......... .......... ..........  1% 6.22M 34s
  2900K .......... .......... .......... .......... ..........  1% 12.5M 33s
  2950K .......... .......... .......... .......... ..........  1% 3.64M 34s
  3000K .......... .......... .......... .......... ..........  1% 6.26M 34s
  3050K .......... .......... .......... .......... ..........  1% 67.3M 34s
  3100K .......... .......... .......... .......... ..........  1% 54.8M 33s
  3150K .......... .......... .......... .......... ..........  1% 22.1M 33s
  3200K .......... .......... .......... .......... ..........  1% 16.4M 33s
  3250K .......... .......... .......... .......... ..........  1% 15.3M 32s
  3300K .......... .......... .......... .......... ..........  1% 13.6M 32s
  3350K .......... .......... .......... .......... ..........  1% 8.01M 32s
  3400K .......... .......... .......... .......... ..........  1% 7.25M 32s
  3450K .......... .......... .......... .......... ..........  1% 4.35M 33s
  3500K .......... .......... .......... .......... ..........  1% 1.09M 35s
  3550K .......... .......... .......... .......... ..........  1% 1.76M 37s
  3600K .......... .......... .......... .......... ..........  1% 47.7M 36s
  3650K .......... .......... .......... .......... ..........  1% 49.9M 36s
  3700K .......... .......... .......... .......... ..........  1%  862K 40s
  3750K .......... .......... .......... .......... ..........  1% 6.87M 40s
  3800K .......... .......... .......... .......... ..........  1% 6.44M 40s
  3850K .......... .......... .......... .......... ..........  1% 1.20M 42s
  3900K .......... .......... .......... .......... ..........  1% 51.0M 41s
  3950K .......... .......... .......... .......... ..........  1%  670K 46s
  4000K .......... .......... .......... .......... ..........  1%  119M 45s
  4050K .......... .......... .......... .......... ..........  1%  116M 45s
  4100K .......... .......... .......... .......... ..........  1% 7.13M 44s
  4150K .......... .......... .......... .......... ..........  1% 7.86M 44s
  4200K .......... .......... .......... .......... ..........  1% 7.40M 44s
  4250K .......... .......... .......... .......... ..........  1% 8.52M 44s
  4300K .......... .......... .......... .......... ..........  1% 10.3M 44s
  4350K .......... .......... .......... .......... ..........  1% 9.62M 44s
  4400K .......... .......... .......... .......... ..........  1% 11.0M 43s
  4450K .......... .......... .......... .......... ..........  1% 11.0M 43s
  4500K .......... .......... .......... .......... ..........  1% 13.3M 43s
  4550K .......... .......... .......... .......... ..........  1% 14.6M 43s
  4600K .......... .......... .......... .......... ..........  1% 25.7M 42s
  4650K .......... .......... .......... .......... ..........  1% 14.3M 42s
  4700K .......... .......... .......... .......... ..........  1% 19.4M 42s
  4750K .......... .......... .......... .......... ..........  1% 15.2M 41s
  4800K .......... .......... .......... .......... ..........  1% 13.4M 41s
  4850K .......... .......... .......... .......... ..........  1% 12.0M 41s
  4900K .......... .......... .......... .......... ..........  1% 9.44M 41s
  4950K .......... .......... .......... .......... ..........  1% 16.6M 40s
  5000K .......... .......... .......... .......... ..........  1% 12.4M 40s
  5050K .......... .......... .......... .......... ..........  1% 9.13M 40s
  5100K .......... .......... .......... .......... ..........  1% 8.63M 40s
  5150K .......... .......... .......... .......... ..........  1% 6.80M 40s
  5200K .......... .......... .......... .......... ..........  1% 5.21M 40s
  5250K .......... .......... .......... .......... ..........  1% 7.89M 40s
  5300K .......... .......... .......... .......... ..........  2% 7.15M 40s
  5350K .......... .......... .......... .......... ..........  2% 5.66M 40s
  5400K .......... .......... .......... .......... ..........  2% 3.54M 40s
  5450K .......... .......... .......... .......... ..........  2% 1.95M 41s
  5500K .......... .......... .......... .......... ..........  2% 45.2M 41s
  5550K .......... .......... .......... .......... ..........  2% 78.8M 40s
  5600K .......... .......... .......... .......... ..........  2% 5.94M 40s
  5650K .......... .......... .......... .......... ..........  2% 8.93M 40s
  5700K .......... .......... .......... .......... ..........  2% 4.07M 40s
  5750K .......... .......... .......... .......... ..........  2% 56.3M 40s
  5800K .......... .......... .......... .......... ..........  2% 61.1M 40s
  5850K .......... .......... .......... .......... ..........  2% 17.2M 40s
  5900K .......... .......... .......... .......... ..........  2% 11.7M 39s
  5950K .......... .......... .......... .......... ..........  2% 6.27M 39s
  6000K .......... .......... .......... .......... ..........  2% 6.00M 39s
  6050K .......... .......... .......... .......... ..........  2% 23.3M 39s
  6100K .......... .......... .......... .......... ..........  2% 2.04M 40s
  6150K .......... .......... .......... .......... ..........  2% 3.40M 40s
  6200K .......... .......... .......... .......... ..........  2% 6.72M 40s
  6250K .......... .......... .......... .......... ..........  2% 11.2M 40s
  6300K .......... .......... .......... .......... ..........  2% 3.35M 40s
  6350K .......... .......... .......... .......... ..........  2% 15.5M 40s
  6400K .......... .......... .......... .......... ..........  2% 5.76M 40s
  6450K .......... .......... .......... .......... ..........  2% 2.15M 41s
  6500K .......... .......... .......... .......... ..........  2% 14.5M 41s
  6550K .......... .......... .......... .......... ..........  2% 23.8M 40s
  6600K .......... .......... .......... .......... ..........  2% 7.14M 40s
  6650K .......... .......... .......... .......... ..........  2% 44.8M 40s
  6700K .......... .......... .......... .......... ..........  2% 23.6M 40s
  6750K .......... .......... .......... .......... ..........  2% 46.9M 40s
  6800K .......... .......... .......... .......... ..........  2% 14.1M 39s
  6850K .......... .......... .......... .......... ..........  2% 13.3M 39s
  6900K .......... .......... .......... .......... ..........  2% 9.46M 39s
  6950K .......... .......... .......... .......... ..........  2% 16.4M 39s
  7000K .......... .......... .......... .......... ..........  2% 13.4M 39s
  7050K .......... .......... .......... .......... ..........  2% 14.1M 39s
  7100K .......... .......... .......... .......... ..........  2% 9.91M 39s
  7150K .......... .......... .......... .......... ..........  2% 9.16M 38s
  7200K .......... .......... .......... .......... ..........  2% 7.15M 38s
  7250K .......... .......... .......... .......... ..........  2% 6.97M 38s
  7300K .......... .......... .......... .......... ..........  2% 7.05M 38s
  7350K .......... .......... .......... .......... ..........  2% 5.58M 38s
  7400K .......... .......... .......... .......... ..........  2% 7.14M 38s
  7450K .......... .......... .......... .......... ..........  2% 5.85M 38s
  7500K .......... .......... .......... .......... ..........  2% 9.06M 38s
  7550K .......... .......... .......... .......... ..........  2% 16.0M 38s
  7600K .......... .......... .......... .......... ..........  2% 14.8M 38s
  7650K .......... .......... .......... .......... ..........  2% 19.1M 38s
  7700K .......... .......... .......... .......... ..........  2% 14.2M 38s
  7750K .......... .......... .......... .......... ..........  2% 13.7M 38s
  7800K .......... .......... .......... .......... ..........  2% 25.2M 37s
  7850K .......... .......... .......... .......... ..........  2% 10.1M 37s
  7900K .......... .......... .......... .......... ..........  2% 11.4M 37s
  7950K .......... .......... .......... .......... ..........  3% 6.29M 37s
  8000K .......... .......... .......... .......... ..........  3% 7.26M 37s
  8050K .......... .......... .......... .......... ..........  3% 7.08M 37s
  8100K .......... .......... .......... .......... ..........  3% 4.77M 37s
  8150K .......... .......... .......... .......... ..........  3% 3.58M 37s
  8200K .......... .......... .......... .......... ..........  3% 2.40M 38s
  8250K .......... .......... .......... .......... ..........  3% 1.39M 39s
  8300K .......... .......... .......... .......... ..........  3% 1.52M 39s
  8350K .......... .......... .......... .......... ..........  3% 1.65M 40s
  8400K .......... .......... .......... .......... ..........  3% 1.38M 41s
  8450K .......... .......... .......... .......... ..........  3% 3.07M 41s
  8500K .......... .......... .......... .......... ..........  3% 3.04M 41s
  8550K .......... .......... .......... .......... ..........  3% 4.42M 42s
  8600K .......... .......... .......... .......... ..........  3% 10.6M 41s
  8650K .......... .......... .......... .......... ..........  3% 9.80M 41s
  8700K .......... .......... .......... .......... ..........  3% 15.7M 41s
  8750K .......... .......... .......... .......... ..........  3% 10.8M 41s
  8800K .......... .......... .......... .......... ..........  3% 14.1M 41s
  8850K .......... .......... .......... .......... ..........  3% 8.65M 41s
  8900K .......... .......... .......... .......... ..........  3% 7.16M 41s
  8950K .......... .......... .......... .......... ..........  3% 8.03M 41s
  9000K .......... .......... .......... .......... ..........  3% 8.51M 41s
  9050K .......... .......... .......... .......... ..........  3% 12.0M 41s
  9100K .......... .......... .......... .......... ..........  3% 8.30M 40s
  9150K .......... .......... .......... .......... ..........  3% 9.69M 40s
  9200K .......... .......... .......... .......... ..........  3% 8.81M 40s
  9250K .......... .......... .......... .......... ..........  3% 9.14M 40s
  9300K .......... .......... .......... .......... ..........  3% 10.5M 40s
  9350K .......... .......... .......... .......... ..........  3% 6.35M 40s
  9400K .......... .......... .......... .......... ..........  3% 7.67M 40s
  9450K .......... .......... .......... .......... ..........  3% 4.03M 40s
  9500K .......... .......... .......... .......... ..........  3% 5.65M 40s
  9550K .......... .......... .......... .......... ..........  3% 5.23M 40s
  9600K .......... .......... .......... .......... ..........  3% 4.29M 40s
  9650K .......... .......... .......... .......... ..........  3% 9.77M 40s
  9700K .......... .......... .......... .......... ..........  3% 13.8M 40s
  9750K .......... .......... .......... .......... ..........  3% 16.6M 40s
  9800K .......... .......... .......... .......... ..........  3% 11.1M 40s
  9850K .......... .......... .......... .......... ..........  3% 21.0M 40s
  9900K .......... .......... .......... .......... ..........  3% 10.7M 40s
  9950K .......... .......... .......... .......... ..........  3% 19.1M 40s
 10000K .......... .......... .......... .......... ..........  3% 11.1M 39s
 10050K .......... .......... .......... .......... ..........  3% 9.64M 39s
 10100K .......... .......... .......... .......... ..........  3% 9.50M 39s
 10150K .......... .......... .......... .......... ..........  3% 9.60M 39s
 10200K .......... .......... .......... .......... ..........  3% 7.41M 39s
 10250K .......... .......... .......... .......... ..........  3% 11.0M 39s
 10300K .......... .......... .......... .......... ..........  3% 9.48M 39s
 10350K .......... .......... .......... .......... ..........  3% 7.09M 39s
 10400K .......... .......... .......... .......... ..........  3% 7.32M 39s
 10450K .......... .......... .......... .......... ..........  3% 6.16M 39s
 10500K .......... .......... .......... .......... ..........  3% 6.71M 39s
 10550K .......... .......... .......... .......... ..........  3% 6.08M 39s
 10600K .......... .......... .......... .......... ..........  4% 6.13M 39s
 10650K .......... .......... .......... .......... ..........  4% 7.03M 39s
 10700K .......... .......... .......... .......... ..........  4% 5.34M 39s
 10750K .......... .......... .......... .......... ..........  4% 5.29M 39s
 10800K .......... .......... .......... .......... ..........  4% 5.11M 39s
 10850K .......... .......... .......... .......... ..........  4% 4.46M 39s
 10900K .......... .......... .......... .......... ..........  4% 8.08M 39s
 10950K .......... .......... .......... .......... ..........  4% 20.7M 39s
 11000K .......... .......... .......... .......... ..........  4% 10.2M 39s
 11050K .......... .......... .......... .......... ..........  4% 11.8M 39s
 11100K .......... .......... .......... .......... ..........  4% 9.39M 39s
 11150K .......... .......... .......... .......... ..........  4% 10.6M 39s
 11200K .......... .......... .......... .......... ..........  4% 11.7M 39s
 11250K .......... .......... .......... .......... ..........  4% 8.68M 38s
 11300K .......... .......... .......... .......... ..........  4% 9.02M 38s
 11350K .......... .......... .......... .......... ..........  4% 8.07M 38s
 11400K .......... .......... .......... .......... ..........  4% 8.86M 38s
 11450K .......... .......... .......... .......... ..........  4% 8.08M 38s
 11500K .......... .......... .......... .......... ..........  4% 7.17M 38s
 11550K .......... .......... .......... .......... ..........  4% 6.29M 38s
 11600K .......... .......... .......... .......... ..........  4% 5.41M 38s
 11650K .......... .......... .......... .......... ..........  4% 7.20M 38s
 11700K .......... .......... .......... .......... ..........  4% 4.71M 38s
 11750K .......... .......... .......... .......... ..........  4% 5.86M 38s
 11800K .......... .......... .......... .......... ..........  4% 7.20M 38s
 11850K .......... .......... .......... .......... ..........  4% 5.12M 38s
 11900K .......... .......... .......... .......... ..........  4% 5.62M 38s
 11950K .......... .......... .......... .......... ..........  4% 5.05M 38s
 12000K .......... .......... .......... .......... ..........  4% 5.99M 38s
 12050K .......... .......... .......... .......... ..........  4% 15.1M 38s
 12100K .......... .......... .......... .......... ..........  4% 15.2M 38s
 12150K .......... .......... .......... .......... ..........  4% 12.0M 38s
 12200K .......... .......... .......... .......... ..........  4% 26.4M 38s
 12250K .......... .......... .......... .......... ..........  4% 17.3M 38s
 12300K .......... .......... .......... .......... ..........  4% 16.2M 38s
 12350K .......... .......... .......... .......... ..........  4% 13.7M 38s
 12400K .......... .......... .......... .......... ..........  4% 8.82M 38s
 12450K .......... .......... .......... .......... ..........  4% 9.67M 38s
 12500K .......... .......... .......... .......... ..........  4% 12.3M 38s
 12550K .......... .......... .......... .......... ..........  4% 12.7M 37s
 12600K .......... .......... .......... .......... ..........  4% 9.69M 37s
 12650K .......... .......... .......... .......... ..........  4% 11.5M 37s
 12700K .......... .......... .......... .......... ..........  4% 8.00M 37s
 12750K .......... .......... .......... .......... ..........  4% 8.34M 37s
 12800K .......... .......... .......... .......... ..........  4% 5.71M 37s
 12850K .......... .......... .......... .......... ..........  4% 5.02M 37s
 12900K .......... .......... .......... .......... ..........  4% 4.52M 37s
 12950K .......... .......... .......... .......... ..........  4% 4.54M 37s
 13000K .......... .......... .......... .......... ..........  4% 6.06M 37s
 13050K .......... .......... .......... .......... ..........  4% 4.45M 37s
 13100K .......... .......... .......... .......... ..........  4% 3.84M 38s
 13150K .......... .......... .......... .......... ..........  4% 4.14M 38s
 13200K .......... .......... .......... .......... ..........  4% 4.45M 38s
 13250K .......... .......... .......... .......... ..........  5% 14.6M 38s
 13300K .......... .......... .......... .......... ..........  5% 12.4M 38s
 13350K .......... .......... .......... .......... ..........  5% 8.46M 38s
 13400K .......... .......... .......... .......... ..........  5% 7.95M 37s
 13450K .......... .......... .......... .......... ..........  5% 5.73M 37s
 13500K .......... .......... .......... .......... ..........  5% 7.89M 37s
 13550K .......... .......... .......... .......... ..........  5% 5.63M 37s
 13600K .......... .......... .......... .......... ..........  5% 4.40M 38s
 13650K .......... .......... .......... .......... ..........  5% 6.17M 38s
 13700K .......... .......... .......... .......... ..........  5% 3.56M 38s
 13750K .......... .......... .......... .......... ..........  5% 9.73M 38s
 13800K .......... .......... .......... .......... ..........  5% 2.55M 38s
 13850K .......... .......... .......... .......... ..........  5% 1.09M 38s
 13900K .......... .......... .......... .......... ..........  5% 3.14M 39s
 13950K .......... .......... .......... .......... ..........  5% 10.7M 39s
 14000K .......... .......... .......... .......... ..........  5% 10.6M 38s
 14050K .......... .......... .......... .......... ..........  5% 10.7M 38s
 14100K .......... .......... .......... .......... ..........  5% 13.6M 38s
 14150K .......... .......... .......... .......... ..........  5% 11.3M 38s
 14200K .......... .......... .......... .......... ..........  5% 6.69M 38s
 14250K .......... .......... .......... .......... ..........  5% 5.03M 38s
 14300K .......... .......... .......... .......... ..........  5% 11.1M 38s
 14350K .......... .......... .......... .......... ..........  5% 6.71M 38s
 14400K .......... .......... .......... .......... ..........  5% 7.52M 38s
 14450K .......... .......... .......... .......... ..........  5% 7.66M 38s
 14500K .......... .......... .......... .......... ..........  5% 8.89M 38s
 14550K .......... .......... .......... .......... ..........  5% 10.0M 38s
 14600K .......... .......... .......... .......... ..........  5% 13.8M 38s
 14650K .......... .......... .......... .......... ..........  5% 15.6M 38s
 14700K .......... .......... .......... .......... ..........  5% 8.41M 38s
 14750K .......... .......... .......... .......... ..........  5% 14.3M 38s
 14800K .......... .......... .......... .......... ..........  5% 9.81M 38s
 14850K .......... .......... .......... .......... ..........  5% 6.84M 38s
 14900K .......... .......... .......... .......... ..........  5% 11.8M 38s
 14950K .......... .......... .......... .......... ..........  5% 11.5M 38s
 15000K .......... .......... .......... .......... ..........  5% 11.4M 38s
 15050K .......... .......... .......... .......... ..........  5% 14.1M 37s
 15100K .......... .......... .......... .......... ..........  5% 9.17M 37s
 15150K .......... .......... .......... .......... ..........  5% 10.8M 37s
 15200K .......... .......... .......... .......... ..........  5% 9.05M 37s
 15250K .......... .......... .......... .......... ..........  5% 8.40M 37s
 15300K .......... .......... .......... .......... ..........  5% 10.7M 37s
 15350K .......... .......... .......... .......... ..........  5% 4.98M 37s
 15400K .......... .......... .......... .......... ..........  5% 5.48M 37s
 15450K .......... .......... .......... .......... ..........  5% 4.57M 37s
 15500K .......... .......... .......... .......... ..........  5% 4.67M 37s
 15550K .......... .......... .......... .......... ..........  5% 6.00M 37s
 15600K .......... .......... .......... .......... ..........  5% 6.77M 37s
 15650K .......... .......... .......... .......... ..........  5% 5.21M 37s
 15700K .......... .......... .......... .......... ..........  5% 7.63M 37s
 15750K .......... .......... .......... .......... ..........  5% 6.94M 37s
 15800K .......... .......... .......... .......... ..........  5% 5.69M 37s
 15850K .......... .......... .......... .......... ..........  5% 4.07M 37s
 15900K .......... .......... .......... .......... ..........  6% 4.73M 37s
 15950K .......... .......... .......... .......... ..........  6% 3.91M 38s
 16000K .......... .......... .......... .......... ..........  6% 7.06M 38s
 16050K .......... .......... .......... .......... ..........  6% 18.3M 37s
 16100K .......... .......... .......... .......... ..........  6% 7.14M 37s
 16150K .......... .......... .......... .......... ..........  6% 8.22M 37s
 16200K .......... .......... .......... .......... ..........  6% 4.48M 37s
 16250K .......... .......... .......... .......... ..........  6% 5.59M 37s
 16300K .......... .......... .......... .......... ..........  6% 6.10M 37s
 16350K .......... .......... .......... .......... ..........  6% 4.52M 37s
 16400K .......... .......... .......... .......... ..........  6% 6.25M 37s
 16450K .......... .......... .......... .......... ..........  6% 5.50M 37s
 16500K .......... .......... .......... .......... ..........  6% 6.13M 37s
 16550K .......... .......... .......... .......... ..........  6% 6.94M 37s
 16600K .......... .......... .......... .......... ..........  6% 14.4M 37s
 16650K .......... .......... .......... .......... ..........  6% 10.6M 37s
 16700K .......... .......... .......... .......... ..........  6% 8.54M 37s
 16750K .......... .......... .......... .......... ..........  6% 10.1M 37s
 16800K .......... .......... .......... .......... ..........  6% 7.25M 37s
 16850K .......... .......... .......... .......... ..........  6% 7.26M 37s
 16900K .......... .......... .......... .......... ..........  6% 5.07M 37s
 16950K .......... .......... .......... .......... ..........  6% 7.20M 37s
 17000K .......... .......... .......... .......... ..........  6% 4.97M 37s
 17050K .......... .......... .......... .......... ..........  6% 7.89M 37s
 17100K .......... .......... .......... .......... ..........  6% 4.15M 37s
 17150K .......... .......... .......... .......... ..........  6% 4.85M 37s
 17200K .......... .......... .......... .......... ..........  6% 5.21M 37s
 17250K .......... .......... .......... .......... ..........  6% 15.8M 37s
 17300K .......... .......... .......... .......... ..........  6% 15.7M 37s
 17350K .......... .......... .......... .......... ..........  6% 17.5M 37s
 17400K .......... .......... .......... .......... ..........  6% 16.3M 37s
 17450K .......... .......... .......... .......... ..........  6% 13.7M 37s
 17500K .......... .......... .......... .......... ..........  6% 9.42M 37s
 17550K .......... .......... .......... .......... ..........  6% 9.14M 37s
 17600K .......... .......... .......... .......... ..........  6% 5.70M 37s
 17650K .......... .......... .......... .......... ..........  6% 6.52M 37s
 17700K .......... .......... .......... .......... ..........  6% 6.12M 37s
 17750K .......... .......... .......... .......... ..........  6% 6.98M 37s
 17800K .......... .......... .......... .......... ..........  6% 8.71M 37s
 17850K .......... .......... .......... .......... ..........  6% 11.0M 37s
 17900K .......... .......... .......... .......... ..........  6% 18.6M 37s
 17950K .......... .......... .......... .......... ..........  6% 19.7M 37s
 18000K .......... .......... .......... .......... ..........  6% 13.0M 37s
 18050K .......... .......... .......... .......... ..........  6% 13.3M 37s
 18100K .......... .......... .......... .......... ..........  6% 10.4M 37s
 18150K .......... .......... .......... .......... ..........  6% 9.66M 36s
 18200K .......... .......... .......... .......... ..........  6% 9.88M 36s
 18250K .......... .......... .......... .......... ..........  6% 11.3M 36s
 18300K .......... .......... .......... .......... ..........  6% 9.10M 36s
 18350K .......... .......... .......... .......... ..........  6% 9.32M 36s
 18400K .......... .......... .......... .......... ..........  6% 6.77M 36s
 18450K .......... .......... .......... .......... ..........  6% 23.9M 36s
 18500K .......... .......... .......... .......... ..........  6% 6.90M 36s
 18550K .......... .......... .......... .......... ..........  6% 8.51M 36s
 18600K .......... .......... .......... .......... ..........  7% 6.71M 36s
 18650K .......... .......... .......... .......... ..........  7% 9.43M 36s
 18700K .......... .......... .......... .......... ..........  7% 5.64M 36s
 18750K .......... .......... .......... .......... ..........  7% 6.82M 36s
 18800K .......... .......... .......... .......... ..........  7% 8.18M 36s
 18850K .......... .......... .......... .......... ..........  7% 6.93M 36s
 18900K .......... .......... .......... .......... ..........  7% 7.95M 36s
 18950K .......... .......... .......... .......... ..........  7% 5.88M 36s
 19000K .......... .......... .......... .......... ..........  7% 5.04M 36s
 19050K .......... .......... .......... .......... ..........  7% 4.59M 36s
 19100K .......... .......... .......... .......... ..........  7% 4.14M 36s
 19150K .......... .......... .......... .......... ..........  7% 6.78M 36s
 19200K .......... .......... .......... .......... ..........  7% 11.2M 36s
 19250K .......... .......... .......... .......... ..........  7% 13.5M 36s
 19300K .......... .......... .......... .......... ..........  7% 8.77M 36s
 19350K .......... .......... .......... .......... ..........  7% 9.48M 36s
 19400K .......... .......... .......... .......... ..........  7% 11.0M 36s
 19450K .......... .......... .......... .......... ..........  7% 10.4M 36s
 19500K .......... .......... .......... .......... ..........  7% 12.0M 36s
 19550K .......... .......... .......... .......... ..........  7% 9.79M 36s
 19600K .......... .......... .......... .......... ..........  7% 11.0M 36s
 19650K .......... .......... .......... .......... ..........  7% 7.57M 36s
 19700K .......... .......... .......... .......... ..........  7% 7.44M 36s
 19750K .......... .......... .......... .......... ..........  7% 11.2M 36s
 19800K .......... .......... .......... .......... ..........  7% 10.4M 36s
 19850K .......... .......... .......... .......... ..........  7% 7.77M 36s
 19900K .......... .......... .......... .......... ..........  7% 9.77M 36s
 19950K .......... .......... .......... .......... ..........  7% 8.76M 36s
 20000K .......... .......... .......... .......... ..........  7% 8.38M 36s
 20050K .......... .......... .......... .......... ..........  7% 13.7M 36s
 20100K .......... .......... .......... .......... ..........  7% 9.23M 36s
 20150K .......... .......... .......... .......... ..........  7% 9.44M 35s
 20200K .......... .......... .......... .......... ..........  7% 8.38M 35s
 20250K .......... .......... .......... .......... ..........  7% 11.4M 35s
 20300K .......... .......... .......... .......... ..........  7% 11.7M 35s
 20350K .......... .......... .......... .......... ..........  7% 9.41M 35s
 20400K .......... .......... .......... .......... ..........  7% 7.62M 35s
 20450K .......... .......... .......... .......... ..........  7% 8.18M 35s
 20500K .......... .......... .......... .......... ..........  7% 8.87M 35s
 20550K .......... .......... .......... .......... ..........  7% 6.99M 35s
 20600K .......... .......... .......... .......... ..........  7% 5.86M 35s
 20650K .......... .......... .......... .......... ..........  7% 5.37M 35s
 20700K .......... .......... .......... .......... ..........  7% 3.51M 35s
 20750K .......... .......... .......... .......... ..........  7% 2.21M 36s
 20800K .......... .......... .......... .......... ..........  7% 2.81M 36s
 20850K .......... .......... .......... .......... ..........  7% 10.3M 36s
 20900K .......... .......... .......... .......... ..........  7% 8.08M 36s
 20950K .......... .......... .......... .......... ..........  7% 10.7M 36s
 21000K .......... .......... .......... .......... ..........  7% 8.65M 36s
 21050K .......... .......... .......... .......... ..........  7% 5.82M 36s
 21100K .......... .......... .......... .......... ..........  7% 3.96M 36s
 21150K .......... .......... .......... .......... ..........  7% 4.10M 36s
 21200K .......... .......... .......... .......... ..........  7% 4.23M 36s
 21250K .......... .......... .......... .......... ..........  8% 9.66M 36s
 21300K .......... .......... .......... .......... ..........  8% 9.24M 36s
 21350K .......... .......... .......... .......... ..........  8% 30.1M 36s
 21400K .......... .......... .......... .......... ..........  8% 10.4M 35s
 21450K .......... .......... .......... .......... ..........  8% 10.3M 35s
 21500K .......... .......... .......... .......... ..........  8% 6.49M 35s
 21550K .......... .......... .......... .......... ..........  8% 8.26M 35s
 21600K .......... .......... .......... .......... ..........  8% 6.99M 35s
 21650K .......... .......... .......... .......... ..........  8% 6.04M 35s
 21700K .......... .......... .......... .......... ..........  8% 8.43M 35s
 21750K .......... .......... .......... .......... ..........  8% 7.31M 35s
 21800K .......... .......... .......... .......... ..........  8% 6.82M 35s
 21850K .......... .......... .......... .......... ..........  8% 5.27M 35s
 21900K .......... .......... .......... .......... ..........  8% 5.40M 35s
 21950K .......... .......... .......... .......... ..........  8% 4.86M 35s
 22000K .......... .......... .......... .......... ..........  8% 5.72M 35s
 22050K .......... .......... .......... .......... ..........  8% 5.37M 35s
 22100K .......... .......... .......... .......... ..........  8% 5.45M 35s
 22150K .......... .......... .......... .......... ..........  8% 5.08M 35s
 22200K .......... .......... .......... .......... ..........  8% 3.43M 36s
 22250K .......... .......... .......... .......... ..........  8% 4.37M 36s
 22300K .......... .......... .......... .......... ..........  8% 5.38M 36s
 22350K .......... .......... .......... .......... ..........  8% 10.1M 36s
 22400K .......... .......... .......... .......... ..........  8% 24.4M 35s
 22450K .......... .......... .......... .......... ..........  8% 15.6M 35s
 22500K .......... .......... .......... .......... ..........  8% 16.7M 35s
 22550K .......... .......... .......... .......... ..........  8% 22.8M 35s
 22600K .......... .......... .......... .......... ..........  8% 14.1M 35s
 22650K .......... .......... .......... .......... ..........  8% 11.5M 35s
 22700K .......... .......... .......... .......... ..........  8% 9.65M 35s
 22750K .......... .......... .......... .......... ..........  8% 9.96M 35s
 22800K .......... .......... .......... .......... ..........  8% 11.2M 35s
 22850K .......... .......... .......... .......... ..........  8% 7.64M 35s
 22900K .......... .......... .......... .......... ..........  8% 10.2M 35s
 22950K .......... .......... .......... .......... ..........  8% 6.92M 35s
 23000K .......... .......... .......... .......... ..........  8% 6.02M 35s
 23050K .......... .......... .......... .......... ..........  8% 8.34M 35s
 23100K .......... .......... .......... .......... ..........  8% 4.63M 35s
 23150K .......... .......... .......... .......... ..........  8% 8.82M 35s
 23200K .......... .......... .......... .......... ..........  8% 4.40M 35s
 23250K .......... .......... .......... .......... ..........  8% 6.77M 35s
 23300K .......... .......... .......... .......... ..........  8% 6.41M 35s
 23350K .......... .......... .......... .......... ..........  8% 6.41M 35s
 23400K .......... .......... .......... .......... ..........  8% 4.99M 35s
 23450K .......... .......... .......... .......... ..........  8% 4.75M 35s
 23500K .......... .......... .......... .......... ..........  8% 5.36M 35s
 23550K .......... .......... .......... .......... ..........  8% 4.42M 35s
 23600K .......... .......... .......... .......... ..........  8% 8.43M 35s
 23650K .......... .......... .......... .......... ..........  8% 17.9M 35s
 23700K .......... .......... .......... .......... ..........  8% 16.7M 35s
 23750K .......... .......... .......... .......... ..........  8% 10.3M 35s
 23800K .......... .......... .......... .......... ..........  8% 37.3M 35s
 23850K .......... .......... .......... .......... ..........  8% 13.5M 35s
 23900K .......... .......... .......... .......... ..........  9% 13.8M 35s
 23950K .......... .......... .......... .......... ..........  9% 7.18M 35s
 24000K .......... .......... .......... .......... ..........  9% 8.89M 35s
 24050K .......... .......... .......... .......... ..........  9% 5.54M 35s
 24100K .......... .......... .......... .......... ..........  9% 5.46M 35s
 24150K .......... .......... .......... .......... ..........  9% 6.54M 35s
 24200K .......... .......... .......... .......... ..........  9% 5.68M 35s
 24250K .......... .......... .......... .......... ..........  9% 6.57M 35s
 24300K .......... .......... .......... .......... ..........  9% 12.6M 35s
 24350K .......... .......... .......... .......... ..........  9% 16.1M 35s
 24400K .......... .......... .......... .......... ..........  9% 15.4M 35s
 24450K .......... .......... .......... .......... ..........  9% 9.52M 35s
 24500K .......... .......... .......... .......... ..........  9% 10.8M 35s
 24550K .......... .......... .......... .......... ..........  9% 7.91M 35s
 24600K .......... .......... .......... .......... ..........  9% 8.46M 35s
 24650K .......... .......... .......... .......... ..........  9% 11.2M 35s
 24700K .......... .......... .......... .......... ..........  9% 7.94M 35s
 24750K .......... .......... .......... .......... ..........  9% 10.4M 35s
 24800K .......... .......... .......... .......... ..........  9% 10.8M 34s
 24850K .......... .......... .......... .......... ..........  9% 17.6M 34s
 24900K .......... .......... .......... .......... ..........  9% 20.2M 34s
 24950K .......... .......... .......... .......... ..........  9% 13.7M 34s
 25000K .......... .......... .......... .......... ..........  9% 13.9M 34s
 25050K .......... .......... .......... .......... ..........  9% 15.8M 34s
 25100K .......... .......... .......... .......... ..........  9% 8.03M 34s
 25150K .......... .......... .......... .......... ..........  9% 10.6M 34s
 25200K .......... .......... .......... .......... ..........  9% 8.76M 34s
 25250K .......... .......... .......... .......... ..........  9% 10.2M 34s
 25300K .......... .......... .......... .......... ..........  9% 10.7M 34s
 25350K .......... .......... .......... .......... ..........  9% 9.74M 34s
 25400K .......... .......... .......... .......... ..........  9% 10.8M 34s
 25450K .......... .......... .......... .......... ..........  9% 7.33M 34s
 25500K .......... .......... .......... .......... ..........  9% 8.39M 34s
 25550K .......... .......... .......... .......... ..........  9% 7.18M 34s
 25600K .......... .......... .......... .......... ..........  9% 4.56M 34s
 25650K .......... .......... .......... .......... ..........  9% 5.81M 34s
 25700K .......... .......... .......... .......... ..........  9% 4.43M 34s
 25750K .......... .......... .......... .......... ..........  9% 5.60M 34s
 25800K .......... .......... .......... .......... ..........  9% 17.0M 34s
 25850K .......... .......... .......... .......... ..........  9% 16.8M 34s
 25900K .......... .......... .......... .......... ..........  9% 18.8M 34s
 25950K .......... .......... .......... .......... ..........  9% 23.6M 34s
 26000K .......... .......... .......... .......... ..........  9% 14.0M 34s
 26050K .......... .......... .......... .......... ..........  9% 21.5M 34s
 26100K .......... .......... .......... .......... ..........  9% 12.4M 34s
 26150K .......... .......... .......... .......... ..........  9% 19.0M 34s
 26200K .......... .......... .......... .......... ..........  9% 14.7M 34s
 26250K .......... .......... .......... .......... ..........  9% 12.5M 34s
 26300K .......... .......... .......... .......... ..........  9% 8.87M 34s
 26350K .......... .......... .......... .......... ..........  9% 11.4M 34s
 26400K .......... .......... .......... .......... ..........  9% 13.4M 34s
 26450K .......... .......... .......... .......... ..........  9% 7.44M 34s
 26500K .......... .......... .......... .......... ..........  9% 6.92M 34s
 26550K .......... .......... .......... .......... .......... 10% 8.45M 34s
 26600K .......... .......... .......... .......... .......... 10% 6.91M 34s
 26650K .......... .......... .......... .......... .......... 10% 8.42M 33s
 26700K .......... .......... .......... .......... .......... 10% 7.79M 33s
 26750K .......... .......... .......... .......... .......... 10% 16.7M 33s
 26800K .......... .......... .......... .......... .......... 10% 21.8M 33s
 26850K .......... .......... .......... .......... .......... 10% 12.3M 33s
 26900K .......... .......... .......... .......... .......... 10% 28.6M 33s
 26950K .......... .......... .......... .......... .......... 10% 18.0M 33s
 27000K .......... .......... .......... .......... .......... 10% 14.6M 33s
 27050K .......... .......... .......... .......... .......... 10% 23.7M 33s
 27100K .......... .......... .......... .......... .......... 10% 15.0M 33s
 27150K .......... .......... .......... .......... .......... 10% 11.1M 33s
 27200K .......... .......... .......... .......... .......... 10% 15.6M 33s
 27250K .......... .......... .......... .......... .......... 10% 8.29M 33s
 27300K .......... .......... .......... .......... .......... 10% 7.21M 33s
 27350K .......... .......... .......... .......... .......... 10% 4.57M 33s
 27400K .......... .......... .......... .......... .......... 10% 5.22M 33s
 27450K .......... .......... .......... .......... .......... 10% 3.70M 33s
 27500K .......... .......... .......... .......... .......... 10% 3.59M 33s
 27550K .......... .......... .......... .......... .......... 10% 6.30M 33s
 27600K .......... .......... .......... .......... .......... 10% 4.81M 33s
 27650K .......... .......... .......... .......... .......... 10% 6.16M 33s
 27700K .......... .......... .......... .......... .......... 10% 6.03M 33s
 27750K .......... .......... .......... .......... .......... 10% 5.10M 33s
 27800K .......... .......... .......... .......... .......... 10% 4.89M 33s
 27850K .......... .......... .......... .......... .......... 10% 4.23M 33s
 27900K .......... .......... .......... .......... .......... 10% 3.74M 33s
 27950K .......... .......... .......... .......... .......... 10% 4.89M 33s
 28000K .......... .......... .......... .......... .......... 10% 15.2M 33s
 28050K .......... .......... .......... .......... .......... 10% 24.8M 33s
 28100K .......... .......... .......... .......... .......... 10% 17.2M 33s
 28150K .......... .......... .......... .......... .......... 10% 22.8M 33s
 28200K .......... .......... .......... .......... .......... 10% 13.1M 33s
 28250K .......... .......... .......... .......... .......... 10% 13.8M 33s
 28300K .......... .......... .......... .......... .......... 10% 8.73M 33s
 28350K .......... .......... .......... .......... .......... 10% 5.66M 33s
 28400K .......... .......... .......... .......... .......... 10% 9.55M 33s
 28450K .......... .......... .......... .......... .......... 10% 6.24M 33s
 28500K .......... .......... .......... .......... .......... 10% 9.04M 33s
 28550K .......... .......... .......... .......... .......... 10% 7.06M 33s
 28600K .......... .......... .......... .......... .......... 10% 6.07M 33s
 28650K .......... .......... .......... .......... .......... 10% 7.94M 33s
 28700K .......... .......... .......... .......... .......... 10% 5.87M 33s
 28750K .......... .......... .......... .......... .......... 10% 6.76M 33s
 28800K .......... .......... .......... .......... .......... 10% 5.91M 33s
 28850K .......... .......... .......... .......... .......... 10% 4.03M 33s
 28900K .......... .......... .......... .......... .......... 10% 4.40M 33s
 28950K .......... .......... .......... .......... .......... 10% 5.78M 33s
 29000K .......... .......... .......... .......... .......... 10% 7.37M 33s
 29050K .......... .......... .......... .......... .......... 10% 6.36M 33s
 29100K .......... .......... .......... .......... .......... 10% 4.52M 33s
 29150K .......... .......... .......... .......... .......... 10% 5.46M 33s
 29200K .......... .......... .......... .......... .......... 11% 4.60M 33s
 29250K .......... .......... .......... .......... .......... 11% 3.95M 33s
 29300K .......... .......... .......... .......... .......... 11% 4.12M 33s
 29350K .......... .......... .......... .......... .......... 11% 3.60M 33s
 29400K .......... .......... .......... .......... .......... 11% 12.6M 33s
 29450K .......... .......... .......... .......... .......... 11% 8.97M 33s
 29500K .......... .......... .......... .......... .......... 11% 67.6M 33s
 29550K .......... .......... .......... .......... .......... 11% 12.5M 33s
 29600K .......... .......... .......... .......... .......... 11% 10.4M 33s
 29650K .......... .......... .......... .......... .......... 11% 13.6M 33s
 29700K .......... .......... .......... .......... .......... 11% 7.96M 33s
 29750K .......... .......... .......... .......... .......... 11% 7.45M 33s
 29800K .......... .......... .......... .......... .......... 11% 8.35M 33s
 29850K .......... .......... .......... .......... .......... 11% 7.53M 33s
 29900K .......... .......... .......... .......... .......... 11% 7.92M 33s
 29950K .......... .......... .......... .......... .......... 11% 7.88M 33s
 30000K .......... .......... .......... .......... .......... 11% 6.54M 33s
 30050K .......... .......... .......... .......... .......... 11% 8.81M 33s
 30100K .......... .......... .......... .......... .......... 11% 5.37M 33s
 30150K .......... .......... .......... .......... .......... 11% 4.14M 33s
 30200K .......... .......... .......... .......... .......... 11% 4.01M 33s
 30250K .......... .......... .......... .......... .......... 11% 3.57M 33s
 30300K .......... .......... .......... .......... .......... 11% 4.41M 33s
 30350K .......... .......... .......... .......... .......... 11% 3.40M 33s
 30400K .......... .......... .......... .......... .......... 11% 3.61M 33s
 30450K .......... .......... .......... .......... .......... 11% 3.46M 33s
 30500K .......... .......... .......... .......... .......... 11% 7.40M 33s
 30550K .......... .......... .......... .......... .......... 11% 17.1M 33s
 30600K .......... .......... .......... .......... .......... 11% 13.7M 33s
 30650K .......... .......... .......... .......... .......... 11% 12.7M 33s
 30700K .......... .......... .......... .......... .......... 11% 11.1M 33s
 30750K .......... .......... .......... .......... .......... 11% 9.46M 33s
 30800K .......... .......... .......... .......... .......... 11% 7.87M 33s
 30850K .......... .......... .......... .......... .......... 11% 6.58M 33s
 30900K .......... .......... .......... .......... .......... 11% 10.1M 33s
 30950K .......... .......... .......... .......... .......... 11% 7.49M 33s
 31000K .......... .......... .......... .......... .......... 11% 8.94M 33s
 31050K .......... .......... .......... .......... .......... 11% 4.64M 33s
 31100K .......... .......... .......... .......... .......... 11% 5.22M 33s
 31150K .......... .......... .......... .......... .......... 11% 5.26M 33s
 31200K .......... .......... .......... .......... .......... 11% 4.94M 33s
 31250K .......... .......... .......... .......... .......... 11% 11.6M 33s
 31300K .......... .......... .......... .......... .......... 11% 14.1M 33s
 31350K .......... .......... .......... .......... .......... 11% 14.8M 33s
 31400K .......... .......... .......... .......... .......... 11% 15.4M 33s
 31450K .......... .......... .......... .......... .......... 11% 15.3M 33s
 31500K .......... .......... .......... .......... .......... 11% 11.3M 33s
 31550K .......... .......... .......... .......... .......... 11% 23.9M 33s
 31600K .......... .......... .......... .......... .......... 11% 8.17M 33s
 31650K .......... .......... .......... .......... .......... 11% 13.1M 33s
 31700K .......... .......... .......... .......... .......... 11% 10.9M 33s
 31750K .......... .......... .......... .......... .......... 11% 14.2M 33s
 31800K .......... .......... .......... .......... .......... 11% 13.7M 33s
 31850K .......... .......... .......... .......... .......... 12% 7.14M 33s
 31900K .......... .......... .......... .......... .......... 12% 8.69M 33s
 31950K .......... .......... .......... .......... .......... 12% 5.97M 33s
 32000K .......... .......... .......... .......... .......... 12% 8.05M 33s
 32050K .......... .......... .......... .......... .......... 12% 6.94M 33s
 32100K .......... .......... .......... .......... .......... 12% 8.14M 33s
 32150K .......... .......... .......... .......... .......... 12% 9.72M 33s
 32200K .......... .......... .......... .......... .......... 12% 82.1M 33s
 32250K .......... .......... .......... .......... .......... 12% 12.5M 32s
 32300K .......... .......... .......... .......... .......... 12% 15.0M 32s
 32350K .......... .......... .......... .......... .......... 12% 10.7M 32s
 32400K .......... .......... .......... .......... .......... 12% 13.9M 32s
 32450K .......... .......... .......... .......... .......... 12% 12.7M 32s
 32500K .......... .......... .......... .......... .......... 12% 11.2M 32s
 32550K .......... .......... .......... .......... .......... 12% 13.4M 32s
 32600K .......... .......... .......... .......... .......... 12% 7.75M 32s
 32650K .......... .......... .......... .......... .......... 12% 6.72M 32s
 32700K .......... .......... .......... .......... .......... 12% 9.01M 32s
 32750K .......... .......... .......... .......... .......... 12% 7.62M 32s
 32800K .......... .......... .......... .......... .......... 12% 9.20M 32s
 32850K .......... .......... .......... .......... .......... 12% 8.52M 32s
 32900K .......... .......... .......... .......... .......... 12% 7.70M 32s
 32950K .......... .......... .......... .......... .......... 12% 6.62M 32s
 33000K .......... .......... .......... .......... .......... 12% 6.44M 32s
 33050K .......... .......... .......... .......... .......... 12% 8.12M 32s
 33100K .......... .......... .......... .......... .......... 12% 7.75M 32s
 33150K .......... .......... .......... .......... .......... 12% 13.1M 32s
 33200K .......... .......... .......... .......... .......... 12% 7.96M 32s
 33250K .......... .......... .......... .......... .......... 12% 22.7M 32s
 33300K .......... .......... .......... .......... .......... 12% 9.31M 32s
 33350K .......... .......... .......... .......... .......... 12% 6.89M 32s
 33400K .......... .......... .......... .......... .......... 12% 9.74M 32s
 33450K .......... .......... .......... .......... .......... 12% 6.53M 32s
 33500K .......... .......... .......... .......... .......... 12% 8.59M 32s
 33550K .......... .......... .......... .......... .......... 12% 7.53M 32s
 33600K .......... .......... .......... .......... .......... 12% 5.18M 32s
 33650K .......... .......... .......... .......... .......... 12% 6.80M 32s
 33700K .......... .......... .......... .......... .......... 12% 4.24M 32s
 33750K .......... .......... .......... .......... .......... 12% 4.89M 32s
 33800K .......... .......... .......... .......... .......... 12%  217K 34s
 33850K .......... .......... .......... .......... .......... 12% 1.62M 34s
 33900K .......... .......... .......... .......... .......... 12% 2.94M 34s
 33950K .......... .......... .......... .......... .......... 12% 3.44M 34s
 34000K .......... .......... .......... .......... .......... 12% 4.60M 34s
 34050K .......... .......... .......... .......... .......... 12% 10.7M 34s
 34100K .......... .......... .......... .......... .......... 12% 8.47M 34s
 34150K .......... .......... .......... .......... .......... 12% 10.5M 34s
 34200K .......... .......... .......... .......... .......... 12% 8.12M 34s
 34250K .......... .......... .......... .......... .......... 12% 6.86M 34s
 34300K .......... .......... .......... .......... .......... 12% 7.20M 34s
 34350K .......... .......... .......... .......... .......... 12% 6.18M 34s
 34400K .......... .......... .......... .......... .......... 12% 8.72M 34s
 34450K .......... .......... .......... .......... .......... 12% 6.69M 34s
 34500K .......... .......... .......... .......... .......... 12% 7.85M 34s
 34550K .......... .......... .......... .......... .......... 13% 6.94M 34s
 34600K .......... .......... .......... .......... .......... 13% 5.39M 34s
 34650K .......... .......... .......... .......... .......... 13% 4.36M 34s
 34700K .......... .......... .......... .......... .......... 13% 4.21M 34s
 34750K .......... .......... .......... .......... .......... 13% 4.49M 34s
 34800K .......... .......... .......... .......... .......... 13% 3.45M 34s
 34850K .......... .......... .......... .......... .......... 13% 3.31M 34s
 34900K .......... .......... .......... .......... .......... 13% 4.74M 34s
 34950K .......... .......... .......... .......... .......... 13% 5.40M 34s
 35000K .......... .......... .......... .......... .......... 13% 7.22M 34s
 35050K .......... .......... .......... .......... .......... 13% 5.69M 34s
 35100K .......... .......... .......... .......... .......... 13% 6.97M 34s
 35150K .......... .......... .......... .......... .......... 13% 7.48M 34s
 35200K .......... .......... .......... .......... .......... 13% 6.28M 34s
 35250K .......... .......... .......... .......... .......... 13% 6.55M 34s
 35300K .......... .......... .......... .......... .......... 13% 9.28M 34s
 35350K .......... .......... .......... .......... .......... 13% 18.5M 34s
 35400K .......... .......... .......... .......... .......... 13% 20.1M 34s
 35450K .......... .......... .......... .......... .......... 13% 32.4M 34s
 35500K .......... .......... .......... .......... .......... 13% 17.6M 34s
 35550K .......... .......... .......... .......... .......... 13% 17.0M 34s
 35600K .......... .......... .......... .......... .......... 13% 12.0M 34s
 35650K .......... .......... .......... .......... .......... 13% 13.6M 34s
 35700K .......... .......... .......... .......... .......... 13% 10.1M 34s
 35750K .......... .......... .......... .......... .......... 13% 12.3M 34s
 35800K .......... .......... .......... .......... .......... 13% 14.0M 33s
 35850K .......... .......... .......... .......... .......... 13% 9.11M 33s
 35900K .......... .......... .......... .......... .......... 13% 8.14M 33s
 35950K .......... .......... .......... .......... .......... 13% 8.87M 33s
 36000K .......... .......... .......... .......... .......... 13% 8.31M 33s
 36050K .......... .......... .......... .......... .......... 13% 6.97M 33s
 36100K .......... .......... .......... .......... .......... 13% 5.00M 33s
 36150K .......... .......... .......... .......... .......... 13% 6.71M 33s
 36200K .......... .......... .......... .......... .......... 13% 14.5M 33s
 36250K .......... .......... .......... .......... .......... 13% 15.1M 33s
 36300K .......... .......... .......... .......... .......... 13% 23.7M 33s
 36350K .......... .......... .......... .......... .......... 13% 16.9M 33s
 36400K .......... .......... .......... .......... .......... 13% 17.3M 33s
 36450K .......... .......... .......... .......... .......... 13% 10.4M 33s
 36500K .......... .......... .......... .......... .......... 13% 26.6M 33s
 36550K .......... .......... .......... .......... .......... 13% 9.08M 33s
 36600K .......... .......... .......... .......... .......... 13% 7.57M 33s
 36650K .......... .......... .......... .......... .......... 13% 8.66M 33s
 36700K .......... .......... .......... .......... .......... 13% 7.49M 33s
 36750K .......... .......... .......... .......... .......... 13% 9.22M 33s
 36800K .......... .......... .......... .......... .......... 13% 7.73M 33s
 36850K .......... .......... .......... .......... .......... 13% 5.81M 33s
 36900K .......... .......... .......... .......... .......... 13% 7.62M 33s
 36950K .......... .......... .......... .......... .......... 13% 5.83M 33s
 37000K .......... .......... .......... .......... .......... 13% 4.48M 33s
 37050K .......... .......... .......... .......... .......... 13% 5.20M 33s
 37100K .......... .......... .......... .......... .......... 13% 4.37M 33s
 37150K .......... .......... .......... .......... .......... 13% 6.66M 33s
 37200K .......... .......... .......... .......... .......... 14% 7.04M 33s
 37250K .......... .......... .......... .......... .......... 14% 7.90M 33s
 37300K .......... .......... .......... .......... .......... 14% 4.83M 33s
 37350K .......... .......... .......... .......... .......... 14% 4.56M 33s
 37400K .......... .......... .......... .......... .......... 14% 5.02M 33s
 37450K .......... .......... .......... .......... .......... 14% 3.44M 33s
 37500K .......... .......... .......... .......... .......... 14% 3.39M 33s
 37550K .......... .......... .......... .......... .......... 14% 6.42M 33s
 37600K .......... .......... .......... .......... .......... 14% 6.39M 33s
 37650K .......... .......... .......... .......... .......... 14% 5.95M 33s
 37700K .......... .......... .......... .......... .......... 14% 5.58M 33s
 37750K .......... .......... .......... .......... .......... 14% 5.38M 33s
 37800K .......... .......... .......... .......... .......... 14% 5.22M 33s
 37850K .......... .......... .......... .......... .......... 14% 3.12M 33s
 37900K .......... .......... .......... .......... .......... 14% 2.95M 33s
 37950K .......... .......... .......... .......... .......... 14% 1.65M 33s
 38000K .......... .......... .......... .......... .......... 14% 1.95M 33s
 38050K .......... .......... .......... .......... .......... 14% 2.43M 34s
 38100K .......... .......... .......... .......... .......... 14% 2.62M 34s
 38150K .......... .......... .......... .......... .......... 14% 12.2M 34s
 38200K .......... .......... .......... .......... .......... 14% 10.3M 34s
 38250K .......... .......... .......... .......... .......... 14% 14.7M 34s
 38300K .......... .......... .......... .......... .......... 14% 11.5M 34s
 38350K .......... .......... .......... .......... .......... 14% 7.94M 33s
 38400K .......... .......... .......... .......... .......... 14% 9.71M 33s
 38450K .......... .......... .......... .......... .......... 14% 7.52M 33s
 38500K .......... .......... .......... .......... .......... 14% 8.04M 33s
 38550K .......... .......... .......... .......... .......... 14% 6.71M 33s
 38600K .......... .......... .......... .......... .......... 14% 5.58M 33s
 38650K .......... .......... .......... .......... .......... 14% 6.23M 33s
 38700K .......... .......... .......... .......... .......... 14% 5.56M 33s
 38750K .......... .......... .......... .......... .......... 14% 5.55M 33s
 38800K .......... .......... .......... .......... .......... 14% 3.36M 33s
 38850K .......... .......... .......... .......... .......... 14% 1.95M 34s
 38900K .......... .......... .......... .......... .......... 14% 1.46M 34s
 38950K .......... .......... .......... .......... .......... 14% 5.53M 34s
 39000K .......... .......... .......... .......... .......... 14% 5.71M 34s
 39050K .......... .......... .......... .......... .......... 14% 5.29M 34s
 39100K .......... .......... .......... .......... .......... 14% 5.81M 34s
 39150K .......... .......... .......... .......... .......... 14% 10.1M 34s
 39200K .......... .......... .......... .......... .......... 14% 13.0M 34s
 39250K .......... .......... .......... .......... .......... 14% 8.57M 34s
 39300K .......... .......... .......... .......... .......... 14% 8.13M 34s
 39350K .......... .......... .......... .......... .......... 14% 8.43M 34s
 39400K .......... .......... .......... .......... .......... 14% 9.53M 34s
 39450K .......... .......... .......... .......... .......... 14% 7.59M 34s
 39500K .......... .......... .......... .......... .......... 14% 9.66M 34s
 39550K .......... .......... .......... .......... .......... 14% 6.92M 34s
 39600K .......... .......... .......... .......... .......... 14% 15.0M 34s
 39650K .......... .......... .......... .......... .......... 14% 9.09M 33s
 39700K .......... .......... .......... .......... .......... 14% 7.38M 33s
 39750K .......... .......... .......... .......... .......... 14% 7.31M 33s
 39800K .......... .......... .......... .......... .......... 14% 6.98M 33s
 39850K .......... .......... .......... .......... .......... 15% 6.37M 33s
 39900K .......... .......... .......... .......... .......... 15% 9.00M 33s
 39950K .......... .......... .......... .......... .......... 15% 10.4M 33s
 40000K .......... .......... .......... .......... .......... 15% 47.6M 33s
 40050K .......... .......... .......... .......... .......... 15% 15.1M 33s
 40100K .......... .......... .......... .......... .......... 15% 13.4M 33s
 40150K .......... .......... .......... .......... .......... 15% 12.0M 33s
 40200K .......... .......... .......... .......... .......... 15% 10.8M 33s
 40250K .......... .......... .......... .......... .......... 15% 7.87M 33s
 40300K .......... .......... .......... .......... .......... 15% 9.55M 33s
 40350K .......... .......... .......... .......... .......... 15% 7.16M 33s
 40400K .......... .......... .......... .......... .......... 15% 7.64M 33s
 40450K .......... .......... .......... .......... .......... 15% 6.84M 33s
 40500K .......... .......... .......... .......... .......... 15% 7.68M 33s
 40550K .......... .......... .......... .......... .......... 15% 5.59M 33s
 40600K .......... .......... .......... .......... .......... 15% 6.39M 33s
 40650K .......... .......... .......... .......... .......... 15% 8.06M 33s
 40700K .......... .......... .......... .......... .......... 15% 7.22M 33s
 40750K .......... .......... .......... .......... .......... 15% 4.90M 33s
 40800K .......... .......... .......... .......... .......... 15% 4.54M 33s
 40850K .......... .......... .......... .......... .......... 15% 4.22M 33s
 40900K .......... .......... .......... .......... .......... 15% 5.00M 33s
 40950K .......... .......... .......... .......... .......... 15% 8.87M 33s
 41000K .......... .......... .......... .......... .......... 15% 8.55M 33s
 41050K .......... .......... .......... .......... .......... 15% 6.91M 33s
 41100K .......... .......... .......... .......... .......... 15% 6.05M 33s
 41150K .......... .......... .......... .......... .......... 15% 7.41M 33s
 41200K .......... .......... .......... .......... .......... 15% 4.62M 33s
 41250K .......... .......... .......... .......... .......... 15% 6.97M 33s
 41300K .......... .......... .......... .......... .......... 15% 5.38M 33s
 41350K .......... .......... .......... .......... .......... 15% 3.57M 33s
 41400K .......... .......... .......... .......... .......... 15% 3.43M 33s
 41450K .......... .......... .......... .......... .......... 15% 3.30M 33s
 41500K .......... .......... .......... .......... .......... 15% 3.77M 33s
 41550K .......... .......... .......... .......... .......... 15% 2.70M 33s
 41600K .......... .......... .......... .......... .......... 15% 2.79M 33s
 41650K .......... .......... .......... .......... .......... 15% 10.7M 33s
 41700K .......... .......... .......... .......... .......... 15% 16.3M 33s
 41750K .......... .......... .......... .......... .......... 15% 11.6M 33s
 41800K .......... .......... .......... .......... .......... 15% 31.5M 33s
 41850K .......... .......... .......... .......... .......... 15% 9.57M 33s
 41900K .......... .......... .......... .......... .......... 15% 11.4M 33s
 41950K .......... .......... .......... .......... .......... 15% 6.86M 33s
 42000K .......... .......... .......... .......... .......... 15% 49.2M 33s
 42050K .......... .......... .......... .......... .......... 15% 12.2M 33s
 42100K .......... .......... .......... .......... .......... 15% 13.1M 33s
 42150K .......... .......... .......... .......... .......... 15% 9.08M 33s
 42200K .......... .......... .......... .......... .......... 15% 8.46M 33s
 42250K .......... .......... .......... .......... .......... 15% 10.0M 33s
 42300K .......... .......... .......... .......... .......... 15% 11.0M 33s
 42350K .......... .......... .......... .......... .......... 15% 7.63M 33s
 42400K .......... .......... .......... .......... .......... 15% 8.86M 33s
 42450K .......... .......... .......... .......... .......... 15% 8.33M 33s
 42500K .......... .......... .......... .......... .......... 16% 7.98M 33s
 42550K .......... .......... .......... .......... .......... 16% 7.91M 33s
 42600K .......... .......... .......... .......... .......... 16% 6.45M 33s
 42650K .......... .......... .......... .......... .......... 16% 7.84M 33s
 42700K .......... .......... .......... .......... .......... 16% 7.56M 33s
 42750K .......... .......... .......... .......... .......... 16% 9.31M 33s
 42800K .......... .......... .......... .......... .......... 16% 11.2M 33s
 42850K .......... .......... .......... .......... .......... 16% 7.85M 33s
 42900K .......... .......... .......... .......... .......... 16% 7.76M 33s
 42950K .......... .......... .......... .......... .......... 16% 7.67M 33s
 43000K .......... .......... .......... .......... .......... 16% 8.01M 33s
 43050K .......... .......... .......... .......... .......... 16% 4.98M 33s
 43100K .......... .......... .......... .......... .......... 16% 5.06M 33s
 43150K .......... .......... .......... .......... .......... 16% 5.46M 33s
 43200K .......... .......... .......... .......... .......... 16% 5.57M 33s
 43250K .......... .......... .......... .......... .......... 16% 6.97M 33s
 43300K .......... .......... .......... .......... .......... 16% 15.2M 33s
 43350K .......... .......... .......... .......... .......... 16% 14.4M 33s
 43400K .......... .......... .......... .......... .......... 16% 24.1M 33s
 43450K .......... .......... .......... .......... .......... 16% 15.6M 33s
 43500K .......... .......... .......... .......... .......... 16% 11.2M 33s
 43550K .......... .......... .......... .......... .......... 16% 55.2M 33s
 43600K .......... .......... .......... .......... .......... 16% 9.08M 33s
 43650K .......... .......... .......... .......... .......... 16% 14.5M 33s
 43700K .......... .......... .......... .......... .......... 16% 7.61M 33s
 43750K .......... .......... .......... .......... .......... 16% 9.01M 33s
 43800K .......... .......... .......... .......... .......... 16% 9.38M 33s
 43850K .......... .......... .......... .......... .......... 16% 5.23M 33s
 43900K .......... .......... .......... .......... .......... 16% 5.74M 33s
 43950K .......... .......... .......... .......... .......... 16% 3.72M 33s
 44000K .......... .......... .......... .......... .......... 16% 4.69M 33s
 44050K .......... .......... .......... .......... .......... 16% 2.86M 33s
 44100K .......... .......... .......... .......... .......... 16% 2.07M 33s
 44150K .......... .......... .......... .......... .......... 16% 4.31M 33s
 44200K .......... .......... .......... .......... .......... 16% 11.5M 33s
 44250K .......... .......... .......... .......... .......... 16% 9.63M 33s
 44300K .......... .......... .......... .......... .......... 16% 6.58M 33s
 44350K .......... .......... .......... .......... .......... 16% 4.57M 33s
 44400K .......... .......... .......... .......... .......... 16% 4.42M 33s
 44450K .......... .......... .......... .......... .......... 16% 3.67M 33s
 44500K .......... .......... .......... .......... .......... 16% 5.85M 33s
 44550K .......... .......... .......... .......... .......... 16% 14.5M 33s
 44600K .......... .......... .......... .......... .......... 16% 7.74M 33s
 44650K .......... .......... .......... .......... .......... 16% 8.48M 33s
 44700K .......... .......... .......... .......... .......... 16% 6.54M 33s
 44750K .......... .......... .......... .......... .......... 16% 6.74M 33s
 44800K .......... .......... .......... .......... .......... 16% 7.12M 33s
 44850K .......... .......... .......... .......... .......... 16% 5.77M 33s
 44900K .......... .......... .......... .......... .......... 16% 5.87M 33s
 44950K .......... .......... .......... .......... .......... 16% 4.54M 33s
 45000K .......... .......... .......... .......... .......... 16% 5.51M 33s
 45050K .......... .......... .......... .......... .......... 16% 5.64M 33s
 45100K .......... .......... .......... .......... .......... 16% 6.81M 33s
 45150K .......... .......... .......... .......... .......... 17% 18.7M 33s
 45200K .......... .......... .......... .......... .......... 17% 32.4M 33s
 45250K .......... .......... .......... .......... .......... 17% 22.3M 32s
 45300K .......... .......... .......... .......... .......... 17% 14.8M 32s
 45350K .......... .......... .......... .......... .......... 17% 28.3M 32s
 45400K .......... .......... .......... .......... .......... 17% 12.3M 32s
 45450K .......... .......... .......... .......... .......... 17% 11.9M 32s
 45500K .......... .......... .......... .......... .......... 17% 12.3M 32s
 45550K .......... .......... .......... .......... .......... 17% 12.3M 32s
 45600K .......... .......... .......... .......... .......... 17% 12.6M 32s
 45650K .......... .......... .......... .......... .......... 17% 12.7M 32s
 45700K .......... .......... .......... .......... .......... 17% 12.0M 32s
 45750K .......... .......... .......... .......... .......... 17% 9.13M 32s
 45800K .......... .......... .......... .......... .......... 17% 12.8M 32s
 45850K .......... .......... .......... .......... .......... 17% 9.45M 32s
 45900K .......... .......... .......... .......... .......... 17% 9.17M 32s
 45950K .......... .......... .......... .......... .......... 17% 5.98M 32s
 46000K .......... .......... .......... .......... .......... 17% 9.07M 32s
 46050K .......... .......... .......... .......... .......... 17% 8.24M 32s
 46100K .......... .......... .......... .......... .......... 17% 5.08M 32s
 46150K .......... .......... .......... .......... .......... 17% 6.85M 32s
 46200K .......... .......... .......... .......... .......... 17% 5.96M 32s
 46250K .......... .......... .......... .......... .......... 17% 7.03M 32s
 46300K .......... .......... .......... .......... .......... 17% 5.67M 32s
 46350K .......... .......... .......... .......... .......... 17% 5.21M 32s
 46400K .......... .......... .......... .......... .......... 17% 6.86M 32s
 46450K .......... .......... .......... .......... .......... 17% 5.42M 32s
 46500K .......... .......... .......... .......... .......... 17% 11.6M 32s
 46550K .......... .......... .......... .......... .......... 17% 18.4M 32s
 46600K .......... .......... .......... .......... .......... 17% 10.9M 32s
 46650K .......... .......... .......... .......... .......... 17% 10.0M 32s
 46700K .......... .......... .......... .......... .......... 17% 17.9M 32s
 46750K .......... .......... .......... .......... .......... 17% 10.5M 32s
 46800K .......... .......... .......... .......... .......... 17% 7.67M 32s
 46850K .......... .......... .......... .......... .......... 17% 7.47M 32s
 46900K .......... .......... .......... .......... .......... 17% 9.87M 32s
 46950K .......... .......... .......... .......... .......... 17% 6.66M 32s
 47000K .......... .......... .......... .......... .......... 17% 8.18M 32s
 47050K .......... .......... .......... .......... .......... 17% 6.38M 32s
 47100K .......... .......... .......... .......... .......... 17% 6.59M 32s
 47150K .......... .......... .......... .......... .......... 17% 6.65M 32s
 47200K .......... .......... .......... .......... .......... 17% 10.5M 32s
 47250K .......... .......... .......... .......... .......... 17% 20.0M 32s
 47300K .......... .......... .......... .......... .......... 17% 12.9M 32s
 47350K .......... .......... .......... .......... .......... 17% 14.4M 32s
 47400K .......... .......... .......... .......... .......... 17% 11.9M 32s
 47450K .......... .......... .......... .......... .......... 17% 7.98M 32s
 47500K .......... .......... .......... .......... .......... 17% 13.8M 32s
 47550K .......... .......... .......... .......... .......... 17% 9.38M 32s
 47600K .......... .......... .......... .......... .......... 17% 8.34M 32s
 47650K .......... .......... .......... .......... .......... 17% 9.31M 32s
 47700K .......... .......... .......... .......... .......... 17% 8.54M 32s
 47750K .......... .......... .......... .......... .......... 17% 10.3M 32s
 47800K .......... .......... .......... .......... .......... 18% 11.2M 32s
 47850K .......... .......... .......... .......... .......... 18% 20.4M 32s
 47900K .......... .......... .......... .......... .......... 18% 26.0M 32s
 47950K .......... .......... .......... .......... .......... 18% 27.7M 32s
 48000K .......... .......... .......... .......... .......... 18% 16.0M 32s
 48050K .......... .......... .......... .......... .......... 18%  168M 31s
 48100K .......... .......... .......... .......... .......... 18% 12.2M 31s
 48150K .......... .......... .......... .......... .......... 18% 76.9M 31s
 48200K .......... .......... .......... .......... .......... 18% 15.8M 31s
 48250K .......... .......... .......... .......... .......... 18% 12.8M 31s
 48300K .......... .......... .......... .......... .......... 18% 18.0M 31s
 48350K .......... .......... .......... .......... .......... 18% 10.2M 31s
 48400K .......... .......... .......... .......... .......... 18% 9.67M 31s
 48450K .......... .......... .......... .......... .......... 18% 8.25M 31s
 48500K .......... .......... .......... .......... .......... 18% 10.9M 31s
 48550K .......... .......... .......... .......... .......... 18% 9.43M 31s
 48600K .......... .......... .......... .......... .......... 18% 5.53M 31s
 48650K .......... .......... .......... .......... .......... 18% 5.86M 31s
 48700K .......... .......... .......... .......... .......... 18% 4.22M 31s
 48750K .......... .......... .......... .......... .......... 18% 4.33M 31s
 48800K .......... .......... .......... .......... .......... 18% 3.08M 31s
 48850K .......... .......... .......... .......... .......... 18% 4.80M 31s
 48900K .......... .......... .......... .......... .......... 18% 8.17M 31s
 48950K .......... .......... .......... .......... .......... 18% 5.40M 31s
 49000K .......... .......... .......... .......... .......... 18% 4.84M 31s
 49050K .......... .......... .......... .......... .......... 18% 6.33M 31s
 49100K .......... .......... .......... .......... .......... 18% 5.09M 31s
 49150K .......... .......... .......... .......... .......... 18% 6.33M 31s
 49200K .......... .......... .......... .......... .......... 18% 5.68M 31s
 49250K .......... .......... .......... .......... .......... 18% 7.62M 31s
 49300K .......... .......... .......... .......... .......... 18% 5.84M 31s
 49350K .......... .......... .......... .......... .......... 18% 3.94M 31s
 49400K .......... .......... .......... .......... .......... 18% 4.83M 31s
 49450K .......... .......... .......... .......... .......... 18% 2.73M 31s
 49500K .......... .......... .......... .......... .......... 18% 4.05M 31s
 49550K .......... .......... .......... .......... .......... 18% 6.64M 31s
 49600K .......... .......... .......... .......... .......... 18% 5.67M 31s
 49650K .......... .......... .......... .......... .......... 18% 7.50M 31s
 49700K .......... .......... .......... .......... .......... 18% 5.13M 31s
 49750K .......... .......... .......... .......... .......... 18% 9.25M 31s
 49800K .......... .......... .......... .......... .......... 18% 13.0M 31s
 49850K .......... .......... .......... .......... .......... 18% 10.7M 31s
 49900K .......... .......... .......... .......... .......... 18% 13.9M 31s
 49950K .......... .......... .......... .......... .......... 18% 10.2M 31s
 50000K .......... .......... .......... .......... .......... 18% 8.51M 31s
 50050K .......... .......... .......... .......... .......... 18% 13.0M 31s
 50100K .......... .......... .......... .......... .......... 18% 9.12M 31s
 50150K .......... .......... .......... .......... .......... 18% 12.2M 31s
 50200K .......... .......... .......... .......... .......... 18% 9.76M 31s
 50250K .......... .......... .......... .......... .......... 18% 10.4M 31s
 50300K .......... .......... .......... .......... .......... 18% 12.7M 31s
 50350K .......... .......... .......... .......... .......... 18% 11.6M 31s
 50400K .......... .......... .......... .......... .......... 18% 23.9M 31s
 50450K .......... .......... .......... .......... .......... 18% 27.1M 31s
 50500K .......... .......... .......... .......... .......... 19% 38.3M 31s
 50550K .......... .......... .......... .......... .......... 19% 18.8M 31s
 50600K .......... .......... .......... .......... .......... 19% 38.9M 31s
 50650K .......... .......... .......... .......... .......... 19% 26.7M 31s
 50700K .......... .......... .......... .......... .......... 19% 16.1M 31s
 50750K .......... .......... .......... .......... .......... 19% 18.4M 31s
 50800K .......... .......... .......... .......... .......... 19% 13.6M 31s
 50850K .......... .......... .......... .......... .......... 19% 11.6M 31s
 50900K .......... .......... .......... .......... .......... 19% 8.51M 31s
 50950K .......... .......... .......... .......... .......... 19% 9.52M 31s
 51000K .......... .......... .......... .......... .......... 19% 6.47M 31s
 51050K .......... .......... .......... .......... .......... 19% 6.73M 31s
 51100K .......... .......... .......... .......... .......... 19% 5.14M 31s
 51150K .......... .......... .......... .......... .......... 19% 7.03M 31s
 51200K .......... .......... .......... .......... .......... 19% 5.08M 31s
 51250K .......... .......... .......... .......... .......... 19% 8.25M 31s
 51300K .......... .......... .......... .......... .......... 19% 9.59M 31s
 51350K .......... .......... .......... .......... .......... 19% 11.4M 31s
 51400K .......... .......... .......... .......... .......... 19% 8.11M 31s
 51450K .......... .......... .......... .......... .......... 19% 4.84M 31s
 51500K .......... .......... .......... .......... .......... 19% 4.97M 31s
 51550K .......... .......... .......... .......... .......... 19% 5.17M 31s
 51600K .......... .......... .......... .......... .......... 19% 4.81M 31s
 51650K .......... .......... .......... .......... .......... 19% 5.19M 31s
 51700K .......... .......... .......... .......... .......... 19% 4.85M 31s
 51750K .......... .......... .......... .......... .......... 19% 3.41M 31s
 51800K .......... .......... .......... .......... .......... 19% 3.16M 31s
 51850K .......... .......... .......... .......... .......... 19% 2.54M 31s
 51900K .......... .......... .......... .......... .......... 19% 10.8M 31s
 51950K .......... .......... .......... .......... .......... 19% 17.2M 31s
 52000K .......... .......... .......... .......... .......... 19% 19.3M 31s
 52050K .......... .......... .......... .......... .......... 19% 30.7M 31s
 52100K .......... .......... .......... .......... .......... 19% 13.6M 31s
 52150K .......... .......... .......... .......... .......... 19% 16.3M 31s
 52200K .......... .......... .......... .......... .......... 19% 8.68M 31s
 52250K .......... .......... .......... .......... .......... 19% 13.3M 31s
 52300K .......... .......... .......... .......... .......... 19% 8.33M 31s
 52350K .......... .......... .......... .......... .......... 19% 5.54M 31s
 52400K .......... .......... .......... .......... .......... 19% 5.44M 31s
 52450K .......... .......... .......... .......... .......... 19% 6.20M 31s
 52500K .......... .......... .......... .......... .......... 19% 6.48M 31s
 52550K .......... .......... .......... .......... .......... 19% 5.90M 31s
 52600K .......... .......... .......... .......... .......... 19% 11.4M 31s
 52650K .......... .......... .......... .......... .......... 19% 14.4M 31s
 52700K .......... .......... .......... .......... .......... 19% 11.9M 31s
 52750K .......... .......... .......... .......... .......... 19% 9.45M 31s
 52800K .......... .......... .......... .......... .......... 19% 10.4M 31s
 52850K .......... .......... .......... .......... .......... 19% 6.68M 31s
 52900K .......... .......... .......... .......... .......... 19% 10.8M 31s
 52950K .......... .......... .......... .......... .......... 19% 5.35M 31s
 53000K .......... .......... .......... .......... .......... 19% 9.05M 31s
 53050K .......... .......... .......... .......... .......... 19% 5.94M 31s
 53100K .......... .......... .......... .......... .......... 19% 4.76M 31s
 53150K .......... .......... .......... .......... .......... 20% 5.39M 31s
 53200K .......... .......... .......... .......... .......... 20% 4.34M 31s
 53250K .......... .......... .......... .......... .......... 20% 11.2M 31s
 53300K .......... .......... .......... .......... .......... 20% 18.0M 30s
 53350K .......... .......... .......... .......... .......... 20% 13.4M 30s
 53400K .......... .......... .......... .......... .......... 20% 17.4M 30s
 53450K .......... .......... .......... .......... .......... 20% 11.7M 30s
 53500K .......... .......... .......... .......... .......... 20% 14.0M 30s
 53550K .......... .......... .......... .......... .......... 20% 8.70M 30s
 53600K .......... .......... .......... .......... .......... 20% 10.9M 30s
 53650K .......... .......... .......... .......... .......... 20% 9.07M 30s
 53700K .......... .......... .......... .......... .......... 20% 6.46M 30s
 53750K .......... .......... .......... .......... .......... 20% 7.50M 30s
 53800K .......... .......... .......... .......... .......... 20% 4.17M 30s
 53850K .......... .......... .......... .......... .......... 20% 2.87M 30s
 53900K .......... .......... .......... .......... .......... 20% 3.84M 30s
 53950K .......... .......... .......... .......... .......... 20% 2.77M 30s
 54000K .......... .......... .......... .......... .......... 20% 3.68M 30s
 54050K .......... .......... .......... .......... .......... 20% 3.43M 30s
 54100K .......... .......... .......... .......... .......... 20% 12.8M 30s
 54150K .......... .......... .......... .......... .......... 20% 10.6M 30s
 54200K .......... .......... .......... .......... .......... 20% 14.4M 30s
 54250K .......... .......... .......... .......... .......... 20% 8.89M 30s
 54300K .......... .......... .......... .......... .......... 20% 13.1M 30s
 54350K .......... .......... .......... .......... .......... 20% 7.00M 30s
 54400K .......... .......... .......... .......... .......... 20% 6.61M 30s
 54450K .......... .......... .......... .......... .......... 20% 5.19M 30s
 54500K .......... .......... .......... .......... .......... 20% 4.81M 30s
 54550K .......... .......... .......... .......... .......... 20% 5.99M 30s
 54600K .......... .......... .......... .......... .......... 20% 4.34M 30s
 54650K .......... .......... .......... .......... .......... 20% 6.09M 30s
 54700K .......... .......... .......... .......... .......... 20% 5.19M 30s
 54750K .......... .......... .......... .......... .......... 20% 24.8M 30s
 54800K .......... .......... .......... .......... .......... 20% 13.3M 30s
 54850K .......... .......... .......... .......... .......... 20% 13.3M 30s
 54900K .......... .......... .......... .......... .......... 20% 16.7M 30s
 54950K .......... .......... .......... .......... .......... 20% 11.6M 30s
 55000K .......... .......... .......... .......... .......... 20% 21.0M 30s
 55050K .......... .......... .......... .......... .......... 20% 14.3M 30s
 55100K .......... .......... .......... .......... .......... 20% 13.6M 30s
 55150K .......... .......... .......... .......... .......... 20% 15.5M 30s
 55200K .......... .......... .......... .......... .......... 20% 13.0M 30s
 55250K .......... .......... .......... .......... .......... 20% 11.2M 30s
 55300K .......... .......... .......... .......... .......... 20% 16.5M 30s
 55350K .......... .......... .......... .......... .......... 20% 6.26M 30s
 55400K .......... .......... .......... .......... .......... 20% 29.2M 30s
 55450K .......... .......... .......... .......... .......... 20% 7.69M 30s
 55500K .......... .......... .......... .......... .......... 20% 9.40M 30s
 55550K .......... .......... .......... .......... .......... 20% 11.4M 30s
 55600K .......... .......... .......... .......... .......... 20% 5.83M 30s
 55650K .......... .......... .......... .......... .......... 20% 6.37M 30s
 55700K .......... .......... .......... .......... .......... 20% 4.73M 30s
 55750K .......... .......... .......... .......... .......... 20% 5.89M 30s
 55800K .......... .......... .......... .......... .......... 21% 7.72M 30s
 55850K .......... .......... .......... .......... .......... 21% 11.1M 30s
 55900K .......... .......... .......... .......... .......... 21% 22.8M 30s
 55950K .......... .......... .......... .......... .......... 21% 16.0M 30s
 56000K .......... .......... .......... .......... .......... 21% 12.3M 30s
 56050K .......... .......... .......... .......... .......... 21% 9.17M 30s
 56100K .......... .......... .......... .......... .......... 21% 6.23M 30s
 56150K .......... .......... .......... .......... .......... 21% 8.30M 30s
 56200K .......... .......... .......... .......... .......... 21% 6.87M 30s
 56250K .......... .......... .......... .......... .......... 21% 8.10M 30s
 56300K .......... .......... .......... .......... .......... 21% 7.94M 30s
 56350K .......... .......... .......... .......... .......... 21% 7.32M 30s
 56400K .......... .......... .......... .......... .......... 21% 6.44M 30s
 56450K .......... .......... .......... .......... .......... 21% 6.40M 30s
 56500K .......... .......... .......... .......... .......... 21% 3.80M 30s
 56550K .......... .......... .......... .......... .......... 21% 3.33M 30s
 56600K .......... .......... .......... .......... .......... 21% 3.09M 30s
 56650K .......... .......... .......... .......... .......... 21% 4.36M 30s
 56700K .......... .......... .......... .......... .......... 21% 4.45M 30s
 56750K .......... .......... .......... .......... .......... 21% 4.65M 30s
 56800K .......... .......... .......... .......... .......... 21% 10.0M 30s
 56850K .......... .......... .......... .......... .......... 21% 15.5M 30s
 56900K .......... .......... .......... .......... .......... 21% 11.5M 30s
 56950K .......... .......... .......... .......... .......... 21% 8.76M 30s
 57000K .......... .......... .......... .......... .......... 21% 7.95M 30s
 57050K .......... .......... .......... .......... .......... 21% 5.61M 30s
 57100K .......... .......... .......... .......... .......... 21% 4.18M 30s
 57150K .......... .......... .......... .......... .......... 21% 2.90M 30s
 57200K .......... .......... .......... .......... .......... 21% 4.31M 30s
 57250K .......... .......... .......... .......... .......... 21% 10.8M 30s
 57300K .......... .......... .......... .......... .......... 21% 9.97M 30s
 57350K .......... .......... .......... .......... .......... 21% 6.75M 30s
 57400K .......... .......... .......... .......... .......... 21% 8.76M 30s
 57450K .......... .......... .......... .......... .......... 21% 7.09M 30s
 57500K .......... .......... .......... .......... .......... 21% 9.89M 30s
 57550K .......... .......... .......... .......... .......... 21% 5.52M 30s
 57600K .......... .......... .......... .......... .......... 21% 5.55M 30s
 57650K .......... .......... .......... .......... .......... 21% 4.13M 30s
 57700K .......... .......... .......... .......... .......... 21% 3.32M 30s
 57750K .......... .......... .......... .......... .......... 21% 4.36M 30s
 57800K .......... .......... .......... .......... .......... 21% 3.62M 30s
 57850K .......... .......... .......... .......... .......... 21% 7.89M 30s
 57900K .......... .......... .......... .......... .......... 21% 9.28M 30s
 57950K .......... .......... .......... .......... .......... 21% 8.04M 30s
 58000K .......... .......... .......... .......... .......... 21% 9.92M 30s
 58050K .......... .......... .......... .......... .......... 21% 7.52M 30s
 58100K .......... .......... .......... .......... .......... 21% 6.14M 30s
 58150K .......... .......... .......... .......... .......... 21% 8.50M 30s
 58200K .......... .......... .......... .......... .......... 21% 7.15M 30s
 58250K .......... .......... .......... .......... .......... 21% 9.71M 30s
 58300K .......... .......... .......... .......... .......... 21% 9.80M 30s
 58350K .......... .......... .......... .......... .......... 21% 6.18M 30s
 58400K .......... .......... .......... .......... .......... 21% 5.92M 30s
 58450K .......... .......... .......... .......... .......... 22% 5.42M 30s
 58500K .......... .......... .......... .......... .......... 22% 6.98M 30s
 58550K .......... .......... .......... .......... .......... 22% 6.20M 30s
 58600K .......... .......... .......... .......... .......... 22% 5.13M 30s
 58650K .......... .......... .......... .......... .......... 22% 5.28M 30s
 58700K .......... .......... .......... .......... .......... 22% 5.23M 30s
 58750K .......... .......... .......... .......... .......... 22% 7.22M 30s
 58800K .......... .......... .......... .......... .......... 22% 5.28M 30s
 58850K .......... .......... .......... .......... .......... 22% 9.70M 30s
 58900K .......... .......... .......... .......... .......... 22% 18.0M 30s
 58950K .......... .......... .......... .......... .......... 22% 23.3M 30s
 59000K .......... .......... .......... .......... .......... 22% 16.3M 30s
 59050K .......... .......... .......... .......... .......... 22% 20.7M 30s
 59100K .......... .......... .......... .......... .......... 22% 10.2M 30s
 59150K .......... .......... .......... .......... .......... 22% 17.5M 30s
 59200K .......... .......... .......... .......... .......... 22% 7.24M 30s
 59250K .......... .......... .......... .......... .......... 22% 5.99M 30s
 59300K .......... .......... .......... .......... .......... 22% 6.36M 30s
 59350K .......... .......... .......... .......... .......... 22% 6.29M 30s
 59400K .......... .......... .......... .......... .......... 22% 8.91M 30s
 59450K .......... .......... .......... .......... .......... 22% 6.03M 30s
 59500K .......... .......... .......... .......... .......... 22% 7.79M 30s
 59550K .......... .......... .......... .......... .......... 22% 8.49M 30s
 59600K .......... .......... .......... .......... .......... 22% 10.3M 29s
 59650K .......... .......... .......... .......... .......... 22% 17.8M 29s
 59700K .......... .......... .......... .......... .......... 22% 29.4M 29s
 59750K .......... .......... .......... .......... .......... 22% 16.2M 29s
 59800K .......... .......... .......... .......... .......... 22% 21.9M 29s
 59850K .......... .......... .......... .......... .......... 22% 7.54M 29s
 59900K .......... .......... .......... .......... .......... 22% 36.0M 29s
 59950K .......... .......... .......... .......... .......... 22% 11.1M 29s
 60000K .......... .......... .......... .......... .......... 22% 10.0M 29s
 60050K .......... .......... .......... .......... .......... 22% 11.6M 29s
 60100K .......... .......... .......... .......... .......... 22% 5.11M 29s
 60150K .......... .......... .......... .......... .......... 22% 5.86M 29s
 60200K .......... .......... .......... .......... .......... 22% 5.40M 29s
 60250K .......... .......... .......... .......... .......... 22% 6.53M 29s
 60300K .......... .......... .......... .......... .......... 22% 3.76M 29s
 60350K .......... .......... .......... .......... .......... 22% 3.06M 29s
 60400K .......... .......... .......... .......... .......... 22% 2.75M 29s
 60450K .......... .......... .......... .......... .......... 22% 4.55M 29s
 60500K .......... .......... .......... .......... .......... 22% 5.09M 29s
 60550K .......... .......... .......... .......... .......... 22% 4.86M 29s
 60600K .......... .......... .......... .......... .......... 22% 5.19M 29s
 60650K .......... .......... .......... .......... .......... 22% 9.55M 29s
 60700K .......... .......... .......... .......... .......... 22% 7.38M 29s
 60750K .......... .......... .......... .......... .......... 22% 8.45M 29s
 60800K .......... .......... .......... .......... .......... 22% 9.33M 29s
 60850K .......... .......... .......... .......... .......... 22% 7.86M 29s
 60900K .......... .......... .......... .......... .......... 22% 7.48M 29s
 60950K .......... .......... .......... .......... .......... 22% 13.6M 29s
 61000K .......... .......... .......... .......... .......... 22% 13.9M 29s
 61050K .......... .......... .......... .......... .......... 22% 13.9M 29s
 61100K .......... .......... .......... .......... .......... 23% 10.0M 29s
 61150K .......... .......... .......... .......... .......... 23% 12.6M 29s
 61200K .......... .......... .......... .......... .......... 23% 12.4M 29s
 61250K .......... .......... .......... .......... .......... 23% 11.7M 29s
 61300K .......... .......... .......... .......... .......... 23% 11.6M 29s
 61350K .......... .......... .......... .......... .......... 23% 8.67M 29s
 61400K .......... .......... .......... .......... .......... 23% 5.72M 29s
 61450K .......... .......... .......... .......... .......... 23% 5.69M 29s
 61500K .......... .......... .......... .......... .......... 23% 6.38M 29s
 61550K .......... .......... .......... .......... .......... 23% 7.55M 29s
 61600K .......... .......... .......... .......... .......... 23% 6.36M 29s
 61650K .......... .......... .......... .......... .......... 23% 8.32M 29s
 61700K .......... .......... .......... .......... .......... 23% 9.34M 29s
 61750K .......... .......... .......... .......... .......... 23% 19.4M 29s
 61800K .......... .......... .......... .......... .......... 23% 12.8M 29s
 61850K .......... .......... .......... .......... .......... 23% 10.8M 29s
 61900K .......... .......... .......... .......... .......... 23% 13.8M 29s
 61950K .......... .......... .......... .......... .......... 23% 10.6M 29s
 62000K .......... .......... .......... .......... .......... 23% 10.8M 29s
 62050K .......... .......... .......... .......... .......... 23% 9.66M 29s
 62100K .......... .......... .......... .......... .......... 23% 11.0M 29s
 62150K .......... .......... .......... .......... .......... 23% 9.87M 29s
 62200K .......... .......... .......... .......... .......... 23% 5.59M 29s
 62250K .......... .......... .......... .......... .......... 23% 4.85M 29s
 62300K .......... .......... .......... .......... .......... 23% 5.79M 29s
 62350K .......... .......... .......... .......... .......... 23% 4.87M 29s
 62400K .......... .......... .......... .......... .......... 23% 5.81M 29s
 62450K .......... .......... .......... .......... .......... 23% 5.98M 29s
 62500K .......... .......... .......... .......... .......... 23% 18.4M 29s
 62550K .......... .......... .......... .......... .......... 23% 8.58M 29s
 62600K .......... .......... .......... .......... .......... 23% 7.54M 29s
 62650K .......... .......... .......... .......... .......... 23% 10.1M 29s
 62700K .......... .......... .......... .......... .......... 23% 9.08M 29s
 62750K .......... .......... .......... .......... .......... 23% 8.42M 29s
 62800K .......... .......... .......... .......... .......... 23% 9.43M 29s
 62850K .......... .......... .......... .......... .......... 23% 6.11M 29s
 62900K .......... .......... .......... .......... .......... 23% 7.63M 29s
 62950K .......... .......... .......... .......... .......... 23% 5.81M 29s
 63000K .......... .......... .......... .......... .......... 23% 8.63M 29s
 63050K .......... .......... .......... .......... .......... 23% 8.83M 29s
 63100K .......... .......... .......... .......... .......... 23% 7.31M 29s
 63150K .......... .......... .......... .......... .......... 23% 8.99M 29s
 63200K .......... .......... .......... .......... .......... 23% 6.23M 29s
 63250K .......... .......... .......... .......... .......... 23% 6.76M 29s
 63300K .......... .......... .......... .......... .......... 23% 5.83M 29s
 63350K .......... .......... .......... .......... .......... 23% 4.79M 29s
 63400K .......... .......... .......... .......... .......... 23% 5.63M 29s
 63450K .......... .......... .......... .......... .......... 23% 3.69M 29s
 63500K .......... .......... .......... .......... .......... 23% 14.9M 29s
 63550K .......... .......... .......... .......... .......... 23% 16.7M 29s
 63600K .......... .......... .......... .......... .......... 23% 17.1M 29s
 63650K .......... .......... .......... .......... .......... 23% 18.4M 29s
 63700K .......... .......... .......... .......... .......... 23% 20.4M 29s
 63750K .......... .......... .......... .......... .......... 24% 12.5M 29s
 63800K .......... .......... .......... .......... .......... 24% 12.3M 29s
 63850K .......... .......... .......... .......... .......... 24% 9.52M 29s
 63900K .......... .......... .......... .......... .......... 24% 8.41M 29s
 63950K .......... .......... .......... .......... .......... 24% 6.27M 29s
 64000K .......... .......... .......... .......... .......... 24% 7.46M 29s
 64050K .......... .......... .......... .......... .......... 24% 6.24M 29s
 64100K .......... .......... .......... .......... .......... 24% 5.93M 29s
 64150K .......... .......... .......... .......... .......... 24% 6.54M 29s
 64200K .......... .......... .......... .......... .......... 24% 4.46M 29s
 64250K .......... .......... .......... .......... .......... 24% 5.69M 29s
 64300K .......... .......... .......... .......... .......... 24% 4.01M 29s
 64350K .......... .......... .......... .......... .......... 24% 2.90M 29s
 64400K .......... .......... .......... .......... .......... 24% 3.09M 29s
 64450K .......... .......... .......... .......... .......... 24% 2.80M 29s
 64500K .......... .......... .......... .......... .......... 24% 7.57M 29s
 64550K .......... .......... .......... .......... .......... 24% 6.42M 29s
 64600K .......... .......... .......... .......... .......... 24% 6.05M 29s
 64650K .......... .......... .......... .......... .......... 24% 5.67M 29s
 64700K .......... .......... .......... .......... .......... 24% 4.20M 29s
 64750K .......... .......... .......... .......... .......... 24% 5.10M 29s
 64800K .......... .......... .......... .......... .......... 24% 4.36M 29s
 64850K .......... .......... .......... .......... .......... 24% 4.49M 29s
 64900K .......... .......... .......... .......... .......... 24% 4.62M 29s
 64950K .......... .......... .......... .......... .......... 24% 5.76M 29s
 65000K .......... .......... .......... .......... .......... 24% 8.99M 29s
 65050K .......... .......... .......... .......... .......... 24% 8.91M 29s
 65100K .......... .......... .......... .......... .......... 24% 7.23M 29s
 65150K .......... .......... .......... .......... .......... 24% 6.46M 29s
 65200K .......... .......... .......... .......... .......... 24% 4.77M 29s
 65250K .......... .......... .......... .......... .......... 24% 7.82M 29s
 65300K .......... .......... .......... .......... .......... 24% 7.40M 29s
 65350K .......... .......... .......... .......... .......... 24% 4.41M 29s
 65400K .......... .......... .......... .......... .......... 24% 4.99M 29s
 65450K .......... .......... .......... .......... .......... 24% 4.94M 29s
 65500K .......... .......... .......... .......... .......... 24% 6.29M 29s
 65550K .......... .......... .......... .......... .......... 24% 6.39M 29s
 65600K .......... .......... .......... .......... .......... 24% 4.40M 29s
 65650K .......... .......... .......... .......... .......... 24% 8.82M 29s
 65700K .......... .......... .......... .......... .......... 24% 17.3M 29s
 65750K .......... .......... .......... .......... .......... 24% 26.0M 29s
 65800K .......... .......... .......... .......... .......... 24% 19.6M 29s
 65850K .......... .......... .......... .......... .......... 24% 14.4M 29s
 65900K .......... .......... .......... .......... .......... 24% 21.4M 29s
 65950K .......... .......... .......... .......... .......... 24% 12.1M 28s
 66000K .......... .......... .......... .......... .......... 24% 12.6M 28s
 66050K .......... .......... .......... .......... .......... 24% 12.5M 28s
 66100K .......... .......... .......... .......... .......... 24% 9.89M 28s
 66150K .......... .......... .......... .......... .......... 24% 12.5M 28s
 66200K .......... .......... .......... .......... .......... 24% 9.08M 28s
 66250K .......... .......... .......... .......... .......... 24% 9.70M 28s
 66300K .......... .......... .......... .......... .......... 24% 12.0M 28s
 66350K .......... .......... .......... .......... .......... 24% 7.55M 28s
 66400K .......... .......... .......... .......... .......... 24% 7.80M 28s
 66450K .......... .......... .......... .......... .......... 25% 5.58M 28s
 66500K .......... .......... .......... .......... .......... 25% 5.12M 28s
 66550K .......... .......... .......... .......... .......... 25% 5.08M 28s
 66600K .......... .......... .......... .......... .......... 25% 4.25M 28s
 66650K .......... .......... .......... .......... .......... 25% 5.64M 28s
 66700K .......... .......... .......... .......... .......... 25% 4.30M 28s
 66750K .......... .......... .......... .......... .......... 25% 5.93M 28s
 66800K .......... .......... .......... .......... .......... 25% 4.35M 28s
 66850K .......... .......... .......... .......... .......... 25% 4.53M 28s
 66900K .......... .......... .......... .......... .......... 25% 4.78M 28s
 66950K .......... .......... .......... .......... .......... 25% 4.27M 28s
 67000K .......... .......... .......... .......... .......... 25% 4.66M 28s
 67050K .......... .......... .......... .......... .......... 25% 4.73M 28s
 67100K .......... .......... .......... .......... .......... 25% 6.04M 28s
 67150K .......... .......... .......... .......... .......... 25% 18.5M 28s
 67200K .......... .......... .......... .......... .......... 25% 17.4M 28s
 67250K .......... .......... .......... .......... .......... 25% 13.4M 28s
 67300K .......... .......... .......... .......... .......... 25% 34.9M 28s
 67350K .......... .......... .......... .......... .......... 25% 10.0M 28s
 67400K .......... .......... .......... .......... .......... 25% 14.6M 28s
 67450K .......... .......... .......... .......... .......... 25% 11.8M 28s
 67500K .......... .......... .......... .......... .......... 25% 11.2M 28s
 67550K .......... .......... .......... .......... .......... 25% 11.3M 28s
 67600K .......... .......... .......... .......... .......... 25% 8.71M 28s
 67650K .......... .......... .......... .......... .......... 25% 10.2M 28s
 67700K .......... .......... .......... .......... .......... 25% 6.00M 28s
 67750K .......... .......... .......... .......... .......... 25% 11.1M 28s
 67800K .......... .......... .......... .......... .......... 25% 11.9M 28s
 67850K .......... .......... .......... .......... .......... 25% 11.8M 28s
 67900K .......... .......... .......... .......... .......... 25% 10.4M 28s
 67950K .......... .......... .......... .......... .......... 25% 8.59M 28s
 68000K .......... .......... .......... .......... .......... 25% 10.0M 28s
 68050K .......... .......... .......... .......... .......... 25% 10.1M 28s
 68100K .......... .......... .......... .......... .......... 25% 9.11M 28s
 68150K .......... .......... .......... .......... .......... 25% 7.85M 28s
 68200K .......... .......... .......... .......... .......... 25% 6.24M 28s
 68250K .......... .......... .......... .......... .......... 25% 5.48M 28s
 68300K .......... .......... .......... .......... .......... 25% 7.24M 28s
 68350K .......... .......... .......... .......... .......... 25% 6.13M 28s
 68400K .......... .......... .......... .......... .......... 25% 6.54M 28s
 68450K .......... .......... .......... .......... .......... 25% 4.77M 28s
 68500K .......... .......... .......... .......... .......... 25% 4.53M 28s
 68550K .......... .......... .......... .......... .......... 25% 5.51M 28s
 68600K .......... .......... .......... .......... .......... 25% 5.13M 28s
 68650K .......... .......... .......... .......... .......... 25% 8.91M 28s
 68700K .......... .......... .......... .......... .......... 25% 65.3M 28s
 68750K .......... .......... .......... .......... .......... 25% 10.9M 28s
 68800K .......... .......... .......... .......... .......... 25% 9.16M 28s
 68850K .......... .......... .......... .......... .......... 25% 8.43M 28s
 68900K .......... .......... .......... .......... .......... 25% 9.39M 28s
 68950K .......... .......... .......... .......... .......... 25% 9.68M 28s
 69000K .......... .......... .......... .......... .......... 25% 10.4M 28s
 69050K .......... .......... .......... .......... .......... 25% 10.2M 28s
 69100K .......... .......... .......... .......... .......... 26% 6.00M 28s
 69150K .......... .......... .......... .......... .......... 26% 7.12M 28s
 69200K .......... .......... .......... .......... .......... 26% 6.06M 28s
 69250K .......... .......... .......... .......... .......... 26% 8.86M 28s
 69300K .......... .......... .......... .......... .......... 26% 7.10M 28s
 69350K .......... .......... .......... .......... .......... 26% 7.18M 28s
 69400K .......... .......... .......... .......... .......... 26% 9.82M 28s
 69450K .......... .......... .......... .......... .......... 26% 10.8M 28s
 69500K .......... .......... .......... .......... .......... 26%  151M 28s
 69550K .......... .......... .......... .......... .......... 26% 12.7M 28s
 69600K .......... .......... .......... .......... .......... 26% 11.6M 28s
 69650K .......... .......... .......... .......... .......... 26% 15.2M 28s
 69700K .......... .......... .......... .......... .......... 26% 7.90M 28s
 69750K .......... .......... .......... .......... .......... 26% 10.2M 28s
 69800K .......... .......... .......... .......... .......... 26% 9.45M 28s
 69850K .......... .......... .......... .......... .......... 26% 8.67M 28s
 69900K .......... .......... .......... .......... .......... 26% 8.90M 28s
 69950K .......... .......... .......... .......... .......... 26% 8.49M 28s
 70000K .......... .......... .......... .......... .......... 26% 6.08M 28s
 70050K .......... .......... .......... .......... .......... 26% 3.83M 28s
 70100K .......... .......... .......... .......... .......... 26% 3.22M 28s
 70150K .......... .......... .......... .......... .......... 26% 5.93M 28s
 70200K .......... .......... .......... .......... .......... 26% 5.74M 28s
 70250K .......... .......... .......... .......... .......... 26% 4.73M 28s
 70300K .......... .......... .......... .......... .......... 26% 3.64M 28s
 70350K .......... .......... .......... .......... .......... 26% 3.38M 28s
 70400K .......... .......... .......... .......... .......... 26% 4.27M 28s
 70450K .......... .......... .......... .......... .......... 26% 13.5M 28s
 70500K .......... .......... .......... .......... .......... 26% 23.1M 28s
 70550K .......... .......... .......... .......... .......... 26% 12.5M 28s
 70600K .......... .......... .......... .......... .......... 26% 15.8M 28s
 70650K .......... .......... .......... .......... .......... 26% 15.1M 28s
 70700K .......... .......... .......... .......... .......... 26% 16.6M 28s
 70750K .......... .......... .......... .......... .......... 26% 19.4M 28s
 70800K .......... .......... .......... .......... .......... 26% 19.5M 28s
 70850K .......... .......... .......... .......... .......... 26% 12.0M 28s
 70900K .......... .......... .......... .......... .......... 26% 10.5M 28s
 70950K .......... .......... .......... .......... .......... 26% 12.2M 28s
 71000K .......... .......... .......... .......... .......... 26% 8.32M 28s
 71050K .......... .......... .......... .......... .......... 26% 8.83M 28s
 71100K .......... .......... .......... .......... .......... 26% 7.86M 28s
 71150K .......... .......... .......... .......... .......... 26% 7.48M 28s
 71200K .......... .......... .......... .......... .......... 26% 7.32M 28s
 71250K .......... .......... .......... .......... .......... 26% 7.29M 28s
 71300K .......... .......... .......... .......... .......... 26% 8.20M 27s
 71350K .......... .......... .......... .......... .......... 26% 15.8M 27s
 71400K .......... .......... .......... .......... .......... 26% 16.4M 27s
 71450K .......... .......... .......... .......... .......... 26% 10.2M 27s
 71500K .......... .......... .......... .......... .......... 26% 11.6M 27s
 71550K .......... .......... .......... .......... .......... 26% 11.9M 27s
 71600K .......... .......... .......... .......... .......... 26% 9.74M 27s
 71650K .......... .......... .......... .......... .......... 26% 11.4M 27s
 71700K .......... .......... .......... .......... .......... 26% 7.04M 27s
 71750K .......... .......... .......... .......... .......... 27% 14.0M 27s
 71800K .......... .......... .......... .......... .......... 27% 11.0M 27s
 71850K .......... .......... .......... .......... .......... 27% 5.02M 27s
 71900K .......... .......... .......... .......... .......... 27% 6.22M 27s
 71950K .......... .......... .......... .......... .......... 27% 5.05M 27s
 72000K .......... .......... .......... .......... .......... 27% 5.06M 27s
 72050K .......... .......... .......... .......... .......... 27% 5.46M 27s
 72100K .......... .......... .......... .......... .......... 27% 5.01M 27s
 72150K .......... .......... .......... .......... .......... 27% 7.35M 27s
 72200K .......... .......... .......... .......... .......... 27% 3.95M 27s
 72250K .......... .......... .......... .......... .......... 27% 4.11M 27s
 72300K .......... .......... .......... .......... .......... 27% 4.98M 27s
 72350K .......... .......... .......... .......... .......... 27% 6.65M 27s
 72400K .......... .......... .......... .......... .......... 27% 10.8M 27s
 72450K .......... .......... .......... .......... .......... 27% 11.2M 27s
 72500K .......... .......... .......... .......... .......... 27% 12.5M 27s
 72550K .......... .......... .......... .......... .......... 27% 13.2M 27s
 72600K .......... .......... .......... .......... .......... 27% 10.5M 27s
 72650K .......... .......... .......... .......... .......... 27% 11.3M 27s
 72700K .......... .......... .......... .......... .......... 27% 9.38M 27s
 72750K .......... .......... .......... .......... .......... 27% 10.1M 27s
 72800K .......... .......... .......... .......... .......... 27% 9.86M 27s
 72850K .......... .......... .......... .......... .......... 27% 10.0M 27s
 72900K .......... .......... .......... .......... .......... 27% 13.5M 27s
 72950K .......... .......... .......... .......... .......... 27% 11.6M 27s
 73000K .......... .......... .......... .......... .......... 27% 31.2M 27s
 73050K .......... .......... .......... .......... .......... 27% 17.0M 27s
 73100K .......... .......... .......... .......... .......... 27% 26.2M 27s
 73150K .......... .......... .......... .......... .......... 27% 47.0M 27s
 73200K .......... .......... .......... .......... .......... 27% 18.1M 27s
 73250K .......... .......... .......... .......... .......... 27% 20.6M 27s
 73300K .......... .......... .......... .......... .......... 27% 12.9M 27s
 73350K .......... .......... .......... .......... .......... 27% 10.1M 27s
 73400K .......... .......... .......... .......... .......... 27% 12.5M 27s
 73450K .......... .......... .......... .......... .......... 27% 7.56M 27s
 73500K .......... .......... .......... .......... .......... 27% 10.9M 27s
 73550K .......... .......... .......... .......... .......... 27% 7.42M 27s
 73600K .......... .......... .......... .......... .......... 27% 7.15M 27s
 73650K .......... .......... .......... .......... .......... 27% 5.15M 27s
 73700K .......... .......... .......... .......... .......... 27% 4.45M 27s
 73750K .......... .......... .......... .......... .......... 27% 4.47M 27s
 73800K .......... .......... .......... .......... .......... 27% 11.1M 27s
 73850K .......... .......... .......... .......... .......... 27% 17.2M 27s
 73900K .......... .......... .......... .......... .......... 27% 21.7M 27s
 73950K .......... .......... .......... .......... .......... 27% 14.7M 27s
 74000K .......... .......... .......... .......... .......... 27% 19.9M 27s
 74050K .......... .......... .......... .......... .......... 27% 14.7M 27s
 74100K .......... .......... .......... .......... .......... 27% 13.5M 27s
 74150K .......... .......... .......... .......... .......... 27% 17.9M 27s
 74200K .......... .......... .......... .......... .......... 27% 12.7M 27s
 74250K .......... .......... .......... .......... .......... 27% 12.8M 27s
 74300K .......... .......... .......... .......... .......... 27% 13.1M 27s
 74350K .......... .......... .......... .......... .......... 27% 10.2M 27s
 74400K .......... .......... .......... .......... .......... 28% 12.0M 27s
 74450K .......... .......... .......... .......... .......... 28% 6.77M 27s
 74500K .......... .......... .......... .......... .......... 28% 10.2M 27s
 74550K .......... .......... .......... .......... .......... 28% 6.65M 27s
 74600K .......... .......... .......... .......... .......... 28% 6.08M 27s
 74650K .......... .......... .......... .......... .......... 28% 7.47M 27s
 74700K .......... .......... .......... .......... .......... 28% 6.97M 27s
 74750K .......... .......... .......... .......... .......... 28% 6.82M 27s
 74800K .......... .......... .......... .......... .......... 28% 8.35M 27s
 74850K .......... .......... .......... .......... .......... 28% 8.73M 27s
 74900K .......... .......... .......... .......... .......... 28% 7.68M 27s
 74950K .......... .......... .......... .......... .......... 28% 6.22M 27s
 75000K .......... .......... .......... .......... .......... 28% 6.59M 27s
 75050K .......... .......... .......... .......... .......... 28% 7.90M 27s
 75100K .......... .......... .......... .......... .......... 28% 6.15M 27s
 75150K .......... .......... .......... .......... .......... 28% 7.54M 27s
 75200K .......... .......... .......... .......... .......... 28% 4.37M 27s
 75250K .......... .......... .......... .......... .......... 28% 6.55M 27s
 75300K .......... .......... .......... .......... .......... 28% 6.38M 27s
 75350K .......... .......... .......... .......... .......... 28% 5.30M 27s
 75400K .......... .......... .......... .......... .......... 28% 6.13M 27s
 75450K .......... .......... .......... .......... .......... 28% 6.15M 27s
 75500K .......... .......... .......... .......... .......... 28% 11.8M 27s
 75550K .......... .......... .......... .......... .......... 28% 14.0M 27s
 75600K .......... .......... .......... .......... .......... 28% 10.8M 27s
 75650K .......... .......... .......... .......... .......... 28% 11.4M 27s
 75700K .......... .......... .......... .......... .......... 28% 8.98M 27s
 75750K .......... .......... .......... .......... .......... 28% 9.75M 27s
 75800K .......... .......... .......... .......... .......... 28% 10.7M 27s
 75850K .......... .......... .......... .......... .......... 28% 7.37M 27s
 75900K .......... .......... .......... .......... .......... 28% 9.30M 27s
 75950K .......... .......... .......... .......... .......... 28% 8.63M 27s
 76000K .......... .......... .......... .......... .......... 28% 6.84M 27s
 76050K .......... .......... .......... .......... .......... 28% 7.97M 27s
 76100K .......... .......... .......... .......... .......... 28% 8.08M 26s
 76150K .......... .......... .......... .......... .......... 28% 8.48M 26s
 76200K .......... .......... .......... .......... .......... 28% 5.37M 26s
 76250K .......... .......... .......... .......... .......... 28% 4.46M 26s
 76300K .......... .......... .......... .......... .......... 28% 3.83M 26s
 76350K .......... .......... .......... .......... .......... 28% 3.92M 26s
 76400K .......... .......... .......... .......... .......... 28% 4.66M 26s
 76450K .......... .......... .......... .......... .......... 28% 12.5M 26s
 76500K .......... .......... .......... .......... .......... 28% 15.5M 26s
 76550K .......... .......... .......... .......... .......... 28% 15.6M 26s
 76600K .......... .......... .......... .......... .......... 28% 11.8M 26s
 76650K .......... .......... .......... .......... .......... 28% 11.3M 26s
 76700K .......... .......... .......... .......... .......... 28% 7.89M 26s
 76750K .......... .......... .......... .......... .......... 28% 12.4M 26s
 76800K .......... .......... .......... .......... .......... 28% 7.95M 26s
 76850K .......... .......... .......... .......... .......... 28% 7.39M 26s
 76900K .......... .......... .......... .......... .......... 28% 4.24M 26s
 76950K .......... .......... .......... .......... .......... 28% 4.29M 26s
 77000K .......... .......... .......... .......... .......... 28% 4.90M 26s
 77050K .......... .......... .......... .......... .......... 29% 5.82M 26s
 77100K .......... .......... .......... .......... .......... 29% 11.9M 26s
 77150K .......... .......... .......... .......... .......... 29% 15.7M 26s
 77200K .......... .......... .......... .......... .......... 29% 10.8M 26s
 77250K .......... .......... .......... .......... .......... 29% 11.5M 26s
 77300K .......... .......... .......... .......... .......... 29% 14.0M 26s
 77350K .......... .......... .......... .......... .......... 29% 12.5M 26s
 77400K .......... .......... .......... .......... .......... 29% 9.15M 26s
 77450K .......... .......... .......... .......... .......... 29% 10.3M 26s
 77500K .......... .......... .......... .......... .......... 29% 10.2M 26s
 77550K .......... .......... .......... .......... .......... 29% 7.10M 26s
 77600K .......... .......... .......... .......... .......... 29% 6.25M 26s
 77650K .......... .......... .......... .......... .......... 29% 5.22M 26s
 77700K .......... .......... .......... .......... .......... 29% 6.12M 26s
 77750K .......... .......... .......... .......... .......... 29% 7.46M 26s
 77800K .......... .......... .......... .......... .......... 29% 7.87M 26s
 77850K .......... .......... .......... .......... .......... 29% 6.37M 26s
 77900K .......... .......... .......... .......... .......... 29% 7.15M 26s
 77950K .......... .......... .......... .......... .......... 29% 5.21M 26s
 78000K .......... .......... .......... .......... .......... 29% 6.57M 26s
 78050K .......... .......... .......... .......... .......... 29% 6.78M 26s
 78100K .......... .......... .......... .......... .......... 29% 9.34M 26s
 78150K .......... .......... .......... .......... .......... 29% 19.5M 26s
 78200K .......... .......... .......... .......... .......... 29% 20.2M 26s
 78250K .......... .......... .......... .......... .......... 29% 16.7M 26s
 78300K .......... .......... .......... .......... .......... 29% 15.2M 26s
 78350K .......... .......... .......... .......... .......... 29% 10.6M 26s
 78400K .......... .......... .......... .......... .......... 29% 13.4M 26s
 78450K .......... .......... .......... .......... .......... 29% 8.72M 26s
 78500K .......... .......... .......... .......... .......... 29% 8.63M 26s
 78550K .......... .......... .......... .......... .......... 29% 9.93M 26s
 78600K .......... .......... .......... .......... .......... 29% 6.79M 26s
 78650K .......... .......... .......... .......... .......... 29% 7.65M 26s
 78700K .......... .......... .......... .......... .......... 29% 4.75M 26s
 78750K .......... .......... .......... .......... .......... 29% 5.00M 26s
 78800K .......... .......... .......... .......... .......... 29% 6.05M 26s
 78850K .......... .......... .......... .......... .......... 29% 4.88M 26s
 78900K .......... .......... .......... .......... .......... 29% 7.07M 26s
 78950K .......... .......... .......... .......... .......... 29% 17.2M 26s
 79000K .......... .......... .......... .......... .......... 29% 14.3M 26s
 79050K .......... .......... .......... .......... .......... 29% 16.4M 26s
 79100K .......... .......... .......... .......... .......... 29% 10.7M 26s
 79150K .......... .......... .......... .......... .......... 29% 12.6M 26s
 79200K .......... .......... .......... .......... .......... 29% 12.1M 26s
 79250K .......... .......... .......... .......... .......... 29% 18.0M 26s
 79300K .......... .......... .......... .......... .......... 29% 12.2M 26s
 79350K .......... .......... .......... .......... .......... 29% 7.19M 26s
 79400K .......... .......... .......... .......... .......... 29% 13.8M 26s
 79450K .......... .......... .......... .......... .......... 29% 7.69M 26s
 79500K .......... .......... .......... .......... .......... 29% 7.45M 26s
 79550K .......... .......... .......... .......... .......... 29% 5.44M 26s
 79600K .......... .......... .......... .......... .......... 29% 6.13M 26s
 79650K .......... .......... .......... .......... .......... 29% 5.95M 26s
 79700K .......... .......... .......... .......... .......... 30% 4.50M 26s
 79750K .......... .......... .......... .......... .......... 30% 5.31M 26s
 79800K .......... .......... .......... .......... .......... 30% 5.17M 26s
 79850K .......... .......... .......... .......... .......... 30% 4.24M 26s
 79900K .......... .......... .......... .......... .......... 30% 13.9M 26s
 79950K .......... .......... .......... .......... .......... 30% 7.17M 26s
 80000K .......... .......... .......... .......... .......... 30% 7.43M 26s
 80050K .......... .......... .......... .......... .......... 30% 8.69M 26s
 80100K .......... .......... .......... .......... .......... 30% 7.59M 26s
 80150K .......... .......... .......... .......... .......... 30% 9.60M 26s
 80200K .......... .......... .......... .......... .......... 30% 7.50M 26s
 80250K .......... .......... .......... .......... .......... 30% 10.1M 26s
 80300K .......... .......... .......... .......... .......... 30% 11.0M 26s
 80350K .......... .......... .......... .......... .......... 30% 21.6M 26s
 80400K .......... .......... .......... .......... .......... 30% 11.9M 26s
 80450K .......... .......... .......... .......... .......... 30% 33.1M 26s
 80500K .......... .......... .......... .......... .......... 30% 15.8M 26s
 80550K .......... .......... .......... .......... .......... 30% 13.7M 26s
 80600K .......... .......... .......... .......... .......... 30% 11.2M 26s
 80650K .......... .......... .......... .......... .......... 30% 11.7M 26s
 80700K .......... .......... .......... .......... .......... 30% 10.6M 26s
 80750K .......... .......... .......... .......... .......... 30% 11.8M 26s
 80800K .......... .......... .......... .......... .......... 30% 10.2M 26s
 80850K .......... .......... .......... .......... .......... 30% 7.39M 26s
 80900K .......... .......... .......... .......... .......... 30% 9.62M 26s
 80950K .......... .......... .......... .......... .......... 30% 8.73M 26s
 81000K .......... .......... .......... .......... .......... 30% 8.77M 26s
 81050K .......... .......... .......... .......... .......... 30% 7.12M 26s
 81100K .......... .......... .......... .......... .......... 30% 7.85M 26s
 81150K .......... .......... .......... .......... .......... 30% 7.57M 26s
 81200K .......... .......... .......... .......... .......... 30% 6.82M 26s
 81250K .......... .......... .......... .......... .......... 30% 8.03M 26s
 81300K .......... .......... .......... .......... .......... 30% 8.21M 26s
 81350K .......... .......... .......... .......... .......... 30% 6.19M 26s
 81400K .......... .......... .......... .......... .......... 30% 9.24M 26s
 81450K .......... .......... .......... .......... .......... 30% 14.2M 26s
 81500K .......... .......... .......... .......... .......... 30% 17.1M 26s
 81550K .......... .......... .......... .......... .......... 30% 14.0M 25s
 81600K .......... .......... .......... .......... .......... 30% 10.0M 25s
 81650K .......... .......... .......... .......... .......... 30% 8.45M 25s
 81700K .......... .......... .......... .......... .......... 30% 9.34M 25s
 81750K .......... .......... .......... .......... .......... 30% 5.75M 25s
 81800K .......... .......... .......... .......... .......... 30% 5.83M 25s
 81850K .......... .......... .......... .......... .......... 30% 6.14M 25s
 81900K .......... .......... .......... .......... .......... 30% 10.0M 25s
 81950K .......... .......... .......... .......... .......... 30% 9.14M 25s
 82000K .......... .......... .......... .......... .......... 30% 9.24M 25s
 82050K .......... .......... .......... .......... .......... 30% 10.3M 25s
 82100K .......... .......... .......... .......... .......... 30% 7.07M 25s
 82150K .......... .......... .......... .......... .......... 30% 6.78M 25s
 82200K .......... .......... .......... .......... .......... 30% 5.86M 25s
 82250K .......... .......... .......... .......... .......... 30% 7.26M 25s
 82300K .......... .......... .......... .......... .......... 30% 8.00M 25s
 82350K .......... .......... .......... .......... .......... 31% 5.11M 25s
 82400K .......... .......... .......... .......... .......... 31% 6.43M 25s
 82450K .......... .......... .......... .......... .......... 31% 5.50M 25s
 82500K .......... .......... .......... .......... .......... 31% 4.69M 25s
 82550K .......... .......... .......... .......... .......... 31% 4.76M 25s
 82600K .......... .......... .......... .......... .......... 31% 4.82M 25s
 82650K .......... .......... .......... .......... .......... 31% 5.61M 25s
 82700K .......... .......... .......... .......... .......... 31% 6.54M 25s
 82750K .......... .......... .......... .......... .......... 31% 11.1M 25s
 82800K .......... .......... .......... .......... .......... 31% 6.60M 25s
 82850K .......... .......... .......... .......... .......... 31% 3.37M 25s
 82900K .......... .......... .......... .......... .......... 31% 4.21M 25s
 82950K .......... .......... .......... .......... .......... 31% 4.43M 25s
 83000K .......... .......... .......... .......... .......... 31% 14.0M 25s
 83050K .......... .......... .......... .......... .......... 31% 15.0M 25s
 83100K .......... .......... .......... .......... .......... 31% 10.5M 25s
 83150K .......... .......... .......... .......... .......... 31% 17.3M 25s
 83200K .......... .......... .......... .......... .......... 31% 13.7M 25s
 83250K .......... .......... .......... .......... .......... 31% 13.2M 25s
 83300K .......... .......... .......... .......... .......... 31% 13.1M 25s
 83350K .......... .......... .......... .......... .......... 31% 7.24M 25s
 83400K .......... .......... .......... .......... .......... 31% 19.5M 25s
 83450K .......... .......... .......... .......... .......... 31% 10.6M 25s
 83500K .......... .......... .......... .......... .......... 31% 8.85M 25s
 83550K .......... .......... .......... .......... .......... 31% 9.13M 25s
 83600K .......... .......... .......... .......... .......... 31% 6.74M 25s
 83650K .......... .......... .......... .......... .......... 31% 9.36M 25s
 83700K .......... .......... .......... .......... .......... 31% 8.70M 25s
 83750K .......... .......... .......... .......... .......... 31% 11.6M 25s
 83800K .......... .......... .......... .......... .......... 31% 8.87M 25s
 83850K .......... .......... .......... .......... .......... 31% 7.80M 25s
 83900K .......... .......... .......... .......... .......... 31% 8.72M 25s
 83950K .......... .......... .......... .......... .......... 31% 5.77M 25s
 84000K .......... .......... .......... .......... .......... 31% 8.47M 25s
 84050K .......... .......... .......... .......... .......... 31% 8.53M 25s
 84100K .......... .......... .......... .......... .......... 31% 6.45M 25s
 84150K .......... .......... .......... .......... .......... 31% 7.60M 25s
 84200K .......... .......... .......... .......... .......... 31% 7.53M 25s
 84250K .......... .......... .......... .......... .......... 31% 17.1M 25s
 84300K .......... .......... .......... .......... .......... 31% 15.2M 25s
 84350K .......... .......... .......... .......... .......... 31% 19.8M 25s
 84400K .......... .......... .......... .......... .......... 31% 13.9M 25s
 84450K .......... .......... .......... .......... .......... 31% 13.7M 25s
 84500K .......... .......... .......... .......... .......... 31% 9.81M 25s
 84550K .......... .......... .......... .......... .......... 31% 10.4M 25s
 84600K .......... .......... .......... .......... .......... 31% 8.97M 25s
 84650K .......... .......... .......... .......... .......... 31% 11.3M 25s
 84700K .......... .......... .......... .......... .......... 31% 8.27M 25s
 84750K .......... .......... .......... .......... .......... 31% 10.3M 25s
 84800K .......... .......... .......... .......... .......... 31% 9.93M 25s
 84850K .......... .......... .......... .......... .......... 31% 8.02M 25s
 84900K .......... .......... .......... .......... .......... 31% 8.63M 25s
 84950K .......... .......... .......... .......... .......... 31% 9.20M 25s
 85000K .......... .......... .......... .......... .......... 31% 10.5M 25s
 85050K .......... .......... .......... .......... .......... 32% 12.6M 25s
 85100K .......... .......... .......... .......... .......... 32% 9.58M 25s
 85150K .......... .......... .......... .......... .......... 32% 12.0M 25s
 85200K .......... .......... .......... .......... .......... 32% 9.47M 25s
 85250K .......... .......... .......... .......... .......... 32% 9.74M 25s
 85300K .......... .......... .......... .......... .......... 32% 10.7M 25s
 85350K .......... .......... .......... .......... .......... 32% 12.6M 25s
 85400K .......... .......... .......... .......... .......... 32% 15.9M 25s
 85450K .......... .......... .......... .......... .......... 32% 11.1M 25s
 85500K .......... .......... .......... .......... .......... 32% 16.6M 25s
 85550K .......... .......... .......... .......... .......... 32% 10.4M 25s
 85600K .......... .......... .......... .......... .......... 32% 9.46M 25s
 85650K .......... .......... .......... .......... .......... 32% 14.5M 25s
 85700K .......... .......... .......... .......... .......... 32% 9.91M 25s
 85750K .......... .......... .......... .......... .......... 32% 9.59M 25s
 85800K .......... .......... .......... .......... .......... 32% 11.7M 25s
 85850K .......... .......... .......... .......... .......... 32% 10.0M 25s
 85900K .......... .......... .......... .......... .......... 32% 12.0M 25s
 85950K .......... .......... .......... .......... .......... 32% 9.47M 25s
 86000K .......... .......... .......... .......... .......... 32% 10.9M 25s
 86050K .......... .......... .......... .......... .......... 32% 8.00M 25s
 86100K .......... .......... .......... .......... .......... 32% 20.2M 25s
 86150K .......... .......... .......... .......... .......... 32% 15.5M 25s
 86200K .......... .......... .......... .......... .......... 32% 14.1M 25s
 86250K .......... .......... .......... .......... .......... 32% 11.6M 25s
 86300K .......... .......... .......... .......... .......... 32% 12.0M 25s
 86350K .......... .......... .......... .......... .......... 32% 12.6M 25s
 86400K .......... .......... .......... .......... .......... 32% 13.4M 25s
 86450K .......... .......... .......... .......... .......... 32% 9.38M 25s
 86500K .......... .......... .......... .......... .......... 32% 11.0M 25s
 86550K .......... .......... .......... .......... .......... 32% 10.7M 25s
 86600K .......... .......... .......... .......... .......... 32% 10.6M 24s
 86650K .......... .......... .......... .......... .......... 32% 11.6M 24s
 86700K .......... .......... .......... .......... .......... 32% 8.58M 24s
 86750K .......... .......... .......... .......... .......... 32% 16.0M 24s
 86800K .......... .......... .......... .......... .......... 32% 11.4M 24s
 86850K .......... .......... .......... .......... .......... 32% 8.51M 24s
 86900K .......... .......... .......... .......... .......... 32% 10.9M 24s
 86950K .......... .......... .......... .......... .......... 32% 7.66M 24s
 87000K .......... .......... .......... .......... .......... 32% 9.49M 24s
 87050K .......... .......... .......... .......... .......... 32% 6.78M 24s
 87100K .......... .......... .......... .......... .......... 32% 4.64M 24s
 87150K .......... .......... .......... .......... .......... 32% 7.92M 24s
 87200K .......... .......... .......... .......... .......... 32% 3.71M 24s
 87250K .......... .......... .......... .......... .......... 32% 4.81M 24s
 87300K .......... .......... .......... .......... .......... 32% 10.4M 24s
 87350K .......... .......... .......... .......... .......... 32% 6.28M 24s
 87400K .......... .......... .......... .......... .......... 32% 6.60M 24s
 87450K .......... .......... .......... .......... .......... 32% 5.29M 24s
 87500K .......... .......... .......... .......... .......... 32% 6.08M 24s
 87550K .......... .......... .......... .......... .......... 32% 6.75M 24s
 87600K .......... .......... .......... .......... .......... 32% 12.6M 24s
 87650K .......... .......... .......... .......... .......... 32% 35.9M 24s
 87700K .......... .......... .......... .......... .......... 33% 13.9M 24s
 87750K .......... .......... .......... .......... .......... 33%  185M 24s
 87800K .......... .......... .......... .......... .......... 33% 20.2M 24s
 87850K .......... .......... .......... .......... .......... 33% 18.9M 24s
 87900K .......... .......... .......... .......... .......... 33% 12.0M 24s
 87950K .......... .......... .......... .......... .......... 33% 14.9M 24s
 88000K .......... .......... .......... .......... .......... 33% 15.5M 24s
 88050K .......... .......... .......... .......... .......... 33% 13.4M 24s
 88100K .......... .......... .......... .......... .......... 33% 13.5M 24s
 88150K .......... .......... .......... .......... .......... 33% 14.3M 24s
 88200K .......... .......... .......... .......... .......... 33% 13.7M 24s
 88250K .......... .......... .......... .......... .......... 33% 11.4M 24s
 88300K .......... .......... .......... .......... .......... 33% 13.4M 24s
 88350K .......... .......... .......... .......... .......... 33% 10.8M 24s
 88400K .......... .......... .......... .......... .......... 33% 9.52M 24s
 88450K .......... .......... .......... .......... .......... 33% 6.97M 24s
 88500K .......... .......... .......... .......... .......... 33% 8.80M 24s
 88550K .......... .......... .......... .......... .......... 33% 7.11M 24s
 88600K .......... .......... .......... .......... .......... 33% 8.84M 24s
 88650K .......... .......... .......... .......... .......... 33% 7.81M 24s
 88700K .......... .......... .......... .......... .......... 33% 5.61M 24s
 88750K .......... .......... .......... .......... .......... 33% 6.78M 24s
 88800K .......... .......... .......... .......... .......... 33% 7.36M 24s
 88850K .......... .......... .......... .......... .......... 33% 5.90M 24s
 88900K .......... .......... .......... .......... .......... 33% 7.67M 24s
 88950K .......... .......... .......... .......... .......... 33% 6.04M 24s
 89000K .......... .......... .......... .......... .......... 33% 5.74M 24s
 89050K .......... .......... .......... .......... .......... 33% 9.59M 24s
 89100K .......... .......... .......... .......... .......... 33% 6.43M 24s
 89150K .......... .......... .......... .......... .......... 33% 7.24M 24s
 89200K .......... .......... .......... .......... .......... 33% 6.35M 24s
 89250K .......... .......... .......... .......... .......... 33% 8.54M 24s
 89300K .......... .......... .......... .......... .......... 33% 20.9M 24s
 89350K .......... .......... .......... .......... .......... 33% 32.4M 24s
 89400K .......... .......... .......... .......... .......... 33% 18.1M 24s
 89450K .......... .......... .......... .......... .......... 33% 17.0M 24s
 89500K .......... .......... .......... .......... .......... 33% 28.5M 24s
 89550K .......... .......... .......... .......... .......... 33% 11.1M 24s
 89600K .......... .......... .......... .......... .......... 33% 8.73M 24s
 89650K .......... .......... .......... .......... .......... 33% 8.21M 24s
 89700K .......... .......... .......... .......... .......... 33% 10.2M 24s
 89750K .......... .......... .......... .......... .......... 33% 11.0M 24s
 89800K .......... .......... .......... .......... .......... 33% 9.50M 24s
 89850K .......... .......... .......... .......... .......... 33% 7.56M 24s
 89900K .......... .......... .......... .......... .......... 33% 9.00M 24s
 89950K .......... .......... .......... .......... .......... 33% 10.2M 24s
 90000K .......... .......... .......... .......... .......... 33% 10.9M 24s
 90050K .......... .......... .......... .......... .......... 33% 10.3M 24s
 90100K .......... .......... .......... .......... .......... 33% 7.23M 24s
 90150K .......... .......... .......... .......... .......... 33% 8.82M 24s
 90200K .......... .......... .......... .......... .......... 33% 4.76M 24s
 90250K .......... .......... .......... .......... .......... 33% 2.63M 24s
 90300K .......... .......... .......... .......... .......... 33% 2.84M 24s
 90350K .......... .......... .......... .......... .......... 34% 6.22M 24s
 90400K .......... .......... .......... .......... .......... 34% 29.0M 24s
 90450K .......... .......... .......... .......... .......... 34% 12.1M 24s
 90500K .......... .......... .......... .......... .......... 34% 6.75M 24s
 90550K .......... .......... .......... .......... .......... 34% 5.60M 24s
 90600K .......... .......... .......... .......... .......... 34% 5.30M 24s
 90650K .......... .......... .......... .......... .......... 34% 5.99M 24s
 90700K .......... .......... .......... .......... .......... 34% 6.51M 24s
 90750K .......... .......... .......... .......... .......... 34% 16.0M 24s
 90800K .......... .......... .......... .......... .......... 34% 12.9M 24s
 90850K .......... .......... .......... .......... .......... 34% 13.7M 24s
 90900K .......... .......... .......... .......... .......... 34% 14.2M 24s
 90950K .......... .......... .......... .......... .......... 34% 7.21M 24s
 91000K .......... .......... .......... .......... .......... 34% 8.10M 24s
 91050K .......... .......... .......... .......... .......... 34% 6.92M 24s
 91100K .......... .......... .......... .......... .......... 34% 7.47M 24s
 91150K .......... .......... .......... .......... .......... 34% 7.53M 24s
 91200K .......... .......... .......... .......... .......... 34% 9.57M 24s
 91250K .......... .......... .......... .......... .......... 34% 8.61M 24s
 91300K .......... .......... .......... .......... .......... 34% 10.5M 24s
 91350K .......... .......... .......... .......... .......... 34% 11.6M 24s
 91400K .......... .......... .......... .......... .......... 34% 10.2M 24s
 91450K .......... .......... .......... .......... .......... 34% 9.69M 24s
 91500K .......... .......... .......... .......... .......... 34% 7.65M 24s
 91550K .......... .......... .......... .......... .......... 34% 10.0M 24s
 91600K .......... .......... .......... .......... .......... 34% 9.98M 24s
 91650K .......... .......... .......... .......... .......... 34% 8.40M 24s
 91700K .......... .......... .......... .......... .......... 34% 5.91M 24s
 91750K .......... .......... .......... .......... .......... 34% 7.44M 24s
 91800K .......... .......... .......... .......... .......... 34% 9.22M 24s
 91850K .......... .......... .......... .......... .......... 34% 6.37M 24s
 91900K .......... .......... .......... .......... .......... 34% 8.95M 24s
 91950K .......... .......... .......... .......... .......... 34% 7.09M 24s
 92000K .......... .......... .......... .......... .......... 34% 9.48M 24s
 92050K .......... .......... .......... .......... .......... 34% 13.9M 24s
 92100K .......... .......... .......... .......... .......... 34% 92.3M 24s
 92150K .......... .......... .......... .......... .......... 34% 23.9M 24s
 92200K .......... .......... .......... .......... .......... 34% 21.8M 23s
 92250K .......... .......... .......... .......... .......... 34% 28.6M 23s
 92300K .......... .......... .......... .......... .......... 34% 16.1M 23s
 92350K .......... .......... .......... .......... .......... 34% 13.5M 23s
 92400K .......... .......... .......... .......... .......... 34% 14.5M 23s
 92450K .......... .......... .......... .......... .......... 34% 9.05M 23s
 92500K .......... .......... .......... .......... .......... 34% 10.8M 23s
 92550K .......... .......... .......... .......... .......... 34% 8.61M 23s
 92600K .......... .......... .......... .......... .......... 34% 10.0M 23s
 92650K .......... .......... .......... .......... .......... 34% 10.8M 23s
 92700K .......... .......... .......... .......... .......... 34% 11.1M 23s
 92750K .......... .......... .......... .......... .......... 34% 11.9M 23s
 92800K .......... .......... .......... .......... .......... 34% 9.39M 23s
 92850K .......... .......... .......... .......... .......... 34% 10.2M 23s
 92900K .......... .......... .......... .......... .......... 34% 20.6M 23s
 92950K .......... .......... .......... .......... .......... 34% 13.7M 23s
 93000K .......... .......... .......... .......... .......... 35%  208M 23s
 93050K .......... .......... .......... .......... .......... 35% 20.3M 23s
 93100K .......... .......... .......... .......... .......... 35% 22.4M 23s
 93150K .......... .......... .......... .......... .......... 35% 13.2M 23s
 93200K .......... .......... .......... .......... .......... 35% 10.9M 23s
 93250K .......... .......... .......... .......... .......... 35% 8.16M 23s
 93300K .......... .......... .......... .......... .......... 35% 16.1M 23s
 93350K .......... .......... .......... .......... .......... 35% 9.05M 23s
 93400K .......... .......... .......... .......... .......... 35% 8.37M 23s
 93450K .......... .......... .......... .......... .......... 35% 4.45M 23s
 93500K .......... .......... .......... .......... .......... 35% 5.52M 23s
 93550K .......... .......... .......... .......... .......... 35% 6.68M 23s
 93600K .......... .......... .......... .......... .......... 35% 4.89M 23s
 93650K .......... .......... .......... .......... .......... 35% 17.5M 23s
 93700K .......... .......... .......... .......... .......... 35% 9.50M 23s
 93750K .......... .......... .......... .......... .......... 35% 44.6M 23s
 93800K .......... .......... .......... .......... .......... 35% 12.4M 23s
 93850K .......... .......... .......... .......... .......... 35% 9.98M 23s
 93900K .......... .......... .......... .......... .......... 35% 8.27M 23s
 93950K .......... .......... .......... .......... .......... 35% 8.11M 23s
 94000K .......... .......... .......... .......... .......... 35% 8.99M 23s
 94050K .......... .......... .......... .......... .......... 35% 5.61M 23s
 94100K .......... .......... .......... .......... .......... 35% 4.99M 23s
 94150K .......... .......... .......... .......... .......... 35% 6.05M 23s
 94200K .......... .......... .......... .......... .......... 35% 5.80M 23s
 94250K .......... .......... .......... .......... .......... 35% 6.37M 23s
 94300K .......... .......... .......... .......... .......... 35% 6.85M 23s
 94350K .......... .......... .......... .......... .......... 35% 8.17M 23s
 94400K .......... .......... .......... .......... .......... 35% 11.3M 23s
 94450K .......... .......... .......... .......... .......... 35% 12.6M 23s
 94500K .......... .......... .......... .......... .......... 35% 12.3M 23s
 94550K .......... .......... .......... .......... .......... 35% 8.23M 23s
 94600K .......... .......... .......... .......... .......... 35% 5.55M 23s
 94650K .......... .......... .......... .......... .......... 35% 5.23M 23s
 94700K .......... .......... .......... .......... .......... 35% 4.26M 23s
 94750K .......... .......... .......... .......... .......... 35% 10.2M 23s
 94800K .......... .......... .......... .......... .......... 35% 8.29M 23s
 94850K .......... .......... .......... .......... .......... 35% 7.04M 23s
 94900K .......... .......... .......... .......... .......... 35% 11.4M 23s
 94950K .......... .......... .......... .......... .......... 35% 10.4M 23s
 95000K .......... .......... .......... .......... .......... 35% 12.5M 23s
 95050K .......... .......... .......... .......... .......... 35% 10.9M 23s
 95100K .......... .......... .......... .......... .......... 35% 9.99M 23s
 95150K .......... .......... .......... .......... .......... 35% 6.65M 23s
 95200K .......... .......... .......... .......... .......... 35% 5.97M 23s
 95250K .......... .......... .......... .......... .......... 35% 7.00M 23s
 95300K .......... .......... .......... .......... .......... 35% 6.49M 23s
 95350K .......... .......... .......... .......... .......... 35% 7.35M 23s
 95400K .......... .......... .......... .......... .......... 35% 9.49M 23s
 95450K .......... .......... .......... .......... .......... 35% 7.81M 23s
 95500K .......... .......... .......... .......... .......... 35% 9.42M 23s
 95550K .......... .......... .......... .......... .......... 35% 12.1M 23s
 95600K .......... .......... .......... .......... .......... 35% 9.25M 23s
 95650K .......... .......... .......... .......... .......... 36% 6.78M 23s
 95700K .......... .......... .......... .......... .......... 36% 7.37M 23s
 95750K .......... .......... .......... .......... .......... 36% 9.09M 23s
 95800K .......... .......... .......... .......... .......... 36% 7.98M 23s
 95850K .......... .......... .......... .......... .......... 36% 7.46M 23s
 95900K .......... .......... .......... .......... .......... 36% 7.90M 23s
 95950K .......... .......... .......... .......... .......... 36% 7.11M 23s
 96000K .......... .......... .......... .......... .......... 36% 13.0M 23s
 96050K .......... .......... .......... .......... .......... 36% 16.1M 23s
 96100K .......... .......... .......... .......... .......... 36% 16.2M 23s
 96150K .......... .......... .......... .......... .......... 36% 16.4M 23s
 96200K .......... .......... .......... .......... .......... 36% 17.0M 23s
 96250K .......... .......... .......... .......... .......... 36% 15.9M 23s
 96300K .......... .......... .......... .......... .......... 36% 14.6M 23s
 96350K .......... .......... .......... .......... .......... 36% 12.4M 23s
 96400K .......... .......... .......... .......... .......... 36% 22.8M 23s
 96450K .......... .......... .......... .......... .......... 36% 13.2M 23s
 96500K .......... .......... .......... .......... .......... 36% 17.8M 23s
 96550K .......... .......... .......... .......... .......... 36% 21.5M 23s
 96600K .......... .......... .......... .......... .......... 36% 22.6M 23s
 96650K .......... .......... .......... .......... .......... 36% 46.7M 23s
 96700K .......... .......... .......... .......... .......... 36% 37.0M 23s
 96750K .......... .......... .......... .......... .......... 36% 19.9M 23s
 96800K .......... .......... .......... .......... .......... 36%  116M 23s
 96850K .......... .......... .......... .......... .......... 36%  107M 23s
 96900K .......... .......... .......... .......... .......... 36% 27.4M 23s
 96950K .......... .......... .......... .......... .......... 36% 57.2M 23s
 97000K .......... .......... .......... .......... .......... 36% 53.5M 23s
 97050K .......... .......... .......... .......... .......... 36% 40.4M 23s
 97100K .......... .......... .......... .......... .......... 36% 22.2M 22s
 97150K .......... .......... .......... .......... .......... 36% 26.4M 22s
 97200K .......... .......... .......... .......... .......... 36% 25.8M 22s
 97250K .......... .......... .......... .......... .......... 36% 26.5M 22s
 97300K .......... .......... .......... .......... .......... 36% 25.7M 22s
 97350K .......... .......... .......... .......... .......... 36% 22.1M 22s
 97400K .......... .......... .......... .......... .......... 36% 24.9M 22s
 97450K .......... .......... .......... .......... .......... 36% 17.7M 22s
 97500K .......... .......... .......... .......... .......... 36% 27.9M 22s
 97550K .......... .......... .......... .......... .......... 36% 19.0M 22s
 97600K .......... .......... .......... .......... .......... 36% 19.1M 22s
 97650K .......... .......... .......... .......... .......... 36% 22.6M 22s
 97700K .......... .......... .......... .......... .......... 36% 16.8M 22s
 97750K .......... .......... .......... .......... .......... 36% 16.6M 22s
 97800K .......... .......... .......... .......... .......... 36% 8.80M 22s
 97850K .......... .......... .......... .......... .......... 36% 10.3M 22s
 97900K .......... .......... .......... .......... .......... 36% 11.0M 22s
 97950K .......... .......... .......... .......... .......... 36% 8.92M 22s
 98000K .......... .......... .......... .......... .......... 36% 10.1M 22s
 98050K .......... .......... .......... .......... .......... 36% 9.95M 22s
 98100K .......... .......... .......... .......... .......... 36% 7.98M 22s
 98150K .......... .......... .......... .......... .......... 36% 9.20M 22s
 98200K .......... .......... .......... .......... .......... 36% 5.93M 22s
 98250K .......... .......... .......... .......... .......... 36% 7.18M 22s
 98300K .......... .......... .......... .......... .......... 37% 6.61M 22s
 98350K .......... .......... .......... .......... .......... 37% 6.00M 22s
 98400K .......... .......... .......... .......... .......... 37% 10.1M 22s
 98450K .......... .......... .......... .......... .......... 37% 8.20M 22s
 98500K .......... .......... .......... .......... .......... 37% 9.37M 22s
 98550K .......... .......... .......... .......... .......... 37% 7.64M 22s
 98600K .......... .......... .......... .......... .......... 37% 7.61M 22s
 98650K .......... .......... .......... .......... .......... 37% 7.65M 22s
 98700K .......... .......... .......... .......... .......... 37% 6.39M 22s
 98750K .......... .......... .......... .......... .......... 37% 8.44M 22s
 98800K .......... .......... .......... .......... .......... 37% 7.97M 22s
 98850K .......... .......... .......... .......... .......... 37% 7.18M 22s
 98900K .......... .......... .......... .......... .......... 37% 7.38M 22s
 98950K .......... .......... .......... .......... .......... 37% 3.70M 22s
 99000K .......... .......... .......... .......... .......... 37% 3.91M 22s
 99050K .......... .......... .......... .......... .......... 37% 6.38M 22s
 99100K .......... .......... .......... .......... .......... 37% 5.28M 22s
 99150K .......... .......... .......... .......... .......... 37% 4.79M 22s
 99200K .......... .......... .......... .......... .......... 37% 4.35M 22s
 99250K .......... .......... .......... .......... .......... 37% 5.64M 22s
 99300K .......... .......... .......... .......... .......... 37% 6.01M 22s
 99350K .......... .......... .......... .......... .......... 37% 5.82M 22s
 99400K .......... .......... .......... .......... .......... 37% 8.65M 22s
 99450K .......... .......... .......... .......... .......... 37% 8.05M 22s
 99500K .......... .......... .......... .......... .......... 37% 8.96M 22s
 99550K .......... .......... .......... .......... .......... 37% 9.75M 22s
 99600K .......... .......... .......... .......... .......... 37% 7.74M 22s
 99650K .......... .......... .......... .......... .......... 37% 9.12M 22s
 99700K .......... .......... .......... .......... .......... 37% 8.32M 22s
 99750K .......... .......... .......... .......... .......... 37% 56.3M 22s
 99800K .......... .......... .......... .......... .......... 37% 16.5M 22s
 99850K .......... .......... .......... .......... .......... 37% 18.2M 22s
 99900K .......... .......... .......... .......... .......... 37% 10.1M 22s
 99950K .......... .......... .......... .......... .......... 37% 6.81M 22s
100000K .......... .......... .......... .......... .......... 37% 8.07M 22s
100050K .......... .......... .......... .......... .......... 37% 7.91M 22s
100100K .......... .......... .......... .......... .......... 37% 11.8M 22s
100150K .......... .......... .......... .......... .......... 37% 12.6M 22s
100200K .......... .......... .......... .......... .......... 37% 11.2M 22s
100250K .......... .......... .......... .......... .......... 37% 11.5M 22s
100300K .......... .......... .......... .......... .......... 37% 10.6M 22s
100350K .......... .......... .......... .......... .......... 37% 10.8M 22s
100400K .......... .......... .......... .......... .......... 37% 9.10M 22s
100450K .......... .......... .......... .......... .......... 37% 6.88M 22s
100500K .......... .......... .......... .......... .......... 37% 8.67M 22s
100550K .......... .......... .......... .......... .......... 37% 8.43M 22s
100600K .......... .......... .......... .......... .......... 37% 6.81M 22s
100650K .......... .......... .......... .......... .......... 37% 8.26M 22s
100700K .......... .......... .......... .......... .......... 37% 7.78M 22s
100750K .......... .......... .......... .......... .......... 37% 9.02M 22s
100800K .......... .......... .......... .......... .......... 37% 7.86M 22s
100850K .......... .......... .......... .......... .......... 37% 8.85M 22s
100900K .......... .......... .......... .......... .......... 37% 14.1M 22s
100950K .......... .......... .......... .......... .......... 37% 9.71M 22s
101000K .......... .......... .......... .......... .......... 38% 11.6M 22s
101050K .......... .......... .......... .......... .......... 38% 14.6M 22s
101100K .......... .......... .......... .......... .......... 38% 10.9M 22s
101150K .......... .......... .......... .......... .......... 38% 13.3M 22s
101200K .......... .......... .......... .......... .......... 38% 8.89M 22s
101250K .......... .......... .......... .......... .......... 38% 10.8M 22s
101300K .......... .......... .......... .......... .......... 38% 11.0M 22s
101350K .......... .......... .......... .......... .......... 38% 11.1M 22s
101400K .......... .......... .......... .......... .......... 38% 12.7M 22s
101450K .......... .......... .......... .......... .......... 38% 9.93M 22s
101500K .......... .......... .......... .......... .......... 38% 12.5M 22s
101550K .......... .......... .......... .......... .......... 38% 8.18M 22s
101600K .......... .......... .......... .......... .......... 38% 15.8M 22s
101650K .......... .......... .......... .......... .......... 38% 15.4M 22s
101700K .......... .......... .......... .......... .......... 38% 8.59M 22s
101750K .......... .......... .......... .......... .......... 38% 15.0M 22s
101800K .......... .......... .......... .......... .......... 38% 12.9M 22s
101850K .......... .......... .......... .......... .......... 38% 13.1M 22s
101900K .......... .......... .......... .......... .......... 38% 14.0M 22s
101950K .......... .......... .......... .......... .......... 38% 11.1M 22s
102000K .......... .......... .......... .......... .......... 38% 11.6M 22s
102050K .......... .......... .......... .......... .......... 38% 11.8M 22s
102100K .......... .......... .......... .......... .......... 38% 9.65M 22s
102150K .......... .......... .......... .......... .......... 38% 11.4M 22s
102200K .......... .......... .......... .......... .......... 38% 9.27M 22s
102250K .......... .......... .......... .......... .......... 38% 12.2M 22s
102300K .......... .......... .......... .......... .......... 38% 10.0M 22s
102350K .......... .......... .......... .......... .......... 38% 9.06M 22s
102400K .......... .......... .......... .......... .......... 38% 9.33M 22s
102450K .......... .......... .......... .......... .......... 38% 7.73M 22s
102500K .......... .......... .......... .......... .......... 38% 8.90M 22s
102550K .......... .......... .......... .......... .......... 38% 6.11M 22s
102600K .......... .......... .......... .......... .......... 38% 3.46M 22s
102650K .......... .......... .......... .......... .......... 38% 4.24M 22s
102700K .......... .......... .......... .......... .......... 38% 4.39M 22s
102750K .......... .......... .......... .......... .......... 38% 5.88M 22s
102800K .......... .......... .......... .......... .......... 38% 5.25M 22s
102850K .......... .......... .......... .......... .......... 38% 4.65M 22s
102900K .......... .......... .......... .......... .......... 38% 6.79M 22s
102950K .......... .......... .......... .......... .......... 38% 3.85M 22s
103000K .......... .......... .......... .......... .......... 38% 5.36M 22s
103050K .......... .......... .......... .......... .......... 38% 4.77M 22s
103100K .......... .......... .......... .......... .......... 38% 4.24M 22s
103150K .......... .......... .......... .......... .......... 38% 6.60M 22s
103200K .......... .......... .......... .......... .......... 38% 3.77M 22s
103250K .......... .......... .......... .......... .......... 38% 4.06M 22s
103300K .......... .......... .......... .......... .......... 38% 4.45M 22s
103350K .......... .......... .......... .......... .......... 38% 3.20M 22s
103400K .......... .......... .......... .......... .......... 38% 4.39M 22s
103450K .......... .......... .......... .......... .......... 38% 4.22M 22s
103500K .......... .......... .......... .......... .......... 38% 33.6M 22s
103550K .......... .......... .......... .......... .......... 38% 32.1M 21s
103600K .......... .......... .......... .......... .......... 38% 15.2M 21s
103650K .......... .......... .......... .......... .......... 39% 39.6M 21s
103700K .......... .......... .......... .......... .......... 39% 39.5M 21s
103750K .......... .......... .......... .......... .......... 39% 29.6M 21s
103800K .......... .......... .......... .......... .......... 39% 18.5M 21s
103850K .......... .......... .......... .......... .......... 39% 9.94M 21s
103900K .......... .......... .......... .......... .......... 39% 10.2M 21s
103950K .......... .......... .......... .......... .......... 39% 11.4M 21s
104000K .......... .......... .......... .......... .......... 39% 10.2M 21s
104050K .......... .......... .......... .......... .......... 39% 12.4M 21s
104100K .......... .......... .......... .......... .......... 39% 9.37M 21s
104150K .......... .......... .......... .......... .......... 39% 11.4M 21s
104200K .......... .......... .......... .......... .......... 39% 7.85M 21s
104250K .......... .......... .......... .......... .......... 39% 11.7M 21s
104300K .......... .......... .......... .......... .......... 39%  153M 21s
104350K .......... .......... .......... .......... .......... 39% 12.2M 21s
104400K .......... .......... .......... .......... .......... 39% 87.3M 21s
104450K .......... .......... .......... .......... .......... 39% 12.8M 21s
104500K .......... .......... .......... .......... .......... 39% 8.05M 21s
104550K .......... .......... .......... .......... .......... 39% 10.4M 21s
104600K .......... .......... .......... .......... .......... 39% 11.4M 21s
104650K .......... .......... .......... .......... .......... 39% 15.6M 21s
104700K .......... .......... .......... .......... .......... 39% 9.06M 21s
104750K .......... .......... .......... .......... .......... 39% 10.2M 21s
104800K .......... .......... .......... .......... .......... 39% 11.6M 21s
104850K .......... .......... .......... .......... .......... 39% 9.93M 21s
104900K .......... .......... .......... .......... .......... 39% 12.9M 21s
104950K .......... .......... .......... .......... .......... 39% 8.14M 21s
105000K .......... .......... .......... .......... .......... 39% 9.72M 21s
105050K .......... .......... .......... .......... .......... 39% 10.3M 21s
105100K .......... .......... .......... .......... .......... 39% 11.7M 21s
105150K .......... .......... .......... .......... .......... 39% 16.9M 21s
105200K .......... .......... .......... .......... .......... 39% 13.7M 21s
105250K .......... .......... .......... .......... .......... 39% 20.5M 21s
105300K .......... .......... .......... .......... .......... 39% 16.5M 21s
105350K .......... .......... .......... .......... .......... 39% 14.8M 21s
105400K .......... .......... .......... .......... .......... 39% 19.0M 21s
105450K .......... .......... .......... .......... .......... 39% 16.3M 21s
105500K .......... .......... .......... .......... .......... 39% 16.5M 21s
105550K .......... .......... .......... .......... .......... 39% 16.7M 21s
105600K .......... .......... .......... .......... .......... 39% 16.2M 21s
105650K .......... .......... .......... .......... .......... 39% 13.7M 21s
105700K .......... .......... .......... .......... .......... 39% 13.8M 21s
105750K .......... .......... .......... .......... .......... 39% 13.3M 21s
105800K .......... .......... .......... .......... .......... 39% 14.0M 21s
105850K .......... .......... .......... .......... .......... 39% 7.10M 21s
105900K .......... .......... .......... .......... .......... 39% 6.37M 21s
105950K .......... .......... .......... .......... .......... 39% 5.89M 21s
106000K .......... .......... .......... .......... .......... 39% 5.99M 21s
106050K .......... .......... .......... .......... .......... 39% 8.73M 21s
106100K .......... .......... .......... .......... .......... 39% 7.40M 21s
106150K .......... .......... .......... .......... .......... 39% 9.19M 21s
106200K .......... .......... .......... .......... .......... 39% 9.21M 21s
106250K .......... .......... .......... .......... .......... 39% 7.65M 21s
106300K .......... .......... .......... .......... .......... 40% 5.94M 21s
106350K .......... .......... .......... .......... .......... 40% 25.7M 21s
106400K .......... .......... .......... .......... .......... 40% 17.9M 21s
106450K .......... .......... .......... .......... .......... 40% 11.9M 21s
106500K .......... .......... .......... .......... .......... 40% 16.3M 21s
106550K .......... .......... .......... .......... .......... 40% 17.3M 21s
106600K .......... .......... .......... .......... .......... 40% 15.4M 21s
106650K .......... .......... .......... .......... .......... 40% 14.3M 21s
106700K .......... .......... .......... .......... .......... 40% 13.1M 21s
106750K .......... .......... .......... .......... .......... 40% 17.6M 21s
106800K .......... .......... .......... .......... .......... 40% 14.6M 21s
106850K .......... .......... .......... .......... .......... 40% 12.0M 21s
106900K .......... .......... .......... .......... .......... 40% 14.3M 21s
106950K .......... .......... .......... .......... .......... 40% 12.0M 21s
107000K .......... .......... .......... .......... .......... 40% 13.7M 21s
107050K .......... .......... .......... .......... .......... 40% 16.3M 21s
107100K .......... .......... .......... .......... .......... 40% 13.9M 21s
107150K .......... .......... .......... .......... .......... 40% 11.1M 21s
107200K .......... .......... .......... .......... .......... 40% 10.7M 21s
107250K .......... .......... .......... .......... .......... 40% 12.0M 21s
107300K .......... .......... .......... .......... .......... 40% 9.38M 21s
107350K .......... .......... .......... .......... .......... 40% 9.54M 21s
107400K .......... .......... .......... .......... .......... 40% 13.0M 21s
107450K .......... .......... .......... .......... .......... 40% 9.59M 21s
107500K .......... .......... .......... .......... .......... 40% 11.7M 21s
107550K .......... .......... .......... .......... .......... 40% 10.5M 21s
107600K .......... .......... .......... .......... .......... 40% 19.6M 21s
107650K .......... .......... .......... .......... .......... 40% 20.9M 21s
107700K .......... .......... .......... .......... .......... 40%  119M 21s
107750K .......... .......... .......... .......... .......... 40% 24.3M 21s
107800K .......... .......... .......... .......... .......... 40% 84.2M 21s
107850K .......... .......... .......... .......... .......... 40% 20.8M 21s
107900K .......... .......... .......... .......... .......... 40% 21.4M 21s
107950K .......... .......... .......... .......... .......... 40% 13.5M 21s
108000K .......... .......... .......... .......... .......... 40% 13.2M 21s
108050K .......... .......... .......... .......... .......... 40% 16.1M 21s
108100K .......... .......... .......... .......... .......... 40% 13.0M 21s
108150K .......... .......... .......... .......... .......... 40% 14.0M 21s
108200K .......... .......... .......... .......... .......... 40% 12.6M 21s
108250K .......... .......... .......... .......... .......... 40% 15.8M 20s
108300K .......... .......... .......... .......... .......... 40% 13.9M 20s
108350K .......... .......... .......... .......... .......... 40% 13.8M 20s
108400K .......... .......... .......... .......... .......... 40% 15.1M 20s
108450K .......... .......... .......... .......... .......... 40% 20.5M 20s
108500K .......... .......... .......... .......... .......... 40% 17.5M 20s
108550K .......... .......... .......... .......... .......... 40% 66.0M 20s
108600K .......... .......... .......... .......... .......... 40% 24.3M 20s
108650K .......... .......... .......... .......... .......... 40% 52.4M 20s
108700K .......... .......... .......... .......... .......... 40% 18.7M 20s
108750K .......... .......... .......... .......... .......... 40% 17.6M 20s
108800K .......... .......... .......... .......... .......... 40% 16.7M 20s
108850K .......... .......... .......... .......... .......... 40% 10.3M 20s
108900K .......... .......... .......... .......... .......... 40% 12.0M 20s
108950K .......... .......... .......... .......... .......... 41% 10.2M 20s
109000K .......... .......... .......... .......... .......... 41% 12.3M 20s
109050K .......... .......... .......... .......... .......... 41% 8.33M 20s
109100K .......... .......... .......... .......... .......... 41% 5.60M 20s
109150K .......... .......... .......... .......... .......... 41% 8.48M 20s
109200K .......... .......... .......... .......... .......... 41% 8.57M 20s
109250K .......... .......... .......... .......... .......... 41% 9.19M 20s
109300K .......... .......... .......... .......... .......... 41% 9.18M 20s
109350K .......... .......... .......... .......... .......... 41% 6.20M 20s
109400K .......... .......... .......... .......... .......... 41% 5.14M 20s
109450K .......... .......... .......... .......... .......... 41% 3.67M 20s
109500K .......... .......... .......... .......... .......... 41% 3.44M 20s
109550K .......... .......... .......... .......... .......... 41% 3.82M 20s
109600K .......... .......... .......... .......... .......... 41% 9.59M 20s
109650K .......... .......... .......... .......... .......... 41% 42.0M 20s
109700K .......... .......... .......... .......... .......... 41% 16.1M 20s
109750K .......... .......... .......... .......... .......... 41% 15.7M 20s
109800K .......... .......... .......... .......... .......... 41% 17.8M 20s
109850K .......... .......... .......... .......... .......... 41% 16.1M 20s
109900K .......... .......... .......... .......... .......... 41% 16.4M 20s
109950K .......... .......... .......... .......... .......... 41% 18.2M 20s
110000K .......... .......... .......... .......... .......... 41% 18.8M 20s
110050K .......... .......... .......... .......... .......... 41% 18.6M 20s
110100K .......... .......... .......... .......... .......... 41% 15.9M 20s
110150K .......... .......... .......... .......... .......... 41% 18.5M 20s
110200K .......... .......... .......... .......... .......... 41% 9.30M 20s
110250K .......... .......... .......... .......... .......... 41% 30.6M 20s
110300K .......... .......... .......... .......... .......... 41% 29.8M 20s
110350K .......... .......... .......... .......... .......... 41% 35.2M 20s
110400K .......... .......... .......... .......... .......... 41% 19.7M 20s
110450K .......... .......... .......... .......... .......... 41% 56.4M 20s
110500K .......... .......... .......... .......... .......... 41%  102M 20s
110550K .......... .......... .......... .......... .......... 41% 28.1M 20s
110600K .......... .......... .......... .......... .......... 41% 50.1M 20s
110650K .......... .......... .......... .......... .......... 41% 30.1M 20s
110700K .......... .......... .......... .......... .......... 41% 20.5M 20s
110750K .......... .......... .......... .......... .......... 41% 20.6M 20s
110800K .......... .......... .......... .......... .......... 41% 14.8M 20s
110850K .......... .......... .......... .......... .......... 41% 14.3M 20s
110900K .......... .......... .......... .......... .......... 41% 19.3M 20s
110950K .......... .......... .......... .......... .......... 41% 11.4M 20s
111000K .......... .......... .......... .......... .......... 41% 11.7M 20s
111050K .......... .......... .......... .......... .......... 41% 13.3M 20s
111100K .......... .......... .......... .......... .......... 41% 12.0M 20s
111150K .......... .......... .......... .......... .......... 41% 12.0M 20s
111200K .......... .......... .......... .......... .......... 41% 10.6M 20s
111250K .......... .......... .......... .......... .......... 41% 10.8M 20s
111300K .......... .......... .......... .......... .......... 41% 12.6M 20s
111350K .......... .......... .......... .......... .......... 41% 10.3M 20s
111400K .......... .......... .......... .......... .......... 41% 12.1M 20s
111450K .......... .......... .......... .......... .......... 41% 12.2M 20s
111500K .......... .......... .......... .......... .......... 41% 10.1M 20s
111550K .......... .......... .......... .......... .......... 41% 14.1M 20s
111600K .......... .......... .......... .......... .......... 42% 17.2M 20s
111650K .......... .......... .......... .......... .......... 42% 17.0M 20s
111700K .......... .......... .......... .......... .......... 42% 20.7M 20s
111750K .......... .......... .......... .......... .......... 42% 10.4M 20s
111800K .......... .......... .......... .......... .......... 42% 11.2M 20s
111850K .......... .......... .......... .......... .......... 42% 8.36M 20s
111900K .......... .......... .......... .......... .......... 42% 7.31M 20s
111950K .......... .......... .......... .......... .......... 42% 8.08M 20s
112000K .......... .......... .......... .......... .......... 42% 9.46M 20s
112050K .......... .......... .......... .......... .......... 42% 7.92M 20s
112100K .......... .......... .......... .......... .......... 42% 18.6M 20s
112150K .......... .......... .......... .......... .......... 42% 26.1M 20s
112200K .......... .......... .......... .......... .......... 42% 32.5M 20s
112250K .......... .......... .......... .......... .......... 42% 12.8M 20s
112300K .......... .......... .......... .......... .......... 42% 90.3M 20s
112350K .......... .......... .......... .......... .......... 42% 16.0M 20s
112400K .......... .......... .......... .......... .......... 42% 13.3M 20s
112450K .......... .......... .......... .......... .......... 42% 11.5M 20s
112500K .......... .......... .......... .......... .......... 42% 16.2M 20s
112550K .......... .......... .......... .......... .......... 42% 11.4M 20s
112600K .......... .......... .......... .......... .......... 42% 11.2M 20s
112650K .......... .......... .......... .......... .......... 42% 14.0M 20s
112700K .......... .......... .......... .......... .......... 42% 10.5M 20s
112750K .......... .......... .......... .......... .......... 42% 7.79M 20s
112800K .......... .......... .......... .......... .......... 42% 5.94M 20s
112850K .......... .......... .......... .......... .......... 42% 4.57M 20s
112900K .......... .......... .......... .......... .......... 42% 9.08M 20s
112950K .......... .......... .......... .......... .......... 42% 7.96M 20s
113000K .......... .......... .......... .......... .......... 42% 9.50M 20s
113050K .......... .......... .......... .......... .......... 42% 9.13M 20s
113100K .......... .......... .......... .......... .......... 42% 9.53M 20s
113150K .......... .......... .......... .......... .......... 42% 9.13M 20s
113200K .......... .......... .......... .......... .......... 42% 13.7M 20s
113250K .......... .......... .......... .......... .......... 42% 18.3M 20s
113300K .......... .......... .......... .......... .......... 42% 20.6M 20s
113350K .......... .......... .......... .......... .......... 42% 22.7M 19s
113400K .......... .......... .......... .......... .......... 42% 13.2M 19s
113450K .......... .......... .......... .......... .......... 42% 8.81M 19s
113500K .......... .......... .......... .......... .......... 42% 10.9M 19s
113550K .......... .......... .......... .......... .......... 42% 14.9M 19s
113600K .......... .......... .......... .......... .......... 42% 11.3M 19s
113650K .......... .......... .......... .......... .......... 42% 15.2M 19s
113700K .......... .......... .......... .......... .......... 42% 12.0M 19s
113750K .......... .......... .......... .......... .......... 42% 12.2M 19s
113800K .......... .......... .......... .......... .......... 42% 10.2M 19s
113850K .......... .......... .......... .......... .......... 42% 8.48M 19s
113900K .......... .......... .......... .......... .......... 42% 10.2M 19s
113950K .......... .......... .......... .......... .......... 42% 9.89M 19s
114000K .......... .......... .......... .......... .......... 42% 8.42M 19s
114050K .......... .......... .......... .......... .......... 42% 8.63M 19s
114100K .......... .......... .......... .......... .......... 42% 6.97M 19s
114150K .......... .......... .......... .......... .......... 42% 6.98M 19s
114200K .......... .......... .......... .......... .......... 42% 7.30M 19s
114250K .......... .......... .......... .......... .......... 43% 7.74M 19s
114300K .......... .......... .......... .......... .......... 43% 9.83M 19s
114350K .......... .......... .......... .......... .......... 43% 6.82M 19s
114400K .......... .......... .......... .......... .......... 43% 7.43M 19s
114450K .......... .......... .......... .......... .......... 43% 10.4M 19s
114500K .......... .......... .......... .......... .......... 43% 18.2M 19s
114550K .......... .......... .......... .......... .......... 43% 26.7M 19s
114600K .......... .......... .......... .......... .......... 43% 10.1M 19s
114650K .......... .......... .......... .......... .......... 43% 27.5M 19s
114700K .......... .......... .......... .......... .......... 43% 34.2M 19s
114750K .......... .......... .......... .......... .......... 43% 20.2M 19s
114800K .......... .......... .......... .......... .......... 43% 11.5M 19s
114850K .......... .......... .......... .......... .......... 43% 14.1M 19s
114900K .......... .......... .......... .......... .......... 43% 18.4M 19s
114950K .......... .......... .......... .......... .......... 43% 11.2M 19s
115000K .......... .......... .......... .......... .......... 43% 21.6M 19s
115050K .......... .......... .......... .......... .......... 43% 14.8M 19s
115100K .......... .......... .......... .......... .......... 43% 10.3M 19s
115150K .......... .......... .......... .......... .......... 43% 13.4M 19s
115200K .......... .......... .......... .......... .......... 43% 10.6M 19s
115250K .......... .......... .......... .......... .......... 43% 13.5M 19s
115300K .......... .......... .......... .......... .......... 43% 10.4M 19s
115350K .......... .......... .......... .......... .......... 43% 12.5M 19s
115400K .......... .......... .......... .......... .......... 43% 11.7M 19s
115450K .......... .......... .......... .......... .......... 43% 11.8M 19s
115500K .......... .......... .......... .......... .......... 43% 13.8M 19s
115550K .......... .......... .......... .......... .......... 43% 35.7M 19s
115600K .......... .......... .......... .......... .......... 43% 17.3M 19s
115650K .......... .......... .......... .......... .......... 43%  144M 19s
115700K .......... .......... .......... .......... .......... 43% 27.2M 19s
115750K .......... .......... .......... .......... .......... 43% 46.2M 19s
115800K .......... .......... .......... .......... .......... 43% 32.1M 19s
115850K .......... .......... .......... .......... .......... 43% 19.3M 19s
115900K .......... .......... .......... .......... .......... 43% 16.4M 19s
115950K .......... .......... .......... .......... .......... 43% 13.5M 19s
116000K .......... .......... .......... .......... .......... 43% 12.0M 19s
116050K .......... .......... .......... .......... .......... 43% 13.9M 19s
116100K .......... .......... .......... .......... .......... 43% 13.5M 19s
116150K .......... .......... .......... .......... .......... 43% 12.7M 19s
116200K .......... .......... .......... .......... .......... 43% 6.93M 19s
116250K .......... .......... .......... .......... .......... 43% 8.07M 19s
116300K .......... .......... .......... .......... .......... 43% 8.62M 19s
116350K .......... .......... .......... .......... .......... 43% 8.76M 19s
116400K .......... .......... .......... .......... .......... 43% 9.44M 19s
116450K .......... .......... .......... .......... .......... 43% 6.34M 19s
116500K .......... .......... .......... .......... .......... 43% 11.5M 19s
116550K .......... .......... .......... .......... .......... 43% 13.1M 19s
116600K .......... .......... .......... .......... .......... 43% 31.0M 19s
116650K .......... .......... .......... .......... .......... 43% 20.6M 19s
116700K .......... .......... .......... .......... .......... 43% 17.8M 19s
116750K .......... .......... .......... .......... .......... 43% 21.6M 19s
116800K .......... .......... .......... .......... .......... 43% 16.2M 19s
116850K .......... .......... .......... .......... .......... 43% 13.8M 19s
116900K .......... .......... .......... .......... .......... 43% 16.4M 19s
116950K .......... .......... .......... .......... .......... 44% 15.3M 19s
117000K .......... .......... .......... .......... .......... 44% 19.1M 19s
117050K .......... .......... .......... .......... .......... 44% 13.1M 19s
117100K .......... .......... .......... .......... .......... 44% 12.7M 19s
117150K .......... .......... .......... .......... .......... 44% 14.2M 19s
117200K .......... .......... .......... .......... .......... 44% 13.7M 19s
117250K .......... .......... .......... .......... .......... 44% 6.86M 19s
117300K .......... .......... .......... .......... .......... 44% 5.01M 19s
117350K .......... .......... .......... .......... .......... 44% 5.00M 19s
117400K .......... .......... .......... .......... .......... 44% 6.03M 19s
117450K .......... .......... .......... .......... .......... 44% 5.09M 19s
117500K .......... .......... .......... .......... .......... 44% 7.37M 19s
117550K .......... .......... .......... .......... .......... 44% 20.3M 19s
117600K .......... .......... .......... .......... .......... 44% 19.3M 19s
117650K .......... .......... .......... .......... .......... 44% 14.2M 19s
117700K .......... .......... .......... .......... .......... 44% 36.8M 19s
117750K .......... .......... .......... .......... .......... 44% 24.7M 19s
117800K .......... .......... .......... .......... .......... 44% 22.7M 19s
117850K .......... .......... .......... .......... .......... 44% 17.9M 19s
117900K .......... .......... .......... .......... .......... 44% 22.9M 19s
117950K .......... .......... .......... .......... .......... 44% 16.1M 19s
118000K .......... .......... .......... .......... .......... 44% 23.1M 19s
118050K .......... .......... .......... .......... .......... 44% 21.6M 19s
118100K .......... .......... .......... .......... .......... 44% 17.5M 19s
118150K .......... .......... .......... .......... .......... 44% 21.7M 19s
118200K .......... .......... .......... .......... .......... 44% 17.8M 19s
118250K .......... .......... .......... .......... .......... 44% 24.0M 19s
118300K .......... .......... .......... .......... .......... 44% 23.0M 19s
118350K .......... .......... .......... .......... .......... 44% 17.6M 19s
118400K .......... .......... .......... .......... .......... 44% 27.0M 19s
118450K .......... .......... .......... .......... .......... 44% 33.8M 19s
118500K .......... .......... .......... .......... .......... 44% 34.5M 19s
118550K .......... .......... .......... .......... .......... 44% 14.0M 19s
118600K .......... .......... .......... .......... .......... 44%  111M 18s
118650K .......... .......... .......... .......... .......... 44%  190M 18s
118700K .......... .......... .......... .......... .......... 44% 17.4M 18s
118750K .......... .......... .......... .......... .......... 44% 76.5M 18s
118800K .......... .......... .......... .......... .......... 44% 18.5M 18s
118850K .......... .......... .......... .......... .......... 44% 39.9M 18s
118900K .......... .......... .......... .......... .......... 44% 23.9M 18s
118950K .......... .......... .......... .......... .......... 44% 29.1M 18s
119000K .......... .......... .......... .......... .......... 44% 23.7M 18s
119050K .......... .......... .......... .......... .......... 44% 24.0M 18s
119100K .......... .......... .......... .......... .......... 44% 22.7M 18s
119150K .......... .......... .......... .......... .......... 44% 17.0M 18s
119200K .......... .......... .......... .......... .......... 44% 18.6M 18s
119250K .......... .......... .......... .......... .......... 44% 24.6M 18s
119300K .......... .......... .......... .......... .......... 44% 25.6M 18s
119350K .......... .......... .......... .......... .......... 44% 18.0M 18s
119400K .......... .......... .......... .......... .......... 44% 24.3M 18s
119450K .......... .......... .......... .......... .......... 44% 17.4M 18s
119500K .......... .......... .......... .......... .......... 44% 24.3M 18s
119550K .......... .......... .......... .......... .......... 44% 22.8M 18s
119600K .......... .......... .......... .......... .......... 45% 18.0M 18s
119650K .......... .......... .......... .......... .......... 45% 10.0M 18s
119700K .......... .......... .......... .......... .......... 45% 16.2M 18s
119750K .......... .......... .......... .......... .......... 45% 11.7M 18s
119800K .......... .......... .......... .......... .......... 45% 13.2M 18s
119850K .......... .......... .......... .......... .......... 45% 10.1M 18s
119900K .......... .......... .......... .......... .......... 45% 12.6M 18s
119950K .......... .......... .......... .......... .......... 45% 11.6M 18s
120000K .......... .......... .......... .......... .......... 45% 11.7M 18s
120050K .......... .......... .......... .......... .......... 45% 13.1M 18s
120100K .......... .......... .......... .......... .......... 45% 10.6M 18s
120150K .......... .......... .......... .......... .......... 45% 12.7M 18s
120200K .......... .......... .......... .......... .......... 45% 14.6M 18s
120250K .......... .......... .......... .......... .......... 45% 25.0M 18s
120300K .......... .......... .......... .......... .......... 45% 21.7M 18s
120350K .......... .......... .......... .......... .......... 45% 33.7M 18s
120400K .......... .......... .......... .......... .......... 45% 18.7M 18s
120450K .......... .......... .......... .......... .......... 45% 21.3M 18s
120500K .......... .......... .......... .......... .......... 45% 41.8M 18s
120550K .......... .......... .......... .......... .......... 45% 22.6M 18s
120600K .......... .......... .......... .......... .......... 45% 17.4M 18s
120650K .......... .......... .......... .......... .......... 45% 19.0M 18s
120700K .......... .......... .......... .......... .......... 45% 13.8M 18s
120750K .......... .......... .......... .......... .......... 45% 16.4M 18s
120800K .......... .......... .......... .......... .......... 45% 16.0M 18s
120850K .......... .......... .......... .......... .......... 45% 14.0M 18s
120900K .......... .......... .......... .......... .......... 45% 18.4M 18s
120950K .......... .......... .......... .......... .......... 45% 13.7M 18s
121000K .......... .......... .......... .......... .......... 45% 16.8M 18s
121050K .......... .......... .......... .......... .......... 45% 13.3M 18s
121100K .......... .......... .......... .......... .......... 45% 11.2M 18s
121150K .......... .......... .......... .......... .......... 45% 15.0M 18s
121200K .......... .......... .......... .......... .......... 45% 13.6M 18s
121250K .......... .......... .......... .......... .......... 45% 34.0M 18s
121300K .......... .......... .......... .......... .......... 45% 38.2M 18s
121350K .......... .......... .......... .......... .......... 45% 36.9M 18s
121400K .......... .......... .......... .......... .......... 45% 47.5M 18s
121450K .......... .......... .......... .......... .......... 45% 26.2M 18s
121500K .......... .......... .......... .......... .......... 45%  133M 18s
121550K .......... .......... .......... .......... .......... 45% 49.0M 18s
121600K .......... .......... .......... .......... .......... 45% 32.0M 18s
121650K .......... .......... .......... .......... .......... 45% 39.8M 18s
121700K .......... .......... .......... .......... .......... 45% 20.9M 18s
121750K .......... .......... .......... .......... .......... 45% 72.4M 18s
121800K .......... .......... .......... .......... .......... 45% 50.4M 18s
121850K .......... .......... .......... .......... .......... 45% 27.9M 18s
121900K .......... .......... .......... .......... .......... 45% 31.7M 18s
121950K .......... .......... .......... .......... .......... 45% 35.6M 18s
122000K .......... .......... .......... .......... .......... 45% 30.3M 18s
122050K .......... .......... .......... .......... .......... 45% 43.4M 18s
122100K .......... .......... .......... .......... .......... 45% 26.1M 18s
122150K .......... .......... .......... .......... .......... 45% 37.3M 18s
122200K .......... .......... .......... .......... .......... 45% 30.0M 18s
122250K .......... .......... .......... .......... .......... 46% 34.9M 18s
122300K .......... .......... .......... .......... .......... 46% 36.7M 18s
122350K .......... .......... .......... .......... .......... 46% 32.4M 18s
122400K .......... .......... .......... .......... .......... 46% 31.0M 18s
122450K .......... .......... .......... .......... .......... 46% 34.5M 18s
122500K .......... .......... .......... .......... .......... 46% 29.6M 18s
122550K .......... .......... .......... .......... .......... 46% 38.7M 18s
122600K .......... .......... .......... .......... .......... 46% 29.6M 18s
122650K .......... .......... .......... .......... .......... 46% 26.4M 18s
122700K .......... .......... .......... .......... .......... 46% 21.7M 18s
122750K .......... .......... .......... .......... .......... 46% 16.8M 18s
122800K .......... .......... .......... .......... .......... 46% 17.7M 18s
122850K .......... .......... .......... .......... .......... 46% 14.0M 18s
122900K .......... .......... .......... .......... .......... 46% 16.6M 18s
122950K .......... .......... .......... .......... .......... 46% 14.4M 18s
123000K .......... .......... .......... .......... .......... 46% 15.7M 18s
123050K .......... .......... .......... .......... .......... 46% 13.8M 18s
123100K .......... .......... .......... .......... .......... 46% 11.9M 18s
123150K .......... .......... .......... .......... .......... 46% 15.4M 18s
123200K .......... .......... .......... .......... .......... 46% 12.2M 18s
123250K .......... .......... .......... .......... .......... 46% 12.7M 17s
123300K .......... .......... .......... .......... .......... 46% 14.7M 17s
123350K .......... .......... .......... .......... .......... 46% 12.4M 17s
123400K .......... .......... .......... .......... .......... 46% 14.0M 17s
123450K .......... .......... .......... .......... .......... 46% 12.1M 17s
123500K .......... .......... .......... .......... .......... 46% 14.2M 17s
123550K .......... .......... .......... .......... .......... 46% 13.3M 17s
123600K .......... .......... .......... .......... .......... 46% 11.7M 17s
123650K .......... .......... .......... .......... .......... 46% 27.2M 17s
123700K .......... .......... .......... .......... .......... 46% 7.03M 17s
123750K .......... .......... .......... .......... .......... 46% 74.0M 17s
123800K .......... .......... .......... .......... .......... 46% 15.5M 17s
123850K .......... .......... .......... .......... .......... 46% 14.2M 17s
123900K .......... .......... .......... .......... .......... 46% 15.6M 17s
123950K .......... .......... .......... .......... .......... 46% 14.3M 17s
124000K .......... .......... .......... .......... .......... 46% 15.1M 17s
124050K .......... .......... .......... .......... .......... 46% 15.7M 17s
124100K .......... .......... .......... .......... .......... 46% 14.6M 17s
124150K .......... .......... .......... .......... .......... 46% 16.0M 17s
124200K .......... .......... .......... .......... .......... 46% 13.1M 17s
124250K .......... .......... .......... .......... .......... 46% 15.1M 17s
124300K .......... .......... .......... .......... .......... 46% 14.5M 17s
124350K .......... .......... .......... .......... .......... 46% 11.8M 17s
124400K .......... .......... .......... .......... .......... 46% 25.8M 17s
124450K .......... .......... .......... .......... .......... 46% 21.3M 17s
124500K .......... .......... .......... .......... .......... 46% 20.5M 17s
124550K .......... .......... .......... .......... .......... 46% 21.9M 17s
124600K .......... .......... .......... .......... .......... 46% 44.6M 17s
124650K .......... .......... .......... .......... .......... 46% 21.2M 17s
124700K .......... .......... .......... .......... .......... 46% 19.4M 17s
124750K .......... .......... .......... .......... .......... 46% 25.6M 17s
124800K .......... .......... .......... .......... .......... 46% 18.8M 17s
124850K .......... .......... .......... .......... .......... 46% 16.9M 17s
124900K .......... .......... .......... .......... .......... 47% 19.1M 17s
124950K .......... .......... .......... .......... .......... 47% 3.17M 17s
125000K .......... .......... .......... .......... .......... 47%  126M 17s
125050K .......... .......... .......... .......... .......... 47%  116M 17s
125100K .......... .......... .......... .......... .......... 47%  125M 17s
125150K .......... .......... .......... .......... .......... 47% 35.8M 17s
125200K .......... .......... .......... .......... .......... 47% 17.8M 17s
125250K .......... .......... .......... .......... .......... 47% 9.98M 17s
125300K .......... .......... .......... .......... .......... 47%  119M 17s
125350K .......... .......... .......... .......... .......... 47% 18.3M 17s
125400K .......... .......... .......... .......... .......... 47% 47.5M 17s
125450K .......... .......... .......... .......... .......... 47% 16.3M 17s
125500K .......... .......... .......... .......... .......... 47% 15.0M 17s
125550K .......... .......... .......... .......... .......... 47% 21.9M 17s
125600K .......... .......... .......... .......... .......... 47% 10.7M 17s
125650K .......... .......... .......... .......... .......... 47% 10.7M 17s
125700K .......... .......... .......... .......... .......... 47% 9.26M 17s
125750K .......... .......... .......... .......... .......... 47% 11.2M 17s
125800K .......... .......... .......... .......... .......... 47% 11.2M 17s
125850K .......... .......... .......... .......... .......... 47% 8.97M 17s
125900K .......... .......... .......... .......... .......... 47% 9.24M 17s
125950K .......... .......... .......... .......... .......... 47% 5.22M 17s
126000K .......... .......... .......... .......... .......... 47% 8.64M 17s
126050K .......... .......... .......... .......... .......... 47% 6.91M 17s
126100K .......... .......... .......... .......... .......... 47% 7.05M 17s
126150K .......... .......... .......... .......... .......... 47% 7.23M 17s
126200K .......... .......... .......... .......... .......... 47% 5.70M 17s
126250K .......... .......... .......... .......... .......... 47% 6.94M 17s
126300K .......... .......... .......... .......... .......... 47% 8.03M 17s
126350K .......... .......... .......... .......... .......... 47% 12.4M 17s
126400K .......... .......... .......... .......... .......... 47% 12.8M 17s
126450K .......... .......... .......... .......... .......... 47% 10.4M 17s
126500K .......... .......... .......... .......... .......... 47% 12.6M 17s
126550K .......... .......... .......... .......... .......... 47% 13.4M 17s
126600K .......... .......... .......... .......... .......... 47% 10.3M 17s
126650K .......... .......... .......... .......... .......... 47% 13.4M 17s
126700K .......... .......... .......... .......... .......... 47% 17.7M 17s
126750K .......... .......... .......... .......... .......... 47% 31.3M 17s
126800K .......... .......... .......... .......... .......... 47% 38.1M 17s
126850K .......... .......... .......... .......... .......... 47% 33.1M 17s
126900K .......... .......... .......... .......... .......... 47% 25.0M 17s
126950K .......... .......... .......... .......... .......... 47% 48.5M 17s
127000K .......... .......... .......... .......... .......... 47% 26.5M 17s
127050K .......... .......... .......... .......... .......... 47% 32.1M 17s
127100K .......... .......... .......... .......... .......... 47% 18.7M 17s
127150K .......... .......... .......... .......... .......... 47% 59.9M 17s
127200K .......... .......... .......... .......... .......... 47% 19.7M 17s
127250K .......... .......... .......... .......... .......... 47% 23.3M 17s
127300K .......... .......... .......... .......... .......... 47% 33.4M 17s
127350K .......... .......... .......... .......... .......... 47% 20.8M 17s
127400K .......... .......... .......... .......... .......... 47% 32.2M 17s
127450K .......... .......... .......... .......... .......... 47% 24.9M 17s
127500K .......... .......... .......... .......... .......... 47% 21.1M 17s
127550K .......... .......... .......... .......... .......... 48% 24.9M 17s
127600K .......... .......... .......... .......... .......... 48% 28.7M 17s
127650K .......... .......... .......... .......... .......... 48% 28.4M 17s
127700K .......... .......... .......... .......... .......... 48% 22.5M 17s
127750K .......... .......... .......... .......... .......... 48% 29.0M 17s
127800K .......... .......... .......... .......... .......... 48% 15.8M 17s
127850K .......... .......... .......... .......... .......... 48% 39.4M 17s
127900K .......... .......... .......... .......... .......... 48% 23.7M 17s
127950K .......... .......... .......... .......... .......... 48% 14.1M 17s
128000K .......... .......... .......... .......... .......... 48% 22.6M 17s
128050K .......... .......... .......... .......... .......... 48% 41.9M 17s
128100K .......... .......... .......... .......... .......... 48% 18.9M 17s
128150K .......... .......... .......... .......... .......... 48% 26.3M 17s
128200K .......... .......... .......... .......... .......... 48% 21.2M 17s
128250K .......... .......... .......... .......... .......... 48% 25.9M 17s
128300K .......... .......... .......... .......... .......... 48% 21.6M 17s
128350K .......... .......... .......... .......... .......... 48% 18.8M 17s
128400K .......... .......... .......... .......... .......... 48% 20.9M 17s
128450K .......... .......... .......... .......... .......... 48% 20.9M 17s
128500K .......... .......... .......... .......... .......... 48% 22.1M 17s
128550K .......... .......... .......... .......... .......... 48% 24.3M 17s
128600K .......... .......... .......... .......... .......... 48% 24.2M 16s
128650K .......... .......... .......... .......... .......... 48% 70.7M 16s
128700K .......... .......... .......... .......... .......... 48% 17.6M 16s
128750K .......... .......... .......... .......... .......... 48%  138M 16s
128800K .......... .......... .......... .......... .......... 48% 57.6M 16s
128850K .......... .......... .......... .......... .......... 48% 32.7M 16s
128900K .......... .......... .......... .......... .......... 48% 75.7M 16s
128950K .......... .......... .......... .......... .......... 48%  113M 16s
129000K .......... .......... .......... .......... .......... 48% 42.8M 16s
129050K .......... .......... .......... .......... .......... 48% 38.4M 16s
129100K .......... .......... .......... .......... .......... 48% 24.5M 16s
129150K .......... .......... .......... .......... .......... 48% 16.6M 16s
129200K .......... .......... .......... .......... .......... 48% 33.4M 16s
129250K .......... .......... .......... .......... .......... 48% 20.4M 16s
129300K .......... .......... .......... .......... .......... 48% 16.3M 16s
129350K .......... .......... .......... .......... .......... 48% 15.1M 16s
129400K .......... .......... .......... .......... .......... 48% 14.7M 16s
129450K .......... .......... .......... .......... .......... 48% 22.9M 16s
129500K .......... .......... .......... .......... .......... 48% 14.2M 16s
129550K .......... .......... .......... .......... .......... 48% 22.7M 16s
129600K .......... .......... .......... .......... .......... 48% 13.7M 16s
129650K .......... .......... .......... .......... .......... 48% 15.4M 16s
129700K .......... .......... .......... .......... .......... 48% 7.43M 16s
129750K .......... .......... .......... .......... .......... 48% 14.4M 16s
129800K .......... .......... .......... .......... .......... 48% 9.41M 16s
129850K .......... .......... .......... .......... .......... 48% 6.51M 16s
129900K .......... .......... .......... .......... .......... 48% 6.18M 16s
129950K .......... .......... .......... .......... .......... 48% 5.99M 16s
130000K .......... .......... .......... .......... .......... 48% 10.1M 16s
130050K .......... .......... .......... .......... .......... 48%  681K 16s
130100K .......... .......... .......... .......... .......... 48%  102M 16s
130150K .......... .......... .......... .......... .......... 48%  126M 16s
130200K .......... .......... .......... .......... .......... 49%  109M 16s
130250K .......... .......... .......... .......... .......... 49% 15.6M 16s
130300K .......... .......... .......... .......... .......... 49% 8.30M 16s
130350K .......... .......... .......... .......... .......... 49% 6.56M 16s
130400K .......... .......... .......... .......... .......... 49% 9.74M 16s
130450K .......... .......... .......... .......... .......... 49% 8.96M 16s
130500K .......... .......... .......... .......... .......... 49% 11.5M 16s
130550K .......... .......... .......... .......... .......... 49% 18.6M 16s
130600K .......... .......... .......... .......... .......... 49% 20.0M 16s
130650K .......... .......... .......... .......... .......... 49% 21.2M 16s
130700K .......... .......... .......... .......... .......... 49% 14.7M 16s
130750K .......... .......... .......... .......... .......... 49% 24.7M 16s
130800K .......... .......... .......... .......... .......... 49% 21.7M 16s
130850K .......... .......... .......... .......... .......... 49% 16.0M 16s
130900K .......... .......... .......... .......... .......... 49% 20.6M 16s
130950K .......... .......... .......... .......... .......... 49% 21.5M 16s
131000K .......... .......... .......... .......... .......... 49% 21.8M 16s
131050K .......... .......... .......... .......... .......... 49% 23.5M 16s
131100K .......... .......... .......... .......... .......... 49% 22.1M 16s
131150K .......... .......... .......... .......... .......... 49% 22.4M 16s
131200K .......... .......... .......... .......... .......... 49% 15.1M 16s
131250K .......... .......... .......... .......... .......... 49% 39.1M 16s
131300K .......... .......... .......... .......... .......... 49% 39.6M 16s
131350K .......... .......... .......... .......... .......... 49% 41.8M 16s
131400K .......... .......... .......... .......... .......... 49% 21.8M 16s
131450K .......... .......... .......... .......... .......... 49%  138M 16s
131500K .......... .......... .......... .......... .......... 49%  137M 16s
131550K .......... .......... .......... .......... .......... 49% 37.4M 16s
131600K .......... .......... .......... .......... .......... 49% 92.1M 16s
131650K .......... .......... .......... .......... .......... 49% 44.3M 16s
131700K .......... .......... .......... .......... .......... 49% 43.0M 16s
131750K .......... .......... .......... .......... .......... 49% 54.0M 16s
131800K .......... .......... .......... .......... .......... 49% 45.7M 16s
131850K .......... .......... .......... .......... .......... 49% 29.6M 16s
131900K .......... .......... .......... .......... .......... 49% 48.9M 16s
131950K .......... .......... .......... .......... .......... 49% 43.2M 16s
132000K .......... .......... .......... .......... .......... 49% 53.4M 16s
132050K .......... .......... .......... .......... .......... 49% 45.5M 16s
132100K .......... .......... .......... .......... .......... 49% 34.7M 16s
132150K .......... .......... .......... .......... .......... 49% 45.8M 16s
132200K .......... .......... .......... .......... .......... 49% 49.3M 16s
132250K .......... .......... .......... .......... .......... 49% 51.5M 16s
132300K .......... .......... .......... .......... .......... 49% 46.5M 16s
132350K .......... .......... .......... .......... .......... 49% 39.7M 16s
132400K .......... .......... .......... .......... .......... 49% 48.1M 16s
132450K .......... .......... .......... .......... .......... 49% 35.2M 16s
132500K .......... .......... .......... .......... .......... 49% 34.4M 16s
132550K .......... .......... .......... .......... .......... 49% 48.1M 16s
132600K .......... .......... .......... .......... .......... 49% 39.7M 16s
132650K .......... .......... .......... .......... .......... 49% 50.0M 16s
132700K .......... .......... .......... .......... .......... 49% 43.0M 16s
132750K .......... .......... .......... .......... .......... 49% 52.2M 16s
132800K .......... .......... .......... .......... .......... 49% 41.6M 16s
132850K .......... .......... .......... .......... .......... 49% 35.5M 16s
132900K .......... .......... .......... .......... .......... 50% 50.8M 16s
132950K .......... .......... .......... .......... .......... 50% 42.2M 16s
133000K .......... .......... .......... .......... .......... 50% 44.6M 16s
133050K .......... .......... .......... .......... .......... 50% 46.8M 16s
133100K .......... .......... .......... .......... .......... 50% 32.3M 16s
133150K .......... .......... .......... .......... .......... 50% 36.4M 16s
133200K .......... .......... .......... .......... .......... 50% 35.4M 16s
133250K .......... .......... .......... .......... .......... 50% 16.1M 16s
133300K .......... .......... .......... .......... .......... 50% 55.5M 16s
133350K .......... .......... .......... .......... .......... 50%  115M 16s
133400K .......... .......... .......... .......... .......... 50% 19.6M 16s
133450K .......... .......... .......... .......... .......... 50%  117M 16s
133500K .......... .......... .......... .......... .......... 50% 28.5M 16s
133550K .......... .......... .......... .......... .......... 50% 27.7M 16s
133600K .......... .......... .......... .......... .......... 50% 31.2M 16s
133650K .......... .......... .......... .......... .......... 50% 24.3M 16s
133700K .......... .......... .......... .......... .......... 50% 19.6M 16s
133750K .......... .......... .......... .......... .......... 50% 24.0M 16s
133800K .......... .......... .......... .......... .......... 50% 27.1M 16s
133850K .......... .......... .......... .......... .......... 50% 22.7M 16s
133900K .......... .......... .......... .......... .......... 50% 23.8M 16s
133950K .......... .......... .......... .......... .......... 50% 24.0M 16s
134000K .......... .......... .......... .......... .......... 50% 23.6M 16s
134050K .......... .......... .......... .......... .......... 50% 25.9M 15s
134100K .......... .......... .......... .......... .......... 50% 23.3M 15s
134150K .......... .......... .......... .......... .......... 50% 23.8M 15s
134200K .......... .......... .......... .......... .......... 50% 23.2M 15s
134250K .......... .......... .......... .......... .......... 50% 23.7M 15s
134300K .......... .......... .......... .......... .......... 50% 22.6M 15s
134350K .......... .......... .......... .......... .......... 50% 24.1M 15s
134400K .......... .......... .......... .......... .......... 50% 20.5M 15s
134450K .......... .......... .......... .......... .......... 50% 13.6M 15s
134500K .......... .......... .......... .......... .......... 50% 27.8M 15s
134550K .......... .......... .......... .......... .......... 50% 35.6M 15s
134600K .......... .......... .......... .......... .......... 50% 17.8M 15s
134650K .......... .......... .......... .......... .......... 50% 16.5M 15s
134700K .......... .......... .......... .......... .......... 50%  116M 15s
134750K .......... .......... .......... .......... .......... 50% 12.0M 15s
134800K .......... .......... .......... .......... .......... 50% 29.5M 15s
134850K .......... .......... .......... .......... .......... 50% 18.5M 15s
134900K .......... .......... .......... .......... .......... 50% 15.5M 15s
134950K .......... .......... .......... .......... .......... 50% 18.5M 15s
135000K .......... .......... .......... .......... .......... 50% 21.0M 15s
135050K .......... .......... .......... .......... .......... 50% 17.0M 15s
135100K .......... .......... .......... .......... .......... 50% 21.1M 15s
135150K .......... .......... .......... .......... .......... 50% 17.3M 15s
135200K .......... .......... .......... .......... .......... 50% 19.1M 15s
135250K .......... .......... .......... .......... .......... 50% 22.2M 15s
135300K .......... .......... .......... .......... .......... 50% 16.4M 15s
135350K .......... .......... .......... .......... .......... 50% 20.4M 15s
135400K .......... .......... .......... .......... .......... 50% 21.8M 15s
135450K .......... .......... .......... .......... .......... 50% 24.3M 15s
135500K .......... .......... .......... .......... .......... 50% 62.2M 15s
135550K .......... .......... .......... .......... .......... 51% 41.6M 15s
135600K .......... .......... .......... .......... .......... 51% 20.4M 15s
135650K .......... .......... .......... .......... .......... 51% 47.0M 15s
135700K .......... .......... .......... .......... .......... 51% 40.4M 15s
135750K .......... .......... .......... .......... .......... 51%  108M 15s
135800K .......... .......... .......... .......... .......... 51% 62.9M 15s
135850K .......... .......... .......... .......... .......... 51% 34.8M 15s
135900K .......... .......... .......... .......... .......... 51% 37.1M 15s
135950K .......... .......... .......... .......... .......... 51% 27.1M 15s
136000K .......... .......... .......... .......... .......... 51% 39.0M 15s
136050K .......... .......... .......... .......... .......... 51% 40.3M 15s
136100K .......... .......... .......... .......... .......... 51% 39.1M 15s
136150K .......... .......... .......... .......... .......... 51% 46.1M 15s
136200K .......... .......... .......... .......... .......... 51% 9.94M 15s
136250K .......... .......... .......... .......... .......... 51% 96.5M 15s
136300K .......... .......... .......... .......... .......... 51% 64.6M 15s
136350K .......... .......... .......... .......... .......... 51% 17.8M 15s
136400K .......... .......... .......... .......... .......... 51% 21.4M 15s
136450K .......... .......... .......... .......... .......... 51% 16.7M 15s
136500K .......... .......... .......... .......... .......... 51% 19.1M 15s
136550K .......... .......... .......... .......... .......... 51% 17.6M 15s
136600K .......... .......... .......... .......... .......... 51% 19.6M 15s
136650K .......... .......... .......... .......... .......... 51% 17.1M 15s
136700K .......... .......... .......... .......... .......... 51% 17.0M 15s
136750K .......... .......... .......... .......... .......... 51% 20.7M 15s
136800K .......... .......... .......... .......... .......... 51% 16.9M 15s
136850K .......... .......... .......... .......... .......... 51% 15.1M 15s
136900K .......... .......... .......... .......... .......... 51% 21.9M 15s
136950K .......... .......... .......... .......... .......... 51% 17.8M 15s
137000K .......... .......... .......... .......... .......... 51% 12.8M 15s
137050K .......... .......... .......... .......... .......... 51% 8.02M 15s
137100K .......... .......... .......... .......... .......... 51% 9.23M 15s
137150K .......... .......... .......... .......... .......... 51% 13.0M 15s
137200K .......... .......... .......... .......... .......... 51% 12.4M 15s
137250K .......... .......... .......... .......... .......... 51% 14.7M 15s
137300K .......... .......... .......... .......... .......... 51% 14.9M 15s
137350K .......... .......... .......... .......... .......... 51% 13.3M 15s
137400K .......... .......... .......... .......... .......... 51% 16.1M 15s
137450K .......... .......... .......... .......... .......... 51% 12.4M 15s
137500K .......... .......... .......... .......... .......... 51% 14.4M 15s
137550K .......... .......... .......... .......... .......... 51% 16.0M 15s
137600K .......... .......... .......... .......... .......... 51% 10.1M 15s
137650K .......... .......... .......... .......... .......... 51% 14.1M 15s
137700K .......... .......... .......... .......... .......... 51% 19.1M 15s
137750K .......... .......... .......... .......... .......... 51% 12.5M 15s
137800K .......... .......... .......... .......... .......... 51% 19.8M 15s
137850K .......... .......... .......... .......... .......... 51% 18.2M 15s
137900K .......... .......... .......... .......... .......... 51% 27.5M 15s
137950K .......... .......... .......... .......... .......... 51% 14.1M 15s
138000K .......... .......... .......... .......... .......... 51% 32.3M 15s
138050K .......... .......... .......... .......... .......... 51% 26.3M 15s
138100K .......... .......... .......... .......... .......... 51% 26.2M 15s
138150K .......... .......... .......... .......... .......... 51% 11.4M 15s
138200K .......... .......... .......... .......... .......... 52% 37.9M 15s
138250K .......... .......... .......... .......... .......... 52% 26.7M 15s
138300K .......... .......... .......... .......... .......... 52% 28.2M 15s
138350K .......... .......... .......... .......... .......... 52% 14.8M 15s
138400K .......... .......... .......... .......... .......... 52% 19.5M 15s
138450K .......... .......... .......... .......... .......... 52% 16.6M 15s
138500K .......... .......... .......... .......... .......... 52% 20.0M 15s
138550K .......... .......... .......... .......... .......... 52% 8.97M 15s
138600K .......... .......... .......... .......... .......... 52% 13.1M 15s
138650K .......... .......... .......... .......... .......... 52% 16.0M 15s
138700K .......... .......... .......... .......... .......... 52% 9.54M 15s
138750K .......... .......... .......... .......... .......... 52% 15.8M 15s
138800K .......... .......... .......... .......... .......... 52% 10.9M 15s
138850K .......... .......... .......... .......... .......... 52% 4.69M 15s
138900K .......... .......... .......... .......... .......... 52% 8.89M 15s
138950K .......... .......... .......... .......... .......... 52% 8.03M 15s
139000K .......... .......... .......... .......... .......... 52% 10.1M 15s
139050K .......... .......... .......... .......... .......... 52% 8.50M 15s
139100K .......... .......... .......... .......... .......... 52% 9.34M 15s
139150K .......... .......... .......... .......... .......... 52% 7.30M 15s
139200K .......... .......... .......... .......... .......... 52% 15.7M 15s
139250K .......... .......... .......... .......... .......... 52% 1.40M 15s
139300K .......... .......... .......... .......... .......... 52%  176M 15s
139350K .......... .......... .......... .......... .......... 52%  105M 15s
139400K .......... .......... .......... .......... .......... 52%  148M 15s
139450K .......... .......... .......... .......... .......... 52%  100M 15s
139500K .......... .......... .......... .......... .......... 52% 22.9M 15s
139550K .......... .......... .......... .......... .......... 52% 58.0M 15s
139600K .......... .......... .......... .......... .......... 52% 28.9M 15s
139650K .......... .......... .......... .......... .......... 52% 30.4M 15s
139700K .......... .......... .......... .......... .......... 52% 25.8M 15s
139750K .......... .......... .......... .......... .......... 52% 26.7M 15s
139800K .......... .......... .......... .......... .......... 52% 33.3M 15s
139850K .......... .......... .......... .......... .......... 52% 23.1M 15s
139900K .......... .......... .......... .......... .......... 52% 28.1M 14s
139950K .......... .......... .......... .......... .......... 52% 32.0M 14s
140000K .......... .......... .......... .......... .......... 52% 24.5M 14s
140050K .......... .......... .......... .......... .......... 52% 36.4M 14s
140100K .......... .......... .......... .......... .......... 52% 25.1M 14s
140150K .......... .......... .......... .......... .......... 52% 30.0M 14s
140200K .......... .......... .......... .......... .......... 52% 22.9M 14s
140250K .......... .......... .......... .......... .......... 52% 35.2M 14s
140300K .......... .......... .......... .......... .......... 52% 28.9M 14s
140350K .......... .......... .......... .......... .......... 52% 19.8M 14s
140400K .......... .......... .......... .......... .......... 52% 20.0M 14s
140450K .......... .......... .......... .......... .......... 52% 33.0M 14s
140500K .......... .......... .......... .......... .......... 52% 20.8M 14s
140550K .......... .......... .......... .......... .......... 52% 28.1M 14s
140600K .......... .......... .......... .......... .......... 52% 29.5M 14s
140650K .......... .......... .......... .......... .......... 52% 17.6M 14s
140700K .......... .......... .......... .......... .......... 52% 40.5M 14s
140750K .......... .......... .......... .......... .......... 52% 37.0M 14s
140800K .......... .......... .......... .......... .......... 52%  133M 14s
140850K .......... .......... .......... .......... .......... 53% 17.7M 14s
140900K .......... .......... .......... .......... .......... 53%  110M 14s
140950K .......... .......... .......... .......... .......... 53% 29.4M 14s
141000K .......... .......... .......... .......... .......... 53% 37.7M 14s
141050K .......... .......... .......... .......... .......... 53% 16.0M 14s
141100K .......... .......... .......... .......... .......... 53% 35.9M 14s
141150K .......... .......... .......... .......... .......... 53% 23.5M 14s
141200K .......... .......... .......... .......... .......... 53% 17.1M 14s
141250K .......... .......... .......... .......... .......... 53% 22.9M 14s
141300K .......... .......... .......... .......... .......... 53% 21.6M 14s
141350K .......... .......... .......... .......... .......... 53% 16.8M 14s
141400K .......... .......... .......... .......... .......... 53% 23.4M 14s
141450K .......... .......... .......... .......... .......... 53% 17.2M 14s
141500K .......... .......... .......... .......... .......... 53% 23.1M 14s
141550K .......... .......... .......... .......... .......... 53% 21.2M 14s
141600K .......... .......... .......... .......... .......... 53% 17.0M 14s
141650K .......... .......... .......... .......... .......... 53% 21.4M 14s
141700K .......... .......... .......... .......... .......... 53% 19.5M 14s
141750K .......... .......... .......... .......... .......... 53% 16.5M 14s
141800K .......... .......... .......... .......... .......... 53% 20.4M 14s
141850K .......... .......... .......... .......... .......... 53% 34.1M 14s
141900K .......... .......... .......... .......... .......... 53% 32.8M 14s
141950K .......... .......... .......... .......... .......... 53% 18.3M 14s
142000K .......... .......... .......... .......... .......... 53% 25.9M 14s
142050K .......... .......... .......... .......... .......... 53% 42.8M 14s
142100K .......... .......... .......... .......... .......... 53% 37.5M 14s
142150K .......... .......... .......... .......... .......... 53% 27.3M 14s
142200K .......... .......... .......... .......... .......... 53% 29.0M 14s
142250K .......... .......... .......... .......... .......... 53% 25.2M 14s
142300K .......... .......... .......... .......... .......... 53% 34.6M 14s
142350K .......... .......... .......... .......... .......... 53% 25.5M 14s
142400K .......... .......... .......... .......... .......... 53% 34.1M 14s
142450K .......... .......... .......... .......... .......... 53% 24.1M 14s
142500K .......... .......... .......... .......... .......... 53% 38.0M 14s
142550K .......... .......... .......... .......... .......... 53% 26.4M 14s
142600K .......... .......... .......... .......... .......... 53% 34.7M 14s
142650K .......... .......... .......... .......... .......... 53% 25.6M 14s
142700K .......... .......... .......... .......... .......... 53% 33.5M 14s
142750K .......... .......... .......... .......... .......... 53% 25.7M 14s
142800K .......... .......... .......... .......... .......... 53% 36.4M 14s
142850K .......... .......... .......... .......... .......... 53% 25.2M 14s
142900K .......... .......... .......... .......... .......... 53% 35.4M 14s
142950K .......... .......... .......... .......... .......... 53% 25.3M 14s
143000K .......... .......... .......... .......... .......... 53% 37.7M 14s
143050K .......... .......... .......... .......... .......... 53% 26.9M 14s
143100K .......... .......... .......... .......... .......... 53% 28.5M 14s
143150K .......... .......... .......... .......... .......... 53% 13.8M 14s
143200K .......... .......... .......... .......... .......... 53% 12.8M 14s
143250K .......... .......... .......... .......... .......... 53%  144M 14s
143300K .......... .......... .......... .......... .......... 53% 80.4M 14s
143350K .......... .......... .......... .......... .......... 53% 12.8M 14s
143400K .......... .......... .......... .......... .......... 53%  111M 14s
143450K .......... .......... .......... .......... .......... 53% 22.3M 14s
143500K .......... .......... .......... .......... .......... 54% 33.6M 14s
143550K .......... .......... .......... .......... .......... 54% 27.1M 14s
143600K .......... .......... .......... .......... .......... 54% 23.2M 14s
143650K .......... .......... .......... .......... .......... 54% 27.1M 14s
143700K .......... .......... .......... .......... .......... 54% 22.5M 14s
143750K .......... .......... .......... .......... .......... 54% 21.0M 14s
143800K .......... .......... .......... .......... .......... 54% 40.6M 14s
143850K .......... .......... .......... .......... .......... 54% 22.5M 14s
143900K .......... .......... .......... .......... .......... 54% 23.6M 14s
143950K .......... .......... .......... .......... .......... 54% 23.4M 14s
144000K .......... .......... .......... .......... .......... 54% 25.7M 14s
144050K .......... .......... .......... .......... .......... 54% 24.8M 14s
144100K .......... .......... .......... .......... .......... 54% 18.5M 14s
144150K .......... .......... .......... .......... .......... 54% 24.0M 14s
144200K .......... .......... .......... .......... .......... 54% 25.6M 14s
144250K .......... .......... .......... .......... .......... 54% 26.1M 14s
144300K .......... .......... .......... .......... .......... 54% 23.4M 14s
144350K .......... .......... .......... .......... .......... 54% 21.2M 14s
144400K .......... .......... .......... .......... .......... 54% 25.1M 14s
144450K .......... .......... .......... .......... .......... 54% 20.2M 14s
144500K .......... .......... .......... .......... .......... 54% 20.4M 14s
144550K .......... .......... .......... .......... .......... 54% 18.5M 14s
144600K .......... .......... .......... .......... .......... 54% 11.4M 14s
144650K .......... .......... .......... .......... .......... 54% 60.2M 14s
144700K .......... .......... .......... .......... .......... 54% 22.1M 14s
144750K .......... .......... .......... .......... .......... 54% 24.0M 14s
144800K .......... .......... .......... .......... .......... 54% 26.6M 14s
144850K .......... .......... .......... .......... .......... 54% 17.4M 14s
144900K .......... .......... .......... .......... .......... 54% 24.5M 14s
144950K .......... .......... .......... .......... .......... 54% 17.6M 14s
145000K .......... .......... .......... .......... .......... 54% 23.8M 14s
145050K .......... .......... .......... .......... .......... 54% 23.3M 14s
145100K .......... .......... .......... .......... .......... 54% 16.7M 14s
145150K .......... .......... .......... .......... .......... 54% 20.1M 14s
145200K .......... .......... .......... .......... .......... 54% 18.2M 14s
145250K .......... .......... .......... .......... .......... 54% 21.0M 14s
145300K .......... .......... .......... .......... .......... 54% 23.3M 14s
145350K .......... .......... .......... .......... .......... 54% 17.6M 14s
145400K .......... .......... .......... .......... .......... 54% 22.9M 14s
145450K .......... .......... .......... .......... .......... 54% 18.3M 14s
145500K .......... .......... .......... .......... .......... 54% 17.8M 14s
145550K .......... .......... .......... .......... .......... 54% 34.0M 13s
145600K .......... .......... .......... .......... .......... 54% 14.4M 13s
145650K .......... .......... .......... .......... .......... 54% 47.8M 13s
145700K .......... .......... .......... .......... .......... 54% 39.4M 13s
145750K .......... .......... .......... .......... .......... 54% 30.7M 13s
145800K .......... .......... .......... .......... .......... 54% 46.2M 13s
145850K .......... .......... .......... .......... .......... 54% 23.4M 13s
145900K .......... .......... .......... .......... .......... 54% 18.6M 13s
145950K .......... .......... .......... .......... .......... 54% 26.9M 13s
146000K .......... .......... .......... .......... .......... 54% 25.2M 13s
146050K .......... .......... .......... .......... .......... 54% 22.4M 13s
146100K .......... .......... .......... .......... .......... 54% 19.9M 13s
146150K .......... .......... .......... .......... .......... 55% 22.9M 13s
146200K .......... .......... .......... .......... .......... 55% 19.4M 13s
146250K .......... .......... .......... .......... .......... 55% 24.8M 13s
146300K .......... .......... .......... .......... .......... 55% 20.0M 13s
146350K .......... .......... .......... .......... .......... 55% 23.5M 13s
146400K .......... .......... .......... .......... .......... 55% 21.4M 13s
146450K .......... .......... .......... .......... .......... 55% 19.3M 13s
146500K .......... .......... .......... .......... .......... 55% 25.8M 13s
146550K .......... .......... .......... .......... .......... 55% 24.0M 13s
146600K .......... .......... .......... .......... .......... 55% 21.5M 13s
146650K .......... .......... .......... .......... .......... 55% 12.9M 13s
146700K .......... .......... .......... .......... .......... 55% 11.7M 13s
146750K .......... .......... .......... .......... .......... 55% 12.7M 13s
146800K .......... .......... .......... .......... .......... 55% 13.1M 13s
146850K .......... .......... .......... .......... .......... 55% 10.3M 13s
146900K .......... .......... .......... .......... .......... 55% 13.2M 13s
146950K .......... .......... .......... .......... .......... 55% 10.6M 13s
147000K .......... .......... .......... .......... .......... 55% 11.9M 13s
147050K .......... .......... .......... .......... .......... 55% 13.2M 13s
147100K .......... .......... .......... .......... .......... 55% 11.3M 13s
147150K .......... .......... .......... .......... .......... 55% 29.7M 13s
147200K .......... .......... .......... .......... .......... 55% 27.6M 13s
147250K .......... .......... .......... .......... .......... 55% 25.2M 13s
147300K .......... .......... .......... .......... .......... 55% 25.8M 13s
147350K .......... .......... .......... .......... .......... 55% 24.7M 13s
147400K .......... .......... .......... .......... .......... 55% 24.3M 13s
147450K .......... .......... .......... .......... .......... 55% 16.8M 13s
147500K .......... .......... .......... .......... .......... 55% 26.2M 13s
147550K .......... .......... .......... .......... .......... 55% 58.1M 13s
147600K .......... .......... .......... .......... .......... 55% 27.7M 13s
147650K .......... .......... .......... .......... .......... 55% 18.8M 13s
147700K .......... .......... .......... .......... .......... 55% 21.4M 13s
147750K .......... .......... .......... .......... .......... 55% 23.0M 13s
147800K .......... .......... .......... .......... .......... 55% 19.5M 13s
147850K .......... .......... .......... .......... .......... 55% 16.4M 13s
147900K .......... .......... .......... .......... .......... 55% 20.7M 13s
147950K .......... .......... .......... .......... .......... 55% 17.0M 13s
148000K .......... .......... .......... .......... .......... 55% 16.9M 13s
148050K .......... .......... .......... .......... .......... 55% 22.3M 13s
148100K .......... .......... .......... .......... .......... 55% 18.3M 13s
148150K .......... .......... .......... .......... .......... 55% 23.4M 13s
148200K .......... .......... .......... .......... .......... 55% 16.6M 13s
148250K .......... .......... .......... .......... .......... 55% 18.4M 13s
148300K .......... .......... .......... .......... .......... 55% 19.9M 13s
148350K .......... .......... .......... .......... .......... 55% 18.2M 13s
148400K .......... .......... .......... .......... .......... 55% 9.08M 13s
148450K .......... .......... .......... .......... .......... 55% 82.2M 13s
148500K .......... .......... .......... .......... .......... 55% 14.0M 13s
148550K .......... .......... .......... .......... .......... 55% 20.6M 13s
148600K .......... .......... .......... .......... .......... 55% 12.0M 13s
148650K .......... .......... .......... .......... .......... 55% 19.4M 13s
148700K .......... .......... .......... .......... .......... 55% 12.8M 13s
148750K .......... .......... .......... .......... .......... 55% 16.0M 13s
148800K .......... .......... .......... .......... .......... 56% 15.4M 13s
148850K .......... .......... .......... .......... .......... 56% 17.2M 13s
148900K .......... .......... .......... .......... .......... 56% 11.7M 13s
148950K .......... .......... .......... .......... .......... 56% 13.2M 13s
149000K .......... .......... .......... .......... .......... 56% 13.9M 13s
149050K .......... .......... .......... .......... .......... 56% 13.1M 13s
149100K .......... .......... .......... .......... .......... 56% 11.4M 13s
149150K .......... .......... .......... .......... .......... 56% 8.98M 13s
149200K .......... .......... .......... .......... .......... 56% 8.38M 13s
149250K .......... .......... .......... .......... .......... 56% 11.2M 13s
149300K .......... .......... .......... .......... .......... 56% 13.9M 13s
149350K .......... .......... .......... .......... .......... 56% 11.4M 13s
149400K .......... .......... .......... .......... .......... 56% 13.0M 13s
149450K .......... .......... .......... .......... .......... 56% 12.4M 13s
149500K .......... .......... .......... .......... .......... 56% 15.1M 13s
149550K .......... .......... .......... .......... .......... 56% 11.3M 13s
149600K .......... .......... .......... .......... .......... 56% 12.3M 13s
149650K .......... .......... .......... .......... .......... 56% 14.2M 13s
149700K .......... .......... .......... .......... .......... 56% 12.8M 13s
149750K .......... .......... .......... .......... .......... 56% 23.8M 13s
149800K .......... .......... .......... .......... .......... 56% 13.1M 13s
149850K .......... .......... .......... .......... .......... 56% 21.2M 13s
149900K .......... .......... .......... .......... .......... 56% 21.9M 13s
149950K .......... .......... .......... .......... .......... 56% 18.0M 13s
150000K .......... .......... .......... .......... .......... 56% 20.1M 13s
150050K .......... .......... .......... .......... .......... 56% 22.6M 13s
150100K .......... .......... .......... .......... .......... 56% 21.6M 13s
150150K .......... .......... .......... .......... .......... 56% 22.1M 13s
150200K .......... .......... .......... .......... .......... 56% 18.2M 13s
150250K .......... .......... .......... .......... .......... 56% 21.3M 13s
150300K .......... .......... .......... .......... .......... 56% 44.5M 13s
150350K .......... .......... .......... .......... .......... 56% 20.2M 13s
150400K .......... .......... .......... .......... .......... 56% 30.7M 13s
150450K .......... .......... .......... .......... .......... 56% 23.8M 13s
150500K .......... .......... .......... .......... .......... 56% 31.5M 13s
150550K .......... .......... .......... .......... .......... 56% 25.6M 13s
150600K .......... .......... .......... .......... .......... 56% 26.2M 13s
150650K .......... .......... .......... .......... .......... 56% 30.1M 13s
150700K .......... .......... .......... .......... .......... 56% 20.8M 13s
150750K .......... .......... .......... .......... .......... 56% 34.7M 13s
150800K .......... .......... .......... .......... .......... 56% 33.1M 13s
150850K .......... .......... .......... .......... .......... 56% 37.9M 13s
150900K .......... .......... .......... .......... .......... 56%  119M 13s
150950K .......... .......... .......... .......... .......... 56% 53.6M 13s
151000K .......... .......... .......... .......... .......... 56%  105M 13s
151050K .......... .......... .......... .......... .......... 56% 18.9M 13s
151100K .......... .......... .......... .......... .......... 56%  128M 13s
151150K .......... .......... .......... .......... .......... 56%  161M 13s
151200K .......... .......... .......... .......... .......... 56% 34.2M 13s
151250K .......... .......... .......... .......... .......... 56% 24.7M 13s
151300K .......... .......... .......... .......... .......... 56%  120M 13s
151350K .......... .......... .......... .......... .......... 56% 87.7M 13s
151400K .......... .......... .......... .......... .......... 56%  105M 13s
151450K .......... .......... .......... .......... .......... 56%  109M 13s
151500K .......... .......... .......... .......... .......... 57% 83.0M 13s
151550K .......... .......... .......... .......... .......... 57% 19.1M 13s
151600K .......... .......... .......... .......... .......... 57%  111M 13s
151650K .......... .......... .......... .......... .......... 57% 51.7M 13s
151700K .......... .......... .......... .......... .......... 57% 37.7M 13s
151750K .......... .......... .......... .......... .......... 57% 33.1M 13s
151800K .......... .......... .......... .......... .......... 57% 46.0M 12s
151850K .......... .......... .......... .......... .......... 57% 35.7M 12s
151900K .......... .......... .......... .......... .......... 57% 45.4M 12s
151950K .......... .......... .......... .......... .......... 57% 44.9M 12s
152000K .......... .......... .......... .......... .......... 57% 32.1M 12s
152050K .......... .......... .......... .......... .......... 57% 48.4M 12s
152100K .......... .......... .......... .......... .......... 57% 37.0M 12s
152150K .......... .......... .......... .......... .......... 57% 37.6M 12s
152200K .......... .......... .......... .......... .......... 57% 37.2M 12s
152250K .......... .......... .......... .......... .......... 57% 39.0M 12s
152300K .......... .......... .......... .......... .......... 57% 54.0M 12s
152350K .......... .......... .......... .......... .......... 57% 38.0M 12s
152400K .......... .......... .......... .......... .......... 57% 37.6M 12s
152450K .......... .......... .......... .......... .......... 57% 29.3M 12s
152500K .......... .......... .......... .......... .......... 57% 46.9M 12s
152550K .......... .......... .......... .......... .......... 57% 49.2M 12s
152600K .......... .......... .......... .......... .......... 57% 36.7M 12s
152650K .......... .......... .......... .......... .......... 57% 41.9M 12s
152700K .......... .......... .......... .......... .......... 57% 40.6M 12s
152750K .......... .......... .......... .......... .......... 57% 37.3M 12s
152800K .......... .......... .......... .......... .......... 57% 33.9M 12s
152850K .......... .......... .......... .......... .......... 57% 20.0M 12s
152900K .......... .......... .......... .......... .......... 57% 14.9M 12s
152950K .......... .......... .......... .......... .......... 57%  122M 12s
153000K .......... .......... .......... .......... .......... 57% 31.4M 12s
153050K .......... .......... .......... .......... .......... 57%  121M 12s
153100K .......... .......... .......... .......... .......... 57% 21.3M 12s
153150K .......... .......... .......... .......... .......... 57% 43.2M 12s
153200K .......... .......... .......... .......... .......... 57% 25.2M 12s
153250K .......... .......... .......... .......... .......... 57% 23.6M 12s
153300K .......... .......... .......... .......... .......... 57% 37.3M 12s
153350K .......... .......... .......... .......... .......... 57% 19.8M 12s
153400K .......... .......... .......... .......... .......... 57% 20.8M 12s
153450K .......... .......... .......... .......... .......... 57% 28.8M 12s
153500K .......... .......... .......... .......... .......... 57% 20.4M 12s
153550K .......... .......... .......... .......... .......... 57% 33.1M 12s
153600K .......... .......... .......... .......... .......... 57% 22.9M 12s
153650K .......... .......... .......... .......... .......... 57% 21.9M 12s
153700K .......... .......... .......... .......... .......... 57% 21.1M 12s
153750K .......... .......... .......... .......... .......... 57% 20.8M 12s
153800K .......... .......... .......... .......... .......... 57% 28.9M 12s
153850K .......... .......... .......... .......... .......... 57% 21.5M 12s
153900K .......... .......... .......... .......... .......... 57% 37.5M 12s
153950K .......... .......... .......... .......... .......... 57% 19.7M 12s
154000K .......... .......... .......... .......... .......... 57% 19.6M 12s
154050K .......... .......... .......... .......... .......... 57% 12.8M 12s
154100K .......... .......... .......... .......... .......... 57% 17.4M 12s
154150K .......... .......... .......... .......... .......... 58% 21.8M 12s
154200K .......... .......... .......... .......... .......... 58% 16.8M 12s
154250K .......... .......... .......... .......... .......... 58% 16.1M 12s
154300K .......... .......... .......... .......... .......... 58% 19.2M 12s
154350K .......... .......... .......... .......... .......... 58% 20.7M 12s
154400K .......... .......... .......... .......... .......... 58% 18.0M 12s
154450K .......... .......... .......... .......... .......... 58% 18.0M 12s
154500K .......... .......... .......... .......... .......... 58% 17.5M 12s
154550K .......... .......... .......... .......... .......... 58% 21.0M 12s
154600K .......... .......... .......... .......... .......... 58% 17.1M 12s
154650K .......... .......... .......... .......... .......... 58% 18.2M 12s
154700K .......... .......... .......... .......... .......... 58% 17.5M 12s
154750K .......... .......... .......... .......... .......... 58% 25.6M 12s
154800K .......... .......... .......... .......... .......... 58% 18.3M 12s
154850K .......... .......... .......... .......... .......... 58% 16.0M 12s
154900K .......... .......... .......... .......... .......... 58% 41.7M 12s
154950K .......... .......... .......... .......... .......... 58% 15.4M 12s
155000K .......... .......... .......... .......... .......... 58% 19.4M 12s
155050K .......... .......... .......... .......... .......... 58% 18.7M 12s
155100K .......... .......... .......... .......... .......... 58% 19.2M 12s
155150K .......... .......... .......... .......... .......... 58% 16.0M 12s
155200K .......... .......... .......... .......... .......... 58% 12.0M 12s
155250K .......... .......... .......... .......... .......... 58% 15.4M 12s
155300K .......... .......... .......... .......... .......... 58% 14.8M 12s
155350K .......... .......... .......... .......... .......... 58% 10.3M 12s
155400K .......... .......... .......... .......... .......... 58% 15.9M 12s
155450K .......... .......... .......... .......... .......... 58% 12.2M 12s
155500K .......... .......... .......... .......... .......... 58% 15.0M 12s
155550K .......... .......... .......... .......... .......... 58% 14.6M 12s
155600K .......... .......... .......... .......... .......... 58% 17.2M 12s
155650K .......... .......... .......... .......... .......... 58% 12.1M 12s
155700K .......... .......... .......... .......... .......... 58% 57.2M 12s
155750K .......... .......... .......... .......... .......... 58% 23.0M 12s
155800K .......... .......... .......... .......... .......... 58% 29.9M 12s
155850K .......... .......... .......... .......... .......... 58% 15.4M 12s
155900K .......... .......... .......... .......... .......... 58% 16.2M 12s
155950K .......... .......... .......... .......... .......... 58% 15.8M 12s
156000K .......... .......... .......... .......... .......... 58% 21.8M 12s
156050K .......... .......... .......... .......... .......... 58% 17.3M 12s
156100K .......... .......... .......... .......... .......... 58% 16.0M 12s
156150K .......... .......... .......... .......... .......... 58% 28.2M 12s
156200K .......... .......... .......... .......... .......... 58% 15.5M 12s
156250K .......... .......... .......... .......... .......... 58% 17.3M 12s
156300K .......... .......... .......... .......... .......... 58% 16.8M 12s
156350K .......... .......... .......... .......... .......... 58% 17.0M 12s
156400K .......... .......... .......... .......... .......... 58% 22.3M 12s
156450K .......... .......... .......... .......... .......... 58% 19.4M 12s
156500K .......... .......... .......... .......... .......... 58% 23.6M 12s
156550K .......... .......... .......... .......... .......... 58% 85.1M 12s
156600K .......... .......... .......... .......... .......... 58% 31.0M 12s
156650K .......... .......... .......... .......... .......... 58% 33.8M 12s
156700K .......... .......... .......... .......... .......... 58% 12.6M 12s
156750K .......... .......... .......... .......... .......... 58%  131M 12s
156800K .......... .......... .......... .......... .......... 59%  125M 12s
156850K .......... .......... .......... .......... .......... 59% 41.0M 12s
156900K .......... .......... .......... .......... .......... 59%  137M 12s
156950K .......... .......... .......... .......... .......... 59% 36.1M 12s
157000K .......... .......... .......... .......... .......... 59% 48.3M 12s
157050K .......... .......... .......... .......... .......... 59% 39.0M 12s
157100K .......... .......... .......... .......... .......... 59% 39.3M 12s
157150K .......... .......... .......... .......... .......... 59% 35.6M 12s
157200K .......... .......... .......... .......... .......... 59% 26.4M 12s
157250K .......... .......... .......... .......... .......... 59% 49.7M 12s
157300K .......... .......... .......... .......... .......... 59% 42.3M 12s
157350K .......... .......... .......... .......... .......... 59% 40.4M 12s
157400K .......... .......... .......... .......... .......... 59% 29.4M 12s
157450K .......... .......... .......... .......... .......... 59% 39.3M 12s
157500K .......... .......... .......... .......... .......... 59% 41.5M 12s
157550K .......... .......... .......... .......... .......... 59% 44.1M 12s
157600K .......... .......... .......... .......... .......... 59% 30.6M 12s
157650K .......... .......... .......... .......... .......... 59% 43.1M 12s
157700K .......... .......... .......... .......... .......... 59% 40.1M 12s
157750K .......... .......... .......... .......... .......... 59% 36.8M 12s
157800K .......... .......... .......... .......... .......... 59% 40.0M 12s
157850K .......... .......... .......... .......... .......... 59% 40.5M 12s
157900K .......... .......... .......... .......... .......... 59% 44.8M 12s
157950K .......... .......... .......... .......... .......... 59% 28.3M 12s
158000K .......... .......... .......... .......... .......... 59% 36.0M 12s
158050K .......... .......... .......... .......... .......... 59% 48.3M 12s
158100K .......... .......... .......... .......... .......... 59% 33.3M 12s
158150K .......... .......... .......... .......... .......... 59% 39.8M 12s
158200K .......... .......... .......... .......... .......... 59% 42.2M 11s
158250K .......... .......... .......... .......... .......... 59% 26.9M 11s
158300K .......... .......... .......... .......... .......... 59%  115M 11s
158350K .......... .......... .......... .......... .......... 59% 35.4M 11s
158400K .......... .......... .......... .......... .......... 59% 12.2M 11s
158450K .......... .......... .......... .......... .......... 59%  138M 11s
158500K .......... .......... .......... .......... .......... 59% 21.6M 11s
158550K .......... .......... .......... .......... .......... 59%  121M 11s
158600K .......... .......... .......... .......... .......... 59% 89.1M 11s
158650K .......... .......... .......... .......... .......... 59%  108M 11s
158700K .......... .......... .......... .......... .......... 59%  109M 11s
158750K .......... .......... .......... .......... .......... 59%  174M 11s
158800K .......... .......... .......... .......... .......... 59%  182M 11s
158850K .......... .......... .......... .......... .......... 59% 37.5M 11s
158900K .......... .......... .......... .......... .......... 59% 70.3M 11s
158950K .......... .......... .......... .......... .......... 59% 44.6M 11s
159000K .......... .......... .......... .......... .......... 59% 58.3M 11s
159050K .......... .......... .......... .......... .......... 59% 51.8M 11s
159100K .......... .......... .......... .......... .......... 59% 43.4M 11s
159150K .......... .......... .......... .......... .......... 59% 59.7M 11s
159200K .......... .......... .......... .......... .......... 59% 48.1M 11s
159250K .......... .......... .......... .......... .......... 59% 49.8M 11s
159300K .......... .......... .......... .......... .......... 59% 50.3M 11s
159350K .......... .......... .......... .......... .......... 59% 37.1M 11s
159400K .......... .......... .......... .......... .......... 59% 44.8M 11s
159450K .......... .......... .......... .......... .......... 60% 35.1M 11s
159500K .......... .......... .......... .......... .......... 60% 55.2M 11s
159550K .......... .......... .......... .......... .......... 60% 48.7M 11s
159600K .......... .......... .......... .......... .......... 60% 35.1M 11s
159650K .......... .......... .......... .......... .......... 60% 57.9M 11s
159700K .......... .......... .......... .......... .......... 60% 37.4M 11s
159750K .......... .......... .......... .......... .......... 60% 61.2M 11s
159800K .......... .......... .......... .......... .......... 60% 54.2M 11s
159850K .......... .......... .......... .......... .......... 60% 46.0M 11s
159900K .......... .......... .......... .......... .......... 60% 46.2M 11s
159950K .......... .......... .......... .......... .......... 60% 41.0M 11s
160000K .......... .......... .......... .......... .......... 60% 46.5M 11s
160050K .......... .......... .......... .......... .......... 60%  135M 11s
160100K .......... .......... .......... .......... .......... 60% 41.6M 11s
160150K .......... .......... .......... .......... .......... 60% 52.6M 11s
160200K .......... .......... .......... .......... .......... 60% 46.7M 11s
160250K .......... .......... .......... .......... .......... 60% 49.0M 11s
160300K .......... .......... .......... .......... .......... 60% 88.1M 11s
160350K .......... .......... .......... .......... .......... 60% 50.6M 11s
160400K .......... .......... .......... .......... .......... 60% 46.7M 11s
160450K .......... .......... .......... .......... .......... 60% 51.0M 11s
160500K .......... .......... .......... .......... .......... 60% 51.9M 11s
160550K .......... .......... .......... .......... .......... 60% 87.3M 11s
160600K .......... .......... .......... .......... .......... 60% 53.7M 11s
160650K .......... .......... .......... .......... .......... 60% 50.4M 11s
160700K .......... .......... .......... .......... .......... 60% 38.7M 11s
160750K .......... .......... .......... .......... .......... 60% 33.8M 11s
160800K .......... .......... .......... .......... .......... 60%  137M 11s
160850K .......... .......... .......... .......... .......... 60% 17.1M 11s
160900K .......... .......... .......... .......... .......... 60% 30.9M 11s
160950K .......... .......... .......... .......... .......... 60%  131M 11s
161000K .......... .......... .......... .......... .......... 60%  101M 11s
161050K .......... .......... .......... .......... .......... 60%  132M 11s
161100K .......... .......... .......... .......... .......... 60% 79.8M 11s
161150K .......... .......... .......... .......... .......... 60% 71.8M 11s
161200K .......... .......... .......... .......... .......... 60% 71.3M 11s
161250K .......... .......... .......... .......... .......... 60% 74.8M 11s
161300K .......... .......... .......... .......... .......... 60% 46.6M 11s
161350K .......... .......... .......... .......... .......... 60% 42.1M 11s
161400K .......... .......... .......... .......... .......... 60% 47.3M 11s
161450K .......... .......... .......... .......... .......... 60% 42.1M 11s
161500K .......... .......... .......... .......... .......... 60% 51.3M 11s
161550K .......... .......... .......... .......... .......... 60% 45.1M 11s
161600K .......... .......... .......... .......... .......... 60% 25.8M 11s
161650K .......... .......... .......... .......... .......... 60% 41.0M 11s
161700K .......... .......... .......... .......... .......... 60% 45.1M 11s
161750K .......... .......... .......... .......... .......... 60% 46.6M 11s
161800K .......... .......... .......... .......... .......... 60% 42.3M 11s
161850K .......... .......... .......... .......... .......... 60% 39.7M 11s
161900K .......... .......... .......... .......... .......... 60% 42.7M 11s
161950K .......... .......... .......... .......... .......... 60% 40.7M 11s
162000K .......... .......... .......... .......... .......... 60% 39.4M 11s
162050K .......... .......... .......... .......... .......... 60% 54.6M 11s
162100K .......... .......... .......... .......... .......... 61% 37.8M 11s
162150K .......... .......... .......... .......... .......... 61% 39.1M 11s
162200K .......... .......... .......... .......... .......... 61% 40.5M 11s
162250K .......... .......... .......... .......... .......... 61% 28.0M 11s
162300K .......... .......... .......... .......... .......... 61% 35.8M 11s
162350K .......... .......... .......... .......... .......... 61% 44.2M 11s
162400K .......... .......... .......... .......... .......... 61% 37.4M 11s
162450K .......... .......... .......... .......... .......... 61% 35.9M 11s
162500K .......... .......... .......... .......... .......... 61% 40.0M 11s
162550K .......... .......... .......... .......... .......... 61% 32.8M 11s
162600K .......... .......... .......... .......... .......... 61% 37.8M 11s
162650K .......... .......... .......... .......... .......... 61% 38.4M 11s
162700K .......... .......... .......... .......... .......... 61% 88.0M 11s
162750K .......... .......... .......... .......... .......... 61% 31.7M 11s
162800K .......... .......... .......... .......... .......... 61%  105M 11s
162850K .......... .......... .......... .......... .......... 61% 13.2M 11s
162900K .......... .......... .......... .......... .......... 61%  108M 11s
162950K .......... .......... .......... .......... .......... 61%  106M 11s
163000K .......... .......... .......... .......... .......... 61%  149M 11s
163050K .......... .......... .......... .......... .......... 61% 51.2M 11s
163100K .......... .......... .......... .......... .......... 61% 48.1M 11s
163150K .......... .......... .......... .......... .......... 61% 39.5M 11s
163200K .......... .......... .......... .......... .......... 61%  118M 11s
163250K .......... .......... .......... .......... .......... 61%  172M 11s
163300K .......... .......... .......... .......... .......... 61%  138M 11s
163350K .......... .......... .......... .......... .......... 61% 50.5M 11s
163400K .......... .......... .......... .......... .......... 61%  114M 11s
163450K .......... .......... .......... .......... .......... 61% 50.8M 11s
163500K .......... .......... .......... .......... .......... 61% 56.4M 11s
163550K .......... .......... .......... .......... .......... 61% 95.6M 11s
163600K .......... .......... .......... .......... .......... 61% 36.0M 11s
163650K .......... .......... .......... .......... .......... 61% 60.6M 11s
163700K .......... .......... .......... .......... .......... 61% 32.7M 11s
163750K .......... .......... .......... .......... .......... 61% 77.9M 11s
163800K .......... .......... .......... .......... .......... 61% 53.2M 11s
163850K .......... .......... .......... .......... .......... 61% 38.5M 11s
163900K .......... .......... .......... .......... .......... 61% 54.9M 11s
163950K .......... .......... .......... .......... .......... 61% 44.3M 11s
164000K .......... .......... .......... .......... .......... 61% 54.9M 11s
164050K .......... .......... .......... .......... .......... 61% 36.6M 11s
164100K .......... .......... .......... .......... .......... 61% 42.0M 11s
164150K .......... .......... .......... .......... .......... 61% 38.4M 11s
164200K .......... .......... .......... .......... .......... 61% 42.3M 11s
164250K .......... .......... .......... .......... .......... 61% 42.4M 11s
164300K .......... .......... .......... .......... .......... 61% 46.7M 11s
164350K .......... .......... .......... .......... .......... 61% 46.5M 11s
164400K .......... .......... .......... .......... .......... 61% 51.5M 11s
164450K .......... .......... .......... .......... .......... 61% 33.7M 10s
164500K .......... .......... .......... .......... .......... 61% 47.8M 10s
164550K .......... .......... .......... .......... .......... 61% 39.7M 10s
164600K .......... .......... .......... .......... .......... 61% 42.7M 10s
164650K .......... .......... .......... .......... .......... 61% 62.8M 10s
164700K .......... .......... .......... .......... .......... 61% 38.0M 10s
164750K .......... .......... .......... .......... .......... 62% 54.1M 10s
164800K .......... .......... .......... .......... .......... 62% 89.9M 10s
164850K .......... .......... .......... .......... .......... 62% 12.8M 10s
164900K .......... .......... .......... .......... .......... 62% 97.7M 10s
164950K .......... .......... .......... .......... .......... 62% 38.9M 10s
165000K .......... .......... .......... .......... .......... 62% 76.8M 10s
165050K .......... .......... .......... .......... .......... 62% 53.2M 10s
165100K .......... .......... .......... .......... .......... 62% 85.4M 10s
165150K .......... .......... .......... .......... .......... 62%  118M 10s
165200K .......... .......... .......... .......... .......... 62% 14.3M 10s
165250K .......... .......... .......... .......... .......... 62%  146M 10s
165300K .......... .......... .......... .......... .......... 62% 70.2M 10s
165350K .......... .......... .......... .......... .......... 62% 80.0M 10s
165400K .......... .......... .......... .......... .......... 62%  133M 10s
165450K .......... .......... .......... .......... .......... 62% 43.8M 10s
165500K .......... .......... .......... .......... .......... 62%  101M 10s
165550K .......... .......... .......... .......... .......... 62%  118M 10s
165600K .......... .......... .......... .......... .......... 62% 32.1M 10s
165650K .......... .......... .......... .......... .......... 62%  152M 10s
165700K .......... .......... .......... .......... .......... 62%  114M 10s
165750K .......... .......... .......... .......... .......... 62%  133M 10s
165800K .......... .......... .......... .......... .......... 62%  111M 10s
165850K .......... .......... .......... .......... .......... 62%  104M 10s
165900K .......... .......... .......... .......... .......... 62% 67.6M 10s
165950K .......... .......... .......... .......... .......... 62% 41.2M 10s
166000K .......... .......... .......... .......... .......... 62% 45.8M 10s
166050K .......... .......... .......... .......... .......... 62% 41.5M 10s
166100K .......... .......... .......... .......... .......... 62% 51.1M 10s
166150K .......... .......... .......... .......... .......... 62% 80.2M 10s
166200K .......... .......... .......... .......... .......... 62% 42.7M 10s
166250K .......... .......... .......... .......... .......... 62% 46.9M 10s
166300K .......... .......... .......... .......... .......... 62% 48.9M 10s
166350K .......... .......... .......... .......... .......... 62% 41.5M 10s
166400K .......... .......... .......... .......... .......... 62% 50.6M 10s
166450K .......... .......... .......... .......... .......... 62% 46.9M 10s
166500K .......... .......... .......... .......... .......... 62% 71.3M 10s
166550K .......... .......... .......... .......... .......... 62% 53.6M 10s
166600K .......... .......... .......... .......... .......... 62% 45.0M 10s
166650K .......... .......... .......... .......... .......... 62% 54.9M 10s
166700K .......... .......... .......... .......... .......... 62% 48.3M 10s
166750K .......... .......... .......... .......... .......... 62% 43.4M 10s
166800K .......... .......... .......... .......... .......... 62% 58.9M 10s
166850K .......... .......... .......... .......... .......... 62% 42.4M 10s
166900K .......... .......... .......... .......... .......... 62% 40.2M 10s
166950K .......... .......... .......... .......... .......... 62% 34.0M 10s
167000K .......... .......... .......... .......... .......... 62%  105M 10s
167050K .......... .......... .......... .......... .......... 62% 38.8M 10s
167100K .......... .......... .......... .......... .......... 62% 34.1M 10s
167150K .......... .......... .......... .......... .......... 62% 45.4M 10s
167200K .......... .......... .......... .......... .......... 62% 43.6M 10s
167250K .......... .......... .......... .......... .......... 62% 50.0M 10s
167300K .......... .......... .......... .......... .......... 62% 59.5M 10s
167350K .......... .......... .......... .......... .......... 62% 40.2M 10s
167400K .......... .......... .......... .......... .......... 62% 52.2M 10s
167450K .......... .......... .......... .......... .......... 63% 45.8M 10s
167500K .......... .......... .......... .......... .......... 63% 54.3M 10s
167550K .......... .......... .......... .......... .......... 63% 66.9M 10s
167600K .......... .......... .......... .......... .......... 63% 45.5M 10s
167650K .......... .......... .......... .......... .......... 63% 57.0M 10s
167700K .......... .......... .......... .......... .......... 63% 35.7M 10s
167750K .......... .......... .......... .......... .......... 63% 13.6M 10s
167800K .......... .......... .......... .......... .......... 63% 78.1M 10s
167850K .......... .......... .......... .......... .......... 63% 62.9M 10s
167900K .......... .......... .......... .......... .......... 63% 53.2M 10s
167950K .......... .......... .......... .......... .......... 63% 36.6M 10s
168000K .......... .......... .......... .......... .......... 63% 52.3M 10s
168050K .......... .......... .......... .......... .......... 63% 78.1M 10s
168100K .......... .......... .......... .......... .......... 63% 79.1M 10s
168150K .......... .......... .......... .......... .......... 63% 79.8M 10s
168200K .......... .......... .......... .......... .......... 63% 85.5M 10s
168250K .......... .......... .......... .......... .......... 63% 74.8M 10s
168300K .......... .......... .......... .......... .......... 63% 40.1M 10s
168350K .......... .......... .......... .......... .......... 63% 19.8M 10s
168400K .......... .......... .......... .......... .......... 63% 34.4M 10s
168450K .......... .......... .......... .......... .......... 63% 18.6M 10s
168500K .......... .......... .......... .......... .......... 63% 30.7M 10s
168550K .......... .......... .......... .......... .......... 63% 26.7M 10s
168600K .......... .......... .......... .......... .......... 63% 38.8M 10s
168650K .......... .......... .......... .......... .......... 63% 26.0M 10s
168700K .......... .......... .......... .......... .......... 63% 35.5M 10s
168750K .......... .......... .......... .......... .......... 63% 25.0M 10s
168800K .......... .......... .......... .......... .......... 63% 40.7M 10s
168850K .......... .......... .......... .......... .......... 63% 23.5M 10s
168900K .......... .......... .......... .......... .......... 63% 49.1M 10s
168950K .......... .......... .......... .......... .......... 63% 4.68M 10s
169000K .......... .......... .......... .......... .......... 63% 43.9M 10s
169050K .......... .......... .......... .......... .......... 63%  101M 10s
169100K .......... .......... .......... .......... .......... 63% 11.3M 10s
169150K .......... .......... .......... .......... .......... 63% 30.9M 10s
169200K .......... .......... .......... .......... .......... 63%  120M 10s
169250K .......... .......... .......... .......... .......... 63%  147M 10s
169300K .......... .......... .......... .......... .......... 63% 38.9M 10s
169350K .......... .......... .......... .......... .......... 63% 18.7M 10s
169400K .......... .......... .......... .......... .......... 63%  150M 10s
169450K .......... .......... .......... .......... .......... 63% 98.2M 10s
169500K .......... .......... .......... .......... .......... 63% 94.3M 10s
169550K .......... .......... .......... .......... .......... 63% 47.1M 10s
169600K .......... .......... .......... .......... .......... 63% 35.7M 10s
169650K .......... .......... .......... .......... .......... 63% 25.0M 10s
169700K .......... .......... .......... .......... .......... 63% 28.0M 10s
169750K .......... .......... .......... .......... .......... 63% 28.3M 10s
169800K .......... .......... .......... .......... .......... 63% 36.4M 10s
169850K .......... .......... .......... .......... .......... 63% 25.8M 10s
169900K .......... .......... .......... .......... .......... 63% 25.2M 10s
169950K .......... .......... .......... .......... .......... 63% 24.2M 10s
170000K .......... .......... .......... .......... .......... 63% 29.1M 10s
170050K .......... .......... .......... .......... .......... 63% 30.3M 10s
170100K .......... .......... .......... .......... .......... 64% 25.2M 10s
170150K .......... .......... .......... .......... .......... 64% 28.8M 10s
170200K .......... .......... .......... .......... .......... 64% 25.7M 10s
170250K .......... .......... .......... .......... .......... 64% 40.5M 10s
170300K .......... .......... .......... .......... .......... 64% 26.9M 10s
170350K .......... .......... .......... .......... .......... 64% 27.9M 10s
170400K .......... .......... .......... .......... .......... 64% 25.4M 10s
170450K .......... .......... .......... .......... .......... 64% 23.2M 10s
170500K .......... .......... .......... .......... .......... 64% 23.6M 10s
170550K .......... .......... .......... .......... .......... 64% 39.9M 10s
170600K .......... .......... .......... .......... .......... 64% 30.4M 10s
170650K .......... .......... .......... .......... .......... 64%  102M 10s
170700K .......... .......... .......... .......... .......... 64% 28.7M 10s
170750K .......... .......... .......... .......... .......... 64% 13.9M 10s
170800K .......... .......... .......... .......... .......... 64%  106M 10s
170850K .......... .......... .......... .......... .......... 64% 58.9M 10s
170900K .......... .......... .......... .......... .......... 64%  102M 10s
170950K .......... .......... .......... .......... .......... 64% 32.3M 10s
171000K .......... .......... .......... .......... .......... 64% 71.0M 10s
171050K .......... .......... .......... .......... .......... 64%  111M 10s
171100K .......... .......... .......... .......... .......... 64% 32.1M 10s
171150K .......... .......... .......... .......... .......... 64% 39.5M 10s
171200K .......... .......... .......... .......... .......... 64% 31.7M 10s
171250K .......... .......... .......... .......... .......... 64% 28.8M 9s
171300K .......... .......... .......... .......... .......... 64% 31.5M 9s
171350K .......... .......... .......... .......... .......... 64% 32.5M 9s
171400K .......... .......... .......... .......... .......... 64% 25.1M 9s
171450K .......... .......... .......... .......... .......... 64% 35.1M 9s
171500K .......... .......... .......... .......... .......... 64% 26.9M 9s
171550K .......... .......... .......... .......... .......... 64% 43.7M 9s
171600K .......... .......... .......... .......... .......... 64% 24.8M 9s
171650K .......... .......... .......... .......... .......... 64% 36.1M 9s
171700K .......... .......... .......... .......... .......... 64% 24.9M 9s
171750K .......... .......... .......... .......... .......... 64% 36.5M 9s
171800K .......... .......... .......... .......... .......... 64% 41.1M 9s
171850K .......... .......... .......... .......... .......... 64% 25.7M 9s
171900K .......... .......... .......... .......... .......... 64% 47.2M 9s
171950K .......... .......... .......... .......... .......... 64% 26.1M 9s
172000K .......... .......... .......... .......... .......... 64% 33.1M 9s
172050K .......... .......... .......... .......... .......... 64% 28.9M 9s
172100K .......... .......... .......... .......... .......... 64% 41.9M 9s
172150K .......... .......... .......... .......... .......... 64% 23.3M 9s
172200K .......... .......... .......... .......... .......... 64% 37.4M 9s
172250K .......... .......... .......... .......... .......... 64%  121M 9s
172300K .......... .......... .......... .......... .......... 64% 11.7M 9s
172350K .......... .......... .......... .......... .......... 64% 31.5M 9s
172400K .......... .......... .......... .......... .......... 64%  113M 9s
172450K .......... .......... .......... .......... .......... 64%  147M 9s
172500K .......... .......... .......... .......... .......... 64%  119M 9s
172550K .......... .......... .......... .......... .......... 64% 24.1M 9s
172600K .......... .......... .......... .......... .......... 64%  119M 9s
172650K .......... .......... .......... .......... .......... 64% 21.2M 9s
172700K .......... .......... .......... .......... .......... 64% 42.1M 9s
172750K .......... .......... .......... .......... .......... 65% 52.5M 9s
172800K .......... .......... .......... .......... .......... 65% 52.2M 9s
172850K .......... .......... .......... .......... .......... 65% 31.1M 9s
172900K .......... .......... .......... .......... .......... 65% 36.2M 9s
172950K .......... .......... .......... .......... .......... 65% 32.1M 9s
173000K .......... .......... .......... .......... .......... 65% 30.8M 9s
173050K .......... .......... .......... .......... .......... 65% 13.1M 9s
173100K .......... .......... .......... .......... .......... 65% 37.1M 9s
173150K .......... .......... .......... .......... .......... 65% 30.6M 9s
173200K .......... .......... .......... .......... .......... 65% 34.8M 9s
173250K .......... .......... .......... .......... .......... 65% 26.9M 9s
173300K .......... .......... .......... .......... .......... 65% 37.0M 9s
173350K .......... .......... .......... .......... .......... 65% 22.3M 9s
173400K .......... .......... .......... .......... .......... 65% 33.7M 9s
173450K .......... .......... .......... .......... .......... 65% 32.6M 9s
173500K .......... .......... .......... .......... .......... 65% 31.9M 9s
173550K .......... .......... .......... .......... .......... 65% 40.4M 9s
173600K .......... .......... .......... .......... .......... 65% 21.4M 9s
173650K .......... .......... .......... .......... .......... 65% 43.4M 9s
173700K .......... .......... .......... .......... .......... 65% 28.5M 9s
173750K .......... .......... .......... .......... .......... 65% 38.8M 9s
173800K .......... .......... .......... .......... .......... 65% 26.1M 9s
173850K .......... .......... .......... .......... .......... 65% 23.7M 9s
173900K .......... .......... .......... .......... .......... 65% 32.0M 9s
173950K .......... .......... .......... .......... .......... 65% 23.0M 9s
174000K .......... .......... .......... .......... .......... 65% 38.3M 9s
174050K .......... .......... .......... .......... .......... 65% 47.4M 9s
174100K .......... .......... .......... .......... .......... 65% 42.0M 9s
174150K .......... .......... .......... .......... .......... 65% 18.7M 9s
174200K .......... .......... .......... .......... .......... 65% 42.6M 9s
174250K .......... .......... .......... .......... .......... 65% 50.0M 9s
174300K .......... .......... .......... .......... .......... 65% 67.1M 9s
174350K .......... .......... .......... .......... .......... 65% 45.0M 9s
174400K .......... .......... .......... .......... .......... 65% 42.1M 9s
174450K .......... .......... .......... .......... .......... 65% 24.6M 9s
174500K .......... .......... .......... .......... .......... 65% 42.0M 9s
174550K .......... .......... .......... .......... .......... 65% 39.7M 9s
174600K .......... .......... .......... .......... .......... 65% 31.8M 9s
174650K .......... .......... .......... .......... .......... 65% 30.4M 9s
174700K .......... .......... .......... .......... .......... 65% 28.6M 9s
174750K .......... .......... .......... .......... .......... 65% 33.6M 9s
174800K .......... .......... .......... .......... .......... 65% 39.3M 9s
174850K .......... .......... .......... .......... .......... 65% 25.0M 9s
174900K .......... .......... .......... .......... .......... 65% 37.1M 9s
174950K .......... .......... .......... .......... .......... 65% 33.0M 9s
175000K .......... .......... .......... .......... .......... 65% 33.1M 9s
175050K .......... .......... .......... .......... .......... 65% 38.4M 9s
175100K .......... .......... .......... .......... .......... 65% 26.9M 9s
175150K .......... .......... .......... .......... .......... 65% 49.6M 9s
175200K .......... .......... .......... .......... .......... 65% 27.8M 9s
175250K .......... .......... .......... .......... .......... 65% 46.3M 9s
175300K .......... .......... .......... .......... .......... 65% 45.1M 9s
175350K .......... .......... .......... .......... .......... 65% 24.1M 9s
175400K .......... .......... .......... .......... .......... 66% 47.6M 9s
175450K .......... .......... .......... .......... .......... 66% 28.2M 9s
175500K .......... .......... .......... .......... .......... 66% 41.0M 9s
175550K .......... .......... .......... .......... .......... 66% 37.8M 9s
175600K .......... .......... .......... .......... .......... 66% 35.8M 9s
175650K .......... .......... .......... .......... .......... 66% 12.5M 9s
175700K .......... .......... .......... .......... .......... 66% 33.7M 9s
175750K .......... .......... .......... .......... .......... 66% 22.2M 9s
175800K .......... .......... .......... .......... .......... 66% 44.1M 9s
175850K .......... .......... .......... .......... .......... 66%  136M 9s
175900K .......... .......... .......... .......... .......... 66%  123M 9s
175950K .......... .......... .......... .......... .......... 66% 87.3M 9s
176000K .......... .......... .......... .......... .......... 66% 32.4M 9s
176050K .......... .......... .......... .......... .......... 66% 51.7M 9s
176100K .......... .......... .......... .......... .......... 66% 74.5M 9s
176150K .......... .......... .......... .......... .......... 66% 35.9M 9s
176200K .......... .......... .......... .......... .......... 66% 25.7M 9s
176250K .......... .......... .......... .......... .......... 66% 36.6M 9s
176300K .......... .......... .......... .......... .......... 66% 43.3M 9s
176350K .......... .......... .......... .......... .......... 66% 24.3M 9s
176400K .......... .......... .......... .......... .......... 66% 44.3M 9s
176450K .......... .......... .......... .......... .......... 66% 39.5M 9s
176500K .......... .......... .......... .......... .......... 66% 21.9M 9s
176550K .......... .......... .......... .......... .......... 66% 35.8M 9s
176600K .......... .......... .......... .......... .......... 66% 37.9M 9s
176650K .......... .......... .......... .......... .......... 66% 31.9M 9s
176700K .......... .......... .......... .......... .......... 66% 37.4M 9s
176750K .......... .......... .......... .......... .......... 66% 24.3M 9s
176800K .......... .......... .......... .......... .......... 66% 36.8M 9s
176850K .......... .......... .......... .......... .......... 66% 30.2M 9s
176900K .......... .......... .......... .......... .......... 66% 27.6M 9s
176950K .......... .......... .......... .......... .......... 66% 31.0M 9s
177000K .......... .......... .......... .......... .......... 66% 39.5M 9s
177050K .......... .......... .......... .......... .......... 66% 22.3M 9s
177100K .......... .......... .......... .......... .......... 66% 36.9M 9s
177150K .......... .......... .......... .......... .......... 66% 13.9M 9s
177200K .......... .......... .......... .......... .......... 66% 11.8M 9s
177250K .......... .......... .......... .......... .......... 66%  147M 9s
177300K .......... .......... .......... .......... .......... 66% 34.0M 9s
177350K .......... .......... .......... .......... .......... 66% 15.9M 9s
177400K .......... .......... .......... .......... .......... 66%  123M 9s
177450K .......... .......... .......... .......... .......... 66% 95.7M 9s
177500K .......... .......... .......... .......... .......... 66%  151M 9s
177550K .......... .......... .......... .......... .......... 66% 54.3M 9s
177600K .......... .......... .......... .......... .......... 66% 26.6M 9s
177650K .......... .......... .......... .......... .......... 66% 71.6M 9s
177700K .......... .......... .......... .......... .......... 66% 29.8M 9s
177750K .......... .......... .......... .......... .......... 66% 35.2M 9s
177800K .......... .......... .......... .......... .......... 66% 34.9M 9s
177850K .......... .......... .......... .......... .......... 66% 26.1M 9s
177900K .......... .......... .......... .......... .......... 66% 25.1M 9s
177950K .......... .......... .......... .......... .......... 66% 24.6M 9s
178000K .......... .......... .......... .......... .......... 66% 33.7M 9s
178050K .......... .......... .......... .......... .......... 67% 35.5M 9s
178100K .......... .......... .......... .......... .......... 67% 24.6M 9s
178150K .......... .......... .......... .......... .......... 67% 23.6M 9s
178200K .......... .......... .......... .......... .......... 67% 34.0M 9s
178250K .......... .......... .......... .......... .......... 67% 25.1M 9s
178300K .......... .......... .......... .......... .......... 67% 26.8M 9s
178350K .......... .......... .......... .......... .......... 67% 39.5M 9s
178400K .......... .......... .......... .......... .......... 67% 24.4M 9s
178450K .......... .......... .......... .......... .......... 67% 29.2M 9s
178500K .......... .......... .......... .......... .......... 67% 37.5M 9s
178550K .......... .......... .......... .......... .......... 67% 26.1M 9s
178600K .......... .......... .......... .......... .......... 67% 30.6M 9s
178650K .......... .......... .......... .......... .......... 67% 29.2M 9s
178700K .......... .......... .......... .......... .......... 67% 46.5M 8s
178750K .......... .......... .......... .......... .......... 67% 53.2M 8s
178800K .......... .......... .......... .......... .......... 67%  101M 8s
178850K .......... .......... .......... .......... .......... 67% 43.1M 8s
178900K .......... .......... .......... .......... .......... 67% 68.3M 8s
178950K .......... .......... .......... .......... .......... 67% 18.9M 8s
179000K .......... .......... .......... .......... .......... 67%  137M 8s
179050K .......... .......... .......... .......... .......... 67% 65.9M 8s
179100K .......... .......... .......... .......... .......... 67% 94.1M 8s
179150K .......... .......... .......... .......... .......... 67%  104M 8s
179200K .......... .......... .......... .......... .......... 67% 58.3M 8s
179250K .......... .......... .......... .......... .......... 67% 61.1M 8s
179300K .......... .......... .......... .......... .......... 67% 45.8M 8s
179350K .......... .......... .......... .......... .......... 67% 48.3M 8s
179400K .......... .......... .......... .......... .......... 67% 72.7M 8s
179450K .......... .......... .......... .......... .......... 67% 50.9M 8s
179500K .......... .......... .......... .......... .......... 67% 67.6M 8s
179550K .......... .......... .......... .......... .......... 67% 70.9M 8s
179600K .......... .......... .......... .......... .......... 67% 30.1M 8s
179650K .......... .......... .......... .......... .......... 67% 17.9M 8s
179700K .......... .......... .......... .......... .......... 67% 27.1M 8s
179750K .......... .......... .......... .......... .......... 67% 48.3M 8s
179800K .......... .......... .......... .......... .......... 67% 50.4M 8s
179850K .......... .......... .......... .......... .......... 67% 35.9M 8s
179900K .......... .......... .......... .......... .......... 67% 52.2M 8s
179950K .......... .......... .......... .......... .......... 67% 47.3M 8s
180000K .......... .......... .......... .......... .......... 67% 48.1M 8s
180050K .......... .......... .......... .......... .......... 67% 46.7M 8s
180100K .......... .......... .......... .......... .......... 67% 37.5M 8s
180150K .......... .......... .......... .......... .......... 67% 46.0M 8s
180200K .......... .......... .......... .......... .......... 67% 16.8M 8s
180250K .......... .......... .......... .......... .......... 67% 35.5M 8s
180300K .......... .......... .......... .......... .......... 67% 46.7M 8s
180350K .......... .......... .......... .......... .......... 67% 42.4M 8s
180400K .......... .......... .......... .......... .......... 67% 43.4M 8s
180450K .......... .......... .......... .......... .......... 67% 42.2M 8s
180500K .......... .......... .......... .......... .......... 67% 45.7M 8s
180550K .......... .......... .......... .......... .......... 67% 52.4M 8s
180600K .......... .......... .......... .......... .......... 67% 42.1M 8s
180650K .......... .......... .......... .......... .......... 67% 47.1M 8s
180700K .......... .......... .......... .......... .......... 68% 56.7M 8s
180750K .......... .......... .......... .......... .......... 68% 80.0M 8s
180800K .......... .......... .......... .......... .......... 68% 48.3M 8s
180850K .......... .......... .......... .......... .......... 68% 90.6M 8s
180900K .......... .......... .......... .......... .......... 68%  105M 8s
180950K .......... .......... .......... .......... .......... 68% 14.6M 8s
181000K .......... .......... .......... .......... .......... 68%  110M 8s
181050K .......... .......... .......... .......... .......... 68% 24.4M 8s
181100K .......... .......... .......... .......... .......... 68% 75.7M 8s
181150K .......... .......... .......... .......... .......... 68%  130M 8s
181200K .......... .......... .......... .......... .......... 68%  125M 8s
181250K .......... .......... .......... .......... .......... 68%  115M 8s
181300K .......... .......... .......... .......... .......... 68%  153M 8s
181350K .......... .......... .......... .......... .......... 68%  103M 8s
181400K .......... .......... .......... .......... .......... 68%  126M 8s
181450K .......... .......... .......... .......... .......... 68%  140M 8s
181500K .......... .......... .......... .......... .......... 68%  123M 8s
181550K .......... .......... .......... .......... .......... 68% 67.6M 8s
181600K .......... .......... .......... .......... .......... 68% 45.7M 8s
181650K .......... .......... .......... .......... .......... 68% 86.1M 8s
181700K .......... .......... .......... .......... .......... 68% 53.8M 8s
181750K .......... .......... .......... .......... .......... 68% 60.5M 8s
181800K .......... .......... .......... .......... .......... 68% 96.9M 8s
181850K .......... .......... .......... .......... .......... 68% 54.9M 8s
181900K .......... .......... .......... .......... .......... 68%  103M 8s
181950K .......... .......... .......... .......... .......... 68% 55.2M 8s
182000K .......... .......... .......... .......... .......... 68% 59.9M 8s
182050K .......... .......... .......... .......... .......... 68% 63.2M 8s
182100K .......... .......... .......... .......... .......... 68% 56.6M 8s
182150K .......... .......... .......... .......... .......... 68% 69.9M 8s
182200K .......... .......... .......... .......... .......... 68% 73.6M 8s
182250K .......... .......... .......... .......... .......... 68% 59.3M 8s
182300K .......... .......... .......... .......... .......... 68% 43.4M 8s
182350K .......... .......... .......... .......... .......... 68% 79.0M 8s
182400K .......... .......... .......... .......... .......... 68% 65.2M 8s
182450K .......... .......... .......... .......... .......... 68% 56.4M 8s
182500K .......... .......... .......... .......... .......... 68% 56.6M 8s
182550K .......... .......... .......... .......... .......... 68% 95.2M 8s
182600K .......... .......... .......... .......... .......... 68% 48.3M 8s
182650K .......... .......... .......... .......... .......... 68% 75.9M 8s
182700K .......... .......... .......... .......... .......... 68% 60.2M 8s
182750K .......... .......... .......... .......... .......... 68% 50.0M 8s
182800K .......... .......... .......... .......... .......... 68% 57.7M 8s
182850K .......... .......... .......... .......... .......... 68% 72.8M 8s
182900K .......... .......... .......... .......... .......... 68% 61.7M 8s
182950K .......... .......... .......... .......... .......... 68% 55.0M 8s
183000K .......... .......... .......... .......... .......... 68% 91.8M 8s
183050K .......... .......... .......... .......... .......... 68% 64.6M 8s
183100K .......... .......... .......... .......... .......... 68% 54.0M 8s
183150K .......... .......... .......... .......... .......... 68% 88.6M 8s
183200K .......... .......... .......... .......... .......... 68% 59.4M 8s
183250K .......... .......... .......... .......... .......... 68% 58.2M 8s
183300K .......... .......... .......... .......... .......... 68% 55.8M 8s
183350K .......... .......... .......... .......... .......... 68% 55.0M 8s
183400K .......... .......... .......... .......... .......... 69% 72.6M 8s
183450K .......... .......... .......... .......... .......... 69% 55.8M 8s
183500K .......... .......... .......... .......... .......... 69%  102M 8s
183550K .......... .......... .......... .......... .......... 69% 55.4M 8s
183600K .......... .......... .......... .......... .......... 69% 97.7M 8s
183650K .......... .......... .......... .......... .......... 69% 63.2M 8s
183700K .......... .......... .......... .......... .......... 69% 90.4M 8s
183750K .......... .......... .......... .......... .......... 69% 20.3M 8s
183800K .......... .......... .......... .......... .......... 69%  119M 8s
183850K .......... .......... .......... .......... .......... 69% 58.8M 8s
183900K .......... .......... .......... .......... .......... 69%  158M 8s
183950K .......... .......... .......... .......... .......... 69% 66.6M 8s
184000K .......... .......... .......... .......... .......... 69% 84.0M 8s
184050K .......... .......... .......... .......... .......... 69%  128M 8s
184100K .......... .......... .......... .......... .......... 69%  141M 8s
184150K .......... .......... .......... .......... .......... 69%  154M 8s
184200K .......... .......... .......... .......... .......... 69%  103M 8s
184250K .......... .......... .......... .......... .......... 69% 49.6M 8s
184300K .......... .......... .......... .......... .......... 69% 14.3M 8s
184350K .......... .......... .......... .......... .......... 69% 36.9M 8s
184400K .......... .......... .......... .......... .......... 69% 55.7M 8s
184450K .......... .......... .......... .......... .......... 69% 44.6M 8s
184500K .......... .......... .......... .......... .......... 69% 41.2M 8s
184550K .......... .......... .......... .......... .......... 69% 53.7M 8s
184600K .......... .......... .......... .......... .......... 69% 42.3M 8s
184650K .......... .......... .......... .......... .......... 69% 47.8M 8s
184700K .......... .......... .......... .......... .......... 69% 47.2M 8s
184750K .......... .......... .......... .......... .......... 69% 58.8M 8s
184800K .......... .......... .......... .......... .......... 69% 46.5M 8s
184850K .......... .......... .......... .......... .......... 69% 38.4M 8s
184900K .......... .......... .......... .......... .......... 69% 45.8M 8s
184950K .......... .......... .......... .......... .......... 69% 48.4M 8s
185000K .......... .......... .......... .......... .......... 69% 36.1M 8s
185050K .......... .......... .......... .......... .......... 69% 53.7M 8s
185100K .......... .......... .......... .......... .......... 69% 48.9M 8s
185150K .......... .......... .......... .......... .......... 69% 53.5M 8s
185200K .......... .......... .......... .......... .......... 69% 44.0M 8s
185250K .......... .......... .......... .......... .......... 69% 47.1M 8s
185300K .......... .......... .......... .......... .......... 69% 41.1M 8s
185350K .......... .......... .......... .......... .......... 69% 42.1M 8s
185400K .......... .......... .......... .......... .......... 69% 52.1M 8s
185450K .......... .......... .......... .......... .......... 69% 40.2M 8s
185500K .......... .......... .......... .......... .......... 69% 46.8M 8s
185550K .......... .......... .......... .......... .......... 69% 50.0M 8s
185600K .......... .......... .......... .......... .......... 69% 49.8M 8s
185650K .......... .......... .......... .......... .......... 69% 51.7M 8s
185700K .......... .......... .......... .......... .......... 69% 46.4M 8s
185750K .......... .......... .......... .......... .......... 69%  115M 8s
185800K .......... .......... .......... .......... .......... 69% 49.7M 8s
185850K .......... .......... .......... .......... .......... 69%  114M 8s
185900K .......... .......... .......... .......... .......... 69% 51.5M 8s
185950K .......... .......... .......... .......... .......... 69% 15.2M 8s
186000K .......... .......... .......... .......... .......... 69%  141M 8s
186050K .......... .......... .......... .......... .......... 70%  132M 8s
186100K .......... .......... .......... .......... .......... 70% 38.5M 8s
186150K .......... .......... .......... .......... .......... 70%  121M 8s
186200K .......... .......... .......... .......... .......... 70% 83.3M 8s
186250K .......... .......... .......... .......... .......... 70% 99.0M 8s
186300K .......... .......... .......... .......... .......... 70%  100M 7s
186350K .......... .......... .......... .......... .......... 70% 65.8M 7s
186400K .......... .......... .......... .......... .......... 70% 35.6M 7s
186450K .......... .......... .......... .......... .......... 70%  128M 7s
186500K .......... .......... .......... .......... .......... 70%  141M 7s
186550K .......... .......... .......... .......... .......... 70%  126M 7s
186600K .......... .......... .......... .......... .......... 70%  116M 7s
186650K .......... .......... .......... .......... .......... 70% 54.2M 7s
186700K .......... .......... .......... .......... .......... 70% 46.6M 7s
186750K .......... .......... .......... .......... .......... 70% 48.7M 7s
186800K .......... .......... .......... .......... .......... 70% 45.8M 7s
186850K .......... .......... .......... .......... .......... 70% 52.4M 7s
186900K .......... .......... .......... .......... .......... 70% 75.0M 7s
186950K .......... .......... .......... .......... .......... 70% 47.2M 7s
187000K .......... .......... .......... .......... .......... 70% 66.2M 7s
187050K .......... .......... .......... .......... .......... 70% 45.2M 7s
187100K .......... .......... .......... .......... .......... 70% 42.3M 7s
187150K .......... .......... .......... .......... .......... 70% 66.0M 7s
187200K .......... .......... .......... .......... .......... 70% 24.1M 7s
187250K .......... .......... .......... .......... .......... 70%  125M 7s
187300K .......... .......... .......... .......... .......... 70% 68.1M 7s
187350K .......... .......... .......... .......... .......... 70% 42.5M 7s
187400K .......... .......... .......... .......... .......... 70% 43.1M 7s
187450K .......... .......... .......... .......... .......... 70% 43.7M 7s
187500K .......... .......... .......... .......... .......... 70% 27.7M 7s
187550K .......... .......... .......... .......... .......... 70% 53.7M 7s
187600K .......... .......... .......... .......... .......... 70% 38.6M 7s
187650K .......... .......... .......... .......... .......... 70% 44.0M 7s
187700K .......... .......... .......... .......... .......... 70% 21.2M 7s
187750K .......... .......... .......... .......... .......... 70% 93.7M 7s
187800K .......... .......... .......... .......... .......... 70% 45.9M 7s
187850K .......... .......... .......... .......... .......... 70% 21.7M 7s
187900K .......... .......... .......... .......... .......... 70% 27.4M 7s
187950K .......... .......... .......... .......... .......... 70% 28.4M 7s
188000K .......... .......... .......... .......... .......... 70% 33.5M 7s
188050K .......... .......... .......... .......... .......... 70% 30.4M 7s
188100K .......... .......... .......... .......... .......... 70% 21.6M 7s
188150K .......... .......... .......... .......... .......... 70% 30.5M 7s
188200K .......... .......... .......... .......... .......... 70% 24.0M 7s
188250K .......... .......... .......... .......... .......... 70% 23.9M 7s
188300K .......... .......... .......... .......... .......... 70% 32.1M 7s
188350K .......... .......... .......... .......... .......... 70% 18.3M 7s
188400K .......... .......... .......... .......... .......... 70% 19.7M 7s
188450K .......... .......... .......... .......... .......... 70% 35.6M 7s
188500K .......... .......... .......... .......... .......... 70% 14.4M 7s
188550K .......... .......... .......... .......... .......... 70% 37.0M 7s
188600K .......... .......... .......... .......... .......... 70% 17.6M 7s
188650K .......... .......... .......... .......... .......... 70% 21.4M 7s
188700K .......... .......... .......... .......... .......... 71% 18.6M 7s
188750K .......... .......... .......... .......... .......... 71% 21.6M 7s
188800K .......... .......... .......... .......... .......... 71% 19.9M 7s
188850K .......... .......... .......... .......... .......... 71% 15.1M 7s
188900K .......... .......... .......... .......... .......... 71% 24.9M 7s
188950K .......... .......... .......... .......... .......... 71% 20.4M 7s
189000K .......... .......... .......... .......... .......... 71% 20.3M 7s
189050K .......... .......... .......... .......... .......... 71% 19.4M 7s
189100K .......... .......... .......... .......... .......... 71% 16.2M 7s
189150K .......... .......... .......... .......... .......... 71% 26.1M 7s
189200K .......... .......... .......... .......... .......... 71% 16.7M 7s
189250K .......... .......... .......... .......... .......... 71% 21.3M 7s
189300K .......... .......... .......... .......... .......... 71% 26.3M 7s
189350K .......... .......... .......... .......... .......... 71% 16.2M 7s
189400K .......... .......... .......... .......... .......... 71% 21.3M 7s
189450K .......... .......... .......... .......... .......... 71% 21.1M 7s
189500K .......... .......... .......... .......... .......... 71% 32.0M 7s
189550K .......... .......... .......... .......... .......... 71% 19.9M 7s
189600K .......... .......... .......... .......... .......... 71% 42.5M 7s
189650K .......... .......... .......... .......... .......... 71% 28.5M 7s
189700K .......... .......... .......... .......... .......... 71% 49.2M 7s
189750K .......... .......... .......... .......... .......... 71% 26.4M 7s
189800K .......... .......... .......... .......... .......... 71% 53.4M 7s
189850K .......... .......... .......... .......... .......... 71% 29.1M 7s
189900K .......... .......... .......... .......... .......... 71% 34.5M 7s
189950K .......... .......... .......... .......... .......... 71% 25.2M 7s
190000K .......... .......... .......... .......... .......... 71% 26.8M 7s
190050K .......... .......... .......... .......... .......... 71% 37.8M 7s
190100K .......... .......... .......... .......... .......... 71% 22.1M 7s
190150K .......... .......... .......... .......... .......... 71% 33.4M 7s
190200K .......... .......... .......... .......... .......... 71% 25.8M 7s
190250K .......... .......... .......... .......... .......... 71% 33.2M 7s
190300K .......... .......... .......... .......... .......... 71% 28.9M 7s
190350K .......... .......... .......... .......... .......... 71% 25.0M 7s
190400K .......... .......... .......... .......... .......... 71% 27.0M 7s
190450K .......... .......... .......... .......... .......... 71% 18.8M 7s
190500K .......... .......... .......... .......... .......... 71% 38.6M 7s
190550K .......... .......... .......... .......... .......... 71% 25.8M 7s
190600K .......... .......... .......... .......... .......... 71% 21.0M 7s
190650K .......... .......... .......... .......... .......... 71% 36.3M 7s
190700K .......... .......... .......... .......... .......... 71% 26.1M 7s
190750K .......... .......... .......... .......... .......... 71% 24.4M 7s
190800K .......... .......... .......... .......... .......... 71% 41.2M 7s
190850K .......... .......... .......... .......... .......... 71% 27.3M 7s
190900K .......... .......... .......... .......... .......... 71%  119M 7s
190950K .......... .......... .......... .......... .......... 71% 10.5M 7s
191000K .......... .......... .......... .......... .......... 71% 12.4M 7s
191050K .......... .......... .......... .......... .......... 71%  149M 7s
191100K .......... .......... .......... .......... .......... 71% 95.7M 7s
191150K .......... .......... .......... .......... .......... 71%  151M 7s
191200K .......... .......... .......... .......... .......... 71%  163M 7s
191250K .......... .......... .......... .......... .......... 71%  167M 7s
191300K .......... .......... .......... .......... .......... 71%  143M 7s
191350K .......... .......... .......... .......... .......... 72%  109M 7s
191400K .......... .......... .......... .......... .......... 72% 46.6M 7s
191450K .......... .......... .......... .......... .......... 72%  103M 7s
191500K .......... .......... .......... .......... .......... 72% 44.1M 7s
191550K .......... .......... .......... .......... .......... 72% 55.2M 7s
191600K .......... .......... .......... .......... .......... 72% 53.7M 7s
191650K .......... .......... .......... .......... .......... 72%  106M 7s
191700K .......... .......... .......... .......... .......... 72% 22.4M 7s
191750K .......... .......... .......... .......... .......... 72%  139M 7s
191800K .......... .......... .......... .......... .......... 72%  133M 7s
191850K .......... .......... .......... .......... .......... 72% 53.5M 7s
191900K .......... .......... .......... .......... .......... 72% 50.4M 7s
191950K .......... .......... .......... .......... .......... 72% 42.4M 7s
192000K .......... .......... .......... .......... .......... 72% 57.9M 7s
192050K .......... .......... .......... .......... .......... 72% 53.1M 7s
192100K .......... .......... .......... .......... .......... 72% 43.2M 7s
192150K .......... .......... .......... .......... .......... 72% 47.8M 7s
192200K .......... .......... .......... .......... .......... 72% 42.7M 7s
192250K .......... .......... .......... .......... .......... 72% 49.4M 7s
192300K .......... .......... .......... .......... .......... 72% 51.1M 7s
192350K .......... .......... .......... .......... .......... 72% 32.5M 7s
192400K .......... .......... .......... .......... .......... 72% 33.8M 7s
192450K .......... .......... .......... .......... .......... 72% 36.5M 7s
192500K .......... .......... .......... .......... .......... 72% 17.8M 7s
192550K .......... .......... .......... .......... .......... 72% 37.3M 7s
192600K .......... .......... .......... .......... .......... 72% 27.4M 7s
192650K .......... .......... .......... .......... .......... 72% 47.1M 7s
192700K .......... .......... .......... .......... .......... 72% 32.3M 7s
192750K .......... .......... .......... .......... .......... 72%  122M 7s
192800K .......... .......... .......... .......... .......... 72% 37.5M 7s
192850K .......... .......... .......... .......... .......... 72% 28.1M 7s
192900K .......... .......... .......... .......... .......... 72%  108M 7s
192950K .......... .......... .......... .......... .......... 72% 23.8M 7s
193000K .......... .......... .......... .......... .......... 72% 46.2M 7s
193050K .......... .......... .......... .......... .......... 72%  118M 7s
193100K .......... .......... .......... .......... .......... 72% 22.2M 7s
193150K .......... .......... .......... .......... .......... 72% 53.5M 7s
193200K .......... .......... .......... .......... .......... 72% 43.1M 7s
193250K .......... .......... .......... .......... .......... 72% 46.9M 7s
193300K .......... .......... .......... .......... .......... 72% 91.1M 7s
193350K .......... .......... .......... .......... .......... 72% 43.8M 7s
193400K .......... .......... .......... .......... .......... 72%  151M 7s
193450K .......... .......... .......... .......... .......... 72% 12.6M 7s
193500K .......... .......... .......... .......... .......... 72% 61.0M 7s
193550K .......... .......... .......... .......... .......... 72% 61.8M 7s
193600K .......... .......... .......... .......... .......... 72%  113M 7s
193650K .......... .......... .......... .......... .......... 72% 54.3M 7s
193700K .......... .......... .......... .......... .......... 72% 82.6M 7s
193750K .......... .......... .......... .......... .......... 72% 62.5M 7s
193800K .......... .......... .......... .......... .......... 72%  130M 7s
193850K .......... .......... .......... .......... .......... 72% 22.6M 7s
193900K .......... .......... .......... .......... .......... 72%  135M 7s
193950K .......... .......... .......... .......... .......... 72%  118M 7s
194000K .......... .......... .......... .......... .......... 73%  197M 7s
194050K .......... .......... .......... .......... .......... 73%  159M 7s
194100K .......... .......... .......... .......... .......... 73% 42.3M 7s
194150K .......... .......... .......... .......... .......... 73% 44.8M 7s
194200K .......... .......... .......... .......... .......... 73% 37.3M 7s
194250K .......... .......... .......... .......... .......... 73% 47.7M 7s
194300K .......... .......... .......... .......... .......... 73% 47.7M 7s
194350K .......... .......... .......... .......... .......... 73% 35.9M 7s
194400K .......... .......... .......... .......... .......... 73% 39.7M 7s
194450K .......... .......... .......... .......... .......... 73% 40.2M 7s
194500K .......... .......... .......... .......... .......... 73% 34.5M 7s
194550K .......... .......... .......... .......... .......... 73% 40.8M 7s
194600K .......... .......... .......... .......... .......... 73% 32.6M 7s
194650K .......... .......... .......... .......... .......... 73% 37.2M 7s
194700K .......... .......... .......... .......... .......... 73% 35.1M 7s
194750K .......... .......... .......... .......... .......... 73% 39.5M 6s
194800K .......... .......... .......... .......... .......... 73% 40.9M 6s
194850K .......... .......... .......... .......... .......... 73% 47.7M 6s
194900K .......... .......... .......... .......... .......... 73% 35.1M 6s
194950K .......... .......... .......... .......... .......... 73% 38.8M 6s
195000K .......... .......... .......... .......... .......... 73% 50.9M 6s
195050K .......... .......... .......... .......... .......... 73% 44.6M 6s
195100K .......... .......... .......... .......... .......... 73% 35.9M 6s
195150K .......... .......... .......... .......... .......... 73% 47.1M 6s
195200K .......... .......... .......... .......... .......... 73% 21.2M 6s
195250K .......... .......... .......... .......... .......... 73% 45.6M 6s
195300K .......... .......... .......... .......... .......... 73% 45.3M 6s
195350K .......... .......... .......... .......... .......... 73% 46.0M 6s
195400K .......... .......... .......... .......... .......... 73% 37.4M 6s
195450K .......... .......... .......... .......... .......... 73% 52.8M 6s
195500K .......... .......... .......... .......... .......... 73% 54.1M 6s
195550K .......... .......... .......... .......... .......... 73% 96.1M 6s
195600K .......... .......... .......... .......... .......... 73% 13.9M 6s
195650K .......... .......... .......... .......... .......... 73% 40.6M 6s
195700K .......... .......... .......... .......... .......... 73% 23.7M 6s
195750K .......... .......... .......... .......... .......... 73%  130M 6s
195800K .......... .......... .......... .......... .......... 73%  168M 6s
195850K .......... .......... .......... .......... .......... 73%  116M 6s
195900K .......... .......... .......... .......... .......... 73%  144M 6s
195950K .......... .......... .......... .......... .......... 73%  158M 6s
196000K .......... .......... .......... .......... .......... 73%  160M 6s
196050K .......... .......... .......... .......... .......... 73%  117M 6s
196100K .......... .......... .......... .......... .......... 73% 22.6M 6s
196150K .......... .......... .......... .......... .......... 73%  139M 6s
196200K .......... .......... .......... .......... .......... 73% 89.1M 6s
196250K .......... .......... .......... .......... .......... 73% 88.9M 6s
196300K .......... .......... .......... .......... .......... 73% 43.6M 6s
196350K .......... .......... .......... .......... .......... 73% 48.7M 6s
196400K .......... .......... .......... .......... .......... 73% 43.0M 6s
196450K .......... .......... .......... .......... .......... 73% 38.0M 6s
196500K .......... .......... .......... .......... .......... 73% 48.0M 6s
196550K .......... .......... .......... .......... .......... 73% 42.3M 6s
196600K .......... .......... .......... .......... .......... 73% 22.7M 6s
196650K .......... .......... .......... .......... .......... 74% 82.8M 6s
196700K .......... .......... .......... .......... .......... 74% 42.9M 6s
196750K .......... .......... .......... .......... .......... 74% 52.7M 6s
196800K .......... .......... .......... .......... .......... 74% 43.5M 6s
196850K .......... .......... .......... .......... .......... 74% 49.4M 6s
196900K .......... .......... .......... .......... .......... 74% 49.6M 6s
196950K .......... .......... .......... .......... .......... 74% 35.2M 6s
197000K .......... .......... .......... .......... .......... 74% 45.0M 6s
197050K .......... .......... .......... .......... .......... 74% 92.1M 6s
197100K .......... .......... .......... .......... .......... 74% 50.9M 6s
197150K .......... .......... .......... .......... .......... 74% 41.3M 6s
197200K .......... .......... .......... .......... .......... 74% 38.2M 6s
197250K .......... .......... .......... .......... .......... 74% 46.5M 6s
197300K .......... .......... .......... .......... .......... 74% 37.7M 6s
197350K .......... .......... .......... .......... .......... 74% 43.9M 6s
197400K .......... .......... .......... .......... .......... 74% 51.9M 6s
197450K .......... .......... .......... .......... .......... 74% 46.2M 6s
197500K .......... .......... .......... .......... .......... 74% 63.7M 6s
197550K .......... .......... .......... .......... .......... 74% 49.2M 6s
197600K .......... .......... .......... .......... .......... 74% 43.2M 6s
197650K .......... .......... .......... .......... .......... 74% 42.3M 6s
197700K .......... .......... .......... .......... .......... 74% 45.8M 6s
197750K .......... .......... .......... .......... .......... 74% 30.1M 6s
197800K .......... .......... .......... .......... .......... 74% 12.3M 6s
197850K .......... .......... .......... .......... .......... 74% 41.7M 6s
197900K .......... .......... .......... .......... .......... 74%  117M 6s
197950K .......... .......... .......... .......... .......... 74% 39.1M 6s
198000K .......... .......... .......... .......... .......... 74% 45.2M 6s
198050K .......... .......... .......... .......... .......... 74% 29.4M 6s
198100K .......... .......... .......... .......... .......... 74% 23.6M 6s
198150K .......... .......... .......... .......... .......... 74% 24.4M 6s
198200K .......... .......... .......... .......... .......... 74% 25.9M 6s
198250K .......... .......... .......... .......... .......... 74% 26.9M 6s
198300K .......... .......... .......... .......... .......... 74% 24.6M 6s
198350K .......... .......... .......... .......... .......... 74% 22.7M 6s
198400K .......... .......... .......... .......... .......... 74% 23.8M 6s
198450K .......... .......... .......... .......... .......... 74% 23.7M 6s
198500K .......... .......... .......... .......... .......... 74% 23.4M 6s
198550K .......... .......... .......... .......... .......... 74% 37.1M 6s
198600K .......... .......... .......... .......... .......... 74% 20.8M 6s
198650K .......... .......... .......... .......... .......... 74% 25.5M 6s
198700K .......... .......... .......... .......... .......... 74% 20.0M 6s
198750K .......... .......... .......... .......... .......... 74% 33.0M 6s
198800K .......... .......... .......... .......... .......... 74% 22.9M 6s
198850K .......... .......... .......... .......... .......... 74% 26.7M 6s
198900K .......... .......... .......... .......... .......... 74% 45.2M 6s
198950K .......... .......... .......... .......... .......... 74% 55.7M 6s
199000K .......... .......... .......... .......... .......... 74% 92.3M 6s
199050K .......... .......... .......... .......... .......... 74% 97.1M 6s
199100K .......... .......... .......... .......... .......... 74% 45.3M 6s
199150K .......... .......... .......... .......... .......... 74%  122M 6s
199200K .......... .......... .......... .......... .......... 74% 45.0M 6s
199250K .......... .......... .......... .......... .......... 74% 15.2M 6s
199300K .......... .......... .......... .......... .......... 74% 90.1M 6s
199350K .......... .......... .......... .......... .......... 75% 88.1M 6s
199400K .......... .......... .......... .......... .......... 75%  130M 6s
199450K .......... .......... .......... .......... .......... 75% 40.9M 6s
199500K .......... .......... .......... .......... .......... 75% 68.1M 6s
199550K .......... .......... .......... .......... .......... 75% 56.0M 6s
199600K .......... .......... .......... .......... .......... 75% 77.5M 6s
199650K .......... .......... .......... .......... .......... 75% 31.2M 6s
199700K .......... .......... .......... .......... .......... 75% 37.9M 6s
199750K .......... .......... .......... .......... .......... 75% 31.7M 6s
199800K .......... .......... .......... .......... .......... 75% 23.0M 6s
199850K .......... .......... .......... .......... .......... 75% 32.1M 6s
199900K .......... .......... .......... .......... .......... 75% 31.6M 6s
199950K .......... .......... .......... .......... .......... 75% 25.6M 6s
200000K .......... .......... .......... .......... .......... 75% 38.7M 6s
200050K .......... .......... .......... .......... .......... 75% 34.9M 6s
200100K .......... .......... .......... .......... .......... 75% 43.1M 6s
200150K .......... .......... .......... .......... .......... 75% 35.4M 6s
200200K .......... .......... .......... .......... .......... 75% 23.0M 6s
200250K .......... .......... .......... .......... .......... 75% 39.9M 6s
200300K .......... .......... .......... .......... .......... 75% 44.5M 6s
200350K .......... .......... .......... .......... .......... 75% 30.7M 6s
200400K .......... .......... .......... .......... .......... 75% 38.4M 6s
200450K .......... .......... .......... .......... .......... 75% 35.2M 6s
200500K .......... .......... .......... .......... .......... 75% 43.2M 6s
200550K .......... .......... .......... .......... .......... 75% 33.4M 6s
200600K .......... .......... .......... .......... .......... 75% 38.0M 6s
200650K .......... .......... .......... .......... .......... 75% 35.1M 6s
200700K .......... .......... .......... .......... .......... 75% 32.4M 6s
200750K .......... .......... .......... .......... .......... 75% 48.0M 6s
200800K .......... .......... .......... .......... .......... 75% 40.4M 6s
200850K .......... .......... .......... .......... .......... 75% 47.5M 6s
200900K .......... .......... .......... .......... .......... 75% 14.1M 6s
200950K .......... .......... .......... .......... .......... 75% 79.5M 6s
201000K .......... .......... .......... .......... .......... 75%  127M 6s
201050K .......... .......... .......... .......... .......... 75% 56.4M 6s
201100K .......... .......... .......... .......... .......... 75% 49.0M 6s
201150K .......... .......... .......... .......... .......... 75% 65.2M 6s
201200K .......... .......... .......... .......... .......... 75% 58.4M 6s
201250K .......... .......... .......... .......... .......... 75% 51.6M 6s
201300K .......... .......... .......... .......... .......... 75% 79.8M 6s
201350K .......... .......... .......... .......... .......... 75% 99.6M 6s
201400K .......... .......... .......... .......... .......... 75%  123M 6s
201450K .......... .......... .......... .......... .......... 75% 31.0M 6s
201500K .......... .......... .......... .......... .......... 75% 46.2M 6s
201550K .......... .......... .......... .......... .......... 75% 48.1M 6s
201600K .......... .......... .......... .......... .......... 75% 40.8M 6s
201650K .......... .......... .......... .......... .......... 75% 47.1M 6s
201700K .......... .......... .......... .......... .......... 75% 46.4M 6s
201750K .......... .......... .......... .......... .......... 75% 43.4M 6s
201800K .......... .......... .......... .......... .......... 75% 43.2M 6s
201850K .......... .......... .......... .......... .......... 75% 36.4M 6s
201900K .......... .......... .......... .......... .......... 75% 42.0M 6s
201950K .......... .......... .......... .......... .......... 75% 42.5M 6s
202000K .......... .......... .......... .......... .......... 76% 64.1M 6s
202050K .......... .......... .......... .......... .......... 76% 93.9M 6s
202100K .......... .......... .......... .......... .......... 76% 27.5M 6s
202150K .......... .......... .......... .......... .......... 76% 98.0M 6s
202200K .......... .......... .......... .......... .......... 76% 44.5M 6s
202250K .......... .......... .......... .......... .......... 76% 47.1M 6s
202300K .......... .......... .......... .......... .......... 76% 44.8M 6s
202350K .......... .......... .......... .......... .......... 76% 33.0M 6s
202400K .......... .......... .......... .......... .......... 76% 45.9M 6s
202450K .......... .......... .......... .......... .......... 76% 46.9M 6s
202500K .......... .......... .......... .......... .......... 76% 46.2M 6s
202550K .......... .......... .......... .......... .......... 76% 48.4M 6s
202600K .......... .......... .......... .......... .......... 76% 47.4M 6s
202650K .......... .......... .......... .......... .......... 76% 50.0M 6s
202700K .......... .......... .......... .......... .......... 76% 45.8M 6s
202750K .......... .......... .......... .......... .......... 76% 28.2M 6s
202800K .......... .......... .......... .......... .......... 76% 89.3M 6s
202850K .......... .......... .......... .......... .......... 76% 32.0M 6s
202900K .......... .......... .......... .......... .......... 76% 50.4M 6s
202950K .......... .......... .......... .......... .......... 76% 32.0M 6s
203000K .......... .......... .......... .......... .......... 76% 47.3M 6s
203050K .......... .......... .......... .......... .......... 76% 81.7M 6s
203100K .......... .......... .......... .......... .......... 76% 39.0M 6s
203150K .......... .......... .......... .......... .......... 76%  126M 6s
203200K .......... .......... .......... .......... .......... 76% 13.1M 6s
203250K .......... .......... .......... .......... .......... 76%  115M 6s
203300K .......... .......... .......... .......... .......... 76%  132M 6s
203350K .......... .......... .......... .......... .......... 76% 64.2M 6s
203400K .......... .......... .......... .......... .......... 76% 22.8M 6s
203450K .......... .......... .......... .......... .......... 76%  107M 6s
203500K .......... .......... .......... .......... .......... 76%  143M 6s
203550K .......... .......... .......... .......... .......... 76% 47.3M 6s
203600K .......... .......... .......... .......... .......... 76%  109M 6s
203650K .......... .......... .......... .......... .......... 76%  125M 5s
203700K .......... .......... .......... .......... .......... 76%  144M 5s
203750K .......... .......... .......... .......... .......... 76% 55.2M 5s
203800K .......... .......... .......... .......... .......... 76% 25.1M 5s
203850K .......... .......... .......... .......... .......... 76% 43.9M 5s
203900K .......... .......... .......... .......... .......... 76% 43.7M 5s
203950K .......... .......... .......... .......... .......... 76% 29.2M 5s
204000K .......... .......... .......... .......... .......... 76% 43.9M 5s
204050K .......... .......... .......... .......... .......... 76% 28.5M 5s
204100K .......... .......... .......... .......... .......... 76% 43.1M 5s
204150K .......... .......... .......... .......... .......... 76% 44.0M 5s
204200K .......... .......... .......... .......... .......... 76% 25.7M 5s
204250K .......... .......... .......... .......... .......... 76% 41.1M 5s
204300K .......... .......... .......... .......... .......... 76% 38.3M 5s
204350K .......... .......... .......... .......... .......... 76% 31.4M 5s
204400K .......... .......... .......... .......... .......... 76% 37.9M 5s
204450K .......... .......... .......... .......... .......... 76% 30.0M 5s
204500K .......... .......... .......... .......... .......... 76% 44.7M 5s
204550K .......... .......... .......... .......... .......... 76% 39.9M 5s
204600K .......... .......... .......... .......... .......... 76% 28.0M 5s
204650K .......... .......... .......... .......... .......... 77% 47.6M 5s
204700K .......... .......... .......... .......... .......... 77% 38.8M 5s
204750K .......... .......... .......... .......... .......... 77% 29.9M 5s
204800K .......... .......... .......... .......... .......... 77% 14.1M 5s
204850K .......... .......... .......... .......... .......... 77% 38.4M 5s
204900K .......... .......... .......... .......... .......... 77% 48.1M 5s
204950K .......... .......... .......... .......... .......... 77% 26.1M 5s
205000K .......... .......... .......... .......... .......... 77% 63.6M 5s
205050K .......... .......... .......... .......... .......... 77% 46.3M 5s
205100K .......... .......... .......... .......... .......... 77% 87.7M 5s
205150K .......... .......... .......... .......... .......... 77% 13.6M 5s
205200K .......... .......... .......... .......... .......... 77%  114M 5s
205250K .......... .......... .......... .......... .......... 77% 75.4M 5s
205300K .......... .......... .......... .......... .......... 77%  136M 5s
205350K .......... .......... .......... .......... .......... 77% 90.8M 5s
205400K .......... .......... .......... .......... .......... 77% 66.4M 5s
205450K .......... .......... .......... .......... .......... 77% 82.2M 5s
205500K .......... .......... .......... .......... .......... 77% 56.7M 5s
205550K .......... .......... .......... .......... .......... 77%  154M 5s
205600K .......... .......... .......... .......... .......... 77% 66.2M 5s
205650K .......... .......... .......... .......... .......... 77% 42.8M 5s
205700K .......... .......... .......... .......... .......... 77% 30.7M 5s
205750K .......... .......... .......... .......... .......... 77% 31.5M 5s
205800K .......... .......... .......... .......... .......... 77% 43.2M 5s
205850K .......... .......... .......... .......... .......... 77% 43.4M 5s
205900K .......... .......... .......... .......... .......... 77% 42.1M 5s
205950K .......... .......... .......... .......... .......... 77% 26.6M 5s
206000K .......... .......... .......... .......... .......... 77% 50.0M 5s
206050K .......... .......... .......... .......... .......... 77% 45.3M 5s
206100K .......... .......... .......... .......... .......... 77% 44.3M 5s
206150K .......... .......... .......... .......... .......... 77% 41.0M 5s
206200K .......... .......... .......... .......... .......... 77% 41.5M 5s
206250K .......... .......... .......... .......... .......... 77% 28.7M 5s
206300K .......... .......... .......... .......... .......... 77% 55.2M 5s
206350K .......... .......... .......... .......... .......... 77% 38.5M 5s
206400K .......... .......... .......... .......... .......... 77% 44.7M 5s
206450K .......... .......... .......... .......... .......... 77% 37.7M 5s
206500K .......... .......... .......... .......... .......... 77% 38.4M 5s
206550K .......... .......... .......... .......... .......... 77% 30.8M 5s
206600K .......... .......... .......... .......... .......... 77% 37.5M 5s
206650K .......... .......... .......... .......... .......... 77% 36.9M 5s
206700K .......... .......... .......... .......... .......... 77% 37.2M 5s
206750K .......... .......... .......... .......... .......... 77% 40.0M 5s
206800K .......... .......... .......... .......... .......... 77% 40.6M 5s
206850K .......... .......... .......... .......... .......... 77% 27.8M 5s
206900K .......... .......... .......... .......... .......... 77%  112M 5s
206950K .......... .......... .......... .......... .......... 77% 34.1M 5s
207000K .......... .......... .......... .......... .......... 77% 31.6M 5s
207050K .......... .......... .......... .......... .......... 77% 14.5M 5s
207100K .......... .......... .......... .......... .......... 77% 57.2M 5s
207150K .......... .......... .......... .......... .......... 77% 34.0M 5s
207200K .......... .......... .......... .......... .......... 77% 21.5M 5s
207250K .......... .......... .......... .......... .......... 77% 49.5M 5s
207300K .......... .......... .......... .......... .......... 78% 75.7M 5s
207350K .......... .......... .......... .......... .......... 78% 48.8M 5s
207400K .......... .......... .......... .......... .......... 78% 90.1M 5s
207450K .......... .......... .......... .......... .......... 78% 58.0M 5s
207500K .......... .......... .......... .......... .......... 78% 68.8M 5s
207550K .......... .......... .......... .......... .......... 78% 47.6M 5s
207600K .......... .......... .......... .......... .......... 78% 53.6M 5s
207650K .......... .......... .......... .......... .......... 78% 44.0M 5s
207700K .......... .......... .......... .......... .......... 78% 86.0M 5s
207750K .......... .......... .......... .......... .......... 78%  145M 5s
207800K .......... .......... .......... .......... .......... 78%  116M 5s
207850K .......... .......... .......... .......... .......... 78% 95.0M 5s
207900K .......... .......... .......... .......... .......... 78% 41.2M 5s
207950K .......... .......... .......... .......... .......... 78% 35.1M 5s
208000K .......... .......... .......... .......... .......... 78% 48.5M 5s
208050K .......... .......... .......... .......... .......... 78% 40.8M 5s
208100K .......... .......... .......... .......... .......... 78% 40.0M 5s
208150K .......... .......... .......... .......... .......... 78% 46.0M 5s
208200K .......... .......... .......... .......... .......... 78% 40.7M 5s
208250K .......... .......... .......... .......... .......... 78% 38.3M 5s
208300K .......... .......... .......... .......... .......... 78% 42.6M 5s
208350K .......... .......... .......... .......... .......... 78% 34.0M 5s
208400K .......... .......... .......... .......... .......... 78% 48.1M 5s
208450K .......... .......... .......... .......... .......... 78% 39.1M 5s
208500K .......... .......... .......... .......... .......... 78% 46.2M 5s
208550K .......... .......... .......... .......... .......... 78% 42.6M 5s
208600K .......... .......... .......... .......... .......... 78% 45.5M 5s
208650K .......... .......... .......... .......... .......... 78% 36.2M 5s
208700K .......... .......... .......... .......... .......... 78% 41.4M 5s
208750K .......... .......... .......... .......... .......... 78% 47.2M 5s
208800K .......... .......... .......... .......... .......... 78% 45.7M 5s
208850K .......... .......... .......... .......... .......... 78% 26.7M 5s
208900K .......... .......... .......... .......... .......... 78% 6.31M 5s
208950K .......... .......... .......... .......... .......... 78% 73.6M 5s
209000K .......... .......... .......... .......... .......... 78% 14.7M 5s
209050K .......... .......... .......... .......... .......... 78%  127M 5s
209100K .......... .......... .......... .......... .......... 78%  113M 5s
209150K .......... .......... .......... .......... .......... 78% 28.5M 5s
209200K .......... .......... .......... .......... .......... 78% 29.8M 5s
209250K .......... .......... .......... .......... .......... 78%  139M 5s
209300K .......... .......... .......... .......... .......... 78%  117M 5s
209350K .......... .......... .......... .......... .......... 78% 37.6M 5s
209400K .......... .......... .......... .......... .......... 78% 26.7M 5s
209450K .......... .......... .......... .......... .......... 78% 35.5M 5s
209500K .......... .......... .......... .......... .......... 78% 45.4M 5s
209550K .......... .......... .......... .......... .......... 78% 28.0M 5s
209600K .......... .......... .......... .......... .......... 78% 39.5M 5s
209650K .......... .......... .......... .......... .......... 78% 42.6M 5s
209700K .......... .......... .......... .......... .......... 78% 25.1M 5s
209750K .......... .......... .......... .......... .......... 78% 37.4M 5s
209800K .......... .......... .......... .......... .......... 78% 40.9M 5s
209850K .......... .......... .......... .......... .......... 78% 26.7M 5s
209900K .......... .......... .......... .......... .......... 78% 45.9M 5s
209950K .......... .......... .......... .......... .......... 79% 23.5M 5s
210000K .......... .......... .......... .......... .......... 79% 36.1M 5s
210050K .......... .......... .......... .......... .......... 79% 43.5M 5s
210100K .......... .......... .......... .......... .......... 79% 24.5M 5s
210150K .......... .......... .......... .......... .......... 79% 50.4M 5s
210200K .......... .......... .......... .......... .......... 79% 25.7M 5s
210250K .......... .......... .......... .......... .......... 79% 41.5M 5s
210300K .......... .......... .......... .......... .......... 79% 38.4M 5s
210350K .......... .......... .......... .......... .......... 79% 27.5M 5s
210400K .......... .......... .......... .......... .......... 79% 41.4M 5s
210450K .......... .......... .......... .......... .......... 79% 45.2M 5s
210500K .......... .......... .......... .......... .......... 79% 25.5M 5s
210550K .......... .......... .......... .......... .......... 79%  119M 5s
210600K .......... .......... .......... .......... .......... 79% 33.4M 5s
210650K .......... .......... .......... .......... .......... 79% 28.4M 5s
210700K .......... .......... .......... .......... .......... 79% 90.3M 5s
210750K .......... .......... .......... .......... .......... 79% 15.4M 5s
210800K .......... .......... .......... .......... .......... 79% 84.5M 5s
210850K .......... .......... .......... .......... .......... 79% 73.4M 5s
210900K .......... .......... .......... .......... .......... 79% 30.8M 5s
210950K .......... .......... .......... .......... .......... 79% 97.5M 5s
211000K .......... .......... .......... .......... .......... 79%  127M 5s
211050K .......... .......... .......... .......... .......... 79%  151M 5s
211100K .......... .......... .......... .......... .......... 79%  110M 5s
211150K .......... .......... .......... .......... .......... 79% 45.5M 5s
211200K .......... .......... .......... .......... .......... 79% 30.3M 5s
211250K .......... .......... .......... .......... .......... 79% 44.5M 5s
211300K .......... .......... .......... .......... .......... 79% 42.7M 5s
211350K .......... .......... .......... .......... .......... 79% 41.4M 5s
211400K .......... .......... .......... .......... .......... 79% 39.6M 5s
211450K .......... .......... .......... .......... .......... 79% 29.7M 5s
211500K .......... .......... .......... .......... .......... 79% 49.2M 5s
211550K .......... .......... .......... .......... .......... 79% 45.7M 5s
211600K .......... .......... .......... .......... .......... 79% 39.4M 5s
211650K .......... .......... .......... .......... .......... 79% 46.9M 5s
211700K .......... .......... .......... .......... .......... 79% 27.4M 5s
211750K .......... .......... .......... .......... .......... 79% 38.7M 5s
211800K .......... .......... .......... .......... .......... 79% 53.0M 5s
211850K .......... .......... .......... .......... .......... 79% 44.1M 5s
211900K .......... .......... .......... .......... .......... 79% 44.0M 5s
211950K .......... .......... .......... .......... .......... 79% 38.8M 5s
212000K .......... .......... .......... .......... .......... 79% 32.2M 5s
212050K .......... .......... .......... .......... .......... 79% 47.0M 5s
212100K .......... .......... .......... .......... .......... 79% 33.7M 5s
212150K .......... .......... .......... .......... .......... 79% 48.3M 5s
212200K .......... .......... .......... .......... .......... 79% 42.6M 5s
212250K .......... .......... .......... .......... .......... 79% 46.6M 5s
212300K .......... .......... .......... .......... .......... 79% 30.4M 5s
212350K .......... .......... .......... .......... .......... 79% 39.2M 5s
212400K .......... .......... .......... .......... .......... 79% 45.4M 5s
212450K .......... .......... .......... .......... .......... 79% 31.6M 5s
212500K .......... .......... .......... .......... .......... 79% 31.0M 5s
212550K .......... .......... .......... .......... .......... 79% 43.9M 5s
212600K .......... .......... .......... .......... .......... 80% 34.4M 5s
212650K .......... .......... .......... .......... .......... 80%  143M 5s
212700K .......... .......... .......... .......... .......... 80% 11.7M 5s
212750K .......... .......... .......... .......... .......... 80% 53.2M 5s
212800K .......... .......... .......... .......... .......... 80%  116M 5s
212850K .......... .......... .......... .......... .......... 80% 96.3M 5s
212900K .......... .......... .......... .......... .......... 80% 37.4M 5s
212950K .......... .......... .......... .......... .......... 80%  110M 5s
213000K .......... .......... .......... .......... .......... 80% 81.8M 5s
213050K .......... .......... .......... .......... .......... 80% 38.8M 5s
213100K .......... .......... .......... .......... .......... 80% 72.8M 5s
213150K .......... .......... .......... .......... .......... 80%  116M 5s
213200K .......... .......... .......... .......... .......... 80%  108M 5s
213250K .......... .......... .......... .......... .......... 80% 43.4M 4s
213300K .......... .......... .......... .......... .......... 80% 46.0M 4s
213350K .......... .......... .......... .......... .......... 80% 44.1M 4s
213400K .......... .......... .......... .......... .......... 80% 41.6M 4s
213450K .......... .......... .......... .......... .......... 80% 30.1M 4s
213500K .......... .......... .......... .......... .......... 80% 73.9M 4s
213550K .......... .......... .......... .......... .......... 80% 44.3M 4s
213600K .......... .......... .......... .......... .......... 80% 44.2M 4s
213650K .......... .......... .......... .......... .......... 80% 44.3M 4s
213700K .......... .......... .......... .......... .......... 80% 50.0M 4s
213750K .......... .......... .......... .......... .......... 80% 45.0M 4s
213800K .......... .......... .......... .......... .......... 80% 49.0M 4s
213850K .......... .......... .......... .......... .......... 80% 35.5M 4s
213900K .......... .......... .......... .......... .......... 80% 40.1M 4s
213950K .......... .......... .......... .......... .......... 80% 35.9M 4s
214000K .......... .......... .......... .......... .......... 80% 20.5M 4s
214050K .......... .......... .......... .......... .......... 80% 32.9M 4s
214100K .......... .......... .......... .......... .......... 80% 28.5M 4s
214150K .......... .......... .......... .......... .......... 80% 36.0M 4s
214200K .......... .......... .......... .......... .......... 80% 43.7M 4s
214250K .......... .......... .......... .......... .......... 80% 36.8M 4s
214300K .......... .......... .......... .......... .......... 80% 40.0M 4s
214350K .......... .......... .......... .......... .......... 80% 32.0M 4s
214400K .......... .......... .......... .......... .......... 80% 41.6M 4s
214450K .......... .......... .......... .......... .......... 80% 41.3M 4s
214500K .......... .......... .......... .......... .......... 80% 45.1M 4s
214550K .......... .......... .......... .......... .......... 80% 42.9M 4s
214600K .......... .......... .......... .......... .......... 80% 49.8M 4s
214650K .......... .......... .......... .......... .......... 80% 41.7M 4s
214700K .......... .......... .......... .......... .......... 80% 86.9M 4s
214750K .......... .......... .......... .......... .......... 80% 12.9M 4s
214800K .......... .......... .......... .......... .......... 80%  149M 4s
214850K .......... .......... .......... .......... .......... 80%  136M 4s
214900K .......... .......... .......... .......... .......... 80% 42.1M 4s
214950K .......... .......... .......... .......... .......... 80% 92.1M 4s
215000K .......... .......... .......... .......... .......... 80%  117M 4s
215050K .......... .......... .......... .......... .......... 80% 78.9M 4s
215100K .......... .......... .......... .......... .......... 80% 23.2M 4s
215150K .......... .......... .......... .......... .......... 80%  141M 4s
215200K .......... .......... .......... .......... .......... 80%  111M 4s
215250K .......... .......... .......... .......... .......... 81%  113M 4s
215300K .......... .......... .......... .......... .......... 81%  118M 4s
215350K .......... .......... .......... .......... .......... 81%  111M 4s
215400K .......... .......... .......... .......... .......... 81%  155M 4s
215450K .......... .......... .......... .......... .......... 81%  122M 4s
215500K .......... .......... .......... .......... .......... 81% 87.0M 4s
215550K .......... .......... .......... .......... .......... 81% 35.2M 4s
215600K .......... .......... .......... .......... .......... 81% 78.6M 4s
215650K .......... .......... .......... .......... .......... 81% 49.0M 4s
215700K .......... .......... .......... .......... .......... 81% 38.2M 4s
215750K .......... .......... .......... .......... .......... 81% 44.3M 4s
215800K .......... .......... .......... .......... .......... 81% 97.7M 4s
215850K .......... .......... .......... .......... .......... 81% 34.2M 4s
215900K .......... .......... .......... .......... .......... 81% 45.0M 4s
215950K .......... .......... .......... .......... .......... 81% 42.1M 4s
216000K .......... .......... .......... .......... .......... 81% 43.3M 4s
216050K .......... .......... .......... .......... .......... 81%  102M 4s
216100K .......... .......... .......... .......... .......... 81% 29.2M 4s
216150K .......... .......... .......... .......... .......... 81% 54.8M 4s
216200K .......... .......... .......... .......... .......... 81% 58.2M 4s
216250K .......... .......... .......... .......... .......... 81% 41.5M 4s
216300K .......... .......... .......... .......... .......... 81%  103M 4s
216350K .......... .......... .......... .......... .......... 81% 35.7M 4s
216400K .......... .......... .......... .......... .......... 81% 36.1M 4s
216450K .......... .......... .......... .......... .......... 81% 43.2M 4s
216500K .......... .......... .......... .......... .......... 81% 48.3M 4s
216550K .......... .......... .......... .......... .......... 81% 50.1M 4s
216600K .......... .......... .......... .......... .......... 81% 69.0M 4s
216650K .......... .......... .......... .......... .......... 81% 44.5M 4s
216700K .......... .......... .......... .......... .......... 81% 46.9M 4s
216750K .......... .......... .......... .......... .......... 81% 58.9M 4s
216800K .......... .......... .......... .......... .......... 81% 42.6M 4s
216850K .......... .......... .......... .......... .......... 81% 53.2M 4s
216900K .......... .......... .......... .......... .......... 81% 81.0M 4s
216950K .......... .......... .......... .......... .......... 81% 45.1M 4s
217000K .......... .......... .......... .......... .......... 81% 50.5M 4s
217050K .......... .......... .......... .......... .......... 81% 59.8M 4s
217100K .......... .......... .......... .......... .......... 81% 44.1M 4s
217150K .......... .......... .......... .......... .......... 81% 41.8M 4s
217200K .......... .......... .......... .......... .......... 81%  115M 4s
217250K .......... .......... .......... .......... .......... 81% 49.1M 4s
217300K .......... .......... .......... .......... .......... 81%  108M 4s
217350K .......... .......... .......... .......... .......... 81% 36.1M 4s
217400K .......... .......... .......... .......... .......... 81% 13.4M 4s
217450K .......... .......... .......... .......... .......... 81%  104M 4s
217500K .......... .......... .......... .......... .......... 81%  116M 4s
217550K .......... .......... .......... .......... .......... 81% 95.9M 4s
217600K .......... .......... .......... .......... .......... 81%  133M 4s
217650K .......... .......... .......... .......... .......... 81%  145M 4s
217700K .......... .......... .......... .......... .......... 81% 43.4M 4s
217750K .......... .......... .......... .......... .......... 81% 64.8M 4s
217800K .......... .......... .......... .......... .......... 81% 96.5M 4s
217850K .......... .......... .......... .......... .......... 81% 64.2M 4s
217900K .......... .......... .......... .......... .......... 81% 97.1M 4s
217950K .......... .......... .......... .......... .......... 82% 40.8M 4s
218000K .......... .......... .......... .......... .......... 82% 36.5M 4s
218050K .......... .......... .......... .......... .......... 82% 37.5M 4s
218100K .......... .......... .......... .......... .......... 82% 24.0M 4s
218150K .......... .......... .......... .......... .......... 82% 47.9M 4s
218200K .......... .......... .......... .......... .......... 82% 41.7M 4s
218250K .......... .......... .......... .......... .......... 82% 53.5M 4s
218300K .......... .......... .......... .......... .......... 82% 94.4M 4s
218350K .......... .......... .......... .......... .......... 82% 43.8M 4s
218400K .......... .......... .......... .......... .......... 82% 43.9M 4s
218450K .......... .......... .......... .......... .......... 82% 46.2M 4s
218500K .......... .......... .......... .......... .......... 82% 47.8M 4s
218550K .......... .......... .......... .......... .......... 82% 38.6M 4s
218600K .......... .......... .......... .......... .......... 82% 35.5M 4s
218650K .......... .......... .......... .......... .......... 82% 45.8M 4s
218700K .......... .......... .......... .......... .......... 82% 43.2M 4s
218750K .......... .......... .......... .......... .......... 82% 48.3M 4s
218800K .......... .......... .......... .......... .......... 82% 41.0M 4s
218850K .......... .......... .......... .......... .......... 82% 38.1M 4s
218900K .......... .......... .......... .......... .......... 82% 48.2M 4s
218950K .......... .......... .......... .......... .......... 82% 43.1M 4s
219000K .......... .......... .......... .......... .......... 82% 48.9M 4s
219050K .......... .......... .......... .......... .......... 82% 45.3M 4s
219100K .......... .......... .......... .......... .......... 82% 38.1M 4s
219150K .......... .......... .......... .......... .......... 82% 38.8M 4s
219200K .......... .......... .......... .......... .......... 82% 48.8M 4s
219250K .......... .......... .......... .......... .......... 82% 43.0M 4s
219300K .......... .......... .......... .......... .......... 82% 38.5M 4s
219350K .......... .......... .......... .......... .......... 82% 39.3M 4s
219400K .......... .......... .......... .......... .......... 82% 35.8M 4s
219450K .......... .......... .......... .......... .......... 82%  103M 4s
219500K .......... .......... .......... .......... .......... 82% 36.2M 4s
219550K .......... .......... .......... .......... .......... 82% 75.1M 4s
219600K .......... .......... .......... .......... .......... 82% 35.5M 4s
219650K .......... .......... .......... .......... .......... 82% 74.7M 4s
219700K .......... .......... .......... .......... .......... 82% 13.4M 4s
219750K .......... .......... .......... .......... .......... 82% 78.4M 4s
219800K .......... .......... .......... .......... .......... 82% 80.3M 4s
219850K .......... .......... .......... .......... .......... 82% 55.8M 4s
219900K .......... .......... .......... .......... .......... 82% 67.3M 4s
219950K .......... .......... .......... .......... .......... 82% 63.0M 4s
220000K .......... .......... .......... .......... .......... 82% 81.1M 4s
220050K .......... .......... .......... .......... .......... 82% 54.1M 4s
220100K .......... .......... .......... .......... .......... 82% 72.4M 4s
220150K .......... .......... .......... .......... .......... 82% 77.6M 4s
220200K .......... .......... .......... .......... .......... 82% 81.2M 4s
220250K .......... .......... .......... .......... .......... 82%  109M 4s
220300K .......... .......... .......... .......... .......... 82% 56.4M 4s
220350K .......... .......... .......... .......... .......... 82% 34.5M 4s
220400K .......... .......... .......... .......... .......... 82% 54.3M 4s
220450K .......... .......... .......... .......... .......... 82% 46.6M 4s
220500K .......... .......... .......... .......... .......... 82% 48.4M 4s
220550K .......... .......... .......... .......... .......... 82% 42.0M 4s
220600K .......... .......... .......... .......... .......... 83% 43.7M 4s
220650K .......... .......... .......... .......... .......... 83% 80.7M 4s
220700K .......... .......... .......... .......... .......... 83% 47.2M 4s
220750K .......... .......... .......... .......... .......... 83% 34.9M 4s
220800K .......... .......... .......... .......... .......... 83% 54.1M 4s
220850K .......... .......... .......... .......... .......... 83% 44.0M 4s
220900K .......... .......... .......... .......... .......... 83% 42.8M 4s
220950K .......... .......... .......... .......... .......... 83% 37.6M 4s
221000K .......... .......... .......... .......... .......... 83% 62.3M 4s
221050K .......... .......... .......... .......... .......... 83% 54.1M 4s
221100K .......... .......... .......... .......... .......... 83% 47.0M 4s
221150K .......... .......... .......... .......... .......... 83% 39.8M 4s
221200K .......... .......... .......... .......... .......... 83% 32.8M 4s
221250K .......... .......... .......... .......... .......... 83% 55.6M 4s
221300K .......... .......... .......... .......... .......... 83% 44.5M 4s
221350K .......... .......... .......... .......... .......... 83% 46.6M 4s
221400K .......... .......... .......... .......... .......... 83% 45.6M 4s
221450K .......... .......... .......... .......... .......... 83% 42.6M 4s
221500K .......... .......... .......... .......... .......... 83% 97.1M 4s
221550K .......... .......... .......... .......... .......... 83% 57.4M 4s
221600K .......... .......... .......... .......... .......... 83% 45.6M 4s
221650K .......... .......... .......... .......... .......... 83% 44.2M 4s
221700K .......... .......... .......... .......... .......... 83% 37.4M 4s
221750K .......... .......... .......... .......... .......... 83% 47.2M 4s
221800K .......... .......... .......... .......... .......... 83% 75.6M 4s
221850K .......... .......... .......... .......... .......... 83% 66.7M 4s
221900K .......... .......... .......... .......... .......... 83% 43.8M 4s
221950K .......... .......... .......... .......... .......... 83% 15.8M 4s
222000K .......... .......... .......... .......... .......... 83% 92.3M 4s
222050K .......... .......... .......... .......... .......... 83%  110M 4s
222100K .......... .......... .......... .......... .......... 83%  104M 4s
222150K .......... .......... .......... .......... .......... 83% 38.6M 4s
222200K .......... .......... .......... .......... .......... 83% 24.7M 4s
222250K .......... .......... .......... .......... .......... 83%  159M 4s
222300K .......... .......... .......... .......... .......... 83%  160M 4s
222350K .......... .......... .......... .......... .......... 83%  135M 4s
222400K .......... .......... .......... .......... .......... 83% 78.0M 4s
222450K .......... .......... .......... .......... .......... 83% 36.9M 4s
222500K .......... .......... .......... .......... .......... 83% 50.5M 4s
222550K .......... .......... .......... .......... .......... 83% 45.8M 4s
222600K .......... .......... .......... .......... .......... 83% 41.7M 4s
222650K .......... .......... .......... .......... .......... 83% 44.6M 4s
222700K .......... .......... .......... .......... .......... 83% 26.4M 4s
222750K .......... .......... .......... .......... .......... 83% 46.8M 4s
222800K .......... .......... .......... .......... .......... 83% 49.3M 4s
222850K .......... .......... .......... .......... .......... 83% 34.9M 4s
222900K .......... .......... .......... .......... .......... 83% 49.0M 4s
222950K .......... .......... .......... .......... .......... 83% 24.7M 4s
223000K .......... .......... .......... .......... .......... 83% 49.4M 4s
223050K .......... .......... .......... .......... .......... 83% 48.2M 4s
223100K .......... .......... .......... .......... .......... 83% 46.2M 4s
223150K .......... .......... .......... .......... .......... 83% 48.6M 4s
223200K .......... .......... .......... .......... .......... 83% 44.1M 4s
223250K .......... .......... .......... .......... .......... 84% 48.6M 4s
223300K .......... .......... .......... .......... .......... 84% 52.1M 4s
223350K .......... .......... .......... .......... .......... 84% 33.8M 4s
223400K .......... .......... .......... .......... .......... 84% 47.8M 4s
223450K .......... .......... .......... .......... .......... 84% 41.6M 3s
223500K .......... .......... .......... .......... .......... 84% 36.8M 3s
223550K .......... .......... .......... .......... .......... 84% 46.2M 3s
223600K .......... .......... .......... .......... .......... 84% 50.6M 3s
223650K .......... .......... .......... .......... .......... 84% 50.6M 3s
223700K .......... .......... .......... .......... .......... 84% 28.1M 3s
223750K .......... .......... .......... .......... .......... 84% 48.9M 3s
223800K .......... .......... .......... .......... .......... 84% 39.5M 3s
223850K .......... .......... .......... .......... .......... 84% 44.2M 3s
223900K .......... .......... .......... .......... .......... 84%  114M 3s
223950K .......... .......... .......... .......... .......... 84% 37.3M 3s
224000K .......... .......... .......... .......... .......... 84%  106M 3s
224050K .......... .......... .......... .......... .......... 84% 32.5M 3s
224100K .......... .......... .......... .......... .......... 84% 87.8M 3s
224150K .......... .......... .......... .......... .......... 84% 10.6M 3s
224200K .......... .......... .......... .......... .......... 84%  126M 3s
224250K .......... .......... .......... .......... .......... 84%  122M 3s
224300K .......... .......... .......... .......... .......... 84%  202M 3s
224350K .......... .......... .......... .......... .......... 84%  133M 3s
224400K .......... .......... .......... .......... .......... 84%  154M 3s
224450K .......... .......... .......... .......... .......... 84%  119M 3s
224500K .......... .......... .......... .......... .......... 84% 50.1M 3s
224550K .......... .......... .......... .......... .......... 84%  138M 3s
224600K .......... .......... .......... .......... .......... 84% 72.4M 3s
224650K .......... .......... .......... .......... .......... 84% 45.5M 3s
224700K .......... .......... .......... .......... .......... 84% 42.5M 3s
224750K .......... .......... .......... .......... .......... 84% 36.5M 3s
224800K .......... .......... .......... .......... .......... 84% 42.2M 3s
224850K .......... .......... .......... .......... .......... 84% 36.7M 3s
224900K .......... .......... .......... .......... .......... 84% 44.4M 3s
224950K .......... .......... .......... .......... .......... 84% 36.8M 3s
225000K .......... .......... .......... .......... .......... 84% 47.1M 3s
225050K .......... .......... .......... .......... .......... 84% 37.3M 3s
225100K .......... .......... .......... .......... .......... 84% 38.3M 3s
225150K .......... .......... .......... .......... .......... 84% 41.9M 3s
225200K .......... .......... .......... .......... .......... 84% 47.0M 3s
225250K .......... .......... .......... .......... .......... 84% 48.1M 3s
225300K .......... .......... .......... .......... .......... 84% 42.2M 3s
225350K .......... .......... .......... .......... .......... 84% 44.6M 3s
225400K .......... .......... .......... .......... .......... 84% 51.8M 3s
225450K .......... .......... .......... .......... .......... 84% 43.1M 3s
225500K .......... .......... .......... .......... .......... 84% 46.0M 3s
225550K .......... .......... .......... .......... .......... 84% 83.9M 3s
225600K .......... .......... .......... .......... .......... 84% 32.0M 3s
225650K .......... .......... .......... .......... .......... 84% 96.1M 3s
225700K .......... .......... .......... .......... .......... 84% 30.1M 3s
225750K .......... .......... .......... .......... .......... 84% 79.4M 3s
225800K .......... .......... .......... .......... .......... 84% 51.5M 3s
225850K .......... .......... .......... .......... .......... 84% 46.3M 3s
225900K .......... .......... .......... .......... .......... 85% 43.1M 3s
225950K .......... .......... .......... .......... .......... 85% 50.8M 3s
226000K .......... .......... .......... .......... .......... 85% 38.1M 3s
226050K .......... .......... .......... .......... .......... 85% 45.8M 3s
226100K .......... .......... .......... .......... .......... 85% 46.6M 3s
226150K .......... .......... .......... .......... .......... 85% 47.1M 3s
226200K .......... .......... .......... .......... .......... 85% 41.3M 3s
226250K .......... .......... .......... .......... .......... 85% 33.9M 3s
226300K .......... .......... .......... .......... .......... 85% 14.1M 3s
226350K .......... .......... .......... .......... .......... 85%  107M 3s
226400K .......... .......... .......... .......... .......... 85%  115M 3s
226450K .......... .......... .......... .......... .......... 85%  126M 3s
226500K .......... .......... .......... .......... .......... 85% 95.0M 3s
226550K .......... .......... .......... .......... .......... 85% 25.4M 3s
226600K .......... .......... .......... .......... .......... 85% 45.6M 3s
226650K .......... .......... .......... .......... .......... 85%  147M 3s
226700K .......... .......... .......... .......... .......... 85% 21.2M 3s
226750K .......... .......... .......... .......... .......... 85% 63.7M 3s
226800K .......... .......... .......... .......... .......... 85%  124M 3s
226850K .......... .......... .......... .......... .......... 85%  109M 3s
226900K .......... .......... .......... .......... .......... 85% 49.5M 3s
226950K .......... .......... .......... .......... .......... 85% 37.4M 3s
227000K .......... .......... .......... .......... .......... 85% 38.8M 3s
227050K .......... .......... .......... .......... .......... 85%  115M 3s
227100K .......... .......... .......... .......... .......... 85% 38.9M 3s
227150K .......... .......... .......... .......... .......... 85% 46.9M 3s
227200K .......... .......... .......... .......... .......... 85% 43.4M 3s
227250K .......... .......... .......... .......... .......... 85% 38.7M 3s
227300K .......... .......... .......... .......... .......... 85% 44.4M 3s
227350K .......... .......... .......... .......... .......... 85% 32.4M 3s
227400K .......... .......... .......... .......... .......... 85%  102M 3s
227450K .......... .......... .......... .......... .......... 85% 29.7M 3s
227500K .......... .......... .......... .......... .......... 85% 29.6M 3s
227550K .......... .......... .......... .......... .......... 85% 21.7M 3s
227600K .......... .......... .......... .......... .......... 85% 26.2M 3s
227650K .......... .......... .......... .......... .......... 85% 32.5M 3s
227700K .......... .......... .......... .......... .......... 85% 33.5M 3s
227750K .......... .......... .......... .......... .......... 85% 46.5M 3s
227800K .......... .......... .......... .......... .......... 85% 95.0M 3s
227850K .......... .......... .......... .......... .......... 85% 46.1M 3s
227900K .......... .......... .......... .......... .......... 85% 44.1M 3s
227950K .......... .......... .......... .......... .......... 85% 46.6M 3s
228000K .......... .......... .......... .......... .......... 85% 49.7M 3s
228050K .......... .......... .......... .......... .......... 85% 42.9M 3s
228100K .......... .......... .......... .......... .......... 85% 46.7M 3s
228150K .......... .......... .......... .......... .......... 85% 42.9M 3s
228200K .......... .......... .......... .......... .......... 85% 39.9M 3s
228250K .......... .......... .......... .......... .......... 85% 43.7M 3s
228300K .......... .......... .......... .......... .......... 85%  104M 3s
228350K .......... .......... .......... .......... .......... 85% 12.5M 3s
228400K .......... .......... .......... .......... .......... 85% 95.2M 3s
228450K .......... .......... .......... .......... .......... 85% 95.7M 3s
228500K .......... .......... .......... .......... .......... 85%  114M 3s
228550K .......... .......... .......... .......... .......... 86% 46.7M 3s
228600K .......... .......... .......... .......... .......... 86%  126M 3s
228650K .......... .......... .......... .......... .......... 86%  130M 3s
228700K .......... .......... .......... .......... .......... 86% 32.8M 3s
228750K .......... .......... .......... .......... .......... 86% 36.9M 3s
228800K .......... .......... .......... .......... .......... 86% 48.5M 3s
228850K .......... .......... .......... .......... .......... 86% 29.3M 3s
228900K .......... .......... .......... .......... .......... 86% 44.2M 3s
228950K .......... .......... .......... .......... .......... 86% 36.1M 3s
229000K .......... .......... .......... .......... .......... 86% 38.1M 3s
229050K .......... .......... .......... .......... .......... 86% 42.7M 3s
229100K .......... .......... .......... .......... .......... 86% 42.6M 3s
229150K .......... .......... .......... .......... .......... 86% 28.4M 3s
229200K .......... .......... .......... .......... .......... 86% 42.0M 3s
229250K .......... .......... .......... .......... .......... 86% 43.1M 3s
229300K .......... .......... .......... .......... .......... 86% 44.4M 3s
229350K .......... .......... .......... .......... .......... 86% 37.4M 3s
229400K .......... .......... .......... .......... .......... 86% 50.1M 3s
229450K .......... .......... .......... .......... .......... 86% 25.7M 3s
229500K .......... .......... .......... .......... .......... 86% 41.5M 3s
229550K .......... .......... .......... .......... .......... 86% 38.8M 3s
229600K .......... .......... .......... .......... .......... 86% 37.7M 3s
229650K .......... .......... .......... .......... .......... 86% 41.9M 3s
229700K .......... .......... .......... .......... .......... 86% 28.4M 3s
229750K .......... .......... .......... .......... .......... 86% 45.8M 3s
229800K .......... .......... .......... .......... .......... 86% 38.4M 3s
229850K .......... .......... .......... .......... .......... 86% 42.3M 3s
229900K .......... .......... .......... .......... .......... 86% 44.6M 3s
229950K .......... .......... .......... .......... .......... 86% 23.1M 3s
230000K .......... .......... .......... .......... .......... 86% 40.3M 3s
230050K .......... .......... .......... .......... .......... 86% 32.5M 3s
230100K .......... .......... .......... .......... .......... 86% 47.5M 3s
230150K .......... .......... .......... .......... .......... 86% 12.7M 3s
230200K .......... .......... .......... .......... .......... 86%  103M 3s
230250K .......... .......... .......... .......... .......... 86%  137M 3s
230300K .......... .......... .......... .......... .......... 86% 34.2M 3s
230350K .......... .......... .......... .......... .......... 86% 27.5M 3s
230400K .......... .......... .......... .......... .......... 86% 28.1M 3s
230450K .......... .......... .......... .......... .......... 86%  139M 3s
230500K .......... .......... .......... .......... .......... 86% 30.4M 3s
230550K .......... .......... .......... .......... .......... 86% 51.3M 3s
230600K .......... .......... .......... .......... .......... 86% 20.2M 3s
230650K .......... .......... .......... .......... .......... 86% 29.5M 3s
230700K .......... .......... .......... .......... .......... 86% 19.3M 3s
230750K .......... .......... .......... .......... .......... 86% 32.1M 3s
230800K .......... .......... .......... .......... .......... 86% 27.1M 3s
230850K .......... .......... .......... .......... .......... 86% 23.7M 3s
230900K .......... .......... .......... .......... .......... 86% 37.8M 3s
230950K .......... .......... .......... .......... .......... 86% 23.1M 3s
231000K .......... .......... .......... .......... .......... 86% 23.5M 3s
231050K .......... .......... .......... .......... .......... 86% 27.3M 3s
231100K .......... .......... .......... .......... .......... 86% 21.9M 3s
231150K .......... .......... .......... .......... .......... 86% 37.4M 3s
231200K .......... .......... .......... .......... .......... 87% 20.4M 3s
231250K .......... .......... .......... .......... .......... 87% 28.3M 3s
231300K .......... .......... .......... .......... .......... 87% 19.5M 3s
231350K .......... .......... .......... .......... .......... 87% 26.6M 3s
231400K .......... .......... .......... .......... .......... 87% 33.2M 3s
231450K .......... .......... .......... .......... .......... 87% 19.2M 3s
231500K .......... .......... .......... .......... .......... 87%  103M 3s
231550K .......... .......... .......... .......... .......... 87% 8.87M 3s
231600K .......... .......... .......... .......... .......... 87% 95.9M 3s
231650K .......... .......... .......... .......... .......... 87%  204M 3s
231700K .......... .......... .......... .......... .......... 87% 42.6M 3s
231750K .......... .......... .......... .......... .......... 87% 42.9M 3s
231800K .......... .......... .......... .......... .......... 87% 80.8M 3s
231850K .......... .......... .......... .......... .......... 87% 49.1M 3s
231900K .......... .......... .......... .......... .......... 87%  130M 3s
231950K .......... .......... .......... .......... .......... 87% 23.8M 3s
232000K .......... .......... .......... .......... .......... 87% 38.5M 3s
232050K .......... .......... .......... .......... .......... 87% 31.2M 3s
232100K .......... .......... .......... .......... .......... 87% 27.6M 3s
232150K .......... .......... .......... .......... .......... 87% 30.5M 3s
232200K .......... .......... .......... .......... .......... 87% 42.7M 3s
232250K .......... .......... .......... .......... .......... 87% 22.7M 3s
232300K .......... .......... .......... .......... .......... 87% 38.9M 3s
232350K .......... .......... .......... .......... .......... 87% 26.0M 3s
232400K .......... .......... .......... .......... .......... 87% 41.1M 3s
232450K .......... .......... .......... .......... .......... 87% 20.0M 3s
232500K .......... .......... .......... .......... .......... 87% 36.8M 3s
232550K .......... .......... .......... .......... .......... 87% 36.2M 3s
232600K .......... .......... .......... .......... .......... 87% 24.4M 3s
232650K .......... .......... .......... .......... .......... 87% 40.2M 3s
232700K .......... .......... .......... .......... .......... 87% 23.8M 3s
232750K .......... .......... .......... .......... .......... 87% 44.1M 3s
232800K .......... .......... .......... .......... .......... 87% 15.0M 3s
232850K .......... .......... .......... .......... .......... 87% 34.8M 3s
232900K .......... .......... .......... .......... .......... 87% 39.4M 3s
232950K .......... .......... .......... .......... .......... 87% 23.7M 3s
233000K .......... .......... .......... .......... .......... 87% 37.2M 3s
233050K .......... .......... .......... .......... .......... 87% 96.7M 3s
233100K .......... .......... .......... .......... .......... 87% 62.9M 3s
233150K .......... .......... .......... .......... .......... 87% 34.3M 3s
233200K .......... .......... .......... .......... .......... 87%  108M 3s
233250K .......... .......... .......... .......... .......... 87% 15.4M 3s
233300K .......... .......... .......... .......... .......... 87% 67.6M 3s
233350K .......... .......... .......... .......... .......... 87%  102M 3s
233400K .......... .......... .......... .......... .......... 87% 55.2M 3s
233450K .......... .......... .......... .......... .......... 87% 75.7M 3s
233500K .......... .......... .......... .......... .......... 87% 67.0M 3s
233550K .......... .......... .......... .......... .......... 87%  119M 3s
233600K .......... .......... .......... .......... .......... 87% 64.8M 3s
233650K .......... .......... .......... .......... .......... 87% 62.6M 3s
233700K .......... .......... .......... .......... .......... 87%  108M 3s
233750K .......... .......... .......... .......... .......... 87% 62.8M 3s
233800K .......... .......... .......... .......... .......... 87% 52.6M 3s
233850K .......... .......... .......... .......... .......... 87% 44.1M 3s
233900K .......... .......... .......... .......... .......... 88% 50.4M 3s
233950K .......... .......... .......... .......... .......... 88% 26.1M 3s
234000K .......... .......... .......... .......... .......... 88% 80.2M 3s
234050K .......... .......... .......... .......... .......... 88% 44.6M 3s
234100K .......... .......... .......... .......... .......... 88% 41.9M 3s
234150K .......... .......... .......... .......... .......... 88% 41.1M 3s
234200K .......... .......... .......... .......... .......... 88% 42.3M 3s
234250K .......... .......... .......... .......... .......... 88% 58.2M 3s
234300K .......... .......... .......... .......... .......... 88% 51.0M 3s
234350K .......... .......... .......... .......... .......... 88% 45.8M 3s
234400K .......... .......... .......... .......... .......... 88% 33.0M 3s
234450K .......... .......... .......... .......... .......... 88% 47.2M 3s
234500K .......... .......... .......... .......... .......... 88% 35.4M 2s
234550K .......... .......... .......... .......... .......... 88% 45.6M 2s
234600K .......... .......... .......... .......... .......... 88% 40.6M 2s
234650K .......... .......... .......... .......... .......... 88% 51.6M 2s
234700K .......... .......... .......... .......... .......... 88% 49.5M 2s
234750K .......... .......... .......... .......... .......... 88% 46.6M 2s
234800K .......... .......... .......... .......... .......... 88% 38.8M 2s
234850K .......... .......... .......... .......... .......... 88% 39.9M 2s
234900K .......... .......... .......... .......... .......... 88% 48.4M 2s
234950K .......... .......... .......... .......... .......... 88% 46.1M 2s
235000K .......... .......... .......... .......... .......... 88% 46.8M 2s
235050K .......... .......... .......... .......... .......... 88% 37.6M 2s
235100K .......... .......... .......... .......... .......... 88% 45.2M 2s
235150K .......... .......... .......... .......... .......... 88% 40.3M 2s
235200K .......... .......... .......... .......... .......... 88% 41.0M 2s
235250K .......... .......... .......... .......... .......... 88% 51.6M 2s
235300K .......... .......... .......... .......... .......... 88% 70.1M 2s
235350K .......... .......... .......... .......... .......... 88% 42.5M 2s
235400K .......... .......... .......... .......... .......... 88%  115M 2s
235450K .......... .......... .......... .......... .......... 88% 12.9M 2s
235500K .......... .......... .......... .......... .......... 88% 92.8M 2s
235550K .......... .......... .......... .......... .......... 88%  121M 2s
235600K .......... .......... .......... .......... .......... 88% 41.3M 2s
235650K .......... .......... .......... .......... .......... 88%  136M 2s
235700K .......... .......... .......... .......... .......... 88%  105M 2s
235750K .......... .......... .......... .......... .......... 88% 73.0M 2s
235800K .......... .......... .......... .......... .......... 88%  126M 2s
235850K .......... .......... .......... .......... .......... 88% 53.5M 2s
235900K .......... .......... .......... .......... .......... 88% 35.4M 2s
235950K .......... .......... .......... .......... .......... 88% 83.3M 2s
236000K .......... .......... .......... .......... .......... 88%  108M 2s
236050K .......... .......... .......... .......... .......... 88%  133M 2s
236100K .......... .......... .......... .......... .......... 88%  121M 2s
236150K .......... .......... .......... .......... .......... 88% 50.8M 2s
236200K .......... .......... .......... .......... .......... 88% 29.8M 2s
236250K .......... .......... .......... .......... .......... 88% 42.3M 2s
236300K .......... .......... .......... .......... .......... 88% 38.4M 2s
236350K .......... .......... .......... .......... .......... 88% 46.0M 2s
236400K .......... .......... .......... .......... .......... 88% 46.8M 2s
236450K .......... .......... .......... .......... .......... 88% 41.7M 2s
236500K .......... .......... .......... .......... .......... 88% 29.8M 2s
236550K .......... .......... .......... .......... .......... 89% 7.43M 2s
236600K .......... .......... .......... .......... .......... 89% 42.1M 2s
236650K .......... .......... .......... .......... .......... 89% 40.9M 2s
236700K .......... .......... .......... .......... .......... 89% 35.9M 2s
236750K .......... .......... .......... .......... .......... 89% 37.3M 2s
236800K .......... .......... .......... .......... .......... 89% 46.2M 2s
236850K .......... .......... .......... .......... .......... 89% 33.3M 2s
236900K .......... .......... .......... .......... .......... 89% 51.2M 2s
236950K .......... .......... .......... .......... .......... 89% 36.5M 2s
237000K .......... .......... .......... .......... .......... 89% 42.2M 2s
237050K .......... .......... .......... .......... .......... 89% 38.8M 2s
237100K .......... .......... .......... .......... .......... 89% 40.9M 2s
237150K .......... .......... .......... .......... .......... 89% 27.0M 2s
237200K .......... .......... .......... .......... .......... 89% 36.2M 2s
237250K .......... .......... .......... .......... .......... 89% 46.6M 2s
237300K .......... .......... .......... .......... .......... 89%  122M 2s
237350K .......... .......... .......... .......... .......... 89% 38.6M 2s
237400K .......... .......... .......... .......... .......... 89% 34.4M 2s
237450K .......... .......... .......... .......... .......... 89%  107M 2s
237500K .......... .......... .......... .......... .......... 89% 14.4M 2s
237550K .......... .......... .......... .......... .......... 89%  105M 2s
237600K .......... .......... .......... .......... .......... 89% 42.9M 2s
237650K .......... .......... .......... .......... .......... 89%  150M 2s
237700K .......... .......... .......... .......... .......... 89%  113M 2s
237750K .......... .......... .......... .......... .......... 89%  117M 2s
237800K .......... .......... .......... .......... .......... 89% 64.8M 2s
237850K .......... .......... .......... .......... .......... 89% 43.2M 2s
237900K .......... .......... .......... .......... .......... 89% 55.5M 2s
237950K .......... .......... .......... .......... .......... 89% 68.1M 2s
238000K .......... .......... .......... .......... .......... 89% 51.9M 2s
238050K .......... .......... .......... .......... .......... 89% 26.5M 2s
238100K .......... .......... .......... .......... .......... 89% 33.4M 2s
238150K .......... .......... .......... .......... .......... 89% 26.9M 2s
238200K .......... .......... .......... .......... .......... 89% 40.7M 2s
238250K .......... .......... .......... .......... .......... 89% 29.3M 2s
238300K .......... .......... .......... .......... .......... 89% 40.1M 2s
238350K .......... .......... .......... .......... .......... 89% 28.0M 2s
238400K .......... .......... .......... .......... .......... 89% 36.7M 2s
238450K .......... .......... .......... .......... .......... 89% 22.2M 2s
238500K .......... .......... .......... .......... .......... 89% 47.3M 2s
238550K .......... .......... .......... .......... .......... 89% 32.5M 2s
238600K .......... .......... .......... .......... .......... 89% 24.9M 2s
238650K .......... .......... .......... .......... .......... 89% 34.2M 2s
238700K .......... .......... .......... .......... .......... 89% 38.6M 2s
238750K .......... .......... .......... .......... .......... 89% 28.2M 2s
238800K .......... .......... .......... .......... .......... 89% 37.9M 2s
238850K .......... .......... .......... .......... .......... 89% 26.7M 2s
238900K .......... .......... .......... .......... .......... 89% 40.8M 2s
238950K .......... .......... .......... .......... .......... 89% 24.7M 2s
239000K .......... .......... .......... .......... .......... 89% 48.2M 2s
239050K .......... .......... .......... .......... .......... 89% 30.6M 2s
239100K .......... .......... .......... .......... .......... 89% 28.3M 2s
239150K .......... .......... .......... .......... .......... 89% 46.1M 2s
239200K .......... .......... .......... .......... .......... 90% 24.8M 2s
239250K .......... .......... .......... .......... .......... 90% 40.5M 2s
239300K .......... .......... .......... .......... .......... 90% 51.4M 2s
239350K .......... .......... .......... .......... .......... 90% 43.8M 2s
239400K .......... .......... .......... .......... .......... 90% 54.4M 2s
239450K .......... .......... .......... .......... .......... 90% 64.2M 2s
239500K .......... .......... .......... .......... .......... 90%  180M 2s
239550K .......... .......... .......... .......... .......... 90%  152M 2s
239600K .......... .......... .......... .......... .......... 90% 17.2M 2s
239650K .......... .......... .......... .......... .......... 90% 92.1M 2s
239700K .......... .......... .......... .......... .......... 90%  137M 2s
239750K .......... .......... .......... .......... .......... 90% 41.1M 2s
239800K .......... .......... .......... .......... .......... 90% 60.6M 2s
239850K .......... .......... .......... .......... .......... 90% 55.2M 2s
239900K .......... .......... .......... .......... .......... 90% 48.0M 2s
239950K .......... .......... .......... .......... .......... 90%  137M 2s
240000K .......... .......... .......... .......... .......... 90% 41.9M 2s
240050K .......... .......... .......... .......... .......... 90% 38.8M 2s
240100K .......... .......... .......... .......... .......... 90% 40.1M 2s
240150K .......... .......... .......... .......... .......... 90% 44.3M 2s
240200K .......... .......... .......... .......... .......... 90% 39.2M 2s
240250K .......... .......... .......... .......... .......... 90% 36.1M 2s
240300K .......... .......... .......... .......... .......... 90% 45.7M 2s
240350K .......... .......... .......... .......... .......... 90% 29.4M 2s
240400K .......... .......... .......... .......... .......... 90% 42.6M 2s
240450K .......... .......... .......... .......... .......... 90% 36.9M 2s
240500K .......... .......... .......... .......... .......... 90% 47.4M 2s
240550K .......... .......... .......... .......... .......... 90% 44.7M 2s
240600K .......... .......... .......... .......... .......... 90% 31.5M 2s
240650K .......... .......... .......... .......... .......... 90% 44.4M 2s
240700K .......... .......... .......... .......... .......... 90% 25.4M 2s
240750K .......... .......... .......... .......... .......... 90% 37.6M 2s
240800K .......... .......... .......... .......... .......... 90% 36.8M 2s
240850K .......... .......... .......... .......... .......... 90% 41.8M 2s
240900K .......... .......... .......... .......... .......... 90% 51.6M 2s
240950K .......... .......... .......... .......... .......... 90% 45.5M 2s
241000K .......... .......... .......... .......... .......... 90% 37.0M 2s
241050K .......... .......... .......... .......... .......... 90% 28.9M 2s
241100K .......... .......... .......... .......... .......... 90% 42.0M 2s
241150K .......... .......... .......... .......... .......... 90% 42.9M 2s
241200K .......... .......... .......... .......... .......... 90% 44.1M 2s
241250K .......... .......... .......... .......... .......... 90% 46.0M 2s
241300K .......... .......... .......... .......... .......... 90% 41.0M 2s
241350K .......... .......... .......... .......... .......... 90% 26.7M 2s
241400K .......... .......... .......... .......... .......... 90% 94.4M 2s
241450K .......... .......... .......... .......... .......... 90% 32.9M 2s
241500K .......... .......... .......... .......... .......... 90% 12.1M 2s
241550K .......... .......... .......... .......... .......... 90%  124M 2s
241600K .......... .......... .......... .......... .......... 90% 94.1M 2s
241650K .......... .......... .......... .......... .......... 90%  106M 2s
241700K .......... .......... .......... .......... .......... 90%  106M 2s
241750K .......... .......... .......... .......... .......... 90% 18.1M 2s
241800K .......... .......... .......... .......... .......... 90%  120M 2s
241850K .......... .......... .......... .......... .......... 91% 63.2M 2s
241900K .......... .......... .......... .......... .......... 91%  107M 2s
241950K .......... .......... .......... .......... .......... 91% 29.7M 2s
242000K .......... .......... .......... .......... .......... 91% 60.4M 2s
242050K .......... .......... .......... .......... .......... 91% 39.0M 2s
242100K .......... .......... .......... .......... .......... 91% 24.9M 2s
242150K .......... .......... .......... .......... .......... 91% 21.5M 2s
242200K .......... .......... .......... .......... .......... 91% 35.9M 2s
242250K .......... .......... .......... .......... .......... 91% 23.3M 2s
242300K .......... .......... .......... .......... .......... 91% 34.2M 2s
242350K .......... .......... .......... .......... .......... 91% 19.6M 2s
242400K .......... .......... .......... .......... .......... 91% 33.0M 2s
242450K .......... .......... .......... .......... .......... 91% 30.6M 2s
242500K .......... .......... .......... .......... .......... 91% 25.0M 2s
242550K .......... .......... .......... .......... .......... 91% 41.2M 2s
242600K .......... .......... .......... .......... .......... 91% 24.3M 2s
242650K .......... .......... .......... .......... .......... 91% 27.8M 2s
242700K .......... .......... .......... .......... .......... 91% 28.5M 2s
242750K .......... .......... .......... .......... .......... 91% 28.3M 2s
242800K .......... .......... .......... .......... .......... 91% 43.2M 2s
242850K .......... .......... .......... .......... .......... 91% 27.5M 2s
242900K .......... .......... .......... .......... .......... 91% 22.5M 2s
242950K .......... .......... .......... .......... .......... 91% 19.6M 2s
243000K .......... .......... .......... .......... .......... 91% 98.0M 2s
243050K .......... .......... .......... .......... .......... 91% 27.5M 2s
243100K .......... .......... .......... .......... .......... 91% 12.2M 2s
243150K .......... .......... .......... .......... .......... 91%  121M 2s
243200K .......... .......... .......... .......... .......... 91%  120M 2s
243250K .......... .......... .......... .......... .......... 91% 20.3M 2s
243300K .......... .......... .......... .......... .......... 91% 25.1M 2s
243350K .......... .......... .......... .......... .......... 91% 58.7M 2s
243400K .......... .......... .......... .......... .......... 91% 25.1M 2s
243450K .......... .......... .......... .......... .......... 91% 36.3M 2s
243500K .......... .......... .......... .......... .......... 91% 22.3M 2s
243550K .......... .......... .......... .......... .......... 91% 29.8M 2s
243600K .......... .......... .......... .......... .......... 91% 34.5M 2s
243650K .......... .......... .......... .......... .......... 91% 24.9M 2s
243700K .......... .......... .......... .......... .......... 91% 21.5M 2s
243750K .......... .......... .......... .......... .......... 91% 36.5M 2s
243800K .......... .......... .......... .......... .......... 91% 23.6M 2s
243850K .......... .......... .......... .......... .......... 91% 28.6M 2s
243900K .......... .......... .......... .......... .......... 91% 29.8M 2s
243950K .......... .......... .......... .......... .......... 91% 19.9M 2s
244000K .......... .......... .......... .......... .......... 91% 40.0M 2s
244050K .......... .......... .......... .......... .......... 91% 24.5M 2s
244100K .......... .......... .......... .......... .......... 91% 20.9M 2s
244150K .......... .......... .......... .......... .......... 91% 20.2M 2s
244200K .......... .......... .......... .......... .......... 91% 37.1M 2s
244250K .......... .......... .......... .......... .......... 91% 22.5M 2s
244300K .......... .......... .......... .......... .......... 91% 30.1M 2s
244350K .......... .......... .......... .......... .......... 91% 32.4M 2s
244400K .......... .......... .......... .......... .......... 91% 44.7M 2s
244450K .......... .......... .......... .......... .......... 91% 10.4M 2s
244500K .......... .......... .......... .......... .......... 92%  121M 2s
244550K .......... .......... .......... .......... .......... 92%  106M 2s
244600K .......... .......... .......... .......... .......... 92% 32.2M 2s
244650K .......... .......... .......... .......... .......... 92%  172M 2s
244700K .......... .......... .......... .......... .......... 92% 30.9M 2s
244750K .......... .......... .......... .......... .......... 92% 72.4M 2s
244800K .......... .......... .......... .......... .......... 92% 67.2M 2s
244850K .......... .......... .......... .......... .......... 92% 29.0M 2s
244900K .......... .......... .......... .......... .......... 92% 20.9M 2s
244950K .......... .......... .......... .......... .......... 92% 32.2M 2s
245000K .......... .......... .......... .......... .......... 92% 28.1M 2s
245050K .......... .......... .......... .......... .......... 92% 35.0M 2s
245100K .......... .......... .......... .......... .......... 92% 31.9M 2s
245150K .......... .......... .......... .......... .......... 92% 18.6M 2s
245200K .......... .......... .......... .......... .......... 92% 27.8M 2s
245250K .......... .......... .......... .......... .......... 92% 33.3M 2s
245300K .......... .......... .......... .......... .......... 92% 25.7M 2s
245350K .......... .......... .......... .......... .......... 92% 35.2M 2s
245400K .......... .......... .......... .......... .......... 92% 18.8M 2s
245450K .......... .......... .......... .......... .......... 92% 25.8M 2s
245500K .......... .......... .......... .......... .......... 92% 32.1M 2s
245550K .......... .......... .......... .......... .......... 92% 43.4M 2s
245600K .......... .......... .......... .......... .......... 92% 22.9M 2s
245650K .......... .......... .......... .......... .......... 92% 32.2M 2s
245700K .......... .......... .......... .......... .......... 92% 27.3M 2s
245750K .......... .......... .......... .......... .......... 92% 25.8M 2s
245800K .......... .......... .......... .......... .......... 92% 78.9M 2s
245850K .......... .......... .......... .......... .......... 92% 11.1M 2s
245900K .......... .......... .......... .......... .......... 92% 65.7M 2s
245950K .......... .......... .......... .......... .......... 92% 65.1M 2s
246000K .......... .......... .......... .......... .......... 92% 82.9M 2s
246050K .......... .......... .......... .......... .......... 92% 66.3M 2s
246100K .......... .......... .......... .......... .......... 92%  113M 2s
246150K .......... .......... .......... .......... .......... 92% 41.7M 2s
246200K .......... .......... .......... .......... .......... 92% 50.4M 2s
246250K .......... .......... .......... .......... .......... 92% 44.1M 2s
246300K .......... .......... .......... .......... .......... 92% 59.4M 2s
246350K .......... .......... .......... .......... .......... 92% 78.6M 2s
246400K .......... .......... .......... .......... .......... 92% 30.2M 1s
246450K .......... .......... .......... .......... .......... 92% 31.9M 1s
246500K .......... .......... .......... .......... .......... 92% 31.1M 1s
246550K .......... .......... .......... .......... .......... 92% 38.2M 1s
246600K .......... .......... .......... .......... .......... 92% 24.7M 1s
246650K .......... .......... .......... .......... .......... 92% 46.3M 1s
246700K .......... .......... .......... .......... .......... 92% 23.8M 1s
246750K .......... .......... .......... .......... .......... 92% 34.5M 1s
246800K .......... .......... .......... .......... .......... 92% 38.9M 1s
246850K .......... .......... .......... .......... .......... 92% 31.8M 1s
246900K .......... .......... .......... .......... .......... 92% 46.9M 1s
246950K .......... .......... .......... .......... .......... 92% 26.8M 1s
247000K .......... .......... .......... .......... .......... 92% 35.6M 1s
247050K .......... .......... .......... .......... .......... 92% 32.9M 1s
247100K .......... .......... .......... .......... .......... 92% 31.3M 1s
247150K .......... .......... .......... .......... .......... 93% 34.2M 1s
247200K .......... .......... .......... .......... .......... 93% 28.1M 1s
247250K .......... .......... .......... .......... .......... 93% 36.1M 1s
247300K .......... .......... .......... .......... .......... 93% 34.9M 1s
247350K .......... .......... .......... .......... .......... 93% 33.6M 1s
247400K .......... .......... .......... .......... .......... 93% 26.7M 1s
247450K .......... .......... .......... .......... .......... 93% 43.6M 1s
247500K .......... .......... .......... .......... .......... 93% 27.6M 1s
247550K .......... .......... .......... .......... .......... 93% 38.6M 1s
247600K .......... .......... .......... .......... .......... 93% 36.9M 1s
247650K .......... .......... .......... .......... .......... 93% 39.0M 1s
247700K .......... .......... .......... .......... .......... 93% 14.4M 1s
247750K .......... .......... .......... .......... .......... 93% 27.9M 1s
247800K .......... .......... .......... .......... .......... 93%  139M 1s
247850K .......... .......... .......... .......... .......... 93% 56.3M 1s
247900K .......... .......... .......... .......... .......... 93%  101M 1s
247950K .......... .......... .......... .......... .......... 93% 40.3M 1s
248000K .......... .......... .......... .......... .......... 93% 58.7M 1s
248050K .......... .......... .......... .......... .......... 93% 93.4M 1s
248100K .......... .......... .......... .......... .......... 93% 44.8M 1s
248150K .......... .......... .......... .......... .......... 93% 46.4M 1s
248200K .......... .......... .......... .......... .......... 93% 44.4M 1s
248250K .......... .......... .......... .......... .......... 93% 48.7M 1s
248300K .......... .......... .......... .......... .......... 93% 38.1M 1s
248350K .......... .......... .......... .......... .......... 93% 35.3M 1s
248400K .......... .......... .......... .......... .......... 93% 37.1M 1s
248450K .......... .......... .......... .......... .......... 93% 31.3M 1s
248500K .......... .......... .......... .......... .......... 93% 49.0M 1s
248550K .......... .......... .......... .......... .......... 93% 33.5M 1s
248600K .......... .......... .......... .......... .......... 93% 44.1M 1s
248650K .......... .......... .......... .......... .......... 93% 44.8M 1s
248700K .......... .......... .......... .......... .......... 93% 34.6M 1s
248750K .......... .......... .......... .......... .......... 93% 46.0M 1s
248800K .......... .......... .......... .......... .......... 93% 13.5M 1s
248850K .......... .......... .......... .......... .......... 93% 37.4M 1s
248900K .......... .......... .......... .......... .......... 93% 45.5M 1s
248950K .......... .......... .......... .......... .......... 93% 42.2M 1s
249000K .......... .......... .......... .......... .......... 93% 31.0M 1s
249050K .......... .......... .......... .......... .......... 93% 44.2M 1s
249100K .......... .......... .......... .......... .......... 93% 35.4M 1s
249150K .......... .......... .......... .......... .......... 93% 46.5M 1s
249200K .......... .......... .......... .......... .......... 93% 35.0M 1s
249250K .......... .......... .......... .......... .......... 93% 46.3M 1s
249300K .......... .......... .......... .......... .......... 93% 45.5M 1s
249350K .......... .......... .......... .......... .......... 93% 26.6M 1s
249400K .......... .......... .......... .......... .......... 93% 42.1M 1s
249450K .......... .......... .......... .......... .......... 93% 39.3M 1s
249500K .......... .......... .......... .......... .......... 93%  125M 1s
249550K .......... .......... .......... .......... .......... 93% 15.1M 1s
249600K .......... .......... .......... .......... .......... 93% 34.7M 1s
249650K .......... .......... .......... .......... .......... 93%  150M 1s
249700K .......... .......... .......... .......... .......... 93% 97.5M 1s
249750K .......... .......... .......... .......... .......... 93% 56.7M 1s
249800K .......... .......... .......... .......... .......... 93%  144M 1s
249850K .......... .......... .......... .......... .......... 94% 27.9M 1s
249900K .......... .......... .......... .......... .......... 94%  156M 1s
249950K .......... .......... .......... .......... .......... 94%  101M 1s
250000K .......... .......... .......... .......... .......... 94%  105M 1s
250050K .......... .......... .......... .......... .......... 94% 48.5M 1s
250100K .......... .......... .......... .......... .......... 94% 31.4M 1s
250150K .......... .......... .......... .......... .......... 94% 53.0M 1s
250200K .......... .......... .......... .......... .......... 94% 41.8M 1s
250250K .......... .......... .......... .......... .......... 94% 45.5M 1s
250300K .......... .......... .......... .......... .......... 94% 40.5M 1s
250350K .......... .......... .......... .......... .......... 94% 39.5M 1s
250400K .......... .......... .......... .......... .......... 94% 43.6M 1s
250450K .......... .......... .......... .......... .......... 94% 31.3M 1s
250500K .......... .......... .......... .......... .......... 94% 47.8M 1s
250550K .......... .......... .......... .......... .......... 94% 47.2M 1s
250600K .......... .......... .......... .......... .......... 94% 30.5M 1s
250650K .......... .......... .......... .......... .......... 94% 52.7M 1s
250700K .......... .......... .......... .......... .......... 94% 36.3M 1s
250750K .......... .......... .......... .......... .......... 94% 44.1M 1s
250800K .......... .......... .......... .......... .......... 94% 45.8M 1s
250850K .......... .......... .......... .......... .......... 94% 44.5M 1s
250900K .......... .......... .......... .......... .......... 94% 40.3M 1s
250950K .......... .......... .......... .......... .......... 94% 41.5M 1s
251000K .......... .......... .......... .......... .......... 94% 50.1M 1s
251050K .......... .......... .......... .......... .......... 94% 44.7M 1s
251100K .......... .......... .......... .......... .......... 94% 38.0M 1s
251150K .......... .......... .......... .......... .......... 94% 47.0M 1s
251200K .......... .......... .......... .......... .......... 94% 41.8M 1s
251250K .......... .......... .......... .......... .......... 94% 37.8M 1s
251300K .......... .......... .......... .......... .......... 94% 42.7M 1s
251350K .......... .......... .......... .......... .......... 94% 38.8M 1s
251400K .......... .......... .......... .......... .......... 94% 46.7M 1s
251450K .......... .......... .......... .......... .......... 94% 36.5M 1s
251500K .......... .......... .......... .......... .......... 94%  101M 1s
251550K .......... .......... .......... .......... .......... 94% 12.3M 1s
251600K .......... .......... .......... .......... .......... 94% 14.4M 1s
251650K .......... .......... .......... .......... .......... 94%  135M 1s
251700K .......... .......... .......... .......... .......... 94%  119M 1s
251750K .......... .......... .......... .......... .......... 94%  121M 1s
251800K .......... .......... .......... .......... .......... 94%  101M 1s
251850K .......... .......... .......... .......... .......... 94%  106M 1s
251900K .......... .......... .......... .......... .......... 94% 50.4M 1s
251950K .......... .......... .......... .......... .......... 94% 85.7M 1s
252000K .......... .......... .......... .......... .......... 94%  122M 1s
252050K .......... .......... .......... .......... .......... 94%  124M 1s
252100K .......... .......... .......... .......... .......... 94%  103M 1s
252150K .......... .......... .......... .......... .......... 94%  104M 1s
252200K .......... .......... .......... .......... .......... 94% 46.5M 1s
252250K .......... .......... .......... .......... .......... 94% 40.2M 1s
252300K .......... .......... .......... .......... .......... 94% 45.5M 1s
252350K .......... .......... .......... .......... .......... 94% 43.5M 1s
252400K .......... .......... .......... .......... .......... 94% 33.8M 1s
252450K .......... .......... .......... .......... .......... 94% 28.1M 1s
252500K .......... .......... .......... .......... .......... 95% 35.7M 1s
252550K .......... .......... .......... .......... .......... 95% 37.2M 1s
252600K .......... .......... .......... .......... .......... 95% 35.5M 1s
252650K .......... .......... .......... .......... .......... 95% 51.0M 1s
252700K .......... .......... .......... .......... .......... 95% 45.3M 1s
252750K .......... .......... .......... .......... .......... 95% 35.4M 1s
252800K .......... .......... .......... .......... .......... 95% 44.2M 1s
252850K .......... .......... .......... .......... .......... 95% 46.2M 1s
252900K .......... .......... .......... .......... .......... 95% 21.0M 1s
252950K .......... .......... .......... .......... .......... 95% 37.2M 1s
253000K .......... .......... .......... .......... .......... 95% 48.5M 1s
253050K .......... .......... .......... .......... .......... 95% 48.3M 1s
253100K .......... .......... .......... .......... .......... 95% 40.9M 1s
253150K .......... .......... .......... .......... .......... 95% 50.9M 1s
253200K .......... .......... .......... .......... .......... 95% 35.3M 1s
253250K .......... .......... .......... .......... .......... 95% 41.2M 1s
253300K .......... .......... .......... .......... .......... 95% 41.6M 1s
253350K .......... .......... .......... .......... .......... 95% 41.0M 1s
253400K .......... .......... .......... .......... .......... 95% 67.6M 1s
253450K .......... .......... .......... .......... .......... 95% 38.9M 1s
253500K .......... .......... .......... .......... .......... 95% 57.0M 1s
253550K .......... .......... .......... .......... .......... 95% 50.8M 1s
253600K .......... .......... .......... .......... .......... 95% 43.8M 1s
253650K .......... .......... .......... .......... .......... 95%  124M 1s
253700K .......... .......... .......... .......... .......... 95% 35.4M 1s
253750K .......... .......... .......... .......... .......... 95%  118M 1s
253800K .......... .......... .......... .......... .......... 95%  139M 1s
253850K .......... .......... .......... .......... .......... 95% 12.8M 1s
253900K .......... .......... .......... .......... .......... 95%  113M 1s
253950K .......... .......... .......... .......... .......... 95% 70.8M 1s
254000K .......... .......... .......... .......... .......... 95% 21.2M 1s
254050K .......... .......... .......... .......... .......... 95%  133M 1s
254100K .......... .......... .......... .......... .......... 95% 95.0M 1s
254150K .......... .......... .......... .......... .......... 95%  126M 1s
254200K .......... .......... .......... .......... .......... 95%  118M 1s
254250K .......... .......... .......... .......... .......... 95%  151M 1s
254300K .......... .......... .......... .......... .......... 95%  165M 1s
254350K .......... .......... .......... .......... .......... 95% 79.5M 1s
254400K .......... .......... .......... .......... .......... 95% 44.3M 1s
254450K .......... .......... .......... .......... .......... 95% 46.5M 1s
254500K .......... .......... .......... .......... .......... 95% 48.4M 1s
254550K .......... .......... .......... .......... .......... 95% 73.6M 1s
254600K .......... .......... .......... .......... .......... 95% 34.9M 1s
254650K .......... .......... .......... .......... .......... 95% 93.2M 1s
254700K .......... .......... .......... .......... .......... 95% 46.2M 1s
254750K .......... .......... .......... .......... .......... 95% 48.1M 1s
254800K .......... .......... .......... .......... .......... 95% 57.0M 1s
254850K .......... .......... .......... .......... .......... 95% 45.5M 1s
254900K .......... .......... .......... .......... .......... 95%  106M 1s
254950K .......... .......... .......... .......... .......... 95% 40.2M 1s
255000K .......... .......... .......... .......... .......... 95% 34.4M 1s
255050K .......... .......... .......... .......... .......... 95% 54.7M 1s
255100K .......... .......... .......... .......... .......... 95% 46.2M 1s
255150K .......... .......... .......... .......... .......... 96% 44.6M 1s
255200K .......... .......... .......... .......... .......... 96% 43.8M 1s
255250K .......... .......... .......... .......... .......... 96%  107M 1s
255300K .......... .......... .......... .......... .......... 96% 53.7M 1s
255350K .......... .......... .......... .......... .......... 96% 36.4M 1s
255400K .......... .......... .......... .......... .......... 96% 52.5M 1s
255450K .......... .......... .......... .......... .......... 96% 41.3M 1s
255500K .......... .......... .......... .......... .......... 96% 50.1M 1s
255550K .......... .......... .......... .......... .......... 96% 92.1M 1s
255600K .......... .......... .......... .......... .......... 96% 45.4M 1s
255650K .......... .......... .......... .......... .......... 96% 58.0M 1s
255700K .......... .......... .......... .......... .......... 96% 41.6M 1s
255750K .......... .......... .......... .......... .......... 96% 40.0M 1s
255800K .......... .......... .......... .......... .......... 96% 96.7M 1s
255850K .......... .......... .......... .......... .......... 96% 35.3M 1s
255900K .......... .......... .......... .......... .......... 96% 50.8M 1s
255950K .......... .......... .......... .......... .......... 96% 37.2M 1s
256000K .......... .......... .......... .......... .......... 96% 39.5M 1s
256050K .......... .......... .......... .......... .......... 96% 56.1M 1s
256100K .......... .......... .......... .......... .......... 96% 66.3M 1s
256150K .......... .......... .......... .......... .......... 96% 44.1M 1s
256200K .......... .......... .......... .......... .......... 96%  121M 1s
256250K .......... .......... .......... .......... .......... 96% 10.3M 1s
256300K .......... .......... .......... .......... .......... 96%  131M 1s
256350K .......... .......... .......... .......... .......... 96%  118M 1s
256400K .......... .......... .......... .......... .......... 96%  132M 1s
256450K .......... .......... .......... .......... .......... 96% 70.8M 1s
256500K .......... .......... .......... .......... .......... 96% 64.5M 1s
256550K .......... .......... .......... .......... .......... 96% 31.8M 1s
256600K .......... .......... .......... .......... .......... 96%  137M 1s
256650K .......... .......... .......... .......... .......... 96%  125M 1s
256700K .......... .......... .......... .......... .......... 96% 44.4M 1s
256750K .......... .......... .......... .......... .......... 96% 73.2M 1s
256800K .......... .......... .......... .......... .......... 96%  150M 1s
256850K .......... .......... .......... .......... .......... 96% 29.3M 1s
256900K .......... .......... .......... .......... .......... 96% 41.9M 1s
256950K .......... .......... .......... .......... .......... 96% 26.4M 1s
257000K .......... .......... .......... .......... .......... 96% 20.5M 1s
257050K .......... .......... .......... .......... .......... 96% 23.2M 1s
257100K .......... .......... .......... .......... .......... 96% 36.9M 1s
257150K .......... .......... .......... .......... .......... 96% 26.0M 1s
257200K .......... .......... .......... .......... .......... 96% 35.3M 1s
257250K .......... .......... .......... .......... .......... 96% 33.7M 1s
257300K .......... .......... .......... .......... .......... 96% 29.1M 1s
257350K .......... .......... .......... .......... .......... 96% 37.5M 1s
257400K .......... .......... .......... .......... .......... 96% 28.8M 1s
257450K .......... .......... .......... .......... .......... 96% 35.0M 1s
257500K .......... .......... .......... .......... .......... 96% 18.9M 1s
257550K .......... .......... .......... .......... .......... 96% 39.4M 1s
257600K .......... .......... .......... .......... .......... 96% 21.8M 1s
257650K .......... .......... .......... .......... .......... 96% 37.8M 1s
257700K .......... .......... .......... .......... .......... 96% 24.2M 1s
257750K .......... .......... .......... .......... .......... 96% 40.4M 1s
257800K .......... .......... .......... .......... .......... 97% 38.5M 1s
257850K .......... .......... .......... .......... .......... 97% 22.1M 1s
257900K .......... .......... .......... .......... .......... 97%  142M 1s
257950K .......... .......... .......... .......... .......... 97% 33.9M 1s
258000K .......... .......... .......... .......... .......... 97%  124M 1s
258050K .......... .......... .......... .......... .......... 97% 69.2M 1s
258100K .......... .......... .......... .......... .......... 97% 74.4M 1s
258150K .......... .......... .......... .......... .......... 97% 72.1M 1s
258200K .......... .......... .......... .......... .......... 97% 87.5M 1s
258250K .......... .......... .......... .......... .......... 97% 64.9M 1s
258300K .......... .......... .......... .......... .......... 97%  119M 1s
258350K .......... .......... .......... .......... .......... 97% 57.1M 1s
258400K .......... .......... .......... .......... .......... 97%  100M 1s
258450K .......... .......... .......... .......... .......... 97% 62.4M 1s
258500K .......... .......... .......... .......... .......... 97%  119M 1s
258550K .......... .......... .......... .......... .......... 97%  109M 1s
258600K .......... .......... .......... .......... .......... 97% 67.4M 1s
258650K .......... .......... .......... .......... .......... 97% 86.4M 1s
258700K .......... .......... .......... .......... .......... 97% 58.8M 1s
258750K .......... .......... .......... .......... .......... 97% 62.6M 1s
258800K .......... .......... .......... .......... .......... 97% 45.4M 1s
258850K .......... .......... .......... .......... .......... 97% 48.5M 1s
258900K .......... .......... .......... .......... .......... 97% 74.7M 1s
258950K .......... .......... .......... .......... .......... 97% 56.4M 1s
259000K .......... .......... .......... .......... .......... 97% 55.8M 1s
259050K .......... .......... .......... .......... .......... 97% 70.5M 1s
259100K .......... .......... .......... .......... .......... 97%  136M 0s
259150K .......... .......... .......... .......... .......... 97%  150M 0s
259200K .......... .......... .......... .......... .......... 97%  109M 0s
259250K .......... .......... .......... .......... .......... 97% 77.3M 0s
259300K .......... .......... .......... .......... .......... 97%  142M 0s
259350K .......... .......... .......... .......... .......... 97% 42.8M 0s
259400K .......... .......... .......... .......... .......... 97%  139M 0s
259450K .......... .......... .......... .......... .......... 97% 39.8M 0s
259500K .......... .......... .......... .......... .......... 97% 94.3M 0s
259550K .......... .......... .......... .......... .......... 97% 75.2M 0s
259600K .......... .......... .......... .......... .......... 97% 86.9M 0s
259650K .......... .......... .......... .......... .......... 97%  119M 0s
259700K .......... .......... .......... .......... .......... 97% 67.0M 0s
259750K .......... .......... .......... .......... .......... 97% 91.4M 0s
259800K .......... .......... .......... .......... .......... 97% 76.7M 0s
259850K .......... .......... .......... .......... .......... 97% 82.3M 0s
259900K .......... .......... .......... .......... .......... 97% 78.4M 0s
259950K .......... .......... .......... .......... .......... 97% 61.3M 0s
260000K .......... .......... .......... .......... .......... 97% 82.6M 0s
260050K .......... .......... .......... .......... .......... 97% 99.0M 0s
260100K .......... .......... .......... .......... .......... 97% 65.5M 0s
260150K .......... .......... .......... .......... .......... 97%  111M 0s
260200K .......... .......... .......... .......... .......... 97% 47.9M 0s
260250K .......... .......... .......... .......... .......... 97%  117M 0s
260300K .......... .......... .......... .......... .......... 97% 58.0M 0s
260350K .......... .......... .......... .......... .......... 97%  110M 0s
260400K .......... .......... .......... .......... .......... 97% 49.6M 0s
260450K .......... .......... .......... .......... .......... 98%  103M 0s
260500K .......... .......... .......... .......... .......... 98% 55.7M 0s
260550K .......... .......... .......... .......... .......... 98%  102M 0s
260600K .......... .......... .......... .......... .......... 98% 97.9M 0s
260650K .......... .......... .......... .......... .......... 98% 46.8M 0s
260700K .......... .......... .......... .......... .......... 98% 89.6M 0s
260750K .......... .......... .......... .......... .......... 98% 62.2M 0s
260800K .......... .......... .......... .......... .......... 98%  103M 0s
260850K .......... .......... .......... .......... .......... 98%  102M 0s
260900K .......... .......... .......... .......... .......... 98% 59.0M 0s
260950K .......... .......... .......... .......... .......... 98%  120M 0s
261000K .......... .......... .......... .......... .......... 98% 76.1M 0s
261050K .......... .......... .......... .......... .......... 98% 95.2M 0s
261100K .......... .......... .......... .......... .......... 98% 28.6M 0s
261150K .......... .......... .......... .......... .......... 98%  147M 0s
261200K .......... .......... .......... .......... .......... 98%  176M 0s
261250K .......... .......... .......... .......... .......... 98%  133M 0s
261300K .......... .......... .......... .......... .......... 98%  108M 0s
261350K .......... .......... .......... .......... .......... 98% 69.6M 0s
261400K .......... .......... .......... .......... .......... 98% 75.8M 0s
261450K .......... .......... .......... .......... .......... 98% 83.0M 0s
261500K .......... .......... .......... .......... .......... 98%  126M 0s
261550K .......... .......... .......... .......... .......... 98% 83.9M 0s
261600K .......... .......... .......... .......... .......... 98% 84.8M 0s
261650K .......... .......... .......... .......... .......... 98% 86.7M 0s
261700K .......... .......... .......... .......... .......... 98% 96.3M 0s
261750K .......... .......... .......... .......... .......... 98% 90.1M 0s
261800K .......... .......... .......... .......... .......... 98%  101M 0s
261850K .......... .......... .......... .......... .......... 98% 71.6M 0s
261900K .......... .......... .......... .......... .......... 98%  127M 0s
261950K .......... .......... .......... .......... .......... 98% 66.3M 0s
262000K .......... .......... .......... .......... .......... 98%  119M 0s
262050K .......... .......... .......... .......... .......... 98%  105M 0s
262100K .......... .......... .......... .......... .......... 98% 91.4M 0s
262150K .......... .......... .......... .......... .......... 98% 76.5M 0s
262200K .......... .......... .......... .......... .......... 98% 95.7M 0s
262250K .......... .......... .......... .......... .......... 98%  112M 0s
262300K .......... .......... .......... .......... .......... 98% 84.3M 0s
262350K .......... .......... .......... .......... .......... 98% 90.8M 0s
262400K .......... .......... .......... .......... .......... 98% 64.0M 0s
262450K .......... .......... .......... .......... .......... 98%  105M 0s
262500K .......... .......... .......... .......... .......... 98% 91.6M 0s
262550K .......... .......... .......... .......... .......... 98%  116M 0s
262600K .......... .......... .......... .......... .......... 98% 68.1M 0s
262650K .......... .......... .......... .......... .......... 98%  105M 0s
262700K .......... .......... .......... .......... .......... 98% 72.9M 0s
262750K .......... .......... .......... .......... .......... 98%  102M 0s
262800K .......... .......... .......... .......... .......... 98%  130M 0s
262850K .......... .......... .......... .......... .......... 98% 68.9M 0s
262900K .......... .......... .......... .......... .......... 98% 92.0M 0s
262950K .......... .......... .......... .......... .......... 98% 87.8M 0s
263000K .......... .......... .......... .......... .......... 98%  128M 0s
263050K .......... .......... .......... .......... .......... 98% 84.3M 0s
263100K .......... .......... .......... .......... .......... 99% 95.9M 0s
263150K .......... .......... .......... .......... .......... 99%  102M 0s
263200K .......... .......... .......... .......... .......... 99%  101M 0s
263250K .......... .......... .......... .......... .......... 99% 82.2M 0s
263300K .......... .......... .......... .......... .......... 99%  122M 0s
263350K .......... .......... .......... .......... .......... 99% 65.2M 0s
263400K .......... .......... .......... .......... .......... 99%  120M 0s
263450K .......... .......... .......... .......... .......... 99% 99.4M 0s
263500K .......... .......... .......... .......... .......... 99%  102M 0s
263550K .......... .......... .......... .......... .......... 99% 74.1M 0s
263600K .......... .......... .......... .......... .......... 99% 94.6M 0s
263650K .......... .......... .......... .......... .......... 99% 80.2M 0s
263700K .......... .......... .......... .......... .......... 99%  126M 0s
263750K .......... .......... .......... .......... .......... 99% 77.3M 0s
263800K .......... .......... .......... .......... .......... 99%  145M 0s
263850K .......... .......... .......... .......... .......... 99% 65.6M 0s
263900K .......... .......... .......... .......... .......... 99%  116M 0s
263950K .......... .......... .......... .......... .......... 99% 95.7M 0s
264000K .......... .......... .......... .......... .......... 99% 67.1M 0s
264050K .......... .......... .......... .......... .......... 99%  113M 0s
264100K .......... .......... .......... .......... .......... 99% 47.8M 0s
264150K .......... .......... .......... .......... .......... 99%  142M 0s
264200K .......... .......... .......... .......... .......... 99% 76.1M 0s
264250K .......... .......... .......... .......... .......... 99% 86.4M 0s
264300K .......... .......... .......... .......... .......... 99% 85.8M 0s
264350K .......... .......... .......... .......... .......... 99% 86.7M 0s
264400K .......... .......... .......... .......... .......... 99%  105M 0s
264450K .......... .......... .......... .......... .......... 99% 79.9M 0s
264500K .......... .......... .......... .......... .......... 99% 95.7M 0s
264550K .......... .......... .......... .......... .......... 99% 96.3M 0s
264600K .......... .......... .......... .......... .......... 99% 67.0M 0s
264650K .......... .......... .......... .......... .......... 99%  113M 0s
264700K .......... .......... .......... .......... .......... 99% 96.5M 0s
264750K .......... .......... .......... .......... .......... 99% 86.0M 0s
264800K .......... .......... .......... .......... .......... 99%  101M 0s
264850K .......... .......... .......... .......... .......... 99%  101M 0s
264900K .......... .......... .......... .......... .......... 99% 68.3M 0s
264950K .......... .......... .......... .......... .......... 99% 84.8M 0s
265000K .......... .......... .......... .......... .......... 99% 99.9M 0s
265050K .......... .......... .......... .......... .......... 99% 97.9M 0s
265100K .......... .......... .......... .......... .......... 99% 94.4M 0s
265150K .......... .......... .......... .......... .......... 99%  108M 0s
265200K .......... .......... .......... .......... .......... 99% 29.0M 0s
265250K .......... .......... .......... .......... .......... 99%  167M 0s
265300K .......... .......... .......... .......... .......... 99%  133M 0s
265350K .......... .......... .......... .......... .......... 99%  115M 0s
265400K .......... .......... .......... .......... .......... 99%  116M 0s
265450K .......... .......... .......... .......... .......... 99% 77.6M 0s
265500K .......... .......... .......... .......... .......... 99%  105M 0s
265550K .......... .......... .......... .......... .......... 99%  113M 0s
265600K .......... .......... .......... .......... .......... 99% 80.7M 0s
265650K .......... .......... .......... .......... .......... 99%  106M 0s
265700K .......... .......... .......... .......... .......... 99% 72.9M 0s
265750K .......... .......... .......... .......... .......... 99%  114M 0s
265800K                                                       100% 7.89K=19s

2024-06-24 23:10:24 (13.3 MB/s) - ‘ESPbeta.tgz’ saved [272179604/272179604]

+ 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/DARWIN64/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/DARWIN64/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 = DARWIN64
ESP_ROOT = /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad
EFCOMP   = gfortran

CARCH    = DARWIN64
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/DARWIN64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN64
++ ESP_ARCH=DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/Users/jenkins/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/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=
++ CAPS_GLYPH=
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/ESP/ESP.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/ESP/ESP.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/wvClient/wv.html'
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src
+ make
(cd EGADS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/DARWIN64
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/DARWIN64
cp -p ../include/DARWIN64 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/DARWIN64
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/STANALYZER.make
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/STANALYZER.make
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads_dot.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads_dot.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.inc
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.inc
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/emp.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/emp.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/prm.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/prm.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.inc
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.inc
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsss.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsss.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTris.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTris.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineFit.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineFit.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineVels.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineVels.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsf90.inc
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsf90.inc
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/always_inline.h
clang++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7  -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  -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  -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  -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  -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  -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  -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  -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  -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  -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  -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  -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  -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  -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  -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  -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  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include ../util/emp.c \
		-o ./emp.o
clang++ -g  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -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  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -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  -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  -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1

SurrealD1_test_suite Complete!

clang++ -g  -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
./SurrealD4

SurrealD4_test_suite Complete!

clang++ -g  -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
./SurrealS1

SurrealS1_test_suite Complete!

clang++ -g  -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
./SurrealS4

SurrealS4_test_suite Complete!

/Library/Developer/CommandLineTools/usr/bin/make -C ../util
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 uvmap/main/uvmap.c -Iuvmap \
		-o ./uvmap.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
clang -g  -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  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
clang -g  -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  -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  -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  -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  -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  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
clang -g  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
clang -g  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
clang -g  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
clang -g  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
clang -g  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
clang -g  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
clang -g  -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/DARWIN64/EngSketchPad/lib/libuvmap.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a
clang -g  -o ./uvmap.exe ./uvmap.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -luvmap -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegads.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegads.dylib
(cd .; clang -g  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o   egadsSplineFit.o egadsSkinning.o egadsTessSens.o  BRepLib_FuseEdges.o  \
		egadsBase.o egadsMemory.o egadsAttrs.o  egadsTess.o   egadsTessInp.o egadsTris.o egadsQuads.o  egadsFit.o    egadsRobust.o egadsSBO.o prmCfit.o   prmGrid.o     prmUV.o       egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/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 1.0.26 )
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a
cp /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a
(cd .; \
		ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o  egadsTess.o   egadsTessInp.o egadsTris.o egadsQuads.o  egadsFit.o    egadsRobust.o egadsSBO.o prmCfit.o   prmGrid.o     prmUV.o       egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o   egadsSplineFit.o egadsSkinning.o egadsTessSens.o  BRepLib_FuseEdges.o  emp.o \
		evaluate.o rational.o regQuads.o;  )
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7  -I../include fgadsBase.c -o ./fgadsBase.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7  -I../include fgadsMemory.c -o ./fgadsMemory.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7  -I../include fgadsAttrs.c -o ./fgadsAttrs.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7  -I../include fgadsTess.c -o ./fgadsTess.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7  -I../include fgadsHLevel.c -o ./fgadsHLevel.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7  -I../include fgadsGeom.c -o ./fgadsGeom.o
clang -g  -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/DARWIN64/EngSketchPad/lib/libfgads.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o  fgadsTess.o   fgadsHLevel.o fgadsGeom.o fgadsTopo.o;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a emp.o;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a
 *** EGADS Build Complete! ***
(cd EGADS/lite; make)
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
		liteBase.c -o ./liteBase.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
		liteMemory.c -o ./liteMemory.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
		liteGeom.c -o ./liteGeom.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
		liteTopo.c -o ./liteTopo.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
		liteAttrs.c -o ./liteAttrs.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
		liteImport.c -o ./liteImport.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
		liteString.c -o ./liteString.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
                ../src/egadsTess.c -o ./liteTess.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
                ../src/egadsTris.c -o ./liteTris.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src \
                ../src/egadsQuads.c -o ./liteQuads.o
clang -g  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 ../src/egadsRobust.c \
		-o ./egadsRobust.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DDARWIN64 -I../include ../util/emp.c \
		-o ./emp.o
clang -g  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE ../util/rational.c \
		-o ./ratLite.o
clang -g  -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  -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  -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/DARWIN64/EngSketchPad/lib/libegadslite.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslite.dylib
(cd .; clang -g  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslite.dylib \
                liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \
		egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \
		liteEffect.o liteUVmap.o \
		-install_name '@rpath/libegadslite.dylib' \
                -current_version 1.0.26 )
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
                liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
		emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
		liteUVmap.o ;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a
(cd wvServer; make)
clang++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 map.cpp -o ./map.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include base64-decode.c -o ./base64-decode.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include handshake.c -o ./handshake.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include client-handshake.c -o ./client-handshake.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include md5.c -o ./md5.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include parsers.c -o ./parsers.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include extension.c -o ./extension.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include sha-1.c -o ./sha-1.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include server.c -o ./server.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include wv.c -o ./wv.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include browserMessage.c -o ./browserMessage.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fwv.c -o ./fwv.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
		./fwv.o;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \
		-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -o ./servertest.o
clang++ -g  -o ./server ./servertest.o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a  \
		-lpthread -lz -lm
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.dylib
(cd .; clang++ -g  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.dylib \
		base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \
		-install_name '@rpath/libwsserver.dylib' \
		-compatibility_version 7.7 \
		-current_version 1.0.26 )
(cd EGADS/examples; make -f egads2cart.make)
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include egads2cart.c \
		-o ./egads2cart.o
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vCurvature ./vCurvature.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd EGADS/examples; make -f vGeom.make)
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vGeom.c -o ./vGeom.o
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vGeom ./vGeom.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd EGADS/examples; make -f vTess.make)
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vTess.c -o ./vTess.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include ../util/retessFaces.c \
		-o ./retessFaces.o
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd OpenCSM; make)
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udp.c -o ./udp.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libocsm.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libocsm.dylib
clang -g  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libocsm.dylib ./OpenCSM.o ./udp.o ./tim.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.26 -current_version 1.0.26
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveESP ./serveESP.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
clang -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bezier.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bezier.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/biconvex.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/biconvex.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/box.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/box.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/box.so ./udpBox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bspline.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bspline.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/catmull.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/catmull.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/compare.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/compare.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/compare.so ./udfCompare.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createBEM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createBEM.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createPoly.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createPoly.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/csm.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/csm.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/csm.so ./udpCsm.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/deform.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/deform.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/deform.so ./udfDeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/droop.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/droop.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/droop.so ./udfDroop.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/dumpPmtrs.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/dumpPmtrs.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/editAttr.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/editAttr.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ellipse.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ellipse.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/eqn2body.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/eqn2body.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fitcurve.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fitcurve.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flend.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flend.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flend.so ./udfFlend.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/freeform.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/freeform.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ganged.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ganged.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/guide.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/guide.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/guide.so ./udfGuide.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hex.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hex.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hex.so ./udpHex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/import.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/import.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/import.so ./udpImport.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/kulfan.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/kulfan.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/linalg.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/linalg.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/matchBodys.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/matchBodys.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mechanism.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mechanism.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca.so ./udpNaca.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca6mc.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca6mc.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nacelle.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nacelle.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nurbbody.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nurbbody.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nuscale.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nuscale.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/offset.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/offset.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/offset.so ./udfOffset.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parabaloid.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parabaloid.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parsec.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parsec.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pod.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pod.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pod.so ./udpPod.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/poly.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/poly.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/poly.so ./udpPoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBbox.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBbox.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBrep.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBrep.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printEgo.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printEgo.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/prop.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/prop.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/prop.so ./udpProp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/radwaf.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/radwaf.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sample.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sample.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sample.so ./udpSample.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sew.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sew.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sew.so ./udpSew.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/shadow.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/shadow.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slices.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slices.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slices.so ./udfSlices.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stag.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stag.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stag.so ./udpStag.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stiffener.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stiffener.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/supell.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/supell.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/supell.so ./udpSupell.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester1.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester1.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester2.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester2.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vsp3.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vsp3.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/waffle.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/waffle.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfWarp.c -o ./udfWarp.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/warp.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/warp.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/warp.so ./udfWarp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/PDT2.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/PDT2.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g  -c -O -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca456.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca456.so
gfortran -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm -Wl,-w
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ereped.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ereped.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ereped.so ./timEreped.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mitten.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mitten.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mitten.so ./timMitten.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plotter.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plotter.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plugs.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slugs.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vspSetup.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vspSetup.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/OpenCSM.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/OpenCSM.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/common.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/common.h
cp -p common.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/common.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udp.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udp.h
cp -p udp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udp.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/esp.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/esp.h
cp -p esp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/esp.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/tim.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/tim.h
cp -p tim.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/tim.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egg.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egg.h
cp -p egg.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egg.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.c
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.c
(cd Slugs; make)
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. Fitter.c \
		-o ./Fitter.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. RedBlackTree.c \
		-o ./RedBlackTree.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. Tessellate.c \
		-o ./Tessellate.o
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
		./Tessellate.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads \
		-lpthread -lz -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads \
		-lpthread -lz -lm
(cd CAPS; make)
/bin/cp Cart3D/OSX64_CLANG/libc3dio.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/OSX64_CLANG/libCart3D.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/DARWIN64/avl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/avl
/bin/cp Executables/DARWIN64/pplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/pplot
/bin/cp Executables/DARWIN64/pxplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/pxplot
/bin/cp Executables/DARWIN64/xfoil /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/xfoil
/bin/cp Executables/DARWIN64/mastros.exe /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/DARWIN64/ASTRO.D01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/DARWIN64/ASTRO.IDX /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/DARWIN64/mses /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/mses
/bin/cp Executables/DARWIN64/mset /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/mset
/bin/cp udunits/include/*.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include
/bin/cp udunits/DARWIN64/libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib
/bin/ln -sf libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libudunits2.dylib
/bin/cp Libraries/DARWIN64/aflr2AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/DARWIN64/aflr3AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/DARWIN64/aflr4AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/aflr4AIM.so
(cd CAPS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/caps.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/caps.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimUtil.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimUtil.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimMesh.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimMesh.h
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../include \
		-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include \
		-I/usr/include/udunits2 aimTransferUtil.c \
		-o ./aimTransferUtil.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../include \
		aimMesh.c -o ./aimMesh.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a
ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
		./aimTransferUtil.o 
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcaps.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcaps.dylib
(cd .; clang -g  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcaps.dylib capsBase.o   capsAnalysis.o capsApprox.o capsAttr.o  capsAIM.o capsBound.o  capsProblem.o  capsValue.o  capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o  printObject.o \
			-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
			-install_name '@rpath/libcaps.dylib' \
			-compatibility_version 1.0.26 \
			-current_version 1.0.26 )
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a capsBase.o   capsAnalysis.o capsApprox.o capsAttr.o  capsAIM.o capsBound.o  capsProblem.o  capsValue.o  capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o  printObject.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include testingAIM.c \
		-o ./testingAIM.o
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so
rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include testingWriter.c \
		-o ./testingWriter.o
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so
rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include phaseUtil.c \
		-o ./phaseUtil.o
clang -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
	-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -g  -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include avlTest.c -o ./avlTest.o
clang -g  -o ./avlTest ./avlTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
clang -g  -o ./awaveTest ./awaveTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
clang -g  -o ./frictionTest ./frictionTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
clang -g  -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
	-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
clang -g  -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
	-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
clang -g  -o ./aeroelasticTest ./aeroelasticTest.o \
	-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmTest.c -o ./hsmTest.o   
clang -g  -o ./hsmTest ./hsmTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o  
clang -g  -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o  
clang -g  -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o  
clang -g  -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include interferenceTest.c \
		-o ./interferenceTest.o   
clang -g  -o ./interferenceTest ./interferenceTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include msesTest.c -o ./msesTest.o
clang -g  -o ./msesTest ./msesTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include mystranTest.c -o ./mystranTest.o   
clang -g  -o ./mystranTest ./mystranTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
clang -g  -o ./pointwiseTest ./pointwiseTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/lib/libutils.a
/Library/Developer/CommandLineTools/usr/bin/ranlib: file: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a(attrUtils.o) has no symbols
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils
cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cardUtils.h
cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/vlmUtils.h
/Library/Developer/CommandLineTools/usr/bin/make -C abaqus 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \
		abaqusAIM.c -o ./abaqusAIM.o
clang -g  -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/DARWIN64/EngSketchPad/include -I../utils \
		abaqusUtils.c -o ./abaqusUtils.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils astrosAIM.c \
		-o ./astrosAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils astrosUtils.c \
		-o ./astrosUtils.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils astrosCards.c \
        -o ./astrosCards.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o  ./astrosUtils.o ./astrosCards.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/avlAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/avlAIM.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_CPOML.o ./avlRead_DERMATB.o ./avlRead_DERMATM.o ./avlRead_DERMATS.o ./avlRead_ELE.o ./avlRead_HINGE.o ./avlRead_STRP.o ./avlRead_SURF.o ./avlRead_TOT.o ./avlRead_VM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
		-lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils awaveAIM.c \
		-o ./awaveAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cart3d 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \
		cart3dAIM.c -o ./cart3dAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/c3dio \
		-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \
		writeTrix.c -o ./writeTrix.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/c3dio \
		-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/libCart3D \
		surfTrix.c -o ./surfTrix.o
clang -g  -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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include bodyTess.c -o ./bodyTess.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \
		./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils \
		-laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/ \
		-lc3dio -lCart3D -ldl -lxml2 -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include cart3dTest.c \
		-o ./cart3dTest.o
clang -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/cart3dTest ./cart3dTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I./xddm \
		-I. `xml2-config --cflags` ESPxddm.c -o ./ESPxddm.o
clang -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \
		./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/ -lc3dio -lCart3D \
		-lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lxml2 -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cbaero 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
clang -g  -bundle cbaeroAIM.o -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C cgt 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include egads2cgt.c \
		-o ./egads2cgt.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include aflr4egads.c \
		-o ./aflr4egads.o
clang++ -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils delaundoAIM.c \
		-o ./delaundoAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/delaundoAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/delaundoAIM.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils egadsTessAIM.c \
		-o ./egadsTessAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/egadsTessAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/egadsTessAIM.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -Wno-format -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils frictionAIM.c \
		-o ./frictionAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g  -c -O -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/friction ./friction.o -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C fun3d 
clang -g  -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/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
		fun3dUtils.c -o ./fun3dUtils.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
		-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
		./fun3dNamelist.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hsmAIM.c \
		-o src/hsmAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hsmUtils.c \
		-o src/hsmUtils.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hsmAdj.c \
		-o src/hsmAdj.o
clang++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.7 \
		-o src/rcm.o
clang++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 rcm/genrcmi.cpp -DREVISION=7.7 \
		-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/DARWIN64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hsmAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hsmAIM.so
gfortran -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hsmAIM.so \
		src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
		src/rcm.o src/genrcmi.o \
		 -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \
		-legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C interference 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include interferenceAIM.c \
		-o ./interferenceAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. cloudFns.c \
		-o ./cloudFns.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/interferenceAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/interferenceAIM.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/interferenceAIM.so \
		./interferenceAIM.o ./cloudFns.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib \
		-laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils masstranAIM.cpp \
		-o ./masstranAIM.o
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C meshWriter 
/Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include bstlWriter.c \
		-o ./bstlWriter.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include bvtkWriter.c \
		-o ./bvtkWriter.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -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/DARWIN64/EngSketchPad/include -I/Users/jenkins/util/sandialabs/seacas/include -I. exodusWriter.cpp \
		-o ./exodusWriter.o
clang++ -g  -bundle -std=c++11 -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fastWriter.c \
		-o ./fastWriter.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include libmeshbWriter.c \
		-o ./libmeshbWriter.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7  -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
		-o ./libmeshb7.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include stlWriter.c \
		-o ./stlWriter.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include su2Writer.c \
		-o ./su2Writer.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include tecplotWriter.c \
		-o ./tecplotWriter.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include ugridWriter.c \
		-o ./ugridWriter.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vtkWriter.c \
		-o ./vtkWriter.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mystran 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils mystranAIM.c \
		-o ./mystranAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils mystranUtils.c \
		-o ./mystranUtils.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils nastranAIM.c \
		-o ./nastranAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils  -I/Users/jenkins/util/sandialabs/seacas/include -I. platoAIM.c \
		-o ./platoAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/platoAIM.so ./platoAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils pointwiseAIM.c \
		-o ./pointwiseAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hashElement.c \
		-o ./hashElement.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pointwiseAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pointwiseAIM.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
		-o ./refineAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 \
		-I../meshWriter/libmeshbWriter/libMeshb/sources \
		../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
		-o ./libmeshb7.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/refineAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/refineAIM.so
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils  -I/Users/jenkins/util/sandialabs/seacas/include -I. sierraSDAIM.c \
		-o ./sierraSDAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sierraSDAIM.so ./sierraSDAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils  -I/Users/jenkins/util/sandialabs/seacas/include -I. sierraSMAIM.c \
		-o ./sierraSMAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sierraSMAIM.so ./sierraSMAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils skeletonAIM.c \
		-o ./skeletonAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C spinnaker 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include \
		-I../meshWriter/exodusWriter \
		-I../meshWriter/libmeshbWriter \
		-I../utils -I/Users/jenkins/util/sandialabs/seacas/include \
		-I. \
		spinnakerAIM.c \
		-o ./spinnakerAIM.o
clang -g  -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  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/spinnakerAIM.so ./spinnakerAIM.o ./libmeshb7.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
		-o ./su2AIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2Utils.c \
		-o ./su2Utils.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_4_Cardinal.c \
		-o ./su2_4_Cardinal.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_5_Raven.c \
		-o ./su2_5_Raven.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_6_Falcon.c \
		-o ./su2_6_Falcon.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_7_Blackbird.c \
		-o ./su2_7_Blackbird.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_801_Harrier.c \
		-o ./su2_801_Harrier.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tacs 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils tacsAIM.c \
		-o ./tacsAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils tetgenAIM.cpp \
		-o ./tetgenAIM.o
clang++ -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
		-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
clang++ -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
clang++ -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
		./tetgen_Interface.o ./tetgen.o \
		./predicates.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \
		-legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \
		tsfoilAIM.c -o ./tsfoilAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C unitTest 
make[2]: Nothing to be done for `all'.
/Library/Developer/CommandLineTools/usr/bin/make -C xfoil 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \
		xfoilAIM.c -o ./xfoilAIM.o
clang -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C zaero 
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
clang -g  -bundle  -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
(cd OpenCSM; make -f serveESP.make)
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/capsMode.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flowchart.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/viewer.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/viewer.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/viewer.so ./timViewer.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/lib/pyscript.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pyscript.so
clang++ -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin
++ uname -a
+ [[ Darwin macys.mit.edu 22.6.0 Darwin Kernel Version 22.6.0: Tue Nov  7 21:48:06 PST 2023; root:xnu-8796.141.3.702.9~2/RELEASE_X86_64 x86_64 == *\D\a\r\w\i\n* ]]
+ sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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	0m3.019s
user	0m0.141s
sys	0m0.026s
+ set +x

=============================================
ESP verification case 01 passed (as expected)
=============================================

+ expectSuccess 02 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m1.905s
user	0m0.370s
sys	0m0.062s
+ set +x

=============================================
ESP verification case 02 passed (as expected)
=============================================

+ expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/verify_7.7.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m2.798s
user	0m3.566s
sys	0m0.739s
+ set +x

=============================================
ESP verification case 03 passed (as expected)
=============================================

+ expectSuccess 04 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.730s
user	0m0.707s
sys	0m0.054s
+ set +x

=============================================
ESP verification case 04 passed (as expected)
=============================================

+ expectSuccess 05 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.681s
user	0m0.736s
sys	0m0.064s
+ set +x

=============================================
ESP verification case 05 passed (as expected)
=============================================

+ expectSuccess 06 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/verify_7.7.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.618s
user	0m0.745s
sys	0m0.050s
+ set +x

=============================================
ESP verification case 06 passed (as expected)
=============================================

+ expectSuccess 07 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/verify_7.7.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m3.796s
user	0m5.938s
sys	0m0.686s
+ set +x

=============================================
ESP verification case 07 passed (as expected)
=============================================

+ expectSuccess 08 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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	0m24.391s
user	0m41.800s
sys	0m2.391s
+ set +x

=============================================
ESP verification case 08 passed (as expected)
=============================================

+ expectSuccess 09 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/verify_7.7.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.579s
user	0m0.693s
sys	0m0.029s
+ set +x

=============================================
ESP verification case 09 passed (as expected)
=============================================

+ expectSuccess 10 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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	0m32.127s
user	1m22.275s
sys	0m14.180s
+ set +x

=============================================
ESP verification case 10 passed (as expected)
=============================================

+ expectSuccess 11 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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	0m0.390s
user	0m0.295s
sys	0m0.038s
+ set +x

=============================================
ESP verification case 11 passed (as expected)
=============================================

+ expectSuccess 12 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.598s
user	0m0.749s
sys	0m0.018s
+ set +x

=============================================
ESP verification case 12 passed (as expected)
=============================================

+ expectSuccess 13 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.281s
user	0m0.236s
sys	0m0.013s
+ set +x

=============================================
ESP verification case 13 passed (as expected)
=============================================

+ expectSuccess 14 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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	0m0.497s
user	0m0.442s
sys	0m0.021s
+ set +x

=============================================
ESP verification case 14 passed (as expected)
=============================================

+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 1.855s

OK
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp

real	0m5.289s
user	0m8.145s
sys	0m0.199s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 23.057s

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/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
python -u -m unittest discover --verbose
test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.027   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.064   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
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          =     0.026   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4122      6020
AFLR2 GG : Nodes, Faces      =      5812      9400
AFLR2 GG : Nodes, Faces      =      7299     12374
AFLR2 GG : Nodes, Faces      =      8574     14924
AFLR2 GG : Nodes, Faces      =      9729     17234
AFLR2 GG : Nodes, Faces      =     10787     19350
AFLR2 GG : Nodes, Faces      =     11767     21310
AFLR2 GG : Nodes, Faces      =     12683     23142
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     14278     26332
AFLR2 GG : Nodes, Faces      =     14999     27774
AFLR2 GG : Nodes, Faces      =     15682     29140
AFLR2 GG : Nodes, Faces      =     16312     30400
AFLR2 GG : Nodes, Faces      =     16899     31574
AFLR2 GG : Nodes, Faces      =     17451     32678
AFLR2 GG : Nodes, Faces      =     17959     33694
AFLR2 GG : Nodes, Faces      =     18443     34662
AFLR2 GG : Nodes, Faces      =     18877     35530
AFLR2 GG : Nodes, Faces      =     19283     36342
AFLR2 GG : Nodes, Faces      =     19650     37076
AFLR2 GG : Nodes, Faces      =     19994     37764
AFLR2 GG : Nodes, Faces      =     20325     38426
AFLR2 GG : Nodes, Faces      =     20638     39052
AFLR2 GG : Nodes, Faces      =     20940     39656
AFLR2 GG : Nodes, Faces      =     21240     40256
AFLR2 GG : Nodes, Faces      =     21523     40822
AFLR2 GG : Nodes, Faces      =     21792     41360
AFLR2 GG : Nodes, Faces      =     22053     41882
AFLR2 GG : Nodes, Faces      =     22305     42386
AFLR2 GG : Nodes, Faces      =     22521     42818
AFLR2 GG : Nodes, Faces      =     22696     43168
AFLR2 GG : Nodes, Faces      =     22829     43434
AFLR2 GG : Nodes, Faces      =     22953     43682
AFLR2 GG : Nodes, Faces      =     23050     43876
AFLR2 GG : Nodes, Faces      =     23110     43996
AFLR2 GG : Nodes, Faces      =     23139     44054
AFLR2 GG : Nodes, Faces      =     23157     44090
AFLR2 GG : Nodes, Faces      =     23175     44126
AFLR2 GG : Nodes, Faces      =     23183     44142
AFLR2 GG : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.057   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.006   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.029   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.072   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.008   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2224      2224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       446       894
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =       918      1838
AFLR2 IG : Nodes, Faces      =      1033      2068
AFLR2 IG : Nodes, Faces      =      1133      2268
AFLR2 IG : Nodes, Faces      =      1233      2468
AFLR2 IG : Nodes, Faces      =      1333      2668
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1433      2868
AFLR2 IG : Nodes, Faces      =      1533      3068
AFLR2 IG : Nodes, Faces      =      1633      3268
AFLR2 IG : Nodes, Faces      =      1733      3468
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1833      3668
AFLR2 IG : Nodes, Faces      =      1858      3718
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.029   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4122      6020
AFLR2 GG : Nodes, Faces      =      5812      9400
AFLR2 GG : Nodes, Faces      =      7299     12374
AFLR2 GG : Nodes, Faces      =      8574     14924
AFLR2 GG : Nodes, Faces      =      9729     17234
AFLR2 GG : Nodes, Faces      =     10787     19350
AFLR2 GG : Nodes, Faces      =     11767     21310
AFLR2 GG : Nodes, Faces      =     12683     23142
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     14278     26332
AFLR2 GG : Nodes, Faces      =     14999     27774
AFLR2 GG : Nodes, Faces      =     15682     29140
AFLR2 GG : Nodes, Faces      =     16312     30400
AFLR2 GG : Nodes, Faces      =     16899     31574
AFLR2 GG : Nodes, Faces      =     17451     32678
AFLR2 GG : Nodes, Faces      =     17959     33694
AFLR2 GG : Nodes, Faces      =     18443     34662
AFLR2 GG : Nodes, Faces      =     18877     35530
AFLR2 GG : Nodes, Faces      =     19283     36342
AFLR2 GG : Nodes, Faces      =     19650     37076
AFLR2 GG : Nodes, Faces      =     19994     37764
AFLR2 GG : Nodes, Faces      =     20325     38426
AFLR2 GG : Nodes, Faces      =     20638     39052
AFLR2 GG : Nodes, Faces      =     20940     39656
AFLR2 GG : Nodes, Faces      =     21240     40256
AFLR2 GG : Nodes, Faces      =     21523     40822
AFLR2 GG : Nodes, Faces      =     21792     41360
AFLR2 GG : Nodes, Faces      =     22053     41882
AFLR2 GG : Nodes, Faces      =     22305     42386
AFLR2 GG : Nodes, Faces      =     22521     42818
AFLR2 GG : Nodes, Faces      =     22696     43168
AFLR2 GG : Nodes, Faces      =     22829     43434
AFLR2 GG : Nodes, Faces      =     22953     43682
AFLR2 GG : Nodes, Faces      =     23050     43876
AFLR2 GG : Nodes, Faces      =     23110     43996
AFLR2 GG : Nodes, Faces      =     23139     44054
AFLR2 GG : Nodes, Faces      =     23157     44090
AFLR2 GG : Nodes, Faces      =     23175     44126
AFLR2 GG : Nodes, Faces      =     23183     44142
AFLR2 GG : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.071   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
ok
test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.025   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.061   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.005   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =        48         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        10        22
AFLR2 IG : Nodes, Faces      =        20        42
AFLR2 IG : Nodes, Faces      =        30        62
AFLR2 IG : Nodes, Faces      =        40        82
AFLR2 IG : Nodes, Faces      =        45        92
AFLR2 IG : Nodes, Faces      =        46        94
AFLR2 IG : Nodes, Faces      =        48        98
AFLR2 IG : Nodes, Faces      =        52        98
AFLR2 IG : Nodes, Faces      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =        48        48
AFLR2 GG : Nodes, Faces      =        88       128
AFLR2 GG : Nodes, Faces      =       109       170
AFLR2 GG : Nodes, Faces      =       124       200
AFLR2 GG : Nodes, Faces      =       136       224
AFLR2 GG : Nodes, Faces      =       148       248
AFLR2 GG : Nodes, Faces      =       161       274
AFLR2 GG : Nodes, Faces      =       171       294
AFLR2 GG : Nodes, Faces      =       181       314
AFLR2 GG : Nodes, Faces      =       187       326
AFLR2 GG : Nodes, Faces      =       190       332
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       190       332
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =       344       344
AFLR2 GG : Nodes, Faces      =       679      1014
AFLR2 GG : Nodes, Faces      =      1006      1668
AFLR2 GG : Nodes, Faces      =      1321      2298
AFLR2 GG : Nodes, Faces      =      1604      2864
AFLR2 GG : Nodes, Faces      =      1886      3428
AFLR2 GG : Nodes, Faces      =      2155      3966
AFLR2 GG : Nodes, Faces      =      2409      4474
AFLR2 GG : Nodes, Faces      =      2649      4954
AFLR2 GG : Nodes, Faces      =      2867      5390
AFLR2 GG : Nodes, Faces      =      3063      5782
AFLR2 GG : Nodes, Faces      =      3243      6142
AFLR2 GG : Nodes, Faces      =      3400      6456
AFLR2 GG : Nodes, Faces      =      3540      6736
AFLR2 GG : Nodes, Faces      =      3665      6986
AFLR2 GG : Nodes, Faces      =      3786      7228
AFLR2 GG : Nodes, Faces      =      3900      7456
AFLR2 GG : Nodes, Faces      =      4010      7676
AFLR2 GG : Nodes, Faces      =      4114      7884
AFLR2 GG : Nodes, Faces      =      4209      8074
AFLR2 GG : Nodes, Faces      =      4292      8240
AFLR2 GG : Nodes, Faces      =      4368      8392
AFLR2 GG : Nodes, Faces      =      4439      8534
AFLR2 GG : Nodes, Faces      =      4503      8662
AFLR2 GG : Nodes, Faces      =      4560      8776
AFLR2 GG : Nodes, Faces      =      4611      8878
AFLR2 GG : Nodes, Faces      =      4650      8956
AFLR2 GG : Nodes, Faces      =      4677      9010
AFLR2 GG : Nodes, Faces      =      4695      9046
AFLR2 GG : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.008   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          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.010   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.007   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 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.011   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.007   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:62511)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1189
	Number of elements       = 6249
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4917
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 6353
	Number of elements       = 35297
	Number of triangles      = 4430
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 30867
	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          = 13586
	Number of elements       = 76197
	Number of triangles      = 8142
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 68055
	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          = 42291
	Number of elements       = 240392
	Number of triangles      = 19942
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 220450
	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          = 4366
	Number of elements       = 24242
	Number of triangles      = 3014
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 21228
	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          = 11036
	Number of elements       = 60950
	Number of triangles      = 8628
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52322
	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          = 10730
	Number of elements       = 60223
	Number of triangles      = 6362
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 53861
	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          = 89551
	Number of elements       = 503550
	Number of triangles      = 51850
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 451700
	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:62511)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 16462
	Number of elements       = 93692
	Number of triangles      = 7926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 85766
	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          = 2589
	Number of elements       = 13809
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11051
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3651
	Number of elements       = 19783
	Number of triangles      = 3394
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 16389
	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          = 5487
	Number of elements       = 30509
	Number of triangles      = 3656
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26853
	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          = 4694
	Number of elements       = 25935
	Number of triangles      = 3326
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22609
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5554
	Number of elements       = 30862
	Number of triangles      = 3756
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 27106
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2260
	Number of elements       = 12133
	Number of triangles      = 2222
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9911
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 2392
	Number of elements       = 12577
	Number of triangles      = 2666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9911
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3341
	Number of elements       = 18069
	Number of triangles      = 3110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 3606
	Number of elements       = 18961
	Number of triangles      = 4002
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4414
	Number of elements       = 23974
	Number of triangles      = 3998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19976
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 4811
	Number of elements       = 25310
	Number of triangles      = 5334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19976
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5490
	Number of elements       = 29891
	Number of triangles      = 4886
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25005
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 6019
	Number of elements       = 31671
	Number of triangles      = 6666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25005
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6542
	Number of elements       = 35667
	Number of triangles      = 5774
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29893
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 7203
	Number of elements       = 37891
	Number of triangles      = 7998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29893
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 7601
	Number of elements       = 41489
	Number of triangles      = 6662
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 8394
	Number of elements       = 44157
	Number of triangles      = 9330
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1191
	Number of elements       = 6266
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4934
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 19800
	Number of elements       = 109798
	Number of triangles      = 15540
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 22741
	Number of elements       = 119570
	Number of triangles      = 25312
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1191
	Number of elements       = 6266
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4934
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1193
	Number of elements       = 6272
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4940
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1176
	Number of elements       = 6165
	Number of triangles      = 1330
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4835
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1203
	Number of elements       = 6314
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4982
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1192
	Number of elements       = 6269
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4937
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1192
	Number of elements       = 6269
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4937
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1198
	Number of elements       = 6296
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4964
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1223
	Number of elements       = 6443
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5111
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1184
	Number of elements       = 6224
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4892
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1195
	Number of elements       = 6287
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4955
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1197
	Number of elements       = 6311
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4979
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1203
	Number of elements       = 6310
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4978
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1191
	Number of elements       = 6253
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4921
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8857
	Number of elements       = 49191
	Number of triangles      = 6284
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42907
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 8989
	Number of elements       = 49635
	Number of triangles      = 6728
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42907
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 7796
	Number of elements       = 43368
	Number of triangles      = 5396
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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       = 6267
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4935
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9944
	Number of elements       = 55193
	Number of triangles      = 7174
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 48019
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 10218
	Number of elements       = 56081
	Number of triangles      = 8062
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 48019
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 7818
	Number of elements       = 43469
	Number of triangles      = 5398
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 38071
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1202
	Number of elements       = 6320
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4988
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1198
	Number of elements       = 6292
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4960
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9609
	Number of elements       = 53228
	Number of triangles      = 6994
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46234
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 9829
	Number of elements       = 53956
	Number of triangles      = 7722
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46234
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 7789
	Number of elements       = 43295
	Number of triangles      = 5394
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37901
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1186
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 854
	Number of elements       = 4431
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3435
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9348
	Number of elements       = 51734
	Number of triangles      = 6812
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44922
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 9531
	Number of elements       = 52330
	Number of triangles      = 7408
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44922
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 7804
	Number of elements       = 43358
	Number of triangles      = 5386
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1200
	Number of elements       = 6311
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4979
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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       = 2661
	Number of triangles      = 690
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9183
	Number of elements       = 50871
	Number of triangles      = 6632
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44239
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 9322
	Number of elements       = 51307
	Number of triangles      = 7068
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44239
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 7927
	Number of elements       = 44116
	Number of triangles      = 5382
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 38734
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 868
	Number of elements       = 4530
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3534
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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       = 2661
	Number of triangles      = 690
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10181
	Number of elements       = 56797
	Number of triangles      = 6782
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 50015
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 10671
	Number of elements       = 58561
	Number of triangles      = 8546
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 50015
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 7741
	Number of elements       = 43010
	Number of triangles      = 5362
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37648
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 2692
	Number of elements       = 14435
	Number of triangles      = 2800
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11635
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 238
	Number of elements       = 1116
	Number of triangles      = 384
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 732
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1500
	Number of elements       = 7757
	Number of triangles      = 1986
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5771
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1564
	Number of elements       = 7881
	Number of triangles      = 2110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5771
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1160
	Number of elements       = 6087
	Number of triangles      = 1308
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4779
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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       = 1635
	Number of triangles      = 718
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 917
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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       = 159
	Number of triangles      = 84
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 75
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5087
	Number of elements       = 27862
	Number of triangles      = 4076
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23786
	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          = 5233
	Number of elements       = 28414
	Number of triangles      = 4628
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23786
	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          = 4894
	Number of elements       = 26891
	Number of triangles      = 4044
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22847
	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          = 339
	Number of elements       = 1523
	Number of triangles      = 584
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 939
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 33276
	Number of elements       = 192711
	Number of triangles      = 8496
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 184215
	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          = 36617
	Number of elements       = 206043
	Number of triangles      = 21828
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 184215
	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          = 29045
	Number of elements       = 165042
	Number of triangles      = 15162
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 149880
	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          = 1430
	Number of elements       = 7607
	Number of triangles      = 1456
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6151
	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          = 4174
	Number of elements       = 23119
	Number of triangles      = 2942
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20177
	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          = 711
	Number of elements       = 3685
	Number of triangles      = 844
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 2841
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 1257
	Number of elements       = 6590
	Number of triangles      = 1424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5166
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 17008
	Number of elements       = 96545
	Number of triangles      = 8794
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 87751
	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          = 18932
	Number of elements       = 103921
	Number of triangles      = 16170
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 87751
	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          = 12392
	Number of elements       = 69753
	Number of triangles      = 7134
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 62619
	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          = 6540
	Number of elements       = 34168
	Number of triangles      = 9036
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25132
	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          = 3013
	Number of elements       = 13107
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7655
	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          = 2470
	Number of elements       = 10756
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6204
	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          = 3013
	Number of elements       = 13107
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7655
	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          = 2470
	Number of elements       = 10756
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6204
	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          = 3013
	Number of elements       = 13107
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7655
	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          = 2470
	Number of elements       = 10756
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6204
	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          = 3013
	Number of elements       = 13107
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7655
	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 7655
	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          = 2470
	Number of elements       = 10756
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6204
	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 6204
	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          = 5047
	Number of elements       = 27987
	Number of triangles      = 3464
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24523
	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          = 6467
	Number of elements       = 36212
	Number of triangles      = 4048
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 32164
	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          = 60330
	Number of elements       = 351943
	Number of triangles      = 12928
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 339015
	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          = 59025
	Number of elements       = 343722
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 331294
	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          = 60330
	Number of elements       = 351443
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 339015
	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:62511)
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:62511)
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:62511)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
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:62511)
 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:62511)
 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:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 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:62511)
 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:62511)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
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:62511)
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 9126
	Block: 'cut_tri', blk_id 2, num_entries 1286
	Sideset: 'box', set_id 1, num_entries 9126
	Sideset: 'cut', set_id 2, num_entries 1286
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 16904
	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 16904
	Sideset: 'Spar1', set_id 4, num_entries 422
	Sideset: 'Spar2', set_id 5, num_entries 166
	Sideset: 'Skin_Top', set_id 6, num_entries 8555
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 IEEE_DENORMAL
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
ok
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - VTail1
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - VTail2
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
	Section 1 of 2 (ID = 0)
	Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 2)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 0)
	  Control surface 1 of 1 
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice control surface data
	VLM control surface name - Elevator
	VLM control surface name - LeftAileron
	VLM control surface name - RightAileron
	VLM control surface name - Rudder
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 2)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 0)
	  Control surface 1 of 1 
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... 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
   (23:22:00) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:22:02) 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
   (23:22:04) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:22:08) 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
   (23:22:11) Linearizing cut-cells
   (23:22:11) ... done
   o Number of simultaneous xsensit jobs:  1
   (23:22:12) Computing gradients
   (23:22:20) ... 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
   (23:22:24) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:22:30) 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
   (23:22:32) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:22:38) 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
   (23:22:41) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:22:45) 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
   (23:22:45) Linearizing cut-cells
   (23:22:45) ... done
   o Number of simultaneous xsensit jobs:  1
   (23:22:45) Computing gradients
   (23:22:54) ... 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
   (23:22:57) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:01) 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
   (23:23:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:04) 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
   (23:23:06) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:07) 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
   (23:23:08) Linearizing cut-cells
   (23:23:08) ... done
   o Number of simultaneous xsensit jobs:  1
   (23:23:08) Computing gradients
   (23:23:12) ... 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
   (23:23:13) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:15) 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
   (23:23:17) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:19) 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
   (23:23:21) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:23) 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
   (23:23:23) Linearizing cut-cells
   (23:23:23) ... done
   o Number of simultaneous xsensit jobs:  1
   (23:23:24) Computing gradients
   (23:23:28) ... 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
   (23:23:30) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:33) 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
   (23:23:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:36) 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
   (23:23:38) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:40) 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
   (23:23:40) Linearizing cut-cells
   (23:23:40) ... done
   o Number of simultaneous xsensit jobs:  1
   (23:23:40) Computing gradients
   (23:23:44) ... 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
   (23:23:46) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:48) 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
   (23:23:49) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:52) 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
   (23:23:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:23:55) 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
   (23:23:56) Linearizing cut-cells
   (23:23:56) ... done
   o Number of simultaneous xsensit jobs:  1
   (23:23:56) Computing gradients
   (23:24:00) ... 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
   (23:24:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:24:05) 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
   (23:24:06) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:24:09) 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
   (23:24:11) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:24:12) 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
   (23:24:13) Linearizing cut-cells
   (23:24:13) ... done
   o Number of simultaneous xsensit jobs:  1
   (23:24:13) Computing gradients
   (23:24:17) ... 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
   (23:24:19) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:24:22) 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
   (23:24:24) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:24:26) 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
   (23:24:28) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:24:40) 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
   (23:24:41) Linearizing cut-cells
   (23:24:41) ... done
   o Number of simultaneous xsensit jobs:  1
   (23:24:41) Computing gradients
   (23:24:45) ... 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
   (23:24:47) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:24:50) 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
   (23:24:54) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:24:56) 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
   (23:24:59) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:25:04) 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
   (23:25:05) Linearizing cut-cells
   (23:25:07) ... done
   o Number of simultaneous xsensit jobs:  2
   (23:25:07) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (23:25:15) ... 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
   (23:25:18) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (23:25:22) 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:62511)
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
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000EDFA000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 70000EDFA000 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
 70000EDFA000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 70000EDFA000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7FF8487D9780 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7FF8487D9780 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
 70000EDFA000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 70000EDFA000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7FF8487D9780 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7FF8487D9780 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
 70000EDFA000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 70000EDFA000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7FF8487D9780 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7FF8487D9780 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:62511)
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:62511)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
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:62511)
 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:62511)
 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:62511)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
 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:62511)
 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:62511)
 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:62511)
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:62511)
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:62511)
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 19154
	Sideset: 'Farfield', set_id 1, num_entries 48
	Sideset: 'Wing1', set_id 2, num_entries 19154
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 14302
	Sideset: 'Farfield', set_id 1, num_entries 12
	Sideset: 'Wing1', set_id 2, num_entries 14302
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    = 7819
Number of elements = 15634
Number of triangle elements      = 15634
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5889
Number of elements = 11774
Number of triangle elements      = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 516
Number of elements = 1028
Number of triangle elements      = 1028
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14224
Total number of elements = 28436
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 - 14224, elements - 28436
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.119935
Creating surface mesh ...
Surface mesh seconds:  0.019435
Recovering boundaries...
Boundary recovery seconds:  0.105525
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.037841
Recovering Delaunayness...
Delaunay recovery seconds:  0.050329
Refining mesh...
  18960 insertions, added 14017 points, 701008 tetrahedra in queue.
  6313 insertions, added 2494 points, 554976 tetrahedra in queue.
  8415 insertions, added 1753 points, 70 tetrahedra in queue.
Refinement seconds:  1.87613
Smoothing vertices...
Mesh smoothing seconds:  1.58372
Improving mesh...
Mesh improvement seconds:  0.038171

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.010447
Total running seconds:  3.84203

Statistics:

  Input points: 14224
  Input facets: 28436
  Input segments: 42654
  Input holes: 2
  Input regions: 0

  Mesh points: 33058
  Mesh tetrahedra: 159464
  Mesh faces: 333146
  Mesh faces on exterior boundary: 28436
  Mesh faces on input facets: 28436
  Mesh edges on input segments: 42654
  Steiner points inside domain: 18834

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    = 7819
Number of elements = 15634
Number of triangle elements      = 15634
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5889
Number of elements = 11774
Number of triangle elements      = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 516
Number of elements = 1028
Number of triangle elements      = 1028
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14224
Total number of elements = 28436
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 - 14224, elements - 28436
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.16624
Creating surface mesh ...
Surface mesh seconds:  0.039286
Recovering boundaries...
Boundary recovery seconds:  0.130428
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.057268
Recovering Delaunayness...
Delaunay recovery seconds:  0.064644
Refining mesh...
  18960 insertions, added 14017 points, 701008 tetrahedra in queue.
  6313 insertions, added 2494 points, 554976 tetrahedra in queue.
  8415 insertions, added 1753 points, 70 tetrahedra in queue.
Refinement seconds:  2.21153
Smoothing vertices...
Mesh smoothing seconds:  2.19395
Improving mesh...
Mesh improvement seconds:  0.052119

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.017455
Total running seconds:  4.93353

Statistics:

  Input points: 14224
  Input facets: 28436
  Input segments: 42654
  Input holes: 2
  Input regions: 0

  Mesh points: 33058
  Mesh tetrahedra: 159464
  Mesh faces: 333146
  Mesh faces on exterior boundary: 28436
  Mesh faces on input facets: 28436
  Mesh edges on input segments: 42654
  Steiner points inside domain: 18834

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/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml .....
	Appending namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok
test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found!
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

	Reading /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml .....
	Appending namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions
	Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - X
ok
test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 5071, elements - 10130
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 - 5071, elements - 10130
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 - 14224, elements - 28436
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - box2
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4009
	Number of elements = 8014
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8014
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6178
	Combined Number of elements = 12347
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12346
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4000
	Number of elements = 7996
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7996
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6169
	Combined Number of elements = 12329
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12328
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4009
	Number of elements = 8014
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8014
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6178
	Combined Number of elements = 12347
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12346
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4009
	Number of elements = 8014
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8014
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6178
	Combined Number of elements = 12347
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12346
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4000
	Number of elements = 7996
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7996
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6169
	Combined Number of elements = 12329
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12328
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4000
	Number of elements = 7996
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7996
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6169
	Combined Number of elements = 12329
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12328
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ... 
Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - alowervar
	Design Variable name - auppervar
	Design Variable name - classvar
	Design Variable name - ztailvar
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ... 
Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - avar
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ... 
Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ... 
Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - camber
	Design Variable name - thick
	Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ... 
Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =        54         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =        54        54
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        12        26
AFLR2 IG : Nodes, Faces      =        24        50
AFLR2 IG : Nodes, Faces      =        36        74
AFLR2 IG : Nodes, Faces      =        48        98
AFLR2 IG : Nodes, Faces      =        52       106
AFLR2 IG : Nodes, Faces      =        53       108
AFLR2 IG : Nodes, Faces      =        54       110
AFLR2 IG : Nodes, Faces      =        58       110
AFLR2 IG : Nodes, Faces      =        54        54
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =        54        54
AFLR2 GG : Nodes, Faces      =       100       146
AFLR2 GG : Nodes, Faces      =       122       190
AFLR2 GG : Nodes, Faces      =       138       222
AFLR2 GG : Nodes, Faces      =       153       252
AFLR2 GG : Nodes, Faces      =       168       282
AFLR2 GG : Nodes, Faces      =       180       306
AFLR2 GG : Nodes, Faces      =       192       330
AFLR2 GG : Nodes, Faces      =       201       348
AFLR2 GG : Nodes, Faces      =       210       366
AFLR2 GG : Nodes, Faces      =       216       378
AFLR2 GG : Nodes, Faces      =       221       388
AFLR2 GG : Nodes, Faces      =       224       394
AFLR2 GG : Nodes, Faces      =       225       396
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       225       396
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 225
Number of elements = 450
Number of tris = 396
Number of quad = 0

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing 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 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1607
	Number of elements       = 8784
	Number of triangles      = 1240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7544
	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       = 13864
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11106
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1056
	Number of elements       = 5616
	Number of triangles      = 998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4618
	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          = 16322
	Number of elements       = 93875
	Number of triangles      = 4632
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 89243
	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 89243
	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 106183
	Sideset: 'Farfield', set_id 1, num_entries 144
	Sideset: 'Wing1', set_id 2, num_entries 4244
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 165364
	Sideset: 'Farfield', set_id 1, num_entries 576
	Sideset: 'Wing1', set_id 2, num_entries 5830
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          = 1607
	Number of elements       = 8784
	Number of triangles      = 1240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7544
	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          = 438
	Number of elements       = 2179
	Number of triangles      = 644
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1535
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 936
	Number of elements       = 5016
	Number of triangles      = 758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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 22.6.0 x86_64
AFLR3    : Compile Date   11/01/23 @ 12:19PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6220         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                         Solid
UG3      :         12                         Solid
UG3      :         13                         Solid
UG3      :         14                         Solid
UG3      :         15                         Solid
UG3      :         16                         Solid
UG3      :         17                      FarField
UG3      :         18                      FarField
 
AFLR3    : CPU Time          =     0.028   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6220         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1246      7331
AFLR3 IG : Nodes, Elements   =      2492     16260
AFLR3 IG : Nodes, Elements   =      3738     25021
AFLR3 IG : Nodes, Elements   =      4984     34304
AFLR3 IG : Nodes, Elements   =      6227     43518
AFLR3 IG : Nodes, Elements   =      6227     43441
AFLR3 IG : Nodes, Elements   =      6227     43476
AFLR3 IG : Nodes, Elements   =      6227     43440
AFLR3 IG : Nodes, Elements   =      6220     26110
AFLR3 IG : Nodes, Elements   =      6220     26133
AFLR3 IG : Nodes, Elements   =      6220     21547
AFLR3 IG : Nodes, Elements   =      6220     19208
 
AFLR3    : CPU Time          =     0.263   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6220     19208
AFLR3 GG : Nodes, Elements   =      9100     28062
AFLR3 GG : Nodes, Elements   =      9100     39158
AFLR3 GG : Nodes, Elements   =      9100     36340
AFLR3 GG : Nodes, Elements   =      9100     34935
AFLR3 GG : Nodes, Elements   =     11679     42981
AFLR3 GG : Nodes, Elements   =     11679     54114
AFLR3 GG : Nodes, Elements   =     11679     50918
AFLR3 GG : Nodes, Elements   =     11679     50048
AFLR3 GG : Nodes, Elements   =     14497     58799
AFLR3 GG : Nodes, Elements   =     14497     70880
AFLR3 GG : Nodes, Elements   =     14497     67499
AFLR3 GG : Nodes, Elements   =     14497     66675
AFLR3 GG : Nodes, Elements   =     17509     75885
AFLR3 GG : Nodes, Elements   =     17509     88926
AFLR3 GG : Nodes, Elements   =     17509     85386
AFLR3 GG : Nodes, Elements   =     17509     84628
AFLR3 GG : Nodes, Elements   =     20720     94416
AFLR3 GG : Nodes, Elements   =     20720    107933
AFLR3 GG : Nodes, Elements   =     20720    104310
AFLR3 GG : Nodes, Elements   =     20720    103487
AFLR3 GG : Nodes, Elements   =     24052    113665
AFLR3 GG : Nodes, Elements   =     24052    127839
AFLR3 GG : Nodes, Elements   =     24052    124140
AFLR3 GG : Nodes, Elements   =     24052    123285
AFLR3 GG : Nodes, Elements   =     27535    133903
AFLR3 GG : Nodes, Elements   =     27535    148583
AFLR3 GG : Nodes, Elements   =     27535    144725
AFLR3 GG : Nodes, Elements   =     27535    143785
AFLR3 GG : Nodes, Elements   =     31083    154544
AFLR3 GG : Nodes, Elements   =     31083    169756
AFLR3 GG : Nodes, Elements   =     31083    165709
AFLR3 GG : Nodes, Elements   =     31083    164924
AFLR3 GG : Nodes, Elements   =     34686    175822
AFLR3 GG : Nodes, Elements   =     34686    191083
AFLR3 GG : Nodes, Elements   =     34686    187131
AFLR3 GG : Nodes, Elements   =     34686    186309
AFLR3 GG : Nodes, Elements   =     38391    197494
AFLR3 GG : Nodes, Elements   =     38391    212948
AFLR3 GG : Nodes, Elements   =     38391    209009
AFLR3 GG : Nodes, Elements   =     38391    208247
AFLR3 GG : Nodes, Elements   =     42024    219214
AFLR3 GG : Nodes, Elements   =     42024    234557
AFLR3 GG : Nodes, Elements   =     42024    230654
AFLR3 GG : Nodes, Elements   =     42024    229854
AFLR3 GG : Nodes, Elements   =     45519    240397
AFLR3 GG : Nodes, Elements   =     45519    255079
AFLR3 GG : Nodes, Elements   =     45519    251321
AFLR3 GG : Nodes, Elements   =     45519    250593
AFLR3 GG : Nodes, Elements   =     48877    260698
AFLR3 GG : Nodes, Elements   =     48877    274904
AFLR3 GG : Nodes, Elements   =     48877    271253
AFLR3 GG : Nodes, Elements   =     48877    270607
AFLR3 GG : Nodes, Elements   =     52099    280296
AFLR3 GG : Nodes, Elements   =     52099    293882
AFLR3 GG : Nodes, Elements   =     52099    290457
AFLR3 GG : Nodes, Elements   =     52099    289776
AFLR3 GG : Nodes, Elements   =     55205    299113
AFLR3 GG : Nodes, Elements   =     55205    312321
AFLR3 GG : Nodes, Elements   =     55205    308986
AFLR3 GG : Nodes, Elements   =     55205    308392
AFLR3 GG : Nodes, Elements   =     58210    317417
AFLR3 GG : Nodes, Elements   =     58210    330007
AFLR3 GG : Nodes, Elements   =     58210    326789
AFLR3 GG : Nodes, Elements   =     58210    326245
AFLR3 GG : Nodes, Elements   =     61058    334793
AFLR3 GG : Nodes, Elements   =     61058    346756
AFLR3 GG : Nodes, Elements   =     61058    343733
AFLR3 GG : Nodes, Elements   =     61058    343280
AFLR3 GG : Nodes, Elements   =     63783    351458
AFLR3 GG : Nodes, Elements   =     63783    362788
AFLR3 GG : Nodes, Elements   =     63783    360008
AFLR3 GG : Nodes, Elements   =     63783    359622
AFLR3 GG : Nodes, Elements   =     66330    367266
AFLR3 GG : Nodes, Elements   =     66330    377752
AFLR3 GG : Nodes, Elements   =     66330    375179
AFLR3 GG : Nodes, Elements   =     66330    374840
AFLR3 GG : Nodes, Elements   =     68498    381349
AFLR3 GG : Nodes, Elements   =     68498    390410
AFLR3 GG : Nodes, Elements   =     68498    388098
AFLR3 GG : Nodes, Elements   =     68498    387821
AFLR3 GG : Nodes, Elements   =     70270    393143
AFLR3 GG : Nodes, Elements   =     70270    400618
AFLR3 GG : Nodes, Elements   =     70270    398604
AFLR3 GG : Nodes, Elements   =     70270    398390
AFLR3 GG : Nodes, Elements   =     71687    402641
AFLR3 GG : Nodes, Elements   =     71687    408661
AFLR3 GG : Nodes, Elements   =     71687    407049
AFLR3 GG : Nodes, Elements   =     71687    406871
AFLR3 GG : Nodes, Elements   =     72770    410121
AFLR3 GG : Nodes, Elements   =     72770    414678
AFLR3 GG : Nodes, Elements   =     72770    413478
AFLR3 GG : Nodes, Elements   =     72770    413365
AFLR3 GG : Nodes, Elements   =     73527    415636
AFLR3 GG : Nodes, Elements   =     73527    418783
AFLR3 GG : Nodes, Elements   =     73527    417930
AFLR3 GG : Nodes, Elements   =     73527    417857
AFLR3 GG : Nodes, Elements   =     74058    419451
AFLR3 GG : Nodes, Elements   =     74058    421716
AFLR3 GG : Nodes, Elements   =     74058    421101
AFLR3 GG : Nodes, Elements   =     74058    421050
AFLR3 GG : Nodes, Elements   =     74384    422030
AFLR3 GG : Nodes, Elements   =     74384    423390
AFLR3 GG : Nodes, Elements   =     74384    423014
AFLR3 GG : Nodes, Elements   =     74384    422981
AFLR3 GG : Nodes, Elements   =     74556    423497
AFLR3 GG : Nodes, Elements   =     74556    424232
AFLR3 GG : Nodes, Elements   =     74556    424026
AFLR3 GG : Nodes, Elements   =     74556    424003
AFLR3 GG : Nodes, Elements   =     74649    424283
AFLR3 GG : Nodes, Elements   =     74649    424652
AFLR3 GG : Nodes, Elements   =     74649    424541
AFLR3 GG : Nodes, Elements   =     74649    424540
AFLR3 GG : Nodes, Elements   =     74680    424633
AFLR3 GG : Nodes, Elements   =     74680    424763
AFLR3 GG : Nodes, Elements   =     74680    424723
AFLR3 GG : Nodes, Elements   =     74680    424720
AFLR3 GG : Nodes, Elements   =     74687    424741
AFLR3 GG : Nodes, Elements   =     74687    424775
AFLR3 GG : Nodes, Elements   =     74687    424761
AFLR3 GG : Nodes, Elements   =     74687    424762
AFLR3 GG : Nodes, Elements   =     74688    424765
AFLR3 GG : Nodes, Elements   =     74688    424770
AFLR3 GG : Nodes, Elements   =     74688    424768
AFLR3 GG : Nodes, Elements   =     74689    424771
AFLR3 GG : Nodes, Elements   =     74689    424777
AFLR3 GG : Nodes, Elements   =     74689    424776
AFLR3 GG : Nodes, Elements   =     74689    424775
AFLR3 GG : Nodes, Elements   =     74715    424853
AFLR3 GG : Nodes, Elements   =     74715    424959
AFLR3 GG : Nodes, Elements   =     74715    424928
AFLR3 GG : Nodes, Elements   =     74715    424923
AFLR3 GG : Nodes, Elements   =     74723    424947
AFLR3 GG : Nodes, Elements   =     74723    424976
AFLR3 GG : Nodes, Elements   =     74723    424967
AFLR3 GG : Nodes, Elements   =     74723    424969
AFLR3 GG : Nodes, Elements   =     74726    424978
AFLR3 GG : Nodes, Elements   =     74726    424988
AFLR3 GG : Nodes, Elements   =     74726    424984
AFLR3 GG : Nodes, Elements   =     74731    424999
AFLR3 GG : Nodes, Elements   =     74731    425019
AFLR3 GG : Nodes, Elements   =     74731    425013
AFLR3 GG : Nodes, Elements   =     74733    425019
AFLR3 GG : Nodes, Elements   =     74733    425026
AFLR3 GG : Nodes, Elements   =     74733    425023
 
AFLR3    : CPU Time          =    10.194   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     74733    425023
AFLR3 QI : Nodes, Elements   =     73272    416779
AFLR3 QI : Nodes, Elements   =     73057    415551
AFLR3 QI : Nodes, Elements   =     73044    415479
AFLR3 QI : Nodes, Elements   =     73043    415473
AFLR3 QI : Nodes, Elements   =     73043    419540
AFLR3 QI : Nodes, Elements   =     73043    415283
AFLR3 QI : Nodes, Elements   =     73043    414827
AFLR3 QI : Nodes, Elements   =     73043    417596
AFLR3 QI : Nodes, Elements   =     73043    414862
AFLR3 QI : Nodes, Elements   =     73043    414790
AFLR3 QI : Nodes, Elements   =     73043    415433
AFLR3 QI : Nodes, Elements   =     73043    414627
AFLR3 QI : Nodes, Elements   =     73043    414482
AFLR3 QI : Nodes, Elements   =     73043    414838
AFLR3 QI : Nodes, Elements   =     73043    414447
AFLR3 QI : Nodes, Elements   =     73043    414356
AFLR3 QI : Nodes, Elements   =     73043    414630
AFLR3 QI : Nodes, Elements   =     73043    414339
AFLR3 QI : Nodes, Elements   =     73043    414270
AFLR3 QI : Nodes, Elements   =     73050    414301
AFLR3 QI : Nodes, Elements   =     73050    414583
AFLR3 QI : Nodes, Elements   =     73050    414319
AFLR3 QI : Nodes, Elements   =     73050    414301
AFLR3 QI : Nodes, Elements   =     73050    414528
AFLR3 QI : Nodes, Elements   =     73050    414305
AFLR3 QI : Nodes, Elements   =     73050    414240
AFLR3 QI : Nodes, Elements   =     73050    414301
 
AFLR3    : CPU Time          =     3.552   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     73050    414301
AFLR3 QRG: Nodes, Elements   =     73062    414368
AFLR3 QRG: Nodes, Elements   =     73063    414375
AFLR3 QRG: Nodes, Elements   =     73070    414414
 
AFLR3    : CPU Time          =     0.157   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    414414
UG3      : Min, Max Ang      =     1.195     172.2
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        58
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    414414
UG3      : Min Vol           =  6.94e-10
UG3      : Average Vol       =      5.12
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol<TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 <= Q <= 1

UG3      : No. Tet Elems     =    414414
UG3      : Min, Max Q        =    0.0775         1
UG3      : Average Q         =     0.891
UG3      : No. Q<       0.1  =        29
UG3      : No. Q<      0.01  =         0

OVERALL  : CPU Time          =    14.648   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    414414
UG3      : Min, Max Ang      =     1.195     172.2
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        58
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    414414
UG3      : Min Vol           =  6.94e-10
UG3      : Average Vol       =      5.12
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol<TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 <= Q <= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =    414414
UG3      : Min, Max Q        =      0.23         1
UG3      : Average Q         =     0.849
UG3      : No. Q<       0.1  =         0
UG3      : No. Q<      0.01  =         0

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.7.0
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          = 73070
	Number of elements       = 426842
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 414414
	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          = 73070
	Number of elements       = 426842
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 414414
	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          = 73070
	Number of elements       = 426842
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 414414
	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          = 73070
	Number of elements       = 426842
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 414414
	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:62511)
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)
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 70000EDFA000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 70000EDFA000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, 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    = 297
Number of elements = 590
Number of triangle elements      = 590
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes    = 487
Number of elements = 970
Number of triangle elements      = 970
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes    = 2048
Number of elements = 4096
Number of triangle elements      = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes    = 152
Number of elements = 300
Number of triangle elements      = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes    = 624
Number of elements = 1248
Number of triangle elements      = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4194
Total number of elements = 8368
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 - 297, elements - 590
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cone, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = torus, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = sphere, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = boxhole, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = bullet, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 297, elements - 590
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4194, elements - 8368
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    = 1352
Number of elements = 2684
Number of triangle elements      = 2684
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    = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
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 - 1352, elements - 2684
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 - 9605, elements - 19202
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 - 9605, elements - 19202
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 - 9605, elements - 19202
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 - 9605, elements - 19202
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 - 9605, elements - 19202
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 - 7161, elements - 14314
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    = 9605
Number of elements = 19202
Number of triangle elements      = 19202
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9605
Total number of elements = 19202
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
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 102292
	Sideset: 'Farfield', set_id 1, num_entries 48
	Sideset: 'Wing1', set_id 2, num_entries 19154
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 - 9605, elements - 19202
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 69792
	Sideset: 'Farfield', set_id 1, num_entries 48
	Sideset: 'Wing1', set_id 2, num_entries 19154
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, 98963.803820, 69822.813290, 6179.981375, 19723.152207, 370546.335523]
ok

----------------------------------------------------------------------
Ran 146 tests in 1069.597s

OK (skipped=10)
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
(make -C cCAPS -f avlTest.make)
make[1]: `avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[1]: `awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[1]: `frictionTest' is up to date.
(make -C cCAPS -f fun3d.make)
make[1]: Nothing to be done for `fun3d'.
(make -C cCAPS -f hsm.make)
make[1]: `hsm' is up to date.
(make -C cCAPS -f interferenceTest.make)
make[1]: `interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[1]: `msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[1]: `mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[1]: `pointwiseTest' is up to date.
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests

All tests pass!


=================================================
=================================================
(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)

=================================================
Using python : /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python
=================================================

Running.... MINIMAL PyTests

=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
CXtot   0.0006119078685747781
CYtot   -6.297054052850572e-15
CZtot   -0.301286139488597
Cltot   -4.785942150399569e-14
Cmtot   -0.1945055953450375
Cntot   -2.337286621027519e-15
Cl'tot  -4.789292355835892e-14
Cn'tot  -1.501668565013235e-15
CLtot   0.3012509314150652
CDtot   0.004646353488232536
CDvis   0.0
CLff    0.3009503023520406
CYff    -7.725269974775701e-15
CDind   0.004646353488232536
CDff    0.004968969500907968
e       0.9669902146157809
StripForces 
Wing  cl =  [0.02994790451347, 0.08555545178933, 0.1329003532587, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805664, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996427, 0.2453427152623, 0.2100182422922, 0.17330251928, 0.1329003532723, 0.08555545180787, 0.0299479045408]
Wing  cd =  [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946408, 0.0005114598078391, 0.0021191472861, 0.004145189908974, 0.006609094404181, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.006609094404439, 0.00414518990926, 0.002119147286384, 0.0005114598080994, -0.0007386538944075, -0.001762021024096, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764544]

real	0m3.383s
user	0m0.733s
sys	0m0.596s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  [1.05475230552582, 1.36488869373661, 1.5660721427212, 2.03059709333553, 1.9727108312101, 1.87307153172578, 1.7605047576016]
Cd =  [0.0131991208675814, 0.0166540240605919, 0.0200551482562995, 0.0458671342053759, 0.0754256009396578, 0.0994469174476091, 0.12747943098905]
Alpha =  [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.496044114417512, 0.46137773204127, 0.442376568201482, 0.361251636517606, 0.27610414085319, 0.214381239319572, 0.132988264746184]

real	0m6.694s
user	0m5.032s
sys	0m0.241s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.3783793240300122
Cd =  0.007775858044231098
Cm =  0.005262576090314894

real	0m4.797s
user	0m3.425s
sys	0m0.316s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]

real	0m1.364s
user	0m0.549s
sys	0m0.221s
+ 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/DARWIN64/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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go.  Other input will terminate the job.
Cl =  0.933417
Cd =  0.000284
Cd Wave =  0.0
Cm =  -0.203436
Cp _Critcal =  -1.303869

real	0m1.134s
user	0m0.557s
sys	0m0.184s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6

Getting mesh sizing parameters
	Mesh sizing name - Airfoil
	Mesh sizing name - AirfoilTE
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
	Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
	Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
	Swapping y and z coordinates!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m1.425s
user	0m0.859s
sys	0m0.417s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Getting mesh sizing parameters
	Mesh sizing name - LeadingEdge
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 3793
Number of elements = 4001
Number of triangle elements      = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 76
Number of elements = 55
Number of triangle elements      = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes    = 100
Number of elements = 73
Number of triangle elements      = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes    = 3970
Total number of elements = 4129

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m10.305s
user	0m17.468s
sys	0m4.213s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.006   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          =     0.026   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          =     0.018   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


real	0m1.906s
user	0m1.030s
sys	0m0.492s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wing1
	Mesh sizing name - Wing2
	Done getting mesh sizing parameters
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 151209
	Number of elements       = 455692
	Number of triangles      = 14380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 220260
	Number of pyramids       = 425
	Number of prisms         = 220627
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m23.849s
user	0m15.829s
sys	0m0.768s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 265
Number of elements = 526
Number of triangle elements      = 526
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3137
Total number of elements = 6262

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 - 3137, elements - 6262
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.027976
Creating surface mesh ...
Surface mesh seconds:  0.007356
Recovering boundaries...
Boundary recovery seconds:  0.06161
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.008516
Suppressing Steiner points ...
Steiner suppression seconds:  1.5e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.012523
Refining mesh...
  4188 insertions, added 2185 points, 134452 tetrahedra in queue.
  1394 insertions, added 466 points, 139158 tetrahedra in queue.
  1858 insertions, added 424 points, 135152 tetrahedra in queue.
  2477 insertions, added 444 points, 115259 tetrahedra in queue.
  3302 insertions, added 499 points, 69620 tetrahedra in queue.
  4401 insertions, added 357 points, 954 tetrahedra in queue.
Refinement seconds:  0.842406
Smoothing vertices...
Mesh smoothing seconds:  0.566492
Improving mesh...
Mesh improvement seconds:  0.014057
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.003281
Total running seconds:  1.54443

Statistics:

  Input points: 3137
  Input facets: 6262
  Input segments: 9393
  Input holes: 2
  Input regions: 0

  Mesh points: 7994
  Mesh tetrahedra: 39231
  Mesh faces: 81593
  Mesh faces on exterior boundary: 6262
  Mesh faces on input facets: 6262
  Mesh edges on input segments: 9393
  Steiner points inside domain: 4857

Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


real	0m4.708s
user	0m3.198s
sys	0m0.424s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       545         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       545       545
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       110       222
AFLR2 IG : Nodes, Faces      =       220       442
AFLR2 IG : Nodes, Faces      =       330       662
AFLR2 IG : Nodes, Faces      =       440       882
AFLR2 IG : Nodes, Faces      =       517      1036
AFLR2 IG : Nodes, Faces      =       545      1092
AFLR2 IG : Nodes, Faces      =       549      1092
AFLR2 IG : Nodes, Faces      =       545       545
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       545       545
AFLR2 GGp: Nodes, Faces      =      1083      1621
AFLR2 GGp: Nodes, Faces      =      1616      2687
AFLR2 GGp: Nodes, Faces      =      2144      3743
AFLR2 GGp: Nodes, Faces      =      2661      4777
AFLR2 GGp: Nodes, Faces      =      3171      5797
AFLR2 GGp: Nodes, Faces      =      3672      6799
AFLR2 GGp: Nodes, Faces      =      4158      7771
AFLR2 GGp: Nodes, Faces      =      4653      8761
AFLR2 GGp: Nodes, Faces      =      5142      9739
AFLR2 GGp: Nodes, Faces      =      5608     10671
AFLR2 GGp: Nodes, Faces      =      6055     11565
AFLR2 GGp: Nodes, Faces      =      6482     12419
AFLR2 GGp: Nodes, Faces      =      6880     13215
AFLR2 GGp: Nodes, Faces      =      7257     13969
AFLR2 GGp: Nodes, Faces      =      7614     14683
AFLR2 GGp: Nodes, Faces      =      7947     15349
AFLR2 GGp: Nodes, Faces      =      8276     16007
AFLR2 GGp: Nodes, Faces      =      8575     16605
AFLR2 GGp: Nodes, Faces      =      8869     17193
AFLR2 GGp: Nodes, Faces      =      9140     17735
AFLR2 GGp: Nodes, Faces      =      9401     18257
AFLR2 GGp: Nodes, Faces      =      9654     18763
AFLR2 GGp: Nodes, Faces      =      9887     19229
AFLR2 GGp: Nodes, Faces      =     10110     19675
AFLR2 GGp: Nodes, Faces      =     10315     20085
AFLR2 GGp: Nodes, Faces      =     10497     20449
AFLR2 GGp: Nodes, Faces      =     10656     20767
AFLR2 GGp: Nodes, Faces      =     10791     21037
AFLR2 GGp: Nodes, Faces      =     10919     21293
AFLR2 GGp: Nodes, Faces      =     11022     21499
AFLR2 GGp: Nodes, Faces      =     11092     21639
AFLR2 GGp: Nodes, Faces      =     11145     21745
AFLR2 GGp: Nodes, Faces      =     11156     21767
 
AFLR2    : CPU Time          =     0.051   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          =     0.027   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        49.3184|             90|
|     CV Face Area Aspect Ratio|        1.00035|        33.4982|
|           CV Sub-Volume Ratio|        1.00001|        7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11153|    1/1.00|        10|
|         1|      2702|    1/4.13|   7.38309|
|         2|       549|    1/4.92|   4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.2623e-01|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.2297e-01|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.2145e-01|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.2103e-01|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.2109e-01|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.1978e-01|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.1992e-01|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.1991e-01|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.1976e-01|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.1962e-01|   -1.221243|    1.499646|    1.130319|    4.189559|   -6.277653|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.22124|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_su2_aflr2.dat  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_su2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_su2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.072253 Cd =  -0.01151
Cmz =  0.070975
Cx =  -0.01151 Cy =  0.072253
Pressure Contribution
Cl_p =  0.072253 Cd_p =  -0.01151
Cmz_p =  0.070975
Cx_p =  -0.01151 Cy_p =  0.072253
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m4.947s
user	0m2.872s
sys	0m0.998s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
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  -0.0012129281
C_N  0.065395002
C_D  0.025961197
C_S  -0.0012129281
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	1m45.610s
user	0m37.209s
sys	0m1.261s
+ 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/DARWIN64/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/DARWIN64/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	0m3.544s
user	0m0.687s
sys	0m0.392s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 96
	Number of elements = 77
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 77
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 97
	Combined Number of elements = 78
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 77
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 96
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Body
	Property name - Edge
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	8 automatic connections were made for capsConnect Root (node id 97)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Flutter
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aero card
	Writing analysis cards
	Writing constraint cards--each subcase individually
	Writing material cards
	Writing property cards
	Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

real	0m2.704s
user	0m1.007s
sys	0m0.522s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 1159
Number of elements = 798
Number of triangle elements      = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes    = 1159
Total number of elements = 798
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1159
	Number of elements = 798
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 798

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input
Area      3.428666259747
Mass      5383.006027803
Centroid  [1.222256036874, 0.1634981473778, -4.234377369776e-11]
CG        [1.222256036874, 0.1634981473778, -4.234490614246e-11]
Ixx       22133.97306033
Iyy       23448.30046709
Izz       1389.213122582
Ixy       164.2055275657
Ixz       -7.454850140458e-06
Iyz       1.707682988152e-06
I         [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454850140458e-06, 1.707682988152e-06]
II        [[22133.97306033, -164.2055275657, 7.454850140458e-06], [-164.2055275657, 23448.30046709, -1.707682988152e-06], [7.454850140458e-06, -1.707682988152e-06, 1389.213122582]]

real	0m9.955s
user	0m11.086s
sys	0m5.585s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 81
	Number of elements = 96
	Elemental Tria3 = 0
	Elemental Quad4 = 64

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
 Matrix Non-zero Entries = 5741

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.130E-01  0.165E+00  0.153E-04    1.000  ddy @ (   0.25   0.06   0.00)
   1*   0.260E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   1*   0.240E-05  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.09   0.00)
   2    0.379E-02  0.505E-01  0.750E-04    1.000  ddy @ (   0.25   0.19   0.00)
   2*   0.420E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   3    0.168E-02  0.225E-01  0.208E-04    1.000  ddy @ (   0.25   0.06   0.00)
   4    0.325E-03  0.427E-02  0.250E-05    1.000  ddy @ (   0.25   0.19   0.00)
   5    0.794E-05  0.112E-03  0.170E-06    1.000  ddy @ (   0.25   0.19   0.00)
   6    0.387E-08  0.598E-07  0.197E-09    1.000  ddy @ (   0.25   0.06   0.00)
   7    0.848E-15  0.147E-13  0.924E-15    1.000  ddy @ (   0.25   0.19   0.00)

 Converging n vectors ...
 it =  1    dn =  0.788E-01   rlx = 1.000  (  59 )
 it =  2    dn =  0.566E-16   rlx = 1.000  (  35 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.691E-03   rlx = 1.000  (  45 )
 it =  2    de =  0.404E-04   rlx = 1.000  (   9 )
 it =  3    de =  0.142E-07   rlx = 1.000  (  46 )
 it =  4    de =  0.521E-11   rlx = 1.000  (  62 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat

real	0m2.158s
user	0m0.959s
sys	0m0.163s
+ 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/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   -21.56250 dimensionless

Variables
---------
   x  :  1.62500   [-]   The X variable
   y  :  1.37500   [-]   The Y variable

Constants
---------
   c   :  3         [-]   A constant
   c2  :  2         [-]   A constant

Sensitivities
-------------
   c   :  + 0.46957   A constant
   c2  :  - 0.22338   A constant

Solve Report
------------
   Solve Method           :  Quadratic Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	1m24.024s
user	0m2.588s
sys	0m0.395s
+ 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/DARWIN64
+ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/test/plugs
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/test/plugs
+ find /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
data/Plugs/plugs0a.csm
data/Plugs/plugs0b.csm
data/Plugs/plugs0c.csm
data/Plugs/plugs0d.csm
total 50352
-rw-r--r--  1 jenkins  staff   1.2M Jun 24 23:14 ASTRO.D01
-rw-r--r--  1 jenkins  staff   277K Jun 24 23:14 ASTRO.IDX
-rwxr-xr-x  1 jenkins  staff   145K Jun 24 23:14 ESPxddm
-rwxr-xr-x  1 jenkins  staff   226K Jun 24 23:14 Slugs
-rwxr-xr-x  1 jenkins  staff   101K Jun 24 23:14 TestFit
-rwxr-xr-x  1 jenkins  staff   1.8M Jun 24 23:14 avl
-rwxr-xr-x  1 jenkins  staff    34K Jun 24 23:14 cart3dTest
-rwxr-xr-x  1 jenkins  staff    34K Jun 24 23:12 egads2cart
-rwxr-xr-x  1 jenkins  staff    85K Jun 24 23:14 egads2cgt
-rwxr-xr-x  1 jenkins  staff    50K Jun 24 23:14 friction
-rwxr-xr-x  1 jenkins  staff   8.9M Jun 24 23:14 mastros.exe
-rwxr-xr-x  1 jenkins  staff   2.2M Jun 24 23:14 mses
-rwxr-xr-x  1 jenkins  staff   2.5M Jun 24 23:14 mset
-rwxr-xr-x  1 jenkins  staff    34K Jun 24 23:14 phaseUtil
-rw-r--r--  1 jenkins  staff   1.6K Jun 24 23:16 pod.egads
-rw-r--r--  1 jenkins  staff     0B Jun 24 23:16 port7681.jrnl
-rwxr-xr-x  1 jenkins  staff   1.2M Jun 24 23:14 pplot
-rwxr-xr-x  1 jenkins  staff   1.2M Jun 24 23:14 pxplot
-rwxr-xr-x  1 jenkins  staff    84K Jun 24 23:13 sensCSM
-rwxr-xr-x  1 jenkins  staff   222K Jun 24 23:13 serveCSM
-rwxr-xr-x  1 jenkins  staff   190K Jun 24 23:13 serveESP
-rwxr-xr-x  1 jenkins  staff    51K Jun 24 23:12 vCurvature
-rwxr-xr-x  1 jenkins  staff    51K Jun 24 23:12 vGeom
-rwxr-xr-x  1 jenkins  staff    36K Jun 24 23:12 vTess
-rwxr-xr-x  1 jenkins  staff   2.0M Jun 24 23:12 vTesstatic
-rw-r--r--  1 jenkins  staff   195K Jun 24 23:16 wingMultiModel.bdf
-rwxr-xr-x  1 jenkins  staff   1.8M Jun 24 23:14 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m14.510s
user	0m12.657s
sys	0m0.742s
++ set +x
data/Plugs/plugs0a                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m14.912s
user	0m14.419s
sys	0m0.146s
++ set +x
data/Plugs/plugs0b                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m35.549s
user	0m45.332s
sys	0m0.275s
++ set +x
data/Plugs/plugs0c                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m35.655s
user	0m44.961s
sys	0m0.285s
++ set +x
data/Plugs/plugs0d                  passed (as expected)
--------------------------------------------------------------------------------------------------
[Execution node] check if [macys] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [macys] 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/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Beta/CASREV=7.7,ESP_ARCH=DARWIN64,buildnode=macys #731'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS