Started by upstream project "ESP_bPreBuilt" build number 69
originally caused by:
 Started by user galbramc
Running as galbramc
[EnvInject] - Loading node environment variables.
Building remotely on macys in workspace /Users/jenkins/workspace/ESP_bPreBuilt
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] Done
Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_bPreBuilt
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-04-28T12:59:25.118 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 2481

Checking out a fresh workspace because /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-04-28T12:59:25.118 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 858

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [macys] is in [[macys, macys_VM, master, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-rhel7, reynolds-ubuntu16, reynolds-ubuntu18, reynolds-ubuntu20]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[ESP_bPreBuilt] $ /bin/bash -xe /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/jenkins7036546001492740579.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_PreBuilt.sh
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.6
++ OCCTREF=7.6
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.34.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ macys == \r\e\y\n\o\l\d\s ]]
++ [[ '' == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.6 != '' ]]
++ [[ '' != '' ]]
++ [[ macys == *\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-.?'
ls: /Users/jenkins/util/ESP/OpenCASCADE-.?: No such file or directory
++ export CASROOT=
++ CASROOT=
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/udunits/udunits2.xml
++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//lib:/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/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_bPreBuilt/ESP//lib:/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-3.34.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/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_bPreBuilt/ESP//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_bPreBuilt/ESP//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_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//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_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ macys == \m\a\c\y\s* ]]
++ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-*'
++ [[ macys == \m\a\c\y\s ]]
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_bPreBuilt/ESP//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_bPreBuilt/ESP//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_bPreBuilt/ESP//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_bPreBuilt/ESP//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_bPreBuilt/ESP//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_bPreBuilt/ESP//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_bPreBuilt/ESP//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_bPreBuilt/ESP//bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB=-L/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
++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/data
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
++ uname -s
+ [[ Darwin == *\D\a\r\w\i\n* ]]
+ DESKTOP=/Users/jenkins/Desktop
+ OSI=macos
++ uname -m
+ ARCH=x86_64
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta-macos-x86_64.tgz
--2024-04-28 12:59:33--  https://acdl.mit.edu/ESP/archive/ESPbeta-macos-x86_64.tgz
Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14
Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected.
HTTP request sent, awaiting response... 200 OK
Length: 517018302 (493M) [application/x-gzip]
Saving to: ‘ESPbeta-macos-x86_64.tgz’

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  6850K .......... .......... .......... .......... ..........  1% 9.15M 39s
  6900K .......... .......... .......... .......... ..........  1% 11.0M 39s
  6950K .......... .......... .......... .......... ..........  1% 11.4M 39s
  7000K .......... .......... .......... .......... ..........  1% 11.4M 39s
  7050K .......... .......... .......... .......... ..........  1% 11.3M 39s
  7100K .......... .......... .......... .......... ..........  1% 11.0M 39s
  7150K .......... .......... .......... .......... ..........  1% 9.54M 39s
  7200K .......... .......... .......... .......... ..........  1% 11.1M 39s
  7250K .......... .......... .......... .......... ..........  1% 17.0M 39s
  7300K .......... .......... .......... .......... ..........  1% 51.6M 39s
  7350K .......... .......... .......... .......... ..........  1% 30.7M 39s
  7400K .......... .......... .......... .......... ..........  1% 22.8M 39s
  7450K .......... .......... .......... .......... ..........  1% 15.7M 39s
  7500K .......... .......... .......... .......... ..........  1% 15.9M 39s
  7550K .......... .......... .......... .......... ..........  1% 13.3M 39s
  7600K .......... .......... .......... .......... ..........  1% 11.7M 39s
  7650K .......... .......... .......... .......... ..........  1% 13.3M 39s
  7700K .......... .......... .......... .......... ..........  1% 15.1M 38s
  7750K .......... .......... .......... .......... ..........  1% 12.7M 38s
  7800K .......... .......... .......... .......... ..........  1% 14.6M 38s
  7850K .......... .......... .......... .......... ..........  1% 12.1M 38s
  7900K .......... .......... .......... .......... ..........  1% 14.3M 38s
  7950K .......... .......... .......... .......... ..........  1% 11.5M 38s
  8000K .......... .......... .......... .......... ..........  1% 12.5M 38s
  8050K .......... .......... .......... .......... ..........  1% 31.1M 38s
  8100K .......... .......... .......... .......... ..........  1% 22.5M 38s
  8150K .......... .......... .......... .......... ..........  1% 7.06M 38s
  8200K .......... .......... .......... .......... ..........  1%  135M 38s
  8250K .......... .......... .......... .......... ..........  1%  143M 38s
  8300K .......... .......... .......... .......... ..........  1% 18.8M 38s
  8350K .......... .......... .......... .......... ..........  1% 11.4M 38s
  8400K .......... .......... .......... .......... ..........  1% 11.1M 38s
  8450K .......... .......... .......... .......... ..........  1% 8.99M 38s
  8500K .......... .......... .......... .......... ..........  1% 11.2M 38s
  8550K .......... .......... .......... .......... ..........  1% 13.3M 38s
  8600K .......... .......... .......... .......... ..........  1% 8.79M 38s
  8650K .......... .......... .......... .......... ..........  1% 11.0M 38s
  8700K .......... .......... .......... .......... ..........  1% 9.33M 38s
  8750K .......... .......... .......... .......... ..........  1% 19.8M 38s
  8800K .......... .......... .......... .......... ..........  1% 22.6M 38s
  8850K .......... .......... .......... .......... ..........  1% 12.5M 38s
  8900K .......... .......... .......... .......... ..........  1% 10.3M 38s
  8950K .......... .......... .......... .......... ..........  1% 11.2M 38s
  9000K .......... .......... .......... .......... ..........  1% 14.1M 38s
  9050K .......... .......... .......... .......... ..........  1% 15.7M 38s
  9100K .......... .......... .......... .......... ..........  1% 8.59M 38s
  9150K .......... .......... .......... .......... ..........  1% 9.81M 38s
  9200K .......... .......... .......... .......... ..........  1% 10.1M 38s
  9250K .......... .......... .......... .......... ..........  1% 9.44M 38s
  9300K .......... .......... .......... .......... ..........  1% 10.2M 38s
  9350K .......... .......... .......... .......... ..........  1% 10.1M 38s
  9400K .......... .......... .......... .......... ..........  1% 9.79M 38s
  9450K .......... .......... .......... .......... ..........  1% 9.89M 39s
  9500K .......... .......... .......... .......... ..........  1% 11.3M 39s
  9550K .......... .......... .......... .......... ..........  1% 10.3M 39s
  9600K .......... .......... .......... .......... ..........  1% 8.88M 39s
  9650K .......... .......... .......... .......... ..........  1% 10.2M 39s
  9700K .......... .......... .......... .......... ..........  1% 9.31M 39s
  9750K .......... .......... .......... .......... ..........  1% 8.36M 39s
  9800K .......... .......... .......... .......... ..........  1% 8.57M 39s
  9850K .......... .......... .......... .......... ..........  1% 9.41M 39s
  9900K .......... .......... .......... .......... ..........  1% 8.73M 39s
  9950K .......... .......... .......... .......... ..........  1% 6.18M 39s
 10000K .......... .......... .......... .......... ..........  1% 7.75M 39s
 10050K .......... .......... .......... .......... ..........  2% 6.26M 40s
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 12050K .......... .......... .......... .......... ..........  2% 18.9M 39s
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 12200K .......... .......... .......... .......... ..........  2% 6.01M 40s
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 12700K .......... .......... .......... .......... ..........  2% 10.1M 40s
 12750K .......... .......... .......... .......... ..........  2% 9.86M 40s
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 14450K .......... .......... .......... .......... ..........  2% 17.7M 42s
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 15100K .......... .......... .......... .......... ..........  3% 8.73M 41s
 15150K .......... .......... .......... .......... ..........  3% 11.2M 41s
 15200K .......... .......... .......... .......... ..........  3% 7.17M 41s
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 15300K .......... .......... .......... .......... ..........  3% 3.93M 42s
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 15400K .......... .......... .......... .......... ..........  3% 2.95M 43s
 15450K .......... .......... .......... .......... ..........  3% 2.40M 43s
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 16300K .......... .......... .......... .......... ..........  3% 14.8M 44s
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 16750K .......... .......... .......... .......... ..........  3% 11.8M 44s
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 16850K .......... .......... .......... .......... ..........  3% 10.5M 44s
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 17350K .......... .......... .......... .......... ..........  3% 7.14M 44s
 17400K .......... .......... .......... .......... ..........  3% 16.9M 44s
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 17500K .......... .......... .......... .......... ..........  3% 18.1M 44s
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 17700K .......... .......... .......... .......... ..........  3% 26.3M 44s
 17750K .......... .......... .......... .......... ..........  3% 17.6M 44s
 17800K .......... .......... .......... .......... ..........  3% 11.4M 44s
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 17900K .......... .......... .......... .......... ..........  3% 16.1M 44s
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 18250K .......... .......... .......... .......... ..........  3% 11.3M 43s
 18300K .......... .......... .......... .......... ..........  3% 16.3M 43s
 18350K .......... .......... .......... .......... ..........  3% 12.7M 43s
 18400K .......... .......... .......... .......... ..........  3% 24.0M 43s
 18450K .......... .......... .......... .......... ..........  3% 42.1M 43s
 18500K .......... .......... .......... .......... ..........  3% 26.0M 43s
 18550K .......... .......... .......... .......... ..........  3%  250M 43s
 18600K .......... .......... .......... .......... ..........  3% 25.0M 43s
 18650K .......... .......... .......... .......... ..........  3%  140M 43s
 18700K .......... .......... .......... .......... ..........  3% 26.1M 43s
 18750K .......... .......... .......... .......... ..........  3% 20.8M 43s
 18800K .......... .......... .......... .......... ..........  3% 23.3M 43s
 18850K .......... .......... .......... .......... ..........  3% 18.1M 43s
 18900K .......... .......... .......... .......... ..........  3% 11.7M 43s
 18950K .......... .......... .......... .......... ..........  3% 16.4M 43s
 19000K .......... .......... .......... .......... ..........  3% 17.3M 43s
 19050K .......... .......... .......... .......... ..........  3% 16.6M 42s
 19100K .......... .......... .......... .......... ..........  3% 12.2M 42s
 19150K .......... .......... .......... .......... ..........  3% 15.4M 42s
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 19250K .......... .......... .......... .......... ..........  3% 14.5M 42s
 19300K .......... .......... .......... .......... ..........  3% 13.4M 42s
 19350K .......... .......... .......... .......... ..........  3% 8.54M 42s
 19400K .......... .......... .......... .......... ..........  3% 7.52M 42s
 19450K .......... .......... .......... .......... ..........  3% 5.68M 43s
 19500K .......... .......... .......... .......... ..........  3% 5.84M 43s
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 19650K .......... .......... .......... .......... ..........  3% 6.73M 43s
 19700K .......... .......... .......... .......... ..........  3% 4.04M 43s
 19750K .......... .......... .......... .......... ..........  3% 3.90M 43s
 19800K .......... .......... .......... .......... ..........  3% 3.15M 44s
 19850K .......... .......... .......... .......... ..........  3% 3.40M 44s
 19900K .......... .......... .......... .......... ..........  3% 6.29M 44s
 19950K .......... .......... .......... .......... ..........  3% 12.5M 44s
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 20050K .......... .......... .......... .......... ..........  3% 11.9M 44s
 20100K .......... .......... .......... .......... ..........  3% 13.5M 44s
 20150K .......... .......... .......... .......... ..........  4% 10.9M 44s
 20200K .......... .......... .......... .......... ..........  4% 9.40M 44s
 20250K .......... .......... .......... .......... ..........  4% 10.7M 44s
 20300K .......... .......... .......... .......... ..........  4% 12.8M 44s
 20350K .......... .......... .......... .......... ..........  4% 7.68M 44s
 20400K .......... .......... .......... .......... ..........  4% 9.84M 44s
 20450K .......... .......... .......... .......... ..........  4% 5.86M 44s
 20500K .......... .......... .......... .......... ..........  4% 7.27M 44s
 20550K .......... .......... .......... .......... ..........  4% 6.24M 44s
 20600K .......... .......... .......... .......... ..........  4% 5.40M 44s
 20650K .......... .......... .......... .......... ..........  4% 9.15M 44s
 20700K .......... .......... .......... .......... ..........  4% 10.9M 44s
 20750K .......... .......... .......... .......... ..........  4% 8.19M 44s
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 34650K .......... .......... .......... .......... ..........  6% 21.1M 44s
 34700K .......... .......... .......... .......... ..........  6% 31.9M 44s
 34750K .......... .......... .......... .......... ..........  6% 16.5M 44s
 34800K .......... .......... .......... .......... ..........  6% 49.7M 44s
 34850K .......... .......... .......... .......... ..........  6% 17.6M 44s
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 47700K .......... .......... .......... .......... ..........  9% 11.6M 42s
 47750K .......... .......... .......... .......... ..........  9% 31.3M 42s
 47800K .......... .......... .......... .......... ..........  9% 17.2M 42s
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 47900K .......... .......... .......... .......... ..........  9% 14.7M 41s
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 48150K .......... .......... .......... .......... ..........  9% 14.2M 41s
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 48600K .......... .......... .......... .......... ..........  9% 65.3M 41s
 48650K .......... .......... .......... .......... ..........  9% 16.0M 41s
 48700K .......... .......... .......... .......... ..........  9% 22.8M 41s
 48750K .......... .......... .......... .......... ..........  9% 16.3M 41s
 48800K .......... .......... .......... .......... ..........  9% 11.9M 41s
 48850K .......... .......... .......... .......... ..........  9% 11.5M 41s
 48900K .......... .......... .......... .......... ..........  9% 13.9M 41s
 48950K .......... .......... .......... .......... ..........  9% 9.19M 41s
 49000K .......... .......... .......... .......... ..........  9% 11.1M 41s
 49050K .......... .......... .......... .......... ..........  9% 13.5M 41s
 49100K .......... .......... .......... .......... ..........  9% 9.01M 41s
 49150K .......... .......... .......... .......... ..........  9% 12.0M 41s
 49200K .......... .......... .......... .......... ..........  9% 9.42M 41s
 49250K .......... .......... .......... .......... ..........  9% 11.2M 41s
 49300K .......... .......... .......... .......... ..........  9% 9.98M 41s
 49350K .......... .......... .......... .......... ..........  9% 18.0M 41s
 49400K .......... .......... .......... .......... ..........  9% 8.65M 41s
 49450K .......... .......... .......... .......... ..........  9% 10.4M 41s
 49500K .......... .......... .......... .......... ..........  9% 15.3M 41s
 49550K .......... .......... .......... .......... ..........  9% 11.7M 41s
 49600K .......... .......... .......... .......... ..........  9% 13.0M 41s
 49650K .......... .......... .......... .......... ..........  9% 14.8M 41s
 49700K .......... .......... .......... .......... ..........  9% 12.4M 41s
 49750K .......... .......... .......... .......... ..........  9% 9.92M 41s
 49800K .......... .......... .......... .......... ..........  9% 15.3M 41s
 49850K .......... .......... .......... .......... ..........  9% 10.8M 41s
 49900K .......... .......... .......... .......... ..........  9% 9.96M 41s
 49950K .......... .......... .......... .......... ..........  9% 7.49M 41s
 50000K .......... .......... .......... .......... ..........  9% 7.63M 41s
 50050K .......... .......... .......... .......... ..........  9% 8.78M 41s
 50100K .......... .......... .......... .......... ..........  9% 6.47M 41s
 50150K .......... .......... .......... .......... ..........  9% 6.30M 41s
 50200K .......... .......... .......... .......... ..........  9% 5.83M 41s
 50250K .......... .......... .......... .......... ..........  9% 6.20M 41s
 50300K .......... .......... .......... .......... ..........  9% 4.76M 41s
 50350K .......... .......... .......... .......... ..........  9% 4.27M 41s
 50400K .......... .......... .......... .......... ..........  9% 5.42M 41s
 50450K .......... .......... .......... .......... .......... 10% 4.96M 41s
 50500K .......... .......... .......... .......... .......... 10% 9.90M 41s
 50550K .......... .......... .......... .......... .......... 10% 11.3M 41s
 50600K .......... .......... .......... .......... .......... 10% 9.40M 41s
 50650K .......... .......... .......... .......... .......... 10% 12.3M 41s
 50700K .......... .......... .......... .......... .......... 10% 6.93M 41s
 50750K .......... .......... .......... .......... .......... 10% 8.47M 41s
 50800K .......... .......... .......... .......... .......... 10% 10.9M 41s
 50850K .......... .......... .......... .......... .......... 10% 10.2M 41s
 50900K .......... .......... .......... .......... .......... 10% 11.5M 41s
 50950K .......... .......... .......... .......... .......... 10% 7.47M 41s
 51000K .......... .......... .......... .......... .......... 10% 9.08M 41s
 51050K .......... .......... .......... .......... .......... 10% 8.17M 41s
 51100K .......... .......... .......... .......... .......... 10% 7.98M 41s
 51150K .......... .......... .......... .......... .......... 10% 7.60M 41s
 51200K .......... .......... .......... .......... .......... 10% 7.88M 41s
 51250K .......... .......... .......... .......... .......... 10% 13.5M 41s
 51300K .......... .......... .......... .......... .......... 10% 25.2M 41s
 51350K .......... .......... .......... .......... .......... 10% 34.8M 41s
 51400K .......... .......... .......... .......... .......... 10% 16.8M 41s
 51450K .......... .......... .......... .......... .......... 10% 46.6M 41s
 51500K .......... .......... .......... .......... .......... 10% 24.5M 41s
 51550K .......... .......... .......... .......... .......... 10% 19.5M 41s
 51600K .......... .......... .......... .......... .......... 10% 16.5M 41s
 51650K .......... .......... .......... .......... .......... 10% 20.3M 41s
 51700K .......... .......... .......... .......... .......... 10% 15.4M 41s
 51750K .......... .......... .......... .......... .......... 10% 21.7M 41s
 51800K .......... .......... .......... .......... .......... 10% 23.3M 41s
 51850K .......... .......... .......... .......... .......... 10% 10.6M 41s
 51900K .......... .......... .......... .......... .......... 10% 14.8M 41s
 51950K .......... .......... .......... .......... .......... 10% 6.10M 41s
 52000K .......... .......... .......... .......... .......... 10% 6.13M 41s
 52050K .......... .......... .......... .......... .......... 10% 7.01M 41s
 52100K .......... .......... .......... .......... .......... 10% 6.37M 41s
 52150K .......... .......... .......... .......... .......... 10% 6.31M 41s
 52200K .......... .......... .......... .......... .......... 10% 16.2M 41s
 52250K .......... .......... .......... .......... .......... 10% 33.1M 41s
 52300K .......... .......... .......... .......... .......... 10% 14.6M 41s
 52350K .......... .......... .......... .......... .......... 10% 39.0M 41s
 52400K .......... .......... .......... .......... .......... 10% 25.9M 41s
 52450K .......... .......... .......... .......... .......... 10% 19.0M 41s
 52500K .......... .......... .......... .......... .......... 10% 13.6M 41s
 52550K .......... .......... .......... .......... .......... 10% 14.6M 41s
 52600K .......... .......... .......... .......... .......... 10% 11.1M 41s
 52650K .......... .......... .......... .......... .......... 10% 9.44M 41s
 52700K .......... .......... .......... .......... .......... 10% 8.96M 41s
 52750K .......... .......... .......... .......... .......... 10% 8.11M 41s
 52800K .......... .......... .......... .......... .......... 10% 8.63M 41s
 52850K .......... .......... .......... .......... .......... 10% 6.62M 41s
 52900K .......... .......... .......... .......... .......... 10% 8.27M 41s
 52950K .......... .......... .......... .......... .......... 10% 6.26M 41s
 53000K .......... .......... .......... .......... .......... 10% 9.33M 41s
 53050K .......... .......... .......... .......... .......... 10% 6.46M 41s
 53100K .......... .......... .......... .......... .......... 10% 5.87M 41s
 53150K .......... .......... .......... .......... .......... 10% 6.71M 41s
 53200K .......... .......... .......... .......... .......... 10% 5.71M 41s
 53250K .......... .......... .......... .......... .......... 10% 7.11M 41s
 53300K .......... .......... .......... .......... .......... 10% 13.9M 41s
 53350K .......... .......... .......... .......... .......... 10% 20.5M 41s
 53400K .......... .......... .......... .......... .......... 10% 11.5M 41s
 53450K .......... .......... .......... .......... .......... 10% 8.01M 41s
 53500K .......... .......... .......... .......... .......... 10% 13.7M 41s
 53550K .......... .......... .......... .......... .......... 10% 8.95M 41s
 53600K .......... .......... .......... .......... .......... 10% 7.74M 41s
 53650K .......... .......... .......... .......... .......... 10% 12.8M 41s
 53700K .......... .......... .......... .......... .......... 10% 9.62M 41s
 53750K .......... .......... .......... .......... .......... 10% 12.4M 41s
 53800K .......... .......... .......... .......... .......... 10% 9.94M 41s
 53850K .......... .......... .......... .......... .......... 10% 10.2M 41s
 53900K .......... .......... .......... .......... .......... 10% 11.2M 41s
 53950K .......... .......... .......... .......... .......... 10% 12.1M 41s
 54000K .......... .......... .......... .......... .......... 10% 13.1M 41s
 54050K .......... .......... .......... .......... .......... 10%  144M 41s
 54100K .......... .......... .......... .......... .......... 10% 21.3M 41s
 54150K .......... .......... .......... .......... .......... 10% 49.9M 41s
 54200K .......... .......... .......... .......... .......... 10% 19.2M 41s
 54250K .......... .......... .......... .......... .......... 10% 25.5M 41s
 54300K .......... .......... .......... .......... .......... 10% 23.1M 41s
 54350K .......... .......... .......... .......... .......... 10% 20.3M 41s
 54400K .......... .......... .......... .......... .......... 10% 23.0M 41s
 54450K .......... .......... .......... .......... .......... 10% 17.8M 41s
 54500K .......... .......... .......... .......... .......... 10% 22.6M 41s
 54550K .......... .......... .......... .......... .......... 10% 19.8M 41s
 54600K .......... .......... .......... .......... .......... 10% 20.8M 41s
 54650K .......... .......... .......... .......... .......... 10% 21.4M 41s
 54700K .......... .......... .......... .......... .......... 10% 14.3M 41s
 54750K .......... .......... .......... .......... .......... 10% 24.2M 41s
 54800K .......... .......... .......... .......... .......... 10% 16.8M 41s
 54850K .......... .......... .......... .......... .......... 10% 13.5M 41s
 54900K .......... .......... .......... .......... .......... 10% 21.9M 41s
 54950K .......... .......... .......... .......... .......... 10% 12.8M 41s
 55000K .......... .......... .......... .......... .......... 10% 15.0M 41s
 55050K .......... .......... .......... .......... .......... 10% 19.8M 41s
 55100K .......... .......... .......... .......... .......... 10% 13.6M 41s
 55150K .......... .......... .......... .......... .......... 10% 18.9M 41s
 55200K .......... .......... .......... .......... .......... 10% 9.44M 41s
 55250K .......... .......... .......... .......... .......... 10% 7.68M 41s
 55300K .......... .......... .......... .......... .......... 10% 10.6M 41s
 55350K .......... .......... .......... .......... .......... 10% 6.42M 41s
 55400K .......... .......... .......... .......... .......... 10% 10.8M 41s
 55450K .......... .......... .......... .......... .......... 10% 5.42M 41s
 55500K .......... .......... .......... .......... .......... 11% 9.35M 41s
 55550K .......... .......... .......... .......... .......... 11% 12.1M 41s
 55600K .......... .......... .......... .......... .......... 11% 9.42M 41s
 55650K .......... .......... .......... .......... .......... 11% 11.4M 41s
 55700K .......... .......... .......... .......... .......... 11% 10.0M 41s
 55750K .......... .......... .......... .......... .......... 11% 14.6M 41s
 55800K .......... .......... .......... .......... .......... 11% 12.9M 41s
 55850K .......... .......... .......... .......... .......... 11% 12.1M 41s
 55900K .......... .......... .......... .......... .......... 11% 12.3M 41s
 55950K .......... .......... .......... .......... .......... 11% 11.7M 41s
 56000K .......... .......... .......... .......... .......... 11% 12.2M 41s
 56050K .......... .......... .......... .......... .......... 11% 15.5M 41s
 56100K .......... .......... .......... .......... .......... 11% 10.7M 41s
 56150K .......... .......... .......... .......... .......... 11% 31.0M 41s
 56200K .......... .......... .......... .......... .......... 11% 24.7M 41s
 56250K .......... .......... .......... .......... .......... 11% 17.0M 41s
 56300K .......... .......... .......... .......... .......... 11% 16.7M 40s
 56350K .......... .......... .......... .......... .......... 11% 7.03M 41s
 56400K .......... .......... .......... .......... .......... 11% 6.35M 41s
 56450K .......... .......... .......... .......... .......... 11% 6.14M 41s
 56500K .......... .......... .......... .......... .......... 11% 7.28M 41s
 56550K .......... .......... .......... .......... .......... 11% 6.07M 41s
 56600K .......... .......... .......... .......... .......... 11% 5.82M 41s
 56650K .......... .......... .......... .......... .......... 11% 6.97M 41s
 56700K .......... .......... .......... .......... .......... 11% 4.73M 41s
 56750K .......... .......... .......... .......... .......... 11% 6.49M 41s
 56800K .......... .......... .......... .......... .......... 11% 18.8M 41s
 56850K .......... .......... .......... .......... .......... 11% 31.9M 41s
 56900K .......... .......... .......... .......... .......... 11% 18.8M 41s
 56950K .......... .......... .......... .......... .......... 11% 20.3M 41s
 57000K .......... .......... .......... .......... .......... 11% 17.8M 41s
 57050K .......... .......... .......... .......... .......... 11% 14.0M 41s
 57100K .......... .......... .......... .......... .......... 11% 10.4M 41s
 57150K .......... .......... .......... .......... .......... 11% 13.4M 41s
 57200K .......... .......... .......... .......... .......... 11% 9.51M 41s
 57250K .......... .......... .......... .......... .......... 11% 12.8M 41s
 57300K .......... .......... .......... .......... .......... 11% 10.9M 41s
 57350K .......... .......... .......... .......... .......... 11% 8.82M 41s
 57400K .......... .......... .......... .......... .......... 11% 11.3M 41s
 57450K .......... .......... .......... .......... .......... 11% 7.94M 41s
 57500K .......... .......... .......... .......... .......... 11% 9.44M 41s
 57550K .......... .......... .......... .......... .......... 11% 7.98M 41s
 57600K .......... .......... .......... .......... .......... 11% 6.87M 41s
 57650K .......... .......... .......... .......... .......... 11% 7.20M 41s
 57700K .......... .......... .......... .......... .......... 11% 5.60M 41s
 57750K .......... .......... .......... .......... .......... 11% 6.42M 41s
 57800K .......... .......... .......... .......... .......... 11% 7.03M 41s
 57850K .......... .......... .......... .......... .......... 11% 5.78M 41s
 57900K .......... .......... .......... .......... .......... 11% 10.3M 41s
 57950K .......... .......... .......... .......... .......... 11% 10.3M 41s
 58000K .......... .......... .......... .......... .......... 11% 9.80M 41s
 58050K .......... .......... .......... .......... .......... 11% 6.30M 41s
 58100K .......... .......... .......... .......... .......... 11% 4.88M 41s
 58150K .......... .......... .......... .......... .......... 11% 5.74M 41s
 58200K .......... .......... .......... .......... .......... 11% 5.22M 41s
 58250K .......... .......... .......... .......... .......... 11% 9.01M 41s
 58300K .......... .......... .......... .......... .......... 11% 26.3M 41s
 58350K .......... .......... .......... .......... .......... 11% 20.2M 41s
 58400K .......... .......... .......... .......... .......... 11% 22.8M 41s
 58450K .......... .......... .......... .......... .......... 11% 19.1M 41s
 58500K .......... .......... .......... .......... .......... 11% 23.7M 41s
 58550K .......... .......... .......... .......... .......... 11% 12.0M 41s
 58600K .......... .......... .......... .......... .......... 11% 15.8M 41s
 58650K .......... .......... .......... .......... .......... 11% 16.2M 41s
 58700K .......... .......... .......... .......... .......... 11% 12.0M 41s
 58750K .......... .......... .......... .......... .......... 11% 14.4M 41s
 58800K .......... .......... .......... .......... .......... 11% 16.2M 41s
 58850K .......... .......... .......... .......... .......... 11% 12.2M 41s
 58900K .......... .......... .......... .......... .......... 11% 12.6M 41s
 58950K .......... .......... .......... .......... .......... 11% 10.9M 41s
 59000K .......... .......... .......... .......... .......... 11% 11.0M 41s
 59050K .......... .......... .......... .......... .......... 11% 13.8M 41s
 59100K .......... .......... .......... .......... .......... 11% 10.8M 41s
 59150K .......... .......... .......... .......... .......... 11% 12.4M 41s
 59200K .......... .......... .......... .......... .......... 11% 10.8M 41s
 59250K .......... .......... .......... .......... .......... 11% 8.24M 41s
 59300K .......... .......... .......... .......... .......... 11% 8.44M 41s
 59350K .......... .......... .......... .......... .......... 11% 7.97M 41s
 59400K .......... .......... .......... .......... .......... 11% 14.9M 41s
 59450K .......... .......... .......... .......... .......... 11% 15.9M 41s
 59500K .......... .......... .......... .......... .......... 11% 19.4M 40s
 59550K .......... .......... .......... .......... .......... 11% 15.6M 40s
 59600K .......... .......... .......... .......... .......... 11% 13.7M 40s
 59650K .......... .......... .......... .......... .......... 11% 15.6M 40s
 59700K .......... .......... .......... .......... .......... 11% 11.8M 40s
 59750K .......... .......... .......... .......... .......... 11% 10.7M 40s
 59800K .......... .......... .......... .......... .......... 11% 14.2M 40s
 59850K .......... .......... .......... .......... .......... 11% 10.7M 40s
 59900K .......... .......... .......... .......... .......... 11% 15.3M 40s
 59950K .......... .......... .......... .......... .......... 11% 9.55M 40s
 60000K .......... .......... .......... .......... .......... 11% 12.4M 40s
 60050K .......... .......... .......... .......... .......... 11% 11.7M 40s
 60100K .......... .......... .......... .......... .......... 11% 9.53M 40s
 60150K .......... .......... .......... .......... .......... 11% 12.4M 40s
 60200K .......... .......... .......... .......... .......... 11% 8.53M 40s
 60250K .......... .......... .......... .......... .......... 11% 11.1M 40s
 60300K .......... .......... .......... .......... .......... 11% 11.9M 40s
 60350K .......... .......... .......... .......... .......... 11% 9.20M 40s
 60400K .......... .......... .......... .......... .......... 11% 10.7M 40s
 60450K .......... .......... .......... .......... .......... 11% 10.3M 40s
 60500K .......... .......... .......... .......... .......... 11% 11.8M 40s
 60550K .......... .......... .......... .......... .......... 12% 9.11M 40s
 60600K .......... .......... .......... .......... .......... 12% 17.2M 40s
 60650K .......... .......... .......... .......... .......... 12% 13.4M 40s
 60700K .......... .......... .......... .......... .......... 12% 12.4M 40s
 60750K .......... .......... .......... .......... .......... 12% 16.8M 40s
 60800K .......... .......... .......... .......... .......... 12% 15.7M 40s
 60850K .......... .......... .......... .......... .......... 12% 15.5M 40s
 60900K .......... .......... .......... .......... .......... 12% 15.2M 40s
 60950K .......... .......... .......... .......... .......... 12% 9.67M 40s
 61000K .......... .......... .......... .......... .......... 12% 10.8M 40s
 61050K .......... .......... .......... .......... .......... 12% 10.8M 40s
 61100K .......... .......... .......... .......... .......... 12% 8.91M 40s
 61150K .......... .......... .......... .......... .......... 12% 9.29M 40s
 61200K .......... .......... .......... .......... .......... 12% 6.62M 40s
 61250K .......... .......... .......... .......... .......... 12% 5.24M 40s
 61300K .......... .......... .......... .......... .......... 12% 2.90M 40s
 61350K .......... .......... .......... .......... .......... 12% 2.00M 41s
 61400K .......... .......... .......... .......... .......... 12% 8.82M 41s
 61450K .......... .......... .......... .......... .......... 12% 6.78M 41s
 61500K .......... .......... .......... .......... .......... 12% 6.80M 41s
 61550K .......... .......... .......... .......... .......... 12% 8.02M 41s
 61600K .......... .......... .......... .......... .......... 12% 9.74M 41s
 61650K .......... .......... .......... .......... .......... 12% 27.3M 41s
 61700K .......... .......... .......... .......... .......... 12% 34.2M 41s
 61750K .......... .......... .......... .......... .......... 12% 21.1M 40s
 61800K .......... .......... .......... .......... .......... 12% 75.2M 40s
 61850K .......... .......... .......... .......... .......... 12% 24.7M 40s
 61900K .......... .......... .......... .......... .......... 12% 19.3M 40s
 61950K .......... .......... .......... .......... .......... 12% 14.5M 40s
 62000K .......... .......... .......... .......... .......... 12% 20.3M 40s
 62050K .......... .......... .......... .......... .......... 12% 21.4M 40s
 62100K .......... .......... .......... .......... .......... 12% 16.5M 40s
 62150K .......... .......... .......... .......... .......... 12% 15.3M 40s
 62200K .......... .......... .......... .......... .......... 12% 21.0M 40s
 62250K .......... .......... .......... .......... .......... 12% 22.1M 40s
 62300K .......... .......... .......... .......... .......... 12% 14.7M 40s
 62350K .......... .......... .......... .......... .......... 12% 16.5M 40s
 62400K .......... .......... .......... .......... .......... 12% 14.2M 40s
 62450K .......... .......... .......... .......... .......... 12% 5.83M 40s
 62500K .......... .......... .......... .......... .......... 12% 15.2M 40s
 62550K .......... .......... .......... .......... .......... 12% 14.7M 40s
 62600K .......... .......... .......... .......... .......... 12% 10.5M 40s
 62650K .......... .......... .......... .......... .......... 12% 10.7M 40s
 62700K .......... .......... .......... .......... .......... 12% 9.06M 40s
 62750K .......... .......... .......... .......... .......... 12% 16.2M 40s
 62800K .......... .......... .......... .......... .......... 12% 10.1M 40s
 62850K .......... .......... .......... .......... .......... 12% 9.40M 40s
 62900K .......... .......... .......... .......... .......... 12% 8.73M 40s
 62950K .......... .......... .......... .......... .......... 12% 6.94M 40s
 63000K .......... .......... .......... .......... .......... 12% 9.07M 40s
 63050K .......... .......... .......... .......... .......... 12% 10.2M 40s
 63100K .......... .......... .......... .......... .......... 12% 6.70M 40s
 63150K .......... .......... .......... .......... .......... 12% 6.02M 40s
 63200K .......... .......... .......... .......... .......... 12% 8.83M 40s
 63250K .......... .......... .......... .......... .......... 12% 12.3M 40s
 63300K .......... .......... .......... .......... .......... 12% 8.72M 40s
 63350K .......... .......... .......... .......... .......... 12% 6.45M 40s
 63400K .......... .......... .......... .......... .......... 12% 5.55M 40s
 63450K .......... .......... .......... .......... .......... 12% 11.0M 40s
 63500K .......... .......... .......... .......... .......... 12% 11.8M 40s
 63550K .......... .......... .......... .......... .......... 12% 10.4M 40s
 63600K .......... .......... .......... .......... .......... 12% 8.73M 40s
 63650K .......... .......... .......... .......... .......... 12% 10.7M 40s
 63700K .......... .......... .......... .......... .......... 12% 8.81M 40s
 63750K .......... .......... .......... .......... .......... 12% 8.89M 40s
 63800K .......... .......... .......... .......... .......... 12% 9.46M 40s
 63850K .......... .......... .......... .......... .......... 12% 4.68M 40s
 63900K .......... .......... .......... .......... .......... 12% 5.40M 40s
 63950K .......... .......... .......... .......... .......... 12% 4.52M 40s
 64000K .......... .......... .......... .......... .......... 12% 4.89M 40s
 64050K .......... .......... .......... .......... .......... 12% 9.42M 40s
 64100K .......... .......... .......... .......... .......... 12% 8.08M 40s
 64150K .......... .......... .......... .......... .......... 12% 7.41M 40s
 64200K .......... .......... .......... .......... .......... 12% 7.09M 40s
 64250K .......... .......... .......... .......... .......... 12% 9.32M 40s
 64300K .......... .......... .......... .......... .......... 12% 9.34M 40s
 64350K .......... .......... .......... .......... .......... 12% 7.28M 40s
 64400K .......... .......... .......... .......... .......... 12% 8.61M 40s
 64450K .......... .......... .......... .......... .......... 12% 9.56M 40s
 64500K .......... .......... .......... .......... .......... 12% 28.6M 40s
 64550K .......... .......... .......... .......... .......... 12% 36.2M 40s
 64600K .......... .......... .......... .......... .......... 12% 21.2M 40s
 64650K .......... .......... .......... .......... .......... 12%  105M 40s
 64700K .......... .......... .......... .......... .......... 12% 26.6M 40s
 64750K .......... .......... .......... .......... .......... 12% 20.6M 40s
 64800K .......... .......... .......... .......... .......... 12% 27.8M 40s
 64850K .......... .......... .......... .......... .......... 12% 20.4M 40s
 64900K .......... .......... .......... .......... .......... 12% 26.1M 40s
 64950K .......... .......... .......... .......... .......... 12% 21.1M 40s
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 65050K .......... .......... .......... .......... .......... 12% 36.4M 40s
 65100K .......... .......... .......... .......... .......... 12% 21.6M 40s
 65150K .......... .......... .......... .......... .......... 12% 14.8M 40s
 65200K .......... .......... .......... .......... .......... 12% 13.5M 40s
 65250K .......... .......... .......... .......... .......... 12% 15.3M 40s
 65300K .......... .......... .......... .......... .......... 12% 16.0M 40s
 65350K .......... .......... .......... .......... .......... 12% 13.4M 40s
 65400K .......... .......... .......... .......... .......... 12% 14.0M 40s
 65450K .......... .......... .......... .......... .......... 12% 13.1M 40s
 65500K .......... .......... .......... .......... .......... 12% 5.19M 40s
 65550K .......... .......... .......... .......... .......... 12% 9.16M 40s
 65600K .......... .......... .......... .......... .......... 13% 5.65M 40s
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 65900K .......... .......... .......... .......... .......... 13% 9.65M 40s
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 66000K .......... .......... .......... .......... .......... 13% 9.49M 40s
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 66100K .......... .......... .......... .......... .......... 13% 6.98M 40s
 66150K .......... .......... .......... .......... .......... 13% 7.70M 40s
 66200K .......... .......... .......... .......... .......... 13% 5.48M 40s
 66250K .......... .......... .......... .......... .......... 13% 10.6M 40s
 66300K .......... .......... .......... .......... .......... 13% 23.3M 40s
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 66400K .......... .......... .......... .......... .......... 13% 33.7M 40s
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 66500K .......... .......... .......... .......... .......... 13% 12.6M 40s
 66550K .......... .......... .......... .......... .......... 13% 23.3M 40s
 66600K .......... .......... .......... .......... .......... 13% 11.7M 40s
 66650K .......... .......... .......... .......... .......... 13% 15.4M 40s
 66700K .......... .......... .......... .......... .......... 13% 10.6M 40s
 66750K .......... .......... .......... .......... .......... 13% 14.8M 40s
 66800K .......... .......... .......... .......... .......... 13% 10.6M 40s
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 66900K .......... .......... .......... .......... .......... 13% 14.5M 40s
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 67000K .......... .......... .......... .......... .......... 13% 29.3M 40s
 67050K .......... .......... .......... .......... .......... 13% 16.7M 40s
 67100K .......... .......... .......... .......... .......... 13% 36.1M 40s
 67150K .......... .......... .......... .......... .......... 13% 22.0M 40s
 67200K .......... .......... .......... .......... .......... 13% 20.0M 40s
 67250K .......... .......... .......... .......... .......... 13% 15.4M 40s
 67300K .......... .......... .......... .......... .......... 13% 23.3M 40s
 67350K .......... .......... .......... .......... .......... 13% 11.3M 40s
 67400K .......... .......... .......... .......... .......... 13% 20.5M 40s
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 67500K .......... .......... .......... .......... .......... 13% 8.19M 40s
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 67900K .......... .......... .......... .......... .......... 13% 9.56M 40s
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 68000K .......... .......... .......... .......... .......... 13% 9.35M 40s
 68050K .......... .......... .......... .......... .......... 13% 8.14M 40s
 68100K .......... .......... .......... .......... .......... 13% 8.18M 40s
 68150K .......... .......... .......... .......... .......... 13% 6.24M 40s
 68200K .......... .......... .......... .......... .......... 13% 7.36M 40s
 68250K .......... .......... .......... .......... .......... 13% 6.35M 40s
 68300K .......... .......... .......... .......... .......... 13% 8.91M 40s
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 68400K .......... .......... .......... .......... .......... 13% 8.70M 40s
 68450K .......... .......... .......... .......... .......... 13% 7.35M 40s
 68500K .......... .......... .......... .......... .......... 13% 9.38M 40s
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 68600K .......... .......... .......... .......... .......... 13% 7.53M 40s
 68650K .......... .......... .......... .......... .......... 13% 10.0M 40s
 68700K .......... .......... .......... .......... .......... 13% 7.91M 40s
 68750K .......... .......... .......... .......... .......... 13% 15.2M 40s
 68800K .......... .......... .......... .......... .......... 13% 28.8M 40s
 68850K .......... .......... .......... .......... .......... 13% 23.2M 40s
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 68950K .......... .......... .......... .......... .......... 13% 19.7M 40s
 69000K .......... .......... .......... .......... .......... 13% 20.2M 40s
 69050K .......... .......... .......... .......... .......... 13% 25.8M 40s
 69100K .......... .......... .......... .......... .......... 13% 20.5M 40s
 69150K .......... .......... .......... .......... .......... 13% 17.6M 40s
 69200K .......... .......... .......... .......... .......... 13% 18.2M 40s
 69250K .......... .......... .......... .......... .......... 13% 22.6M 40s
 69300K .......... .......... .......... .......... .......... 13% 19.0M 40s
 69350K .......... .......... .......... .......... .......... 13% 11.4M 40s
 69400K .......... .......... .......... .......... .......... 13% 20.4M 40s
 69450K .......... .......... .......... .......... .......... 13% 11.0M 40s
 69500K .......... .......... .......... .......... .......... 13% 10.8M 40s
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 69650K .......... .......... .......... .......... .......... 13% 11.3M 40s
 69700K .......... .......... .......... .......... .......... 13% 9.05M 40s
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 69850K .......... .......... .......... .......... .......... 13% 7.66M 40s
 69900K .......... .......... .......... .......... .......... 13% 11.7M 40s
 69950K .......... .......... .......... .......... .......... 13% 7.55M 40s
 70000K .......... .......... .......... .......... .......... 13% 9.28M 40s
 70050K .......... .......... .......... .......... .......... 13% 8.68M 40s
 70100K .......... .......... .......... .......... .......... 13% 6.74M 40s
 70150K .......... .......... .......... .......... .......... 13% 11.2M 40s
 70200K .......... .......... .......... .......... .......... 13% 4.62M 40s
 70250K .......... .......... .......... .......... .......... 13% 7.91M 40s
 70300K .......... .......... .......... .......... .......... 13% 6.17M 40s
 70350K .......... .......... .......... .......... .......... 13% 4.81M 40s
 70400K .......... .......... .......... .......... .......... 13% 6.55M 40s
 70450K .......... .......... .......... .......... .......... 13% 5.67M 40s
 70500K .......... .......... .......... .......... .......... 13% 8.72M 40s
 70550K .......... .......... .......... .......... .......... 13% 10.7M 40s
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 70750K .......... .......... .......... .......... .......... 14% 13.8M 40s
 70800K .......... .......... .......... .......... .......... 14% 38.5M 40s
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 70900K .......... .......... .......... .......... .......... 14% 36.9M 40s
 70950K .......... .......... .......... .......... .......... 14% 27.8M 40s
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 71050K .......... .......... .......... .......... .......... 14% 25.8M 40s
 71100K .......... .......... .......... .......... .......... 14% 18.0M 40s
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 71200K .......... .......... .......... .......... .......... 14% 18.6M 40s
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 71300K .......... .......... .......... .......... .......... 14% 15.3M 40s
 71350K .......... .......... .......... .......... .......... 14% 13.2M 40s
 71400K .......... .......... .......... .......... .......... 14% 18.5M 40s
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 71500K .......... .......... .......... .......... .......... 14% 12.3M 40s
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 71600K .......... .......... .......... .......... .......... 14% 17.0M 40s
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 71700K .......... .......... .......... .......... .......... 14% 12.0M 40s
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 71900K .......... .......... .......... .......... .......... 14% 16.6M 40s
 71950K .......... .......... .......... .......... .......... 14% 13.1M 40s
 72000K .......... .......... .......... .......... .......... 14% 12.4M 40s
 72050K .......... .......... .......... .......... .......... 14% 16.0M 40s
 72100K .......... .......... .......... .......... .......... 14% 16.0M 40s
 72150K .......... .......... .......... .......... .......... 14% 16.0M 40s
 72200K .......... .......... .......... .......... .......... 14% 11.5M 40s
 72250K .......... .......... .......... .......... .......... 14% 14.9M 39s
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 72500K .......... .......... .......... .......... .......... 14% 18.5M 39s
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 72800K .......... .......... .......... .......... .......... 14% 15.2M 39s
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 72900K .......... .......... .......... .......... .......... 14% 10.2M 39s
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 73000K .......... .......... .......... .......... .......... 14% 12.1M 39s
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 73150K .......... .......... .......... .......... .......... 14% 16.3M 39s
 73200K .......... .......... .......... .......... .......... 14% 12.3M 39s
 73250K .......... .......... .......... .......... .......... 14% 13.6M 39s
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 73750K .......... .......... .......... .......... .......... 14%  212M 39s
 73800K .......... .......... .......... .......... .......... 14% 24.3M 39s
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 73900K .......... .......... .......... .......... .......... 14% 55.4M 39s
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 74000K .......... .......... .......... .......... .......... 14% 11.8M 39s
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 74250K .......... .......... .......... .......... .......... 14% 9.96M 39s
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 74600K .......... .......... .......... .......... .......... 14% 99.9M 39s
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 75150K .......... .......... .......... .......... .......... 14% 10.7M 39s
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 75250K .......... .......... .......... .......... .......... 14% 9.72M 39s
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 75700K .......... .......... .......... .......... .......... 15% 4.71M 39s
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 76000K .......... .......... .......... .......... .......... 15% 9.23M 39s
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 76150K .......... .......... .......... .......... .......... 15% 9.57M 39s
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 76250K .......... .......... .......... .......... .......... 15% 8.27M 39s
 76300K .......... .......... .......... .......... .......... 15% 5.86M 39s
 76350K .......... .......... .......... .......... .......... 15% 12.4M 39s
 76400K .......... .......... .......... .......... .......... 15% 14.4M 39s
 76450K .......... .......... .......... .......... .......... 15% 27.1M 39s
 76500K .......... .......... .......... .......... .......... 15% 12.2M 39s
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 76650K .......... .......... .......... .......... .......... 15% 11.2M 39s
 76700K .......... .......... .......... .......... .......... 15% 8.09M 39s
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 76800K .......... .......... .......... .......... .......... 15% 10.9M 39s
 76850K .......... .......... .......... .......... .......... 15% 10.2M 39s
 76900K .......... .......... .......... .......... .......... 15% 12.2M 39s
 76950K .......... .......... .......... .......... .......... 15% 18.3M 39s
 77000K .......... .......... .......... .......... .......... 15% 18.6M 39s
 77050K .......... .......... .......... .......... .......... 15% 23.9M 39s
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 77200K .......... .......... .......... .......... .......... 15% 13.2M 39s
 77250K .......... .......... .......... .......... .......... 15% 17.2M 39s
 77300K .......... .......... .......... .......... .......... 15% 15.7M 39s
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 77700K .......... .......... .......... .......... .......... 15% 8.26M 39s
 77750K .......... .......... .......... .......... .......... 15% 11.5M 39s
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 78100K .......... .......... .......... .......... .......... 15% 10.3M 39s
 78150K .......... .......... .......... .......... .......... 15% 14.0M 39s
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 78250K .......... .......... .......... .......... .......... 15% 14.5M 39s
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 78700K .......... .......... .......... .......... .......... 15% 65.6M 39s
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 82100K .......... .......... .......... .......... .......... 16% 5.35M 38s
 82150K .......... .......... .......... .......... .......... 16% 5.80M 38s
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 82250K .......... .......... .......... .......... .......... 16% 7.50M 38s
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 85200K .......... .......... .......... .......... .......... 16% 47.0M 38s
 85250K .......... .......... .......... .......... .......... 16% 27.3M 38s
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 85900K .......... .......... .......... .......... .......... 17% 6.86M 38s
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 86500K .......... .......... .......... .......... .......... 17% 27.8M 38s
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 86950K .......... .......... .......... .......... .......... 17% 11.1M 38s
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 87100K .......... .......... .......... .......... .......... 17% 9.27M 38s
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 87250K .......... .......... .......... .......... .......... 17% 6.47M 38s
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 87400K .......... .......... .......... .......... .......... 17% 11.5M 38s
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 87500K .......... .......... .......... .......... .......... 17% 14.8M 38s
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 88250K .......... .......... .......... .......... .......... 17% 13.5M 38s
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 88600K .......... .......... .......... .......... .......... 17% 11.9M 38s
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 88800K .......... .......... .......... .......... .......... 17% 14.4M 38s
 88850K .......... .......... .......... .......... .......... 17% 7.36M 38s
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 89100K .......... .......... .......... .......... .......... 17% 5.00M 38s
 89150K .......... .......... .......... .......... .......... 17% 9.68M 38s
 89200K .......... .......... .......... .......... .......... 17% 21.9M 38s
 89250K .......... .......... .......... .......... .......... 17% 14.7M 38s
 89300K .......... .......... .......... .......... .......... 17% 34.4M 38s
 89350K .......... .......... .......... .......... .......... 17% 13.9M 38s
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 89500K .......... .......... .......... .......... .......... 17% 7.59M 38s
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 89600K .......... .......... .......... .......... .......... 17% 9.58M 38s
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 89700K .......... .......... .......... .......... .......... 17% 7.77M 38s
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 89800K .......... .......... .......... .......... .......... 17% 10.3M 38s
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 90000K .......... .......... .......... .......... .......... 17% 11.2M 38s
 90050K .......... .......... .......... .......... .......... 17% 9.00M 38s
 90100K .......... .......... .......... .......... .......... 17% 5.44M 38s
 90150K .......... .......... .......... .......... .......... 17% 13.0M 38s
 90200K .......... .......... .......... .......... .......... 17% 6.36M 38s
 90250K .......... .......... .......... .......... .......... 17% 7.36M 38s
 90300K .......... .......... .......... .......... .......... 17% 8.93M 38s
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 90400K .......... .......... .......... .......... .......... 17% 7.05M 38s
 90450K .......... .......... .......... .......... .......... 17% 6.19M 38s
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 90550K .......... .......... .......... .......... .......... 17% 7.81M 38s
 90600K .......... .......... .......... .......... .......... 17% 7.58M 38s
 90650K .......... .......... .......... .......... .......... 17% 19.6M 38s
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 90750K .......... .......... .......... .......... .......... 17% 21.5M 38s
 90800K .......... .......... .......... .......... .......... 17% 15.6M 38s
 90850K .......... .......... .......... .......... .......... 18% 20.8M 38s
 90900K .......... .......... .......... .......... .......... 18% 21.4M 38s
 90950K .......... .......... .......... .......... .......... 18% 13.9M 38s
 91000K .......... .......... .......... .......... .......... 18% 20.7M 38s
 91050K .......... .......... .......... .......... .......... 18% 21.0M 38s
 91100K .......... .......... .......... .......... .......... 18% 19.8M 38s
 91150K .......... .......... .......... .......... .......... 18% 15.1M 38s
 91200K .......... .......... .......... .......... .......... 18% 21.1M 38s
 91250K .......... .......... .......... .......... .......... 18% 13.0M 38s
 91300K .......... .......... .......... .......... .......... 18% 19.6M 38s
 91350K .......... .......... .......... .......... .......... 18% 14.9M 37s
 91400K .......... .......... .......... .......... .......... 18% 9.74M 37s
 91450K .......... .......... .......... .......... .......... 18% 11.9M 37s
 91500K .......... .......... .......... .......... .......... 18% 11.6M 37s
 91550K .......... .......... .......... .......... .......... 18% 11.6M 37s
 91600K .......... .......... .......... .......... .......... 18% 9.77M 37s
 91650K .......... .......... .......... .......... .......... 18% 12.1M 37s
 91700K .......... .......... .......... .......... .......... 18% 10.5M 37s
 91750K .......... .......... .......... .......... .......... 18% 11.9M 37s
 91800K .......... .......... .......... .......... .......... 18% 11.6M 37s
 91850K .......... .......... .......... .......... .......... 18% 8.66M 37s
 91900K .......... .......... .......... .......... .......... 18% 17.9M 37s
 91950K .......... .......... .......... .......... .......... 18% 14.1M 37s
 92000K .......... .......... .......... .......... .......... 18% 16.9M 37s
 92050K .......... .......... .......... .......... .......... 18% 24.4M 37s
 92100K .......... .......... .......... .......... .......... 18% 9.46M 37s
 92150K .......... .......... .......... .......... .......... 18% 15.5M 37s
 92200K .......... .......... .......... .......... .......... 18% 9.36M 37s
 92250K .......... .......... .......... .......... .......... 18% 12.1M 37s
 92300K .......... .......... .......... .......... .......... 18% 13.5M 37s
 92350K .......... .......... .......... .......... .......... 18% 9.21M 37s
 92400K .......... .......... .......... .......... .......... 18% 8.28M 37s
 92450K .......... .......... .......... .......... .......... 18% 9.20M 37s
 92500K .......... .......... .......... .......... .......... 18% 11.3M 37s
 92550K .......... .......... .......... .......... .......... 18% 10.5M 37s
 92600K .......... .......... .......... .......... .......... 18% 7.16M 37s
 92650K .......... .......... .......... .......... .......... 18% 6.17M 37s
 92700K .......... .......... .......... .......... .......... 18% 11.0M 37s
 92750K .......... .......... .......... .......... .......... 18% 12.4M 37s
 92800K .......... .......... .......... .......... .......... 18% 14.0M 37s
 92850K .......... .......... .......... .......... .......... 18% 9.49M 37s
 92900K .......... .......... .......... .......... .......... 18% 7.27M 37s
 92950K .......... .......... .......... .......... .......... 18% 11.4M 37s
 93000K .......... .......... .......... .......... .......... 18% 13.4M 37s
 93050K .......... .......... .......... .......... .......... 18% 13.7M 37s
 93100K .......... .......... .......... .......... .......... 18% 10.2M 37s
 93150K .......... .......... .......... .......... .......... 18% 11.1M 37s
 93200K .......... .......... .......... .......... .......... 18% 11.3M 37s
 93250K .......... .......... .......... .......... .......... 18% 13.4M 37s
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 93400K .......... .......... .......... .......... .......... 18% 16.5M 37s
 93450K .......... .......... .......... .......... .......... 18% 12.2M 37s
 93500K .......... .......... .......... .......... .......... 18% 10.9M 37s
 93550K .......... .......... .......... .......... .......... 18% 12.5M 37s
 93600K .......... .......... .......... .......... .......... 18% 9.75M 37s
 93650K .......... .......... .......... .......... .......... 18% 10.4M 37s
 93700K .......... .......... .......... .......... .......... 18% 7.80M 37s
 93750K .......... .......... .......... .......... .......... 18% 11.9M 37s
 93800K .......... .......... .......... .......... .......... 18% 10.6M 37s
 93850K .......... .......... .......... .......... .......... 18% 9.91M 37s
 93900K .......... .......... .......... .......... .......... 18% 10.1M 37s
 93950K .......... .......... .......... .......... .......... 18% 12.1M 37s
 94000K .......... .......... .......... .......... .......... 18% 9.60M 37s
 94050K .......... .......... .......... .......... .......... 18% 11.9M 37s
 94100K .......... .......... .......... .......... .......... 18% 12.0M 37s
 94150K .......... .......... .......... .......... .......... 18% 25.7M 37s
 94200K .......... .......... .......... .......... .......... 18% 23.8M 37s
 94250K .......... .......... .......... .......... .......... 18% 30.6M 37s
 94300K .......... .......... .......... .......... .......... 18% 21.5M 37s
 94350K .......... .......... .......... .......... .......... 18% 31.8M 37s
 94400K .......... .......... .......... .......... .......... 18% 19.1M 37s
 94450K .......... .......... .......... .......... .......... 18% 17.0M 37s
 94500K .......... .......... .......... .......... .......... 18% 11.9M 37s
 94550K .......... .......... .......... .......... .......... 18% 17.7M 37s
 94600K .......... .......... .......... .......... .......... 18% 9.50M 37s
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 94700K .......... .......... .......... .......... .......... 18% 9.48M 37s
 94750K .......... .......... .......... .......... .......... 18% 11.4M 37s
 94800K .......... .......... .......... .......... .......... 18% 8.35M 37s
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 94900K .......... .......... .......... .......... .......... 18% 11.7M 37s
 94950K .......... .......... .......... .......... .......... 18% 8.54M 37s
 95000K .......... .......... .......... .......... .......... 18% 11.3M 37s
 95050K .......... .......... .......... .......... .......... 18% 11.2M 37s
 95100K .......... .......... .......... .......... .......... 18% 8.98M 37s
 95150K .......... .......... .......... .......... .......... 18% 12.0M 37s
 95200K .......... .......... .......... .......... .......... 18% 14.6M 37s
 95250K .......... .......... .......... .......... .......... 18% 22.9M 37s
 95300K .......... .......... .......... .......... .......... 18% 11.8M 37s
 95350K .......... .......... .......... .......... .......... 18% 13.9M 37s
 95400K .......... .......... .......... .......... .......... 18% 11.1M 37s
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 95650K .......... .......... .......... .......... .......... 18% 12.0M 37s
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 95750K .......... .......... .......... .......... .......... 18% 7.83M 37s
 95800K .......... .......... .......... .......... .......... 18% 11.9M 37s
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 95900K .......... .......... .......... .......... .......... 19% 9.31M 37s
 95950K .......... .......... .......... .......... .......... 19% 6.41M 37s
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 96050K .......... .......... .......... .......... .......... 19% 7.51M 37s
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 96150K .......... .......... .......... .......... .......... 19% 11.2M 37s
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 96250K .......... .......... .......... .......... .......... 19% 11.3M 37s
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 96400K .......... .......... .......... .......... .......... 19% 11.3M 37s
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 96500K .......... .......... .......... .......... .......... 19% 5.51M 37s
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 96600K .......... .......... .......... .......... .......... 19% 6.70M 37s
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 96700K .......... .......... .......... .......... .......... 19% 6.33M 37s
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 96900K .......... .......... .......... .......... .......... 19% 3.64M 37s
 96950K .......... .......... .......... .......... .......... 19% 7.66M 37s
 97000K .......... .......... .......... .......... .......... 19% 6.72M 37s
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 97250K .......... .......... .......... .......... .......... 19% 4.05M 37s
 97300K .......... .......... .......... .......... .......... 19% 6.51M 37s
 97350K .......... .......... .......... .......... .......... 19% 16.4M 37s
 97400K .......... .......... .......... .......... .......... 19% 18.6M 37s
 97450K .......... .......... .......... .......... .......... 19% 21.6M 37s
 97500K .......... .......... .......... .......... .......... 19% 33.4M 37s
 97550K .......... .......... .......... .......... .......... 19% 20.1M 37s
 97600K .......... .......... .......... .......... .......... 19% 17.8M 37s
 97650K .......... .......... .......... .......... .......... 19% 30.5M 37s
 97700K .......... .......... .......... .......... .......... 19% 17.3M 37s
 97750K .......... .......... .......... .......... .......... 19% 20.5M 37s
 97800K .......... .......... .......... .......... .......... 19% 36.2M 37s
 97850K .......... .......... .......... .......... .......... 19% 18.6M 37s
 97900K .......... .......... .......... .......... .......... 19% 20.4M 37s
 97950K .......... .......... .......... .......... .......... 19% 22.9M 37s
 98000K .......... .......... .......... .......... .......... 19% 13.7M 37s
 98050K .......... .......... .......... .......... .......... 19% 42.7M 37s
 98100K .......... .......... .......... .......... .......... 19% 17.7M 37s
 98150K .......... .......... .......... .......... .......... 19% 24.8M 37s
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 98250K .......... .......... .......... .......... .......... 19% 24.1M 37s
 98300K .......... .......... .......... .......... .......... 19% 21.7M 37s
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 98400K .......... .......... .......... .......... .......... 19% 22.5M 37s
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 98500K .......... .......... .......... .......... .......... 19% 22.4M 37s
 98550K .......... .......... .......... .......... .......... 19% 16.1M 37s
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 98900K .......... .......... .......... .......... .......... 19% 31.1M 37s
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 99050K .......... .......... .......... .......... .......... 19% 48.7M 37s
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 99250K .......... .......... .......... .......... .......... 19% 21.7M 37s
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 99900K .......... .......... .......... .......... .......... 19% 15.6M 37s
 99950K .......... .......... .......... .......... .......... 19% 34.7M 37s
100000K .......... .......... .......... .......... .......... 19% 38.6M 36s
100050K .......... .......... .......... .......... .......... 19% 44.5M 36s
100100K .......... .......... .......... .......... .......... 19% 33.0M 36s
100150K .......... .......... .......... .......... .......... 19% 35.4M 36s
100200K .......... .......... .......... .......... .......... 19% 30.3M 36s
100250K .......... .......... .......... .......... .......... 19% 30.9M 36s
100300K .......... .......... .......... .......... .......... 19% 49.0M 36s
100350K .......... .......... .......... .......... .......... 19% 30.2M 36s
100400K .......... .......... .......... .......... .......... 19% 40.5M 36s
100450K .......... .......... .......... .......... .......... 19% 19.6M 36s
100500K .......... .......... .......... .......... .......... 19% 59.8M 36s
100550K .......... .......... .......... .......... .......... 19% 24.1M 36s
100600K .......... .......... .......... .......... .......... 19% 13.4M 36s
100650K .......... .......... .......... .......... .......... 19% 36.5M 36s
100700K .......... .......... .......... .......... .......... 19% 7.90M 36s
100750K .......... .......... .......... .......... .......... 19% 15.1M 36s
100800K .......... .......... .......... .......... .......... 19% 12.6M 36s
100850K .......... .......... .......... .......... .......... 19% 13.6M 36s
100900K .......... .......... .......... .......... .......... 19% 13.4M 36s
100950K .......... .......... .......... .......... .......... 20% 10.7M 36s
101000K .......... .......... .......... .......... .......... 20% 11.7M 36s
101050K .......... .......... .......... .......... .......... 20% 9.17M 36s
101100K .......... .......... .......... .......... .......... 20% 9.77M 36s
101150K .......... .......... .......... .......... .......... 20% 9.31M 36s
101200K .......... .......... .......... .......... .......... 20% 11.2M 36s
101250K .......... .......... .......... .......... .......... 20% 10.6M 36s
101300K .......... .......... .......... .......... .......... 20% 10.1M 36s
101350K .......... .......... .......... .......... .......... 20% 8.19M 36s
101400K .......... .......... .......... .......... .......... 20% 8.05M 36s
101450K .......... .......... .......... .......... .......... 20% 7.37M 36s
101500K .......... .......... .......... .......... .......... 20% 9.24M 36s
101550K .......... .......... .......... .......... .......... 20% 10.3M 36s
101600K .......... .......... .......... .......... .......... 20% 6.49M 36s
101650K .......... .......... .......... .......... .......... 20% 9.66M 36s
101700K .......... .......... .......... .......... .......... 20% 7.82M 36s
101750K .......... .......... .......... .......... .......... 20% 10.7M 36s
101800K .......... .......... .......... .......... .......... 20% 8.94M 36s
101850K .......... .......... .......... .......... .......... 20% 7.90M 36s
101900K .......... .......... .......... .......... .......... 20% 6.16M 36s
101950K .......... .......... .......... .......... .......... 20% 12.3M 36s
102000K .......... .......... .......... .......... .......... 20% 13.6M 36s
102050K .......... .......... .......... .......... .......... 20% 10.4M 36s
102100K .......... .......... .......... .......... .......... 20% 24.0M 36s
102150K .......... .......... .......... .......... .......... 20% 12.4M 36s
102200K .......... .......... .......... .......... .......... 20% 18.5M 36s
102250K .......... .......... .......... .......... .......... 20% 22.0M 36s
102300K .......... .......... .......... .......... .......... 20% 16.1M 36s
102350K .......... .......... .......... .......... .......... 20% 8.13M 36s
102400K .......... .......... .......... .......... .......... 20% 7.21M 36s
102450K .......... .......... .......... .......... .......... 20% 7.66M 36s
102500K .......... .......... .......... .......... .......... 20% 7.10M 36s
102550K .......... .......... .......... .......... .......... 20% 8.18M 36s
102600K .......... .......... .......... .......... .......... 20% 5.52M 36s
102650K .......... .......... .......... .......... .......... 20% 18.9M 36s
102700K .......... .......... .......... .......... .......... 20% 11.1M 36s
102750K .......... .......... .......... .......... .......... 20% 14.4M 36s
102800K .......... .......... .......... .......... .......... 20% 15.8M 36s
102850K .......... .......... .......... .......... .......... 20% 14.7M 36s
102900K .......... .......... .......... .......... .......... 20% 13.5M 36s
102950K .......... .......... .......... .......... .......... 20% 13.6M 36s
103000K .......... .......... .......... .......... .......... 20% 14.2M 36s
103050K .......... .......... .......... .......... .......... 20% 11.1M 36s
103100K .......... .......... .......... .......... .......... 20% 9.20M 36s
103150K .......... .......... .......... .......... .......... 20% 12.2M 36s
103200K .......... .......... .......... .......... .......... 20% 6.09M 36s
103250K .......... .......... .......... .......... .......... 20% 7.31M 36s
103300K .......... .......... .......... .......... .......... 20% 6.99M 36s
103350K .......... .......... .......... .......... .......... 20% 5.82M 36s
103400K .......... .......... .......... .......... .......... 20% 7.43M 36s
103450K .......... .......... .......... .......... .......... 20% 13.8M 36s
103500K .......... .......... .......... .......... .......... 20% 31.3M 36s
103550K .......... .......... .......... .......... .......... 20% 32.0M 36s
103600K .......... .......... .......... .......... .......... 20% 17.8M 36s
103650K .......... .......... .......... .......... .......... 20% 59.5M 36s
103700K .......... .......... .......... .......... .......... 20% 16.4M 36s
103750K .......... .......... .......... .......... .......... 20% 15.0M 36s
103800K .......... .......... .......... .......... .......... 20% 19.4M 36s
103850K .......... .......... .......... .......... .......... 20% 15.0M 36s
103900K .......... .......... .......... .......... .......... 20% 19.9M 36s
103950K .......... .......... .......... .......... .......... 20% 10.6M 36s
104000K .......... .......... .......... .......... .......... 20% 11.5M 36s
104050K .......... .......... .......... .......... .......... 20% 9.65M 36s
104100K .......... .......... .......... .......... .......... 20% 11.7M 36s
104150K .......... .......... .......... .......... .......... 20% 8.79M 36s
104200K .......... .......... .......... .......... .......... 20% 10.5M 36s
104250K .......... .......... .......... .......... .......... 20% 9.64M 36s
104300K .......... .......... .......... .......... .......... 20% 11.4M 36s
104350K .......... .......... .......... .......... .......... 20% 16.1M 36s
104400K .......... .......... .......... .......... .......... 20% 20.9M 36s
104450K .......... .......... .......... .......... .......... 20%  101M 36s
104500K .......... .......... .......... .......... .......... 20% 26.4M 36s
104550K .......... .......... .......... .......... .......... 20% 40.0M 36s
104600K .......... .......... .......... .......... .......... 20% 18.7M 36s
104650K .......... .......... .......... .......... .......... 20% 23.8M 36s
104700K .......... .......... .......... .......... .......... 20% 16.1M 36s
104750K .......... .......... .......... .......... .......... 20% 12.3M 36s
104800K .......... .......... .......... .......... .......... 20% 15.4M 36s
104850K .......... .......... .......... .......... .......... 20% 14.1M 36s
104900K .......... .......... .......... .......... .......... 20% 12.2M 36s
104950K .......... .......... .......... .......... .......... 20% 11.1M 36s
105000K .......... .......... .......... .......... .......... 20% 9.77M 36s
105050K .......... .......... .......... .......... .......... 20% 9.47M 36s
105100K .......... .......... .......... .......... .......... 20% 7.22M 36s
105150K .......... .......... .......... .......... .......... 20% 10.3M 36s
105200K .......... .......... .......... .......... .......... 20% 7.80M 36s
105250K .......... .......... .......... .......... .......... 20% 11.6M 36s
105300K .......... .......... .......... .......... .......... 20% 11.7M 36s
105350K .......... .......... .......... .......... .......... 20% 10.6M 36s
105400K .......... .......... .......... .......... .......... 20% 11.5M 36s
105450K .......... .......... .......... .......... .......... 20% 3.69M 36s
105500K .......... .......... .......... .......... .......... 20% 8.60M 36s
105550K .......... .......... .......... .......... .......... 20% 17.3M 36s
105600K .......... .......... .......... .......... .......... 20% 10.6M 36s
105650K .......... .......... .......... .......... .......... 20% 11.5M 36s
105700K .......... .......... .......... .......... .......... 20% 10.5M 36s
105750K .......... .......... .......... .......... .......... 20% 9.11M 36s
105800K .......... .......... .......... .......... .......... 20% 11.4M 36s
105850K .......... .......... .......... .......... .......... 20% 8.48M 36s
105900K .......... .......... .......... .......... .......... 20% 11.0M 36s
105950K .......... .......... .......... .......... .......... 20% 7.77M 36s
106000K .......... .......... .......... .......... .......... 21% 8.45M 36s
106050K .......... .......... .......... .......... .......... 21% 6.89M 36s
106100K .......... .......... .......... .......... .......... 21% 6.02M 36s
106150K .......... .......... .......... .......... .......... 21% 7.66M 36s
106200K .......... .......... .......... .......... .......... 21% 7.36M 36s
106250K .......... .......... .......... .......... .......... 21% 7.06M 36s
106300K .......... .......... .......... .......... .......... 21% 6.32M 36s
106350K .......... .......... .......... .......... .......... 21% 5.77M 36s
106400K .......... .......... .......... .......... .......... 21% 7.40M 36s
106450K .......... .......... .......... .......... .......... 21% 5.78M 36s
106500K .......... .......... .......... .......... .......... 21% 24.5M 36s
106550K .......... .......... .......... .......... .......... 21% 34.7M 36s
106600K .......... .......... .......... .......... .......... 21% 22.0M 36s
106650K .......... .......... .......... .......... .......... 21% 26.2M 36s
106700K .......... .......... .......... .......... .......... 21% 16.4M 36s
106750K .......... .......... .......... .......... .......... 21% 23.6M 36s
106800K .......... .......... .......... .......... .......... 21% 16.1M 36s
106850K .......... .......... .......... .......... .......... 21% 11.6M 36s
106900K .......... .......... .......... .......... .......... 21% 11.3M 36s
106950K .......... .......... .......... .......... .......... 21% 8.37M 36s
107000K .......... .......... .......... .......... .......... 21% 11.5M 36s
107050K .......... .......... .......... .......... .......... 21% 10.8M 36s
107100K .......... .......... .......... .......... .......... 21% 7.70M 36s
107150K .......... .......... .......... .......... .......... 21% 7.11M 36s
107200K .......... .......... .......... .......... .......... 21% 7.06M 36s
107250K .......... .......... .......... .......... .......... 21% 7.63M 36s
107300K .......... .......... .......... .......... .......... 21% 7.71M 36s
107350K .......... .......... .......... .......... .......... 21% 6.16M 36s
107400K .......... .......... .......... .......... .......... 21% 6.91M 36s
107450K .......... .......... .......... .......... .......... 21% 5.07M 36s
107500K .......... .......... .......... .......... .......... 21% 5.59M 36s
107550K .......... .......... .......... .......... .......... 21% 7.88M 36s
107600K .......... .......... .......... .......... .......... 21% 6.39M 36s
107650K .......... .......... .......... .......... .......... 21% 8.77M 36s
107700K .......... .......... .......... .......... .......... 21% 6.24M 36s
107750K .......... .......... .......... .......... .......... 21% 6.70M 36s
107800K .......... .......... .......... .......... .......... 21% 6.42M 36s
107850K .......... .......... .......... .......... .......... 21% 4.98M 36s
107900K .......... .......... .......... .......... .......... 21% 6.91M 36s
107950K .......... .......... .......... .......... .......... 21% 5.64M 36s
108000K .......... .......... .......... .......... .......... 21% 7.41M 36s
108050K .......... .......... .......... .......... .......... 21% 4.61M 36s
108100K .......... .......... .......... .......... .......... 21% 5.13M 36s
108150K .......... .......... .......... .......... .......... 21% 6.42M 36s
108200K .......... .......... .......... .......... .......... 21% 5.55M 36s
108250K .......... .......... .......... .......... .......... 21% 8.94M 36s
108300K .......... .......... .......... .......... .......... 21% 18.8M 36s
108350K .......... .......... .......... .......... .......... 21% 20.1M 36s
108400K .......... .......... .......... .......... .......... 21% 20.9M 36s
108450K .......... .......... .......... .......... .......... 21% 10.6M 36s
108500K .......... .......... .......... .......... .......... 21% 14.9M 36s
108550K .......... .......... .......... .......... .......... 21% 9.12M 36s
108600K .......... .......... .......... .......... .......... 21% 7.06M 36s
108650K .......... .......... .......... .......... .......... 21% 8.33M 36s
108700K .......... .......... .......... .......... .......... 21% 6.03M 36s
108750K .......... .......... .......... .......... .......... 21% 6.22M 36s
108800K .......... .......... .......... .......... .......... 21% 6.86M 36s
108850K .......... .......... .......... .......... .......... 21% 5.34M 36s
108900K .......... .......... .......... .......... .......... 21% 15.9M 36s
108950K .......... .......... .......... .......... .......... 21% 15.4M 36s
109000K .......... .......... .......... .......... .......... 21% 15.3M 36s
109050K .......... .......... .......... .......... .......... 21% 23.4M 36s
109100K .......... .......... .......... .......... .......... 21% 16.1M 36s
109150K .......... .......... .......... .......... .......... 21% 12.0M 36s
109200K .......... .......... .......... .......... .......... 21% 10.8M 36s
109250K .......... .......... .......... .......... .......... 21% 15.0M 36s
109300K .......... .......... .......... .......... .......... 21% 11.4M 36s
109350K .......... .......... .......... .......... .......... 21% 11.7M 36s
109400K .......... .......... .......... .......... .......... 21% 13.8M 36s
109450K .......... .......... .......... .......... .......... 21% 9.63M 36s
109500K .......... .......... .......... .......... .......... 21% 12.1M 36s
109550K .......... .......... .......... .......... .......... 21% 10.0M 36s
109600K .......... .......... .......... .......... .......... 21% 9.59M 36s
109650K .......... .......... .......... .......... .......... 21% 11.8M 36s
109700K .......... .......... .......... .......... .......... 21% 9.91M 36s
109750K .......... .......... .......... .......... .......... 21% 12.9M 36s
109800K .......... .......... .......... .......... .......... 21% 14.9M 36s
109850K .......... .......... .......... .......... .......... 21% 24.2M 36s
109900K .......... .......... .......... .......... .......... 21% 39.9M 36s
109950K .......... .......... .......... .......... .......... 21% 18.8M 36s
110000K .......... .......... .......... .......... .......... 21% 19.3M 36s
110050K .......... .......... .......... .......... .......... 21% 37.5M 36s
110100K .......... .......... .......... .......... .......... 21% 12.4M 36s
110150K .......... .......... .......... .......... .......... 21% 18.3M 36s
110200K .......... .......... .......... .......... .......... 21% 10.0M 36s
110250K .......... .......... .......... .......... .......... 21% 13.5M 36s
110300K .......... .......... .......... .......... .......... 21% 14.0M 36s
110350K .......... .......... .......... .......... .......... 21% 8.26M 36s
110400K .......... .......... .......... .......... .......... 21% 10.7M 36s
110450K .......... .......... .......... .......... .......... 21% 9.17M 36s
110500K .......... .......... .......... .......... .......... 21% 8.99M 36s
110550K .......... .......... .......... .......... .......... 21% 11.0M 36s
110600K .......... .......... .......... .......... .......... 21% 8.32M 36s
110650K .......... .......... .......... .......... .......... 21% 11.0M 36s
110700K .......... .......... .......... .......... .......... 21% 8.41M 36s
110750K .......... .......... .......... .......... .......... 21% 11.6M 36s
110800K .......... .......... .......... .......... .......... 21% 11.2M 36s
110850K .......... .......... .......... .......... .......... 21% 6.37M 36s
110900K .......... .......... .......... .......... .......... 21% 9.07M 36s
110950K .......... .......... .......... .......... .......... 21% 6.72M 36s
111000K .......... .......... .......... .......... .......... 21% 8.61M 36s
111050K .......... .......... .......... .......... .......... 22% 6.20M 36s
111100K .......... .......... .......... .......... .......... 22% 9.59M 36s
111150K .......... .......... .......... .......... .......... 22% 11.9M 36s
111200K .......... .......... .......... .......... .......... 22% 12.0M 36s
111250K .......... .......... .......... .......... .......... 22% 11.1M 36s
111300K .......... .......... .......... .......... .......... 22% 10.6M 36s
111350K .......... .......... .......... .......... .......... 22% 7.45M 36s
111400K .......... .......... .......... .......... .......... 22% 5.72M 36s
111450K .......... .......... .......... .......... .......... 22% 4.05M 36s
111500K .......... .......... .......... .......... .......... 22% 3.81M 36s
111550K .......... .......... .......... .......... .......... 22% 3.82M 36s
111600K .......... .......... .......... .......... .......... 22% 2.81M 36s
111650K .......... .......... .......... .......... .......... 22% 3.77M 36s
111700K .......... .......... .......... .......... .......... 22% 3.17M 36s
111750K .......... .......... .......... .......... .......... 22% 4.58M 36s
111800K .......... .......... .......... .......... .......... 22% 4.46M 36s
111850K .......... .......... .......... .......... .......... 22% 5.54M 36s
111900K .......... .......... .......... .......... .......... 22% 13.2M 36s
111950K .......... .......... .......... .......... .......... 22% 27.1M 36s
112000K .......... .......... .......... .......... .......... 22% 17.7M 36s
112050K .......... .......... .......... .......... .......... 22% 17.6M 36s
112100K .......... .......... .......... .......... .......... 22% 14.1M 36s
112150K .......... .......... .......... .......... .......... 22% 16.0M 36s
112200K .......... .......... .......... .......... .......... 22% 12.8M 36s
112250K .......... .......... .......... .......... .......... 22% 7.86M 36s
112300K .......... .......... .......... .......... .......... 22% 9.07M 36s
112350K .......... .......... .......... .......... .......... 22% 4.56M 36s
112400K .......... .......... .......... .......... .......... 22% 5.01M 36s
112450K .......... .......... .......... .......... .......... 22% 3.77M 36s
112500K .......... .......... .......... .......... .......... 22% 6.90M 36s
112550K .......... .......... .......... .......... .......... 22% 17.6M 36s
112600K .......... .......... .......... .......... .......... 22% 13.5M 36s
112650K .......... .......... .......... .......... .......... 22% 14.1M 36s
112700K .......... .......... .......... .......... .......... 22% 11.2M 36s
112750K .......... .......... .......... .......... .......... 22% 16.3M 36s
112800K .......... .......... .......... .......... .......... 22% 9.49M 36s
112850K .......... .......... .......... .......... .......... 22% 11.6M 36s
112900K .......... .......... .......... .......... .......... 22% 15.9M 36s
112950K .......... .......... .......... .......... .......... 22% 11.2M 36s
113000K .......... .......... .......... .......... .......... 22% 15.8M 36s
113050K .......... .......... .......... .......... .......... 22% 15.4M 36s
113100K .......... .......... .......... .......... .......... 22% 8.95M 36s
113150K .......... .......... .......... .......... .......... 22% 9.48M 36s
113200K .......... .......... .......... .......... .......... 22% 8.82M 36s
113250K .......... .......... .......... .......... .......... 22% 17.5M 36s
113300K .......... .......... .......... .......... .......... 22% 9.30M 36s
113350K .......... .......... .......... .......... .......... 22% 15.4M 36s
113400K .......... .......... .......... .......... .......... 22% 12.2M 36s
113450K .......... .......... .......... .......... .......... 22% 10.3M 36s
113500K .......... .......... .......... .......... .......... 22% 11.4M 36s
113550K .......... .......... .......... .......... .......... 22% 14.6M 36s
113600K .......... .......... .......... .......... .......... 22% 7.91M 36s
113650K .......... .......... .......... .......... .......... 22% 5.15M 36s
113700K .......... .......... .......... .......... .......... 22% 6.76M 36s
113750K .......... .......... .......... .......... .......... 22% 7.35M 36s
113800K .......... .......... .......... .......... .......... 22% 6.17M 36s
113850K .......... .......... .......... .......... .......... 22% 4.97M 36s
113900K .......... .......... .......... .......... .......... 22% 5.28M 36s
113950K .......... .......... .......... .......... .......... 22% 5.06M 36s
114000K .......... .......... .......... .......... .......... 22% 5.02M 36s
114050K .......... .......... .......... .......... .......... 22% 4.00M 36s
114100K .......... .......... .......... .......... .......... 22% 2.59M 36s
114150K .......... .......... .......... .......... .......... 22% 2.62M 36s
114200K .......... .......... .......... .......... .......... 22% 1.27M 36s
114250K .......... .......... .......... .......... .......... 22% 2.70M 36s
114300K .......... .......... .......... .......... .......... 22% 3.39M 36s
114350K .......... .......... .......... .......... .......... 22% 11.9M 36s
114400K .......... .......... .......... .......... .......... 22% 34.8M 36s
114450K .......... .......... .......... .......... .......... 22% 29.2M 36s
114500K .......... .......... .......... .......... .......... 22% 22.1M 36s
114550K .......... .......... .......... .......... .......... 22% 25.6M 36s
114600K .......... .......... .......... .......... .......... 22% 19.2M 36s
114650K .......... .......... .......... .......... .......... 22% 17.7M 36s
114700K .......... .......... .......... .......... .......... 22% 19.8M 36s
114750K .......... .......... .......... .......... .......... 22% 23.8M 36s
114800K .......... .......... .......... .......... .......... 22% 16.9M 36s
114850K .......... .......... .......... .......... .......... 22% 13.2M 36s
114900K .......... .......... .......... .......... .......... 22% 18.7M 36s
114950K .......... .......... .......... .......... .......... 22% 10.4M 36s
115000K .......... .......... .......... .......... .......... 22% 12.1M 36s
115050K .......... .......... .......... .......... .......... 22% 9.91M 36s
115100K .......... .......... .......... .......... .......... 22% 9.19M 36s
115150K .......... .......... .......... .......... .......... 22% 7.86M 36s
115200K .......... .......... .......... .......... .......... 22% 12.0M 36s
115250K .......... .......... .......... .......... .......... 22% 6.67M 36s
115300K .......... .......... .......... .......... .......... 22% 11.1M 36s
115350K .......... .......... .......... .......... .......... 22% 6.39M 36s
115400K .......... .......... .......... .......... .......... 22% 5.95M 36s
115450K .......... .......... .......... .......... .......... 22% 6.99M 36s
115500K .......... .......... .......... .......... .......... 22% 6.60M 36s
115550K .......... .......... .......... .......... .......... 22% 9.21M 36s
115600K .......... .......... .......... .......... .......... 22% 6.49M 36s
115650K .......... .......... .......... .......... .......... 22% 9.90M 36s
115700K .......... .......... .......... .......... .......... 22% 15.4M 36s
115750K .......... .......... .......... .......... .......... 22% 31.0M 36s
115800K .......... .......... .......... .......... .......... 22% 18.2M 36s
115850K .......... .......... .......... .......... .......... 22% 15.4M 36s
115900K .......... .......... .......... .......... .......... 22% 15.2M 36s
115950K .......... .......... .......... .......... .......... 22% 11.4M 36s
116000K .......... .......... .......... .......... .......... 22% 14.2M 36s
116050K .......... .......... .......... .......... .......... 22% 13.6M 36s
116100K .......... .......... .......... .......... .......... 23% 10.4M 36s
116150K .......... .......... .......... .......... .......... 23% 11.0M 36s
116200K .......... .......... .......... .......... .......... 23% 8.35M 36s
116250K .......... .......... .......... .......... .......... 23% 11.3M 36s
116300K .......... .......... .......... .......... .......... 23% 9.70M 36s
116350K .......... .......... .......... .......... .......... 23% 8.89M 36s
116400K .......... .......... .......... .......... .......... 23% 10.5M 36s
116450K .......... .......... .......... .......... .......... 23% 9.48M 36s
116500K .......... .......... .......... .......... .......... 23% 19.9M 36s
116550K .......... .......... .......... .......... .......... 23% 29.1M 36s
116600K .......... .......... .......... .......... .......... 23% 19.6M 36s
116650K .......... .......... .......... .......... .......... 23% 19.1M 36s
116700K .......... .......... .......... .......... .......... 23% 37.5M 36s
116750K .......... .......... .......... .......... .......... 23% 28.4M 36s
116800K .......... .......... .......... .......... .......... 23% 11.6M 36s
116850K .......... .......... .......... .......... .......... 23% 15.1M 36s
116900K .......... .......... .......... .......... .......... 23% 14.2M 36s
116950K .......... .......... .......... .......... .......... 23% 8.28M 36s
117000K .......... .......... .......... .......... .......... 23% 9.62M 36s
117050K .......... .......... .......... .......... .......... 23% 11.4M 36s
117100K .......... .......... .......... .......... .......... 23% 11.0M 36s
117150K .......... .......... .......... .......... .......... 23% 17.3M 36s
117200K .......... .......... .......... .......... .......... 23% 12.7M 36s
117250K .......... .......... .......... .......... .......... 23% 13.6M 36s
117300K .......... .......... .......... .......... .......... 23% 15.1M 36s
117350K .......... .......... .......... .......... .......... 23% 11.3M 36s
117400K .......... .......... .......... .......... .......... 23% 12.1M 36s
117450K .......... .......... .......... .......... .......... 23% 12.5M 36s
117500K .......... .......... .......... .......... .......... 23% 14.6M 36s
117550K .......... .......... .......... .......... .......... 23% 42.2M 36s
117600K .......... .......... .......... .......... .......... 23% 20.2M 36s
117650K .......... .......... .......... .......... .......... 23% 16.4M 36s
117700K .......... .......... .......... .......... .......... 23% 18.1M 36s
117750K .......... .......... .......... .......... .......... 23% 13.6M 36s
117800K .......... .......... .......... .......... .......... 23% 14.4M 36s
117850K .......... .......... .......... .......... .......... 23% 10.2M 36s
117900K .......... .......... .......... .......... .......... 23% 7.58M 36s
117950K .......... .......... .......... .......... .......... 23% 6.59M 36s
118000K .......... .......... .......... .......... .......... 23% 8.07M 36s
118050K .......... .......... .......... .......... .......... 23% 7.48M 36s
118100K .......... .......... .......... .......... .......... 23% 6.39M 36s
118150K .......... .......... .......... .......... .......... 23% 12.0M 36s
118200K .......... .......... .......... .......... .......... 23% 17.3M 36s
118250K .......... .......... .......... .......... .......... 23% 18.1M 36s
118300K .......... .......... .......... .......... .......... 23% 26.8M 36s
118350K .......... .......... .......... .......... .......... 23% 19.5M 36s
118400K .......... .......... .......... .......... .......... 23% 14.3M 36s
118450K .......... .......... .......... .......... .......... 23% 13.1M 36s
118500K .......... .......... .......... .......... .......... 23% 19.7M 36s
118550K .......... .......... .......... .......... .......... 23% 22.7M 36s
118600K .......... .......... .......... .......... .......... 23% 14.4M 36s
118650K .......... .......... .......... .......... .......... 23% 14.3M 36s
118700K .......... .......... .......... .......... .......... 23% 13.2M 35s
118750K .......... .......... .......... .......... .......... 23% 11.4M 35s
118800K .......... .......... .......... .......... .......... 23% 12.3M 35s
118850K .......... .......... .......... .......... .......... 23% 9.73M 35s
118900K .......... .......... .......... .......... .......... 23% 11.7M 35s
118950K .......... .......... .......... .......... .......... 23% 9.39M 35s
119000K .......... .......... .......... .......... .......... 23% 10.9M 35s
119050K .......... .......... .......... .......... .......... 23% 10.1M 35s
119100K .......... .......... .......... .......... .......... 23% 7.06M 35s
119150K .......... .......... .......... .......... .......... 23% 14.0M 35s
119200K .......... .......... .......... .......... .......... 23% 8.74M 35s
119250K .......... .......... .......... .......... .......... 23% 6.60M 35s
119300K .......... .......... .......... .......... .......... 23% 5.70M 35s
119350K .......... .......... .......... .......... .......... 23% 5.84M 35s
119400K .......... .......... .......... .......... .......... 23% 5.42M 35s
119450K .......... .......... .......... .......... .......... 23% 4.10M 36s
119500K .......... .......... .......... .......... .......... 23% 3.57M 36s
119550K .......... .......... .......... .......... .......... 23% 3.75M 36s
119600K .......... .......... .......... .......... .......... 23% 3.15M 36s
119650K .......... .......... .......... .......... .......... 23% 8.30M 36s
119700K .......... .......... .......... .......... .......... 23% 10.5M 36s
119750K .......... .......... .......... .......... .......... 23% 10.4M 36s
119800K .......... .......... .......... .......... .......... 23% 13.2M 36s
119850K .......... .......... .......... .......... .......... 23% 8.12M 36s
119900K .......... .......... .......... .......... .......... 23% 12.7M 36s
119950K .......... .......... .......... .......... .......... 23% 6.52M 36s
120000K .......... .......... .......... .......... .......... 23% 6.09M 36s
120050K .......... .......... .......... .......... .......... 23% 7.23M 36s
120100K .......... .......... .......... .......... .......... 23% 6.12M 36s
120150K .......... .......... .......... .......... .......... 23% 7.61M 36s
120200K .......... .......... .......... .......... .......... 23% 6.41M 36s
120250K .......... .......... .......... .......... .......... 23% 8.51M 36s
120300K .......... .......... .......... .......... .......... 23% 22.0M 36s
120350K .......... .......... .......... .......... .......... 23% 16.5M 36s
120400K .......... .......... .......... .......... .......... 23% 49.9M 36s
120450K .......... .......... .......... .......... .......... 23% 19.4M 36s
120500K .......... .......... .......... .......... .......... 23% 22.0M 36s
120550K .......... .......... .......... .......... .......... 23% 18.0M 36s
120600K .......... .......... .......... .......... .......... 23% 11.1M 36s
120650K .......... .......... .......... .......... .......... 23% 11.8M 35s
120700K .......... .......... .......... .......... .......... 23% 9.44M 35s
120750K .......... .......... .......... .......... .......... 23% 10.8M 35s
120800K .......... .......... .......... .......... .......... 23% 10.9M 35s
120850K .......... .......... .......... .......... .......... 23% 7.27M 35s
120900K .......... .......... .......... .......... .......... 23% 13.1M 35s
120950K .......... .......... .......... .......... .......... 23% 10.4M 35s
121000K .......... .......... .......... .......... .......... 23% 14.1M 35s
121050K .......... .......... .......... .......... .......... 23% 12.3M 35s
121100K .......... .......... .......... .......... .......... 23% 11.2M 35s
121150K .......... .......... .......... .......... .......... 24% 10.2M 35s
121200K .......... .......... .......... .......... .......... 24% 6.94M 35s
121250K .......... .......... .......... .......... .......... 24% 7.06M 35s
121300K .......... .......... .......... .......... .......... 24% 7.13M 35s
121350K .......... .......... .......... .......... .......... 24% 7.52M 35s
121400K .......... .......... .......... .......... .......... 24% 10.9M 35s
121450K .......... .......... .......... .......... .......... 24% 8.75M 35s
121500K .......... .......... .......... .......... .......... 24% 9.63M 35s
121550K .......... .......... .......... .......... .......... 24% 6.81M 35s
121600K .......... .......... .......... .......... .......... 24% 5.48M 35s
121650K .......... .......... .......... .......... .......... 24% 7.70M 35s
121700K .......... .......... .......... .......... .......... 24% 6.12M 35s
121750K .......... .......... .......... .......... .......... 24% 8.55M 35s
121800K .......... .......... .......... .......... .......... 24% 8.51M 35s
121850K .......... .......... .......... .......... .......... 24% 5.76M 35s
121900K .......... .......... .......... .......... .......... 24% 21.4M 35s
121950K .......... .......... .......... .......... .......... 24% 26.3M 35s
122000K .......... .......... .......... .......... .......... 24% 32.2M 35s
122050K .......... .......... .......... .......... .......... 24% 24.2M 35s
122100K .......... .......... .......... .......... .......... 24% 14.2M 35s
122150K .......... .......... .......... .......... .......... 24% 20.3M 35s
122200K .......... .......... .......... .......... .......... 24% 14.0M 35s
122250K .......... .......... .......... .......... .......... 24% 13.4M 35s
122300K .......... .......... .......... .......... .......... 24% 11.5M 35s
122350K .......... .......... .......... .......... .......... 24% 6.88M 35s
122400K .......... .......... .......... .......... .......... 24% 7.21M 35s
122450K .......... .......... .......... .......... .......... 24% 7.69M 35s
122500K .......... .......... .......... .......... .......... 24% 7.13M 35s
122550K .......... .......... .......... .......... .......... 24% 6.89M 35s
122600K .......... .......... .......... .......... .......... 24% 5.71M 35s
122650K .......... .......... .......... .......... .......... 24% 7.30M 35s
122700K .......... .......... .......... .......... .......... 24% 6.06M 35s
122750K .......... .......... .......... .......... .......... 24% 9.11M 35s
122800K .......... .......... .......... .......... .......... 24% 11.1M 35s
122850K .......... .......... .......... .......... .......... 24% 6.49M 35s
122900K .......... .......... .......... .......... .......... 24% 6.98M 35s
122950K .......... .......... .......... .......... .......... 24% 5.23M 35s
123000K .......... .......... .......... .......... .......... 24% 8.82M 35s
123050K .......... .......... .......... .......... .......... 24% 8.04M 35s
123100K .......... .......... .......... .......... .......... 24% 8.11M 35s
123150K .......... .......... .......... .......... .......... 24% 7.11M 35s
123200K .......... .......... .......... .......... .......... 24% 5.59M 35s
123250K .......... .......... .......... .......... .......... 24% 7.22M 35s
123300K .......... .......... .......... .......... .......... 24% 6.41M 35s
123350K .......... .......... .......... .......... .......... 24% 8.49M 35s
123400K .......... .......... .......... .......... .......... 24% 12.3M 35s
123450K .......... .......... .......... .......... .......... 24% 42.6M 35s
123500K .......... .......... .......... .......... .......... 24% 20.7M 35s
123550K .......... .......... .......... .......... .......... 24% 12.8M 35s
123600K .......... .......... .......... .......... .......... 24% 10.2M 35s
123650K .......... .......... .......... .......... .......... 24% 8.60M 35s
123700K .......... .......... .......... .......... .......... 24% 6.59M 35s
123750K .......... .......... .......... .......... .......... 24% 8.80M 35s
123800K .......... .......... .......... .......... .......... 24% 10.2M 35s
123850K .......... .......... .......... .......... .......... 24% 6.44M 35s
123900K .......... .......... .......... .......... .......... 24% 9.24M 35s
123950K .......... .......... .......... .......... .......... 24% 9.54M 35s
124000K .......... .......... .......... .......... .......... 24% 10.8M 35s
124050K .......... .......... .......... .......... .......... 24% 11.0M 35s
124100K .......... .......... .......... .......... .......... 24% 10.0M 35s
124150K .......... .......... .......... .......... .......... 24% 10.5M 35s
124200K .......... .......... .......... .......... .......... 24% 7.11M 35s
124250K .......... .......... .......... .......... .......... 24% 9.14M 35s
124300K .......... .......... .......... .......... .......... 24% 8.38M 35s
124350K .......... .......... .......... .......... .......... 24% 7.03M 35s
124400K .......... .......... .......... .......... .......... 24% 7.05M 35s
124450K .......... .......... .......... .......... .......... 24% 4.79M 35s
124500K .......... .......... .......... .......... .......... 24% 4.37M 35s
124550K .......... .......... .......... .......... .......... 24% 4.57M 35s
124600K .......... .......... .......... .......... .......... 24% 3.70M 35s
124650K .......... .......... .......... .......... .......... 24% 4.30M 35s
124700K .......... .......... .......... .......... .......... 24% 3.71M 35s
124750K .......... .......... .......... .......... .......... 24% 6.19M 35s
124800K .......... .......... .......... .......... .......... 24% 9.14M 35s
124850K .......... .......... .......... .......... .......... 24% 16.8M 35s
124900K .......... .......... .......... .......... .......... 24% 22.6M 35s
124950K .......... .......... .......... .......... .......... 24% 13.5M 35s
125000K .......... .......... .......... .......... .......... 24% 13.4M 35s
125050K .......... .......... .......... .......... .......... 24% 14.8M 35s
125100K .......... .......... .......... .......... .......... 24% 9.67M 35s
125150K .......... .......... .......... .......... .......... 24% 9.15M 35s
125200K .......... .......... .......... .......... .......... 24% 7.79M 35s
125250K .......... .......... .......... .......... .......... 24% 8.43M 35s
125300K .......... .......... .......... .......... .......... 24% 9.28M 35s
125350K .......... .......... .......... .......... .......... 24% 8.37M 35s
125400K .......... .......... .......... .......... .......... 24% 11.5M 35s
125450K .......... .......... .......... .......... .......... 24% 9.48M 35s
125500K .......... .......... .......... .......... .......... 24% 12.6M 35s
125550K .......... .......... .......... .......... .......... 24% 10.1M 35s
125600K .......... .......... .......... .......... .......... 24% 8.45M 35s
125650K .......... .......... .......... .......... .......... 24% 12.0M 35s
125700K .......... .......... .......... .......... .......... 24% 9.18M 35s
125750K .......... .......... .......... .......... .......... 24% 18.9M 35s
125800K .......... .......... .......... .......... .......... 24% 12.1M 35s
125850K .......... .......... .......... .......... .......... 24% 9.32M 35s
125900K .......... .......... .......... .......... .......... 24% 17.1M 35s
125950K .......... .......... .......... .......... .......... 24% 5.87M 35s
126000K .......... .......... .......... .......... .......... 24% 6.08M 35s
126050K .......... .......... .......... .......... .......... 24% 6.23M 35s
126100K .......... .......... .......... .......... .......... 24% 5.45M 35s
126150K .......... .......... .......... .......... .......... 24% 6.47M 35s
126200K .......... .......... .......... .......... .......... 25% 7.60M 35s
126250K .......... .......... .......... .......... .......... 25% 17.8M 35s
126300K .......... .......... .......... .......... .......... 25% 33.8M 35s
126350K .......... .......... .......... .......... .......... 25% 14.7M 35s
126400K .......... .......... .......... .......... .......... 25%  103M 35s
126450K .......... .......... .......... .......... .......... 25% 15.7M 35s
126500K .......... .......... .......... .......... .......... 25% 14.3M 35s
126550K .......... .......... .......... .......... .......... 25% 13.5M 35s
126600K .......... .......... .......... .......... .......... 25% 9.83M 35s
126650K .......... .......... .......... .......... .......... 25% 9.06M 35s
126700K .......... .......... .......... .......... .......... 25% 6.48M 35s
126750K .......... .......... .......... .......... .......... 25% 6.81M 35s
126800K .......... .......... .......... .......... .......... 25% 6.67M 35s
126850K .......... .......... .......... .......... .......... 25% 5.59M 35s
126900K .......... .......... .......... .......... .......... 25% 7.59M 35s
126950K .......... .......... .......... .......... .......... 25% 8.34M 35s
127000K .......... .......... .......... .......... .......... 25% 7.03M 35s
127050K .......... .......... .......... .......... .......... 25% 7.35M 35s
127100K .......... .......... .......... .......... .......... 25% 7.49M 35s
127150K .......... .......... .......... .......... .......... 25% 19.6M 35s
127200K .......... .......... .......... .......... .......... 25% 11.6M 35s
127250K .......... .......... .......... .......... .......... 25% 14.8M 35s
127300K .......... .......... .......... .......... .......... 25% 16.1M 35s
127350K .......... .......... .......... .......... .......... 25% 8.56M 35s
127400K .......... .......... .......... .......... .......... 25% 8.02M 35s
127450K .......... .......... .......... .......... .......... 25% 8.27M 35s
127500K .......... .......... .......... .......... .......... 25% 9.19M 35s
127550K .......... .......... .......... .......... .......... 25% 10.8M 35s
127600K .......... .......... .......... .......... .......... 25% 8.63M 35s
127650K .......... .......... .......... .......... .......... 25% 6.96M 35s
127700K .......... .......... .......... .......... .......... 25% 7.20M 35s
127750K .......... .......... .......... .......... .......... 25% 9.00M 35s
127800K .......... .......... .......... .......... .......... 25% 6.97M 35s
127850K .......... .......... .......... .......... .......... 25% 5.71M 35s
127900K .......... .......... .......... .......... .......... 25% 7.52M 35s
127950K .......... .......... .......... .......... .......... 25% 6.02M 35s
128000K .......... .......... .......... .......... .......... 25% 5.86M 35s
128050K .......... .......... .......... .......... .......... 25% 5.04M 35s
128100K .......... .......... .......... .......... .......... 25% 4.88M 35s
128150K .......... .......... .......... .......... .......... 25% 4.94M 35s
128200K .......... .......... .......... .......... .......... 25% 10.4M 35s
128250K .......... .......... .......... .......... .......... 25% 18.6M 35s
128300K .......... .......... .......... .......... .......... 25% 14.0M 35s
128350K .......... .......... .......... .......... .......... 25% 13.7M 35s
128400K .......... .......... .......... .......... .......... 25% 18.9M 35s
128450K .......... .......... .......... .......... .......... 25% 8.17M 35s
128500K .......... .......... .......... .......... .......... 25% 10.0M 35s
128550K .......... .......... .......... .......... .......... 25% 11.5M 35s
128600K .......... .......... .......... .......... .......... 25% 7.97M 35s
128650K .......... .......... .......... .......... .......... 25% 8.20M 35s
128700K .......... .......... .......... .......... .......... 25% 7.10M 35s
128750K .......... .......... .......... .......... .......... 25% 10.1M 35s
128800K .......... .......... .......... .......... .......... 25% 8.21M 35s
128850K .......... .......... .......... .......... .......... 25% 7.31M 35s
128900K .......... .......... .......... .......... .......... 25% 11.7M 35s
128950K .......... .......... .......... .......... .......... 25% 9.07M 35s
129000K .......... .......... .......... .......... .......... 25% 9.52M 35s
129050K .......... .......... .......... .......... .......... 25% 7.58M 35s
129100K .......... .......... .......... .......... .......... 25% 9.13M 35s
129150K .......... .......... .......... .......... .......... 25% 9.58M 35s
129200K .......... .......... .......... .......... .......... 25% 7.66M 35s
129250K .......... .......... .......... .......... .......... 25% 8.89M 35s
129300K .......... .......... .......... .......... .......... 25% 8.85M 35s
129350K .......... .......... .......... .......... .......... 25% 5.52M 35s
129400K .......... .......... .......... .......... .......... 25% 15.1M 35s
129450K .......... .......... .......... .......... .......... 25% 28.9M 35s
129500K .......... .......... .......... .......... .......... 25% 21.4M 35s
129550K .......... .......... .......... .......... .......... 25% 17.8M 35s
129600K .......... .......... .......... .......... .......... 25% 13.8M 35s
129650K .......... .......... .......... .......... .......... 25% 13.0M 35s
129700K .......... .......... .......... .......... .......... 25% 10.4M 35s
129750K .......... .......... .......... .......... .......... 25% 11.7M 35s
129800K .......... .......... .......... .......... .......... 25% 12.7M 35s
129850K .......... .......... .......... .......... .......... 25% 9.80M 35s
129900K .......... .......... .......... .......... .......... 25% 10.4M 35s
129950K .......... .......... .......... .......... .......... 25% 8.73M 35s
130000K .......... .......... .......... .......... .......... 25% 11.3M 35s
130050K .......... .......... .......... .......... .......... 25% 5.31M 35s
130100K .......... .......... .......... .......... .......... 25% 10.1M 35s
130150K .......... .......... .......... .......... .......... 25% 12.5M 35s
130200K .......... .......... .......... .......... .......... 25% 24.6M 35s
130250K .......... .......... .......... .......... .......... 25% 15.2M 35s
130300K .......... .......... .......... .......... .......... 25% 23.1M 35s
130350K .......... .......... .......... .......... .......... 25% 11.4M 35s
130400K .......... .......... .......... .......... .......... 25% 15.6M 35s
130450K .......... .......... .......... .......... .......... 25% 14.5M 35s
130500K .......... .......... .......... .......... .......... 25% 12.0M 35s
130550K .......... .......... .......... .......... .......... 25% 17.0M 35s
130600K .......... .......... .......... .......... .......... 25% 7.27M 35s
130650K .......... .......... .......... .......... .......... 25% 8.49M 35s
130700K .......... .......... .......... .......... .......... 25% 7.72M 35s
130750K .......... .......... .......... .......... .......... 25% 9.65M 35s
130800K .......... .......... .......... .......... .......... 25% 10.8M 35s
130850K .......... .......... .......... .......... .......... 25% 4.17M 35s
130900K .......... .......... .......... .......... .......... 25% 3.61M 35s
130950K .......... .......... .......... .......... .......... 25% 3.48M 35s
131000K .......... .......... .......... .......... .......... 25% 9.82M 35s
131050K .......... .......... .......... .......... .......... 25% 13.2M 35s
131100K .......... .......... .......... .......... .......... 25% 7.56M 35s
131150K .......... .......... .......... .......... .......... 25% 7.10M 35s
131200K .......... .......... .......... .......... .......... 25% 6.63M 35s
131250K .......... .......... .......... .......... .......... 26% 7.14M 35s
131300K .......... .......... .......... .......... .......... 26% 8.83M 35s
131350K .......... .......... .......... .......... .......... 26% 6.90M 35s
131400K .......... .......... .......... .......... .......... 26% 17.9M 35s
131450K .......... .......... .......... .......... .......... 26% 12.4M 35s
131500K .......... .......... .......... .......... .......... 26% 11.6M 35s
131550K .......... .......... .......... .......... .......... 26% 9.24M 35s
131600K .......... .......... .......... .......... .......... 26% 11.5M 35s
131650K .......... .......... .......... .......... .......... 26% 9.31M 35s
131700K .......... .......... .......... .......... .......... 26% 9.85M 35s
131750K .......... .......... .......... .......... .......... 26% 9.55M 35s
131800K .......... .......... .......... .......... .......... 26% 12.3M 35s
131850K .......... .......... .......... .......... .......... 26% 12.1M 35s
131900K .......... .......... .......... .......... .......... 26% 8.96M 35s
131950K .......... .......... .......... .......... .......... 26% 5.98M 35s
132000K .......... .......... .......... .......... .......... 26% 14.4M 35s
132050K .......... .......... .......... .......... .......... 26% 6.45M 35s
132100K .......... .......... .......... .......... .......... 26% 4.59M 35s
132150K .......... .......... .......... .......... .......... 26% 5.77M 35s
132200K .......... .......... .......... .......... .......... 26% 5.88M 35s
132250K .......... .......... .......... .......... .......... 26% 12.2M 35s
132300K .......... .......... .......... .......... .......... 26% 10.6M 35s
132350K .......... .......... .......... .......... .......... 26% 9.93M 35s
132400K .......... .......... .......... .......... .......... 26% 10.6M 35s
132450K .......... .......... .......... .......... .......... 26% 6.23M 35s
132500K .......... .......... .......... .......... .......... 26% 6.52M 35s
132550K .......... .......... .......... .......... .......... 26% 5.84M 35s
132600K .......... .......... .......... .......... .......... 26% 4.63M 35s
132650K .......... .......... .......... .......... .......... 26% 5.49M 35s
132700K .......... .......... .......... .......... .......... 26% 4.37M 35s
132750K .......... .......... .......... .......... .......... 26% 8.58M 35s
132800K .......... .......... .......... .......... .......... 26% 9.08M 35s
132850K .......... .......... .......... .......... .......... 26% 7.24M 35s
132900K .......... .......... .......... .......... .......... 26% 9.59M 35s
132950K .......... .......... .......... .......... .......... 26% 8.81M 35s
133000K .......... .......... .......... .......... .......... 26% 8.12M 35s
133050K .......... .......... .......... .......... .......... 26% 29.3M 35s
133100K .......... .......... .......... .......... .......... 26% 21.4M 35s
133150K .......... .......... .......... .......... .......... 26% 26.3M 35s
133200K .......... .......... .......... .......... .......... 26% 30.6M 35s
133250K .......... .......... .......... .......... .......... 26% 20.2M 35s
133300K .......... .......... .......... .......... .......... 26% 17.1M 35s
133350K .......... .......... .......... .......... .......... 26% 14.7M 35s
133400K .......... .......... .......... .......... .......... 26% 14.2M 35s
133450K .......... .......... .......... .......... .......... 26% 15.0M 35s
133500K .......... .......... .......... .......... .......... 26% 12.0M 35s
133550K .......... .......... .......... .......... .......... 26% 12.3M 35s
133600K .......... .......... .......... .......... .......... 26% 10.7M 35s
133650K .......... .......... .......... .......... .......... 26% 13.7M 35s
133700K .......... .......... .......... .......... .......... 26% 12.0M 35s
133750K .......... .......... .......... .......... .......... 26% 11.9M 35s
133800K .......... .......... .......... .......... .......... 26% 6.81M 35s
133850K .......... .......... .......... .......... .......... 26% 5.83M 35s
133900K .......... .......... .......... .......... .......... 26% 5.97M 35s
133950K .......... .......... .......... .......... .......... 26% 4.83M 35s
134000K .......... .......... .......... .......... .......... 26% 8.88M 35s
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134100K .......... .......... .......... .......... .......... 26% 7.73M 35s
134150K .......... .......... .......... .......... .......... 26% 7.38M 35s
134200K .......... .......... .......... .......... .......... 26% 5.37M 35s
134250K .......... .......... .......... .......... .......... 26% 4.86M 35s
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135100K .......... .......... .......... .......... .......... 26% 5.48M 35s
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138250K .......... .......... .......... .......... .......... 27%  201M 35s
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138350K .......... .......... .......... .......... .......... 27% 99.2M 35s
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148050K .......... .......... .......... .......... .......... 29% 8.37M 35s
148100K .......... .......... .......... .......... .......... 29% 6.94M 35s
148150K .......... .......... .......... .......... .......... 29% 6.84M 35s
148200K .......... .......... .......... .......... .......... 29% 8.07M 35s
148250K .......... .......... .......... .......... .......... 29% 10.1M 35s
148300K .......... .......... .......... .......... .......... 29% 9.13M 35s
148350K .......... .......... .......... .......... .......... 29% 8.49M 35s
148400K .......... .......... .......... .......... .......... 29% 8.99M 35s
148450K .......... .......... .......... .......... .......... 29% 9.30M 35s
148500K .......... .......... .......... .......... .......... 29% 35.0M 35s
148550K .......... .......... .......... .......... .......... 29% 34.5M 35s
148600K .......... .......... .......... .......... .......... 29% 19.4M 35s
148650K .......... .......... .......... .......... .......... 29% 79.9M 35s
148700K .......... .......... .......... .......... .......... 29% 20.9M 35s
148750K .......... .......... .......... .......... .......... 29% 60.2M 35s
148800K .......... .......... .......... .......... .......... 29% 14.7M 35s
148850K .......... .......... .......... .......... .......... 29% 14.1M 35s
148900K .......... .......... .......... .......... .......... 29% 12.0M 35s
148950K .......... .......... .......... .......... .......... 29% 15.9M 34s
149000K .......... .......... .......... .......... .......... 29% 8.78M 34s
149050K .......... .......... .......... .......... .......... 29% 7.32M 34s
149100K .......... .......... .......... .......... .......... 29% 6.00M 34s
149150K .......... .......... .......... .......... .......... 29% 11.5M 34s
149200K .......... .......... .......... .......... .......... 29% 9.68M 34s
149250K .......... .......... .......... .......... .......... 29% 11.2M 34s
149300K .......... .......... .......... .......... .......... 29% 6.96M 34s
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149400K .......... .......... .......... .......... .......... 29% 5.52M 34s
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149500K .......... .......... .......... .......... .......... 29% 6.41M 34s
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149900K .......... .......... .......... .......... .......... 29% 7.00M 34s
149950K .......... .......... .......... .......... .......... 29% 9.40M 34s
150000K .......... .......... .......... .......... .......... 29% 8.55M 34s
150050K .......... .......... .......... .......... .......... 29% 4.50M 34s
150100K .......... .......... .......... .......... .......... 29% 3.16M 35s
150150K .......... .......... .......... .......... .......... 29% 4.19M 35s
150200K .......... .......... .......... .......... .......... 29% 9.51M 35s
150250K .......... .......... .......... .......... .......... 29% 31.2M 35s
150300K .......... .......... .......... .......... .......... 29% 21.1M 34s
150350K .......... .......... .......... .......... .......... 29% 33.7M 34s
150400K .......... .......... .......... .......... .......... 29% 27.5M 34s
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150500K .......... .......... .......... .......... .......... 29% 20.6M 34s
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150600K .......... .......... .......... .......... .......... 29% 9.09M 34s
150650K .......... .......... .......... .......... .......... 29% 7.51M 34s
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150750K .......... .......... .......... .......... .......... 29% 7.60M 34s
150800K .......... .......... .......... .......... .......... 29% 5.95M 34s
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150900K .......... .......... .......... .......... .......... 29% 7.78M 34s
150950K .......... .......... .......... .......... .......... 29% 6.27M 34s
151000K .......... .......... .......... .......... .......... 29% 6.02M 34s
151050K .......... .......... .......... .......... .......... 29% 6.56M 34s
151100K .......... .......... .......... .......... .......... 29% 5.50M 34s
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151200K .......... .......... .......... .......... .......... 29% 6.13M 34s
151250K .......... .......... .......... .......... .......... 29% 20.4M 34s
151300K .......... .......... .......... .......... .......... 29% 15.2M 34s
151350K .......... .......... .......... .......... .......... 29% 20.1M 34s
151400K .......... .......... .......... .......... .......... 29% 14.4M 34s
151450K .......... .......... .......... .......... .......... 30% 12.5M 34s
151500K .......... .......... .......... .......... .......... 30% 17.0M 34s
151550K .......... .......... .......... .......... .......... 30% 5.96M 34s
151600K .......... .......... .......... .......... .......... 30% 14.2M 34s
151650K .......... .......... .......... .......... .......... 30% 13.1M 34s
151700K .......... .......... .......... .......... .......... 30% 7.56M 34s
151750K .......... .......... .......... .......... .......... 30% 8.63M 34s
151800K .......... .......... .......... .......... .......... 30% 11.4M 34s
151850K .......... .......... .......... .......... .......... 30% 9.15M 34s
151900K .......... .......... .......... .......... .......... 30% 8.96M 34s
151950K .......... .......... .......... .......... .......... 30% 8.51M 34s
152000K .......... .......... .......... .......... .......... 30% 10.0M 34s
152050K .......... .......... .......... .......... .......... 30% 10.8M 34s
152100K .......... .......... .......... .......... .......... 30% 8.66M 34s
152150K .......... .......... .......... .......... .......... 30% 9.29M 34s
152200K .......... .......... .......... .......... .......... 30% 7.37M 34s
152250K .......... .......... .......... .......... .......... 30% 10.6M 34s
152300K .......... .......... .......... .......... .......... 30% 10.4M 34s
152350K .......... .......... .......... .......... .......... 30% 7.88M 34s
152400K .......... .......... .......... .......... .......... 30% 9.16M 34s
152450K .......... .......... .......... .......... .......... 30% 8.40M 34s
152500K .......... .......... .......... .......... .......... 30% 9.46M 34s
152550K .......... .......... .......... .......... .......... 30% 8.99M 34s
152600K .......... .......... .......... .......... .......... 30% 6.97M 34s
152650K .......... .......... .......... .......... .......... 30% 7.14M 34s
152700K .......... .......... .......... .......... .......... 30% 17.6M 34s
152750K .......... .......... .......... .......... .......... 30% 33.5M 34s
152800K .......... .......... .......... .......... .......... 30% 20.3M 34s
152850K .......... .......... .......... .......... .......... 30% 15.4M 34s
152900K .......... .......... .......... .......... .......... 30% 32.2M 34s
152950K .......... .......... .......... .......... .......... 30% 17.7M 34s
153000K .......... .......... .......... .......... .......... 30% 13.5M 34s
153050K .......... .......... .......... .......... .......... 30% 17.5M 34s
153100K .......... .......... .......... .......... .......... 30% 12.0M 34s
153150K .......... .......... .......... .......... .......... 30% 16.6M 34s
153200K .......... .......... .......... .......... .......... 30% 12.5M 34s
153250K .......... .......... .......... .......... .......... 30% 15.3M 34s
153300K .......... .......... .......... .......... .......... 30% 12.1M 34s
153350K .......... .......... .......... .......... .......... 30% 8.28M 34s
153400K .......... .......... .......... .......... .......... 30% 7.28M 34s
153450K .......... .......... .......... .......... .......... 30% 5.59M 34s
153500K .......... .......... .......... .......... .......... 30% 6.82M 34s
153550K .......... .......... .......... .......... .......... 30% 6.18M 34s
153600K .......... .......... .......... .......... .......... 30% 5.30M 34s
153650K .......... .......... .......... .......... .......... 30% 24.9M 34s
153700K .......... .......... .......... .......... .......... 30% 15.9M 34s
153750K .......... .......... .......... .......... .......... 30% 37.0M 34s
153800K .......... .......... .......... .......... .......... 30% 15.1M 34s
153850K .......... .......... .......... .......... .......... 30% 12.7M 34s
153900K .......... .......... .......... .......... .......... 30% 13.3M 34s
153950K .......... .......... .......... .......... .......... 30% 11.7M 34s
154000K .......... .......... .......... .......... .......... 30% 11.9M 34s
154050K .......... .......... .......... .......... .......... 30% 10.3M 34s
154100K .......... .......... .......... .......... .......... 30% 7.63M 34s
154150K .......... .......... .......... .......... .......... 30% 11.0M 34s
154200K .......... .......... .......... .......... .......... 30% 10.5M 34s
154250K .......... .......... .......... .......... .......... 30% 13.2M 34s
154300K .......... .......... .......... .......... .......... 30% 14.6M 34s
154350K .......... .......... .......... .......... .......... 30% 10.7M 34s
154400K .......... .......... .......... .......... .......... 30% 12.9M 34s
154450K .......... .......... .......... .......... .......... 30% 8.61M 34s
154500K .......... .......... .......... .......... .......... 30% 10.4M 34s
154550K .......... .......... .......... .......... .......... 30% 21.2M 34s
154600K .......... .......... .......... .......... .......... 30% 32.3M 34s
154650K .......... .......... .......... .......... .......... 30% 33.3M 34s
154700K .......... .......... .......... .......... .......... 30% 25.0M 34s
154750K .......... .......... .......... .......... .......... 30% 40.1M 34s
154800K .......... .......... .......... .......... .......... 30% 21.3M 34s
154850K .......... .......... .......... .......... .......... 30% 26.0M 34s
154900K .......... .......... .......... .......... .......... 30% 24.2M 34s
154950K .......... .......... .......... .......... .......... 30% 13.8M 34s
155000K .......... .......... .......... .......... .......... 30% 13.2M 34s
155050K .......... .......... .......... .......... .......... 30% 12.1M 34s
155100K .......... .......... .......... .......... .......... 30% 15.0M 34s
155150K .......... .......... .......... .......... .......... 30% 13.1M 34s
155200K .......... .......... .......... .......... .......... 30% 13.1M 34s
155250K .......... .......... .......... .......... .......... 30% 15.8M 34s
155300K .......... .......... .......... .......... .......... 30% 13.5M 34s
155350K .......... .......... .......... .......... .......... 30% 15.6M 34s
155400K .......... .......... .......... .......... .......... 30% 15.6M 34s
155450K .......... .......... .......... .......... .......... 30% 11.5M 34s
155500K .......... .......... .......... .......... .......... 30% 16.6M 34s
155550K .......... .......... .......... .......... .......... 30% 16.6M 34s
155600K .......... .......... .......... .......... .......... 30% 13.3M 34s
155650K .......... .......... .......... .......... .......... 30% 13.9M 34s
155700K .......... .......... .......... .......... .......... 30% 12.7M 34s
155750K .......... .......... .......... .......... .......... 30% 16.3M 34s
155800K .......... .......... .......... .......... .......... 30% 9.97M 34s
155850K .......... .......... .......... .......... .......... 30% 10.9M 34s
155900K .......... .......... .......... .......... .......... 30% 12.4M 34s
155950K .......... .......... .......... .......... .......... 30% 10.8M 34s
156000K .......... .......... .......... .......... .......... 30% 11.8M 34s
156050K .......... .......... .......... .......... .......... 30% 12.7M 34s
156100K .......... .......... .......... .......... .......... 30% 11.3M 34s
156150K .......... .......... .......... .......... .......... 30% 12.8M 34s
156200K .......... .......... .......... .......... .......... 30% 10.3M 34s
156250K .......... .......... .......... .......... .......... 30% 14.5M 34s
156300K .......... .......... .......... .......... .......... 30% 9.38M 34s
156350K .......... .......... .......... .......... .......... 30% 10.4M 34s
156400K .......... .......... .......... .......... .......... 30% 7.61M 34s
156450K .......... .......... .......... .......... .......... 30% 11.9M 34s
156500K .......... .......... .......... .......... .......... 31% 12.4M 34s
156550K .......... .......... .......... .......... .......... 31% 17.8M 34s
156600K .......... .......... .......... .......... .......... 31% 12.6M 34s
156650K .......... .......... .......... .......... .......... 31% 13.8M 34s
156700K .......... .......... .......... .......... .......... 31% 12.8M 34s
156750K .......... .......... .......... .......... .......... 31% 13.5M 34s
156800K .......... .......... .......... .......... .......... 31% 18.6M 34s
156850K .......... .......... .......... .......... .......... 31% 12.7M 34s
156900K .......... .......... .......... .......... .......... 31% 13.1M 34s
156950K .......... .......... .......... .......... .......... 31% 13.3M 34s
157000K .......... .......... .......... .......... .......... 31% 10.8M 34s
157050K .......... .......... .......... .......... .......... 31% 10.7M 34s
157100K .......... .......... .......... .......... .......... 31% 10.5M 34s
157150K .......... .......... .......... .......... .......... 31% 12.2M 34s
157200K .......... .......... .......... .......... .......... 31% 7.24M 34s
157250K .......... .......... .......... .......... .......... 31% 7.51M 34s
157300K .......... .......... .......... .......... .......... 31% 9.24M 34s
157350K .......... .......... .......... .......... .......... 31% 7.09M 34s
157400K .......... .......... .......... .......... .......... 31% 4.32M 34s
157450K .......... .......... .......... .......... .......... 31% 4.79M 34s
157500K .......... .......... .......... .......... .......... 31% 4.82M 34s
157550K .......... .......... .......... .......... .......... 31% 4.12M 34s
157600K .......... .......... .......... .......... .......... 31% 2.02M 34s
157650K .......... .......... .......... .......... .......... 31% 3.21M 34s
157700K .......... .......... .......... .......... .......... 31% 4.67M 34s
157750K .......... .......... .......... .......... .......... 31% 4.13M 34s
157800K .......... .......... .......... .......... .......... 31% 3.62M 34s
157850K .......... .......... .......... .......... .......... 31% 3.24M 34s
157900K .......... .......... .......... .......... .......... 31% 9.31M 34s
157950K .......... .......... .......... .......... .......... 31% 10.7M 34s
158000K .......... .......... .......... .......... .......... 31% 10.1M 34s
158050K .......... .......... .......... .......... .......... 31% 8.30M 34s
158100K .......... .......... .......... .......... .......... 31% 9.46M 34s
158150K .......... .......... .......... .......... .......... 31% 11.2M 34s
158200K .......... .......... .......... .......... .......... 31% 9.42M 34s
158250K .......... .......... .......... .......... .......... 31% 7.77M 34s
158300K .......... .......... .......... .......... .......... 31% 15.2M 34s
158350K .......... .......... .......... .......... .......... 31% 11.1M 34s
158400K .......... .......... .......... .......... .......... 31% 14.8M 34s
158450K .......... .......... .......... .......... .......... 31% 10.6M 34s
158500K .......... .......... .......... .......... .......... 31% 14.1M 34s
158550K .......... .......... .......... .......... .......... 31% 11.5M 34s
158600K .......... .......... .......... .......... .......... 31% 13.2M 34s
158650K .......... .......... .......... .......... .......... 31% 9.80M 34s
158700K .......... .......... .......... .......... .......... 31% 5.95M 34s
158750K .......... .......... .......... .......... .......... 31% 8.77M 34s
158800K .......... .......... .......... .......... .......... 31% 8.68M 34s
158850K .......... .......... .......... .......... .......... 31% 7.53M 34s
158900K .......... .......... .......... .......... .......... 31% 9.04M 34s
158950K .......... .......... .......... .......... .......... 31% 5.55M 34s
159000K .......... .......... .......... .......... .......... 31% 9.83M 34s
159050K .......... .......... .......... .......... .......... 31% 14.8M 34s
159100K .......... .......... .......... .......... .......... 31% 25.3M 34s
159150K .......... .......... .......... .......... .......... 31% 21.7M 34s
159200K .......... .......... .......... .......... .......... 31% 30.0M 34s
159250K .......... .......... .......... .......... .......... 31% 30.6M 34s
159300K .......... .......... .......... .......... .......... 31% 23.0M 34s
159350K .......... .......... .......... .......... .......... 31% 20.0M 34s
159400K .......... .......... .......... .......... .......... 31% 41.6M 34s
159450K .......... .......... .......... .......... .......... 31% 15.7M 34s
159500K .......... .......... .......... .......... .......... 31% 14.0M 34s
159550K .......... .......... .......... .......... .......... 31% 12.2M 34s
159600K .......... .......... .......... .......... .......... 31% 6.87M 34s
159650K .......... .......... .......... .......... .......... 31% 8.26M 34s
159700K .......... .......... .......... .......... .......... 31% 6.00M 34s
159750K .......... .......... .......... .......... .......... 31% 11.2M 34s
159800K .......... .......... .......... .......... .......... 31% 7.82M 34s
159850K .......... .......... .......... .......... .......... 31% 6.70M 34s
159900K .......... .......... .......... .......... .......... 31% 7.64M 34s
159950K .......... .......... .......... .......... .......... 31% 7.62M 34s
160000K .......... .......... .......... .......... .......... 31% 9.92M 34s
160050K .......... .......... .......... .......... .......... 31% 10.3M 34s
160100K .......... .......... .......... .......... .......... 31% 6.75M 34s
160150K .......... .......... .......... .......... .......... 31% 9.11M 34s
160200K .......... .......... .......... .......... .......... 31% 7.31M 34s
160250K .......... .......... .......... .......... .......... 31% 9.08M 34s
160300K .......... .......... .......... .......... .......... 31% 8.72M 34s
160350K .......... .......... .......... .......... .......... 31% 6.39M 34s
160400K .......... .......... .......... .......... .......... 31% 9.83M 34s
160450K .......... .......... .......... .......... .......... 31% 4.27M 34s
160500K .......... .......... .......... .......... .......... 31% 3.74M 34s
160550K .......... .......... .......... .......... .......... 31% 3.71M 34s
160600K .......... .......... .......... .......... .......... 31% 2.92M 34s
160650K .......... .......... .......... .......... .......... 31% 9.16M 34s
160700K .......... .......... .......... .......... .......... 31% 17.7M 34s
160750K .......... .......... .......... .......... .......... 31% 18.9M 34s
160800K .......... .......... .......... .......... .......... 31% 15.6M 34s
160850K .......... .......... .......... .......... .......... 31% 16.4M 34s
160900K .......... .......... .......... .......... .......... 31% 13.1M 34s
160950K .......... .......... .......... .......... .......... 31% 13.7M 34s
161000K .......... .......... .......... .......... .......... 31% 13.4M 34s
161050K .......... .......... .......... .......... .......... 31% 13.5M 34s
161100K .......... .......... .......... .......... .......... 31% 10.4M 34s
161150K .......... .......... .......... .......... .......... 31% 12.2M 34s
161200K .......... .......... .......... .......... .......... 31% 8.80M 34s
161250K .......... .......... .......... .......... .......... 31% 18.7M 34s
161300K .......... .......... .......... .......... .......... 31% 11.5M 34s
161350K .......... .......... .......... .......... .......... 31% 12.9M 34s
161400K .......... .......... .......... .......... .......... 31% 12.6M 34s
161450K .......... .......... .......... .......... .......... 31% 13.7M 34s
161500K .......... .......... .......... .......... .......... 31% 9.74M 34s
161550K .......... .......... .......... .......... .......... 32% 8.90M 33s
161600K .......... .......... .......... .......... .......... 32% 7.28M 33s
161650K .......... .......... .......... .......... .......... 32% 10.2M 33s
161700K .......... .......... .......... .......... .......... 32% 6.61M 33s
161750K .......... .......... .......... .......... .......... 32% 6.22M 33s
161800K .......... .......... .......... .......... .......... 32% 8.20M 33s
161850K .......... .......... .......... .......... .......... 32% 6.38M 33s
161900K .......... .......... .......... .......... .......... 32% 8.01M 33s
161950K .......... .......... .......... .......... .......... 32% 6.56M 33s
162000K .......... .......... .......... .......... .......... 32% 10.6M 33s
162050K .......... .......... .......... .......... .......... 32% 26.1M 33s
162100K .......... .......... .......... .......... .......... 32% 29.8M 33s
162150K .......... .......... .......... .......... .......... 32% 20.2M 33s
162200K .......... .......... .......... .......... .......... 32% 35.7M 33s
162250K .......... .......... .......... .......... .......... 32% 22.1M 33s
162300K .......... .......... .......... .......... .......... 32% 29.0M 33s
162350K .......... .......... .......... .......... .......... 32% 16.4M 33s
162400K .......... .......... .......... .......... .......... 32% 19.6M 33s
162450K .......... .......... .......... .......... .......... 32% 11.0M 33s
162500K .......... .......... .......... .......... .......... 32% 8.33M 33s
162550K .......... .......... .......... .......... .......... 32% 9.73M 33s
162600K .......... .......... .......... .......... .......... 32% 8.91M 33s
162650K .......... .......... .......... .......... .......... 32% 12.3M 33s
162700K .......... .......... .......... .......... .......... 32% 10.2M 33s
162750K .......... .......... .......... .......... .......... 32% 10.8M 33s
162800K .......... .......... .......... .......... .......... 32% 10.3M 33s
162850K .......... .......... .......... .......... .......... 32% 6.39M 33s
162900K .......... .......... .......... .......... .......... 32% 8.95M 33s
162950K .......... .......... .......... .......... .......... 32% 6.44M 33s
163000K .......... .......... .......... .......... .......... 32% 8.93M 33s
163050K .......... .......... .......... .......... .......... 32% 8.12M 33s
163100K .......... .......... .......... .......... .......... 32% 7.59M 33s
163150K .......... .......... .......... .......... .......... 32% 7.96M 33s
163200K .......... .......... .......... .......... .......... 32% 10.0M 33s
163250K .......... .......... .......... .......... .......... 32% 11.0M 33s
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163350K .......... .......... .......... .......... .......... 32% 10.6M 33s
163400K .......... .......... .......... .......... .......... 32% 11.2M 33s
163450K .......... .......... .......... .......... .......... 32% 5.18M 33s
163500K .......... .......... .......... .......... .......... 32% 8.43M 33s
163550K .......... .......... .......... .......... .......... 32% 13.8M 33s
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163650K .......... .......... .......... .......... .......... 32% 19.7M 33s
163700K .......... .......... .......... .......... .......... 32% 11.6M 33s
163750K .......... .......... .......... .......... .......... 32% 12.1M 33s
163800K .......... .......... .......... .......... .......... 32% 14.2M 33s
163850K .......... .......... .......... .......... .......... 32% 11.4M 33s
163900K .......... .......... .......... .......... .......... 32% 12.3M 33s
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164000K .......... .......... .......... .......... .......... 32% 13.0M 33s
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164100K .......... .......... .......... .......... .......... 32% 7.53M 33s
164150K .......... .......... .......... .......... .......... 32% 9.13M 33s
164200K .......... .......... .......... .......... .......... 32% 10.7M 33s
164250K .......... .......... .......... .......... .......... 32% 10.5M 33s
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164400K .......... .......... .......... .......... .......... 32% 6.63M 33s
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164900K .......... .......... .......... .......... .......... 32% 2.26M 33s
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165000K .......... .......... .......... .......... .......... 32% 26.7M 33s
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165100K .......... .......... .......... .......... .......... 32% 19.1M 33s
165150K .......... .......... .......... .......... .......... 32% 22.2M 33s
165200K .......... .......... .......... .......... .......... 32% 13.2M 33s
165250K .......... .......... .......... .......... .......... 32% 17.0M 33s
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165650K .......... .......... .......... .......... .......... 32% 11.5M 33s
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165750K .......... .......... .......... .......... .......... 32% 9.70M 33s
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165850K .......... .......... .......... .......... .......... 32% 11.0M 33s
165900K .......... .......... .......... .......... .......... 32% 9.23M 33s
165950K .......... .......... .......... .......... .......... 32% 11.9M 33s
166000K .......... .......... .......... .......... .......... 32% 23.0M 33s
166050K .......... .......... .......... .......... .......... 32% 17.6M 33s
166100K .......... .......... .......... .......... .......... 32% 13.8M 33s
166150K .......... .......... .......... .......... .......... 32% 17.0M 33s
166200K .......... .......... .......... .......... .......... 32% 13.5M 33s
166250K .......... .......... .......... .......... .......... 32% 20.8M 33s
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166350K .......... .......... .......... .......... .......... 32% 14.3M 33s
166400K .......... .......... .......... .......... .......... 32% 12.6M 33s
166450K .......... .......... .......... .......... .......... 32% 21.5M 33s
166500K .......... .......... .......... .......... .......... 32% 23.6M 33s
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166600K .......... .......... .......... .......... .......... 33% 13.6M 33s
166650K .......... .......... .......... .......... .......... 33% 21.3M 33s
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166750K .......... .......... .......... .......... .......... 33% 14.4M 33s
166800K .......... .......... .......... .......... .......... 33% 11.9M 33s
166850K .......... .......... .......... .......... .......... 33% 7.40M 33s
166900K .......... .......... .......... .......... .......... 33% 4.25M 33s
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167000K .......... .......... .......... .......... .......... 33% 6.82M 33s
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167100K .......... .......... .......... .......... .......... 33% 10.4M 33s
167150K .......... .......... .......... .......... .......... 33% 11.2M 33s
167200K .......... .......... .......... .......... .......... 33% 16.5M 33s
167250K .......... .......... .......... .......... .......... 33% 12.5M 33s
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167350K .......... .......... .......... .......... .......... 33% 9.01M 33s
167400K .......... .......... .......... .......... .......... 33% 11.5M 33s
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167600K .......... .......... .......... .......... .......... 33% 7.83M 33s
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167700K .......... .......... .......... .......... .......... 33% 7.35M 33s
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167800K .......... .......... .......... .......... .......... 33% 6.31M 33s
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167900K .......... .......... .......... .......... .......... 33% 3.15M 33s
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168000K .......... .......... .......... .......... .......... 33% 9.80M 33s
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168100K .......... .......... .......... .......... .......... 33% 7.39M 33s
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168200K .......... .......... .......... .......... .......... 33% 4.99M 33s
168250K .......... .......... .......... .......... .......... 33% 8.09M 33s
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169000K .......... .......... .......... .......... .......... 33% 9.38M 33s
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169100K .......... .......... .......... .......... .......... 33% 6.93M 33s
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169200K .......... .......... .......... .......... .......... 33% 7.58M 33s
169250K .......... .......... .......... .......... .......... 33% 8.78M 33s
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170000K .......... .......... .......... .......... .......... 33% 10.3M 33s
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170200K .......... .......... .......... .......... .......... 33% 8.74M 33s
170250K .......... .......... .......... .......... .......... 33% 9.67M 33s
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171000K .......... .......... .......... .......... .......... 33% 5.49M 33s
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172000K .......... .......... .......... .......... .......... 34% 36.4M 33s
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172150K .......... .......... .......... .......... .......... 34%  178M 33s
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172250K .......... .......... .......... .......... .......... 34% 35.0M 33s
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174250K .......... .......... .......... .......... .......... 34% 27.4M 33s
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175150K .......... .......... .......... .......... .......... 34% 21.2M 33s
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175250K .......... .......... .......... .......... .......... 34% 28.0M 33s
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176350K .......... .......... .......... .......... .......... 34% 5.61M 32s
176400K .......... .......... .......... .......... .......... 34% 6.61M 32s
176450K .......... .......... .......... .......... .......... 34% 4.37M 32s
176500K .......... .......... .......... .......... .......... 34% 5.03M 32s
176550K .......... .......... .......... .......... .......... 34% 4.49M 32s
176600K .......... .......... .......... .......... .......... 34% 3.57M 32s
176650K .......... .......... .......... .......... .......... 34% 4.82M 33s
176700K .......... .......... .......... .......... .......... 35% 4.43M 33s
176750K .......... .......... .......... .......... .......... 35% 5.65M 33s
176800K .......... .......... .......... .......... .......... 35% 7.44M 33s
176850K .......... .......... .......... .......... .......... 35% 7.14M 33s
176900K .......... .......... .......... .......... .......... 35% 4.55M 33s
176950K .......... .......... .......... .......... .......... 35% 5.07M 33s
177000K .......... .......... .......... .......... .......... 35% 5.73M 33s
177050K .......... .......... .......... .......... .......... 35% 5.47M 33s
177100K .......... .......... .......... .......... .......... 35% 4.96M 33s
177150K .......... .......... .......... .......... .......... 35% 13.7M 33s
177200K .......... .......... .......... .......... .......... 35% 9.46M 33s
177250K .......... .......... .......... .......... .......... 35% 11.9M 33s
177300K .......... .......... .......... .......... .......... 35% 12.8M 32s
177350K .......... .......... .......... .......... .......... 35% 11.6M 32s
177400K .......... .......... .......... .......... .......... 35% 11.1M 32s
177450K .......... .......... .......... .......... .......... 35% 10.4M 32s
177500K .......... .......... .......... .......... .......... 35% 13.3M 32s
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177600K .......... .......... .......... .......... .......... 35% 10.7M 32s
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177700K .......... .......... .......... .......... .......... 35% 7.17M 32s
177750K .......... .......... .......... .......... .......... 35% 8.02M 32s
177800K .......... .......... .......... .......... .......... 35% 10.2M 32s
177850K .......... .......... .......... .......... .......... 35% 7.97M 32s
177900K .......... .......... .......... .......... .......... 35% 7.94M 32s
177950K .......... .......... .......... .......... .......... 35% 6.63M 32s
178000K .......... .......... .......... .......... .......... 35% 8.98M 32s
178050K .......... .......... .......... .......... .......... 35% 9.36M 32s
178100K .......... .......... .......... .......... .......... 35% 4.08M 32s
178150K .......... .......... .......... .......... .......... 35% 5.46M 32s
178200K .......... .......... .......... .......... .......... 35% 6.01M 32s
178250K .......... .......... .......... .......... .......... 35% 5.36M 32s
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178500K .......... .......... .......... .......... .......... 35% 7.16M 32s
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178600K .......... .......... .......... .......... .......... 35% 5.12M 32s
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178800K .......... .......... .......... .......... .......... 35% 8.33M 32s
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178900K .......... .......... .......... .......... .......... 35% 6.03M 32s
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179000K .......... .......... .......... .......... .......... 35% 5.68M 32s
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179100K .......... .......... .......... .......... .......... 35% 6.28M 32s
179150K .......... .......... .......... .......... .......... 35% 8.39M 32s
179200K .......... .......... .......... .......... .......... 35% 6.24M 32s
179250K .......... .......... .......... .......... .......... 35% 7.66M 32s
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179450K .......... .......... .......... .......... .......... 35% 7.13M 32s
179500K .......... .......... .......... .......... .......... 35% 9.43M 32s
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179750K .......... .......... .......... .......... .......... 35% 9.24M 32s
179800K .......... .......... .......... .......... .......... 35% 11.2M 32s
179850K .......... .......... .......... .......... .......... 35% 5.90M 32s
179900K .......... .......... .......... .......... .......... 35% 4.39M 32s
179950K .......... .......... .......... .......... .......... 35% 3.78M 32s
180000K .......... .......... .......... .......... .......... 35% 3.72M 32s
180050K .......... .......... .......... .......... .......... 35% 3.21M 32s
180100K .......... .......... .......... .......... .......... 35% 7.67M 32s
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180200K .......... .......... .......... .......... .......... 35% 10.9M 32s
180250K .......... .......... .......... .......... .......... 35%  210M 32s
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180350K .......... .......... .......... .......... .......... 35% 18.8M 32s
180400K .......... .......... .......... .......... .......... 35% 76.4M 32s
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180550K .......... .......... .......... .......... .......... 35% 19.6M 32s
180600K .......... .......... .......... .......... .......... 35% 12.7M 32s
180650K .......... .......... .......... .......... .......... 35% 12.1M 32s
180700K .......... .......... .......... .......... .......... 35% 8.37M 32s
180750K .......... .......... .......... .......... .......... 35% 11.6M 32s
180800K .......... .......... .......... .......... .......... 35% 10.2M 32s
180850K .......... .......... .......... .......... .......... 35% 7.66M 32s
180900K .......... .......... .......... .......... .......... 35% 7.11M 32s
180950K .......... .......... .......... .......... .......... 35% 5.94M 32s
181000K .......... .......... .......... .......... .......... 35% 9.41M 32s
181050K .......... .......... .......... .......... .......... 35% 12.6M 32s
181100K .......... .......... .......... .......... .......... 35% 10.4M 32s
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181200K .......... .......... .......... .......... .......... 35% 11.2M 32s
181250K .......... .......... .......... .......... .......... 35% 13.2M 32s
181300K .......... .......... .......... .......... .......... 35% 13.1M 32s
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181400K .......... .......... .......... .......... .......... 35% 11.5M 32s
181450K .......... .......... .......... .......... .......... 35% 11.0M 32s
181500K .......... .......... .......... .......... .......... 35% 13.6M 32s
181550K .......... .......... .......... .......... .......... 35% 10.1M 32s
181600K .......... .......... .......... .......... .......... 35% 7.21M 32s
181650K .......... .......... .......... .......... .......... 35% 7.83M 32s
181700K .......... .......... .......... .......... .......... 35% 7.58M 32s
181750K .......... .......... .......... .......... .......... 36% 7.36M 32s
181800K .......... .......... .......... .......... .......... 36% 9.70M 32s
181850K .......... .......... .......... .......... .......... 36% 2.46M 32s
181900K .......... .......... .......... .......... .......... 36% 13.2M 32s
181950K .......... .......... .......... .......... .......... 36%  124M 32s
182000K .......... .......... .......... .......... .......... 36% 16.1M 32s
182050K .......... .......... .......... .......... .......... 36% 22.6M 32s
182100K .......... .......... .......... .......... .......... 36% 12.0M 32s
182150K .......... .......... .......... .......... .......... 36% 14.1M 32s
182200K .......... .......... .......... .......... .......... 36% 14.7M 32s
182250K .......... .......... .......... .......... .......... 36% 14.3M 32s
182300K .......... .......... .......... .......... .......... 36% 13.6M 32s
182350K .......... .......... .......... .......... .......... 36% 10.6M 32s
182400K .......... .......... .......... .......... .......... 36% 11.0M 32s
182450K .......... .......... .......... .......... .......... 36% 11.3M 32s
182500K .......... .......... .......... .......... .......... 36% 9.38M 32s
182550K .......... .......... .......... .......... .......... 36% 10.7M 32s
182600K .......... .......... .......... .......... .......... 36% 12.9M 32s
182650K .......... .......... .......... .......... .......... 36% 11.2M 32s
182700K .......... .......... .......... .......... .......... 36% 8.21M 32s
182750K .......... .......... .......... .......... .......... 36% 11.6M 32s
182800K .......... .......... .......... .......... .......... 36% 13.7M 32s
182850K .......... .......... .......... .......... .......... 36% 9.21M 32s
182900K .......... .......... .......... .......... .......... 36% 9.09M 32s
182950K .......... .......... .......... .......... .......... 36% 12.8M 32s
183000K .......... .......... .......... .......... .......... 36% 14.8M 32s
183050K .......... .......... .......... .......... .......... 36% 13.5M 32s
183100K .......... .......... .......... .......... .......... 36% 11.6M 32s
183150K .......... .......... .......... .......... .......... 36% 13.1M 32s
183200K .......... .......... .......... .......... .......... 36% 10.2M 32s
183250K .......... .......... .......... .......... .......... 36% 15.5M 32s
183300K .......... .......... .......... .......... .......... 36% 14.0M 32s
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183400K .......... .......... .......... .......... .......... 36% 21.5M 32s
183450K .......... .......... .......... .......... .......... 36% 17.0M 32s
183500K .......... .......... .......... .......... .......... 36% 14.1M 32s
183550K .......... .......... .......... .......... .......... 36% 10.5M 32s
183600K .......... .......... .......... .......... .......... 36% 11.0M 32s
183650K .......... .......... .......... .......... .......... 36% 13.7M 32s
183700K .......... .......... .......... .......... .......... 36% 11.6M 32s
183750K .......... .......... .......... .......... .......... 36% 11.4M 32s
183800K .......... .......... .......... .......... .......... 36% 12.6M 32s
183850K .......... .......... .......... .......... .......... 36% 8.84M 32s
183900K .......... .......... .......... .......... .......... 36% 9.68M 32s
183950K .......... .......... .......... .......... .......... 36% 7.91M 32s
184000K .......... .......... .......... .......... .......... 36% 6.83M 32s
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184100K .......... .......... .......... .......... .......... 36% 5.75M 32s
184150K .......... .......... .......... .......... .......... 36% 5.83M 32s
184200K .......... .......... .......... .......... .......... 36% 5.09M 32s
184250K .......... .......... .......... .......... .......... 36% 6.16M 32s
184300K .......... .......... .......... .......... .......... 36% 20.7M 32s
184350K .......... .......... .......... .......... .......... 36% 17.3M 32s
184400K .......... .......... .......... .......... .......... 36% 20.6M 32s
184450K .......... .......... .......... .......... .......... 36% 37.6M 32s
184500K .......... .......... .......... .......... .......... 36% 22.1M 32s
184550K .......... .......... .......... .......... .......... 36% 20.3M 32s
184600K .......... .......... .......... .......... .......... 36% 24.4M 32s
184650K .......... .......... .......... .......... .......... 36% 17.6M 32s
184700K .......... .......... .......... .......... .......... 36% 14.5M 32s
184750K .......... .......... .......... .......... .......... 36% 11.7M 32s
184800K .......... .......... .......... .......... .......... 36% 21.1M 32s
184850K .......... .......... .......... .......... .......... 36% 11.2M 32s
184900K .......... .......... .......... .......... .......... 36% 21.9M 32s
184950K .......... .......... .......... .......... .......... 36% 10.7M 32s
185000K .......... .......... .......... .......... .......... 36% 17.1M 32s
185050K .......... .......... .......... .......... .......... 36% 13.9M 32s
185100K .......... .......... .......... .......... .......... 36% 6.18M 32s
185150K .......... .......... .......... .......... .......... 36% 10.9M 32s
185200K .......... .......... .......... .......... .......... 36% 5.52M 32s
185250K .......... .......... .......... .......... .......... 36% 7.67M 32s
185300K .......... .......... .......... .......... .......... 36% 9.61M 32s
185350K .......... .......... .......... .......... .......... 36% 7.28M 32s
185400K .......... .......... .......... .......... .......... 36% 6.58M 32s
185450K .......... .......... .......... .......... .......... 36% 5.38M 32s
185500K .......... .......... .......... .......... .......... 36% 6.09M 32s
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185600K .......... .......... .......... .......... .......... 36% 4.69M 32s
185650K .......... .......... .......... .......... .......... 36% 22.1M 32s
185700K .......... .......... .......... .......... .......... 36% 7.58M 32s
185750K .......... .......... .......... .......... .......... 36% 9.54M 32s
185800K .......... .......... .......... .......... .......... 36% 7.70M 32s
185850K .......... .......... .......... .......... .......... 36% 4.95M 32s
185900K .......... .......... .......... .......... .......... 36% 6.27M 32s
185950K .......... .......... .......... .......... .......... 36% 2.48M 32s
186000K .......... .......... .......... .......... .......... 36% 5.91M 32s
186050K .......... .......... .......... .......... .......... 36% 2.20M 32s
186100K .......... .......... .......... .......... .......... 36% 12.5M 32s
186150K .......... .......... .......... .......... .......... 36% 8.36M 32s
186200K .......... .......... .......... .......... .......... 36% 6.92M 32s
186250K .......... .......... .......... .......... .......... 36% 7.63M 32s
186300K .......... .......... .......... .......... .......... 36% 6.51M 32s
186350K .......... .......... .......... .......... .......... 36% 5.77M 32s
186400K .......... .......... .......... .......... .......... 36% 5.93M 32s
186450K .......... .......... .......... .......... .......... 36% 4.74M 32s
186500K .......... .......... .......... .......... .......... 36% 9.29M 32s
186550K .......... .......... .......... .......... .......... 36% 6.41M 32s
186600K .......... .......... .......... .......... .......... 36% 6.28M 32s
186650K .......... .......... .......... .......... .......... 36% 6.42M 32s
186700K .......... .......... .......... .......... .......... 36% 3.80M 32s
186750K .......... .......... .......... .......... .......... 36% 6.82M 32s
186800K .......... .......... .......... .......... .......... 37% 9.13M 32s
186850K .......... .......... .......... .......... .......... 37% 6.33M 32s
186900K .......... .......... .......... .......... .......... 37% 10.7M 32s
186950K .......... .......... .......... .......... .......... 37% 7.04M 32s
187000K .......... .......... .......... .......... .......... 37% 6.70M 32s
187050K .......... .......... .......... .......... .......... 37% 5.75M 32s
187100K .......... .......... .......... .......... .......... 37% 6.92M 32s
187150K .......... .......... .......... .......... .......... 37% 8.12M 32s
187200K .......... .......... .......... .......... .......... 37% 7.70M 32s
187250K .......... .......... .......... .......... .......... 37% 8.41M 32s
187300K .......... .......... .......... .......... .......... 37% 7.54M 32s
187350K .......... .......... .......... .......... .......... 37% 6.96M 32s
187400K .......... .......... .......... .......... .......... 37% 11.8M 32s
187450K .......... .......... .......... .......... .......... 37% 5.66M 32s
187500K .......... .......... .......... .......... .......... 37% 7.53M 32s
187550K .......... .......... .......... .......... .......... 37% 6.21M 32s
187600K .......... .......... .......... .......... .......... 37% 7.57M 32s
187650K .......... .......... .......... .......... .......... 37% 9.31M 32s
187700K .......... .......... .......... .......... .......... 37% 9.88M 32s
187750K .......... .......... .......... .......... .......... 37% 9.05M 32s
187800K .......... .......... .......... .......... .......... 37% 9.89M 32s
187850K .......... .......... .......... .......... .......... 37% 9.34M 32s
187900K .......... .......... .......... .......... .......... 37% 18.9M 32s
187950K .......... .......... .......... .......... .......... 37% 27.1M 32s
188000K .......... .......... .......... .......... .......... 37% 32.3M 32s
188050K .......... .......... .......... .......... .......... 37% 21.8M 32s
188100K .......... .......... .......... .......... .......... 37% 41.7M 32s
188150K .......... .......... .......... .......... .......... 37% 22.0M 32s
188200K .......... .......... .......... .......... .......... 37% 11.2M 32s
188250K .......... .......... .......... .......... .......... 37% 43.0M 32s
188300K .......... .......... .......... .......... .......... 37% 15.4M 32s
188350K .......... .......... .......... .......... .......... 37% 16.3M 32s
188400K .......... .......... .......... .......... .......... 37% 19.4M 32s
188450K .......... .......... .......... .......... .......... 37% 12.8M 32s
188500K .......... .......... .......... .......... .......... 37% 20.4M 32s
188550K .......... .......... .......... .......... .......... 37% 11.8M 32s
188600K .......... .......... .......... .......... .......... 37% 11.9M 32s
188650K .......... .......... .......... .......... .......... 37% 11.3M 32s
188700K .......... .......... .......... .......... .......... 37% 10.9M 32s
188750K .......... .......... .......... .......... .......... 37% 11.5M 32s
188800K .......... .......... .......... .......... .......... 37% 10.1M 32s
188850K .......... .......... .......... .......... .......... 37% 8.33M 32s
188900K .......... .......... .......... .......... .......... 37% 9.36M 32s
188950K .......... .......... .......... .......... .......... 37% 9.98M 32s
189000K .......... .......... .......... .......... .......... 37% 12.0M 32s
189050K .......... .......... .......... .......... .......... 37% 10.4M 32s
189100K .......... .......... .......... .......... .......... 37% 10.2M 32s
189150K .......... .......... .......... .......... .......... 37% 8.52M 32s
189200K .......... .......... .......... .......... .......... 37% 10.6M 32s
189250K .......... .......... .......... .......... .......... 37% 13.5M 32s
189300K .......... .......... .......... .......... .......... 37% 28.6M 32s
189350K .......... .......... .......... .......... .......... 37% 25.0M 32s
189400K .......... .......... .......... .......... .......... 37% 24.9M 32s
189450K .......... .......... .......... .......... .......... 37% 27.2M 32s
189500K .......... .......... .......... .......... .......... 37% 25.9M 32s
189550K .......... .......... .......... .......... .......... 37% 18.7M 32s
189600K .......... .......... .......... .......... .......... 37% 27.6M 32s
189650K .......... .......... .......... .......... .......... 37% 15.2M 32s
189700K .......... .......... .......... .......... .......... 37% 16.3M 32s
189750K .......... .......... .......... .......... .......... 37% 12.1M 32s
189800K .......... .......... .......... .......... .......... 37% 11.9M 32s
189850K .......... .......... .......... .......... .......... 37% 9.27M 31s
189900K .......... .......... .......... .......... .......... 37% 8.77M 31s
189950K .......... .......... .......... .......... .......... 37% 8.02M 31s
190000K .......... .......... .......... .......... .......... 37% 7.24M 31s
190050K .......... .......... .......... .......... .......... 37% 6.29M 31s
190100K .......... .......... .......... .......... .......... 37% 4.91M 31s
190150K .......... .......... .......... .......... .......... 37% 6.48M 31s
190200K .......... .......... .......... .......... .......... 37% 12.9M 31s
190250K .......... .......... .......... .......... .......... 37% 17.2M 31s
190300K .......... .......... .......... .......... .......... 37% 13.1M 31s
190350K .......... .......... .......... .......... .......... 37%  135M 31s
190400K .......... .......... .......... .......... .......... 37% 18.0M 31s
190450K .......... .......... .......... .......... .......... 37% 16.5M 31s
190500K .......... .......... .......... .......... .......... 37% 19.5M 31s
190550K .......... .......... .......... .......... .......... 37% 12.3M 31s
190600K .......... .......... .......... .......... .......... 37% 14.0M 31s
190650K .......... .......... .......... .......... .......... 37% 13.7M 31s
190700K .......... .......... .......... .......... .......... 37% 8.59M 31s
190750K .......... .......... .......... .......... .......... 37% 7.44M 31s
190800K .......... .......... .......... .......... .......... 37% 8.96M 31s
190850K .......... .......... .......... .......... .......... 37% 6.50M 31s
190900K .......... .......... .......... .......... .......... 37% 8.23M 31s
190950K .......... .......... .......... .......... .......... 37% 5.02M 31s
191000K .......... .......... .......... .......... .......... 37% 8.20M 31s
191050K .......... .......... .......... .......... .......... 37% 7.45M 31s
191100K .......... .......... .......... .......... .......... 37% 5.66M 31s
191150K .......... .......... .......... .......... .......... 37% 5.76M 31s
191200K .......... .......... .......... .......... .......... 37% 4.45M 31s
191250K .......... .......... .......... .......... .......... 37% 4.44M 31s
191300K .......... .......... .......... .......... .......... 37% 5.30M 31s
191350K .......... .......... .......... .......... .......... 37% 3.89M 31s
191400K .......... .......... .......... .......... .......... 37% 5.93M 31s
191450K .......... .......... .......... .......... .......... 37% 14.1M 31s
191500K .......... .......... .......... .......... .......... 37% 15.2M 31s
191550K .......... .......... .......... .......... .......... 37% 20.0M 31s
191600K .......... .......... .......... .......... .......... 37% 12.6M 31s
191650K .......... .......... .......... .......... .......... 37% 10.5M 31s
191700K .......... .......... .......... .......... .......... 37% 7.79M 31s
191750K .......... .......... .......... .......... .......... 37% 8.88M 31s
191800K .......... .......... .......... .......... .......... 37% 7.24M 31s
191850K .......... .......... .......... .......... .......... 38% 5.68M 31s
191900K .......... .......... .......... .......... .......... 38% 7.28M 31s
191950K .......... .......... .......... .......... .......... 38% 4.43M 31s
192000K .......... .......... .......... .......... .......... 38% 7.54M 31s
192050K .......... .......... .......... .......... .......... 38% 8.48M 31s
192100K .......... .......... .......... .......... .......... 38% 3.76M 31s
192150K .......... .......... .......... .......... .......... 38% 6.30M 31s
192200K .......... .......... .......... .......... .......... 38% 4.17M 31s
192250K .......... .......... .......... .......... .......... 38% 3.69M 31s
192300K .......... .......... .......... .......... .......... 38% 4.16M 31s
192350K .......... .......... .......... .......... .......... 38% 5.20M 31s
192400K .......... .......... .......... .......... .......... 38% 32.8M 31s
192450K .......... .......... .......... .......... .......... 38% 32.3M 31s
192500K .......... .......... .......... .......... .......... 38% 23.5M 31s
192550K .......... .......... .......... .......... .......... 38% 24.0M 31s
192600K .......... .......... .......... .......... .......... 38%  107M 31s
192650K .......... .......... .......... .......... .......... 38% 29.6M 31s
192700K .......... .......... .......... .......... .......... 38% 18.9M 31s
192750K .......... .......... .......... .......... .......... 38% 21.3M 31s
192800K .......... .......... .......... .......... .......... 38% 23.0M 31s
192850K .......... .......... .......... .......... .......... 38% 16.1M 31s
192900K .......... .......... .......... .......... .......... 38% 17.9M 31s
192950K .......... .......... .......... .......... .......... 38% 13.9M 31s
193000K .......... .......... .......... .......... .......... 38% 19.5M 31s
193050K .......... .......... .......... .......... .......... 38% 16.4M 31s
193100K .......... .......... .......... .......... .......... 38% 13.6M 31s
193150K .......... .......... .......... .......... .......... 38% 17.8M 31s
193200K .......... .......... .......... .......... .......... 38% 11.0M 31s
193250K .......... .......... .......... .......... .......... 38% 13.4M 31s
193300K .......... .......... .......... .......... .......... 38% 16.1M 31s
193350K .......... .......... .......... .......... .......... 38% 11.7M 31s
193400K .......... .......... .......... .......... .......... 38% 14.8M 31s
193450K .......... .......... .......... .......... .......... 38% 14.1M 31s
193500K .......... .......... .......... .......... .......... 38% 13.3M 31s
193550K .......... .......... .......... .......... .......... 38% 12.3M 31s
193600K .......... .......... .......... .......... .......... 38% 10.8M 31s
193650K .......... .......... .......... .......... .......... 38% 11.6M 31s
193700K .......... .......... .......... .......... .......... 38% 9.48M 31s
193750K .......... .......... .......... .......... .......... 38% 10.5M 31s
193800K .......... .......... .......... .......... .......... 38% 10.8M 31s
193850K .......... .......... .......... .......... .......... 38% 6.38M 31s
193900K .......... .......... .......... .......... .......... 38% 9.19M 31s
193950K .......... .......... .......... .......... .......... 38% 8.44M 31s
194000K .......... .......... .......... .......... .......... 38% 9.01M 31s
194050K .......... .......... .......... .......... .......... 38% 6.93M 31s
194100K .......... .......... .......... .......... .......... 38% 4.89M 31s
194150K .......... .......... .......... .......... .......... 38% 7.22M 31s
194200K .......... .......... .......... .......... .......... 38% 6.05M 31s
194250K .......... .......... .......... .......... .......... 38% 5.71M 31s
194300K .......... .......... .......... .......... .......... 38% 5.54M 31s
194350K .......... .......... .......... .......... .......... 38% 4.12M 31s
194400K .......... .......... .......... .......... .......... 38% 5.85M 31s
194450K .......... .......... .......... .......... .......... 38% 8.17M 31s
194500K .......... .......... .......... .......... .......... 38% 22.5M 31s
194550K .......... .......... .......... .......... .......... 38% 26.3M 31s
194600K .......... .......... .......... .......... .......... 38% 29.1M 31s
194650K .......... .......... .......... .......... .......... 38% 24.1M 31s
194700K .......... .......... .......... .......... .......... 38% 15.6M 31s
194750K .......... .......... .......... .......... .......... 38% 15.3M 31s
194800K .......... .......... .......... .......... .......... 38% 17.4M 31s
194850K .......... .......... .......... .......... .......... 38% 10.9M 31s
194900K .......... .......... .......... .......... .......... 38% 24.4M 31s
194950K .......... .......... .......... .......... .......... 38% 11.8M 31s
195000K .......... .......... .......... .......... .......... 38% 12.1M 31s
195050K .......... .......... .......... .......... .......... 38% 13.1M 31s
195100K .......... .......... .......... .......... .......... 38% 7.47M 31s
195150K .......... .......... .......... .......... .......... 38% 5.73M 31s
195200K .......... .......... .......... .......... .......... 38% 7.28M 31s
195250K .......... .......... .......... .......... .......... 38% 6.94M 31s
195300K .......... .......... .......... .......... .......... 38% 6.70M 31s
195350K .......... .......... .......... .......... .......... 38% 5.80M 31s
195400K .......... .......... .......... .......... .......... 38% 7.27M 31s
195450K .......... .......... .......... .......... .......... 38% 4.86M 31s
195500K .......... .......... .......... .......... .......... 38% 8.07M 31s
195550K .......... .......... .......... .......... .......... 38% 7.62M 31s
195600K .......... .......... .......... .......... .......... 38% 7.34M 31s
195650K .......... .......... .......... .......... .......... 38% 8.75M 31s
195700K .......... .......... .......... .......... .......... 38% 8.85M 31s
195750K .......... .......... .......... .......... .......... 38% 11.7M 31s
195800K .......... .......... .......... .......... .......... 38% 25.8M 31s
195850K .......... .......... .......... .......... .......... 38% 31.4M 31s
195900K .......... .......... .......... .......... .......... 38% 32.0M 31s
195950K .......... .......... .......... .......... .......... 38% 29.0M 31s
196000K .......... .......... .......... .......... .......... 38% 32.2M 31s
196050K .......... .......... .......... .......... .......... 38% 15.6M 31s
196100K .......... .......... .......... .......... .......... 38% 15.6M 31s
196150K .......... .......... .......... .......... .......... 38% 11.6M 31s
196200K .......... .......... .......... .......... .......... 38% 7.38M 31s
196250K .......... .......... .......... .......... .......... 38% 7.15M 31s
196300K .......... .......... .......... .......... .......... 38% 6.51M 31s
196350K .......... .......... .......... .......... .......... 38% 5.57M 31s
196400K .......... .......... .......... .......... .......... 38% 6.62M 31s
196450K .......... .......... .......... .......... .......... 38% 8.63M 31s
196500K .......... .......... .......... .......... .......... 38% 9.36M 31s
196550K .......... .......... .......... .......... .......... 38% 7.85M 31s
196600K .......... .......... .......... .......... .......... 38% 7.83M 31s
196650K .......... .......... .......... .......... .......... 38% 8.21M 31s
196700K .......... .......... .......... .......... .......... 38% 8.62M 31s
196750K .......... .......... .......... .......... .......... 38% 40.2M 31s
196800K .......... .......... .......... .......... .......... 38% 16.5M 31s
196850K .......... .......... .......... .......... .......... 38% 19.7M 31s
196900K .......... .......... .......... .......... .......... 39% 20.9M 31s
196950K .......... .......... .......... .......... .......... 39% 10.5M 31s
197000K .......... .......... .......... .......... .......... 39% 11.0M 31s
197050K .......... .......... .......... .......... .......... 39% 11.3M 31s
197100K .......... .......... .......... .......... .......... 39% 11.3M 31s
197150K .......... .......... .......... .......... .......... 39% 8.18M 31s
197200K .......... .......... .......... .......... .......... 39% 11.0M 31s
197250K .......... .......... .......... .......... .......... 39% 14.0M 31s
197300K .......... .......... .......... .......... .......... 39% 10.7M 31s
197350K .......... .......... .......... .......... .......... 39% 7.88M 31s
197400K .......... .......... .......... .......... .......... 39% 11.4M 31s
197450K .......... .......... .......... .......... .......... 39% 8.91M 31s
197500K .......... .......... .......... .......... .......... 39% 10.8M 31s
197550K .......... .......... .......... .......... .......... 39% 11.4M 31s
197600K .......... .......... .......... .......... .......... 39% 8.28M 31s
197650K .......... .......... .......... .......... .......... 39% 11.0M 31s
197700K .......... .......... .......... .......... .......... 39% 8.33M 31s
197750K .......... .......... .......... .......... .......... 39% 11.5M 31s
197800K .......... .......... .......... .......... .......... 39% 9.54M 31s
197850K .......... .......... .......... .......... .......... 39% 8.62M 31s
197900K .......... .......... .......... .......... .......... 39% 9.84M 31s
197950K .......... .......... .......... .......... .......... 39% 6.11M 31s
198000K .......... .......... .......... .......... .......... 39% 7.12M 31s
198050K .......... .......... .......... .......... .......... 39% 7.62M 31s
198100K .......... .......... .......... .......... .......... 39% 5.60M 31s
198150K .......... .......... .......... .......... .......... 39% 4.86M 31s
198200K .......... .......... .......... .......... .......... 39% 4.25M 31s
198250K .......... .......... .......... .......... .......... 39% 3.82M 31s
198300K .......... .......... .......... .......... .......... 39% 4.08M 31s
198350K .......... .......... .......... .......... .......... 39% 3.52M 31s
198400K .......... .......... .......... .......... .......... 39% 10.2M 31s
198450K .......... .......... .......... .......... .......... 39% 12.1M 31s
198500K .......... .......... .......... .......... .......... 39% 15.1M 31s
198550K .......... .......... .......... .......... .......... 39% 15.2M 31s
198600K .......... .......... .......... .......... .......... 39% 14.5M 31s
198650K .......... .......... .......... .......... .......... 39% 15.5M 31s
198700K .......... .......... .......... .......... .......... 39% 13.9M 31s
198750K .......... .......... .......... .......... .......... 39% 10.3M 31s
198800K .......... .......... .......... .......... .......... 39% 15.1M 31s
198850K .......... .......... .......... .......... .......... 39% 9.94M 31s
198900K .......... .......... .......... .......... .......... 39% 9.83M 31s
198950K .......... .......... .......... .......... .......... 39% 5.93M 31s
199000K .......... .......... .......... .......... .......... 39% 5.77M 31s
199050K .......... .......... .......... .......... .......... 39% 4.78M 31s
199100K .......... .......... .......... .......... .......... 39% 4.00M 31s
199150K .......... .......... .......... .......... .......... 39% 4.92M 31s
199200K .......... .......... .......... .......... .......... 39% 3.64M 31s
199250K .......... .......... .......... .......... .......... 39% 2.92M 31s
199300K .......... .......... .......... .......... .......... 39% 2.68M 31s
199350K .......... .......... .......... .......... .......... 39% 4.14M 31s
199400K .......... .......... .......... .......... .......... 39% 10.8M 31s
199450K .......... .......... .......... .......... .......... 39% 10.3M 31s
199500K .......... .......... .......... .......... .......... 39% 8.96M 31s
199550K .......... .......... .......... .......... .......... 39% 7.23M 31s
199600K .......... .......... .......... .......... .......... 39% 5.54M 31s
199650K .......... .......... .......... .......... .......... 39% 6.86M 31s
199700K .......... .......... .......... .......... .......... 39% 4.88M 31s
199750K .......... .......... .......... .......... .......... 39% 5.81M 31s
199800K .......... .......... .......... .......... .......... 39% 9.03M 31s
199850K .......... .......... .......... .......... .......... 39% 6.94M 31s
199900K .......... .......... .......... .......... .......... 39% 6.45M 31s
199950K .......... .......... .......... .......... .......... 39% 5.53M 31s
200000K .......... .......... .......... .......... .......... 39% 7.94M 31s
200050K .......... .......... .......... .......... .......... 39% 6.89M 31s
200100K .......... .......... .......... .......... .......... 39% 5.52M 31s
200150K .......... .......... .......... .......... .......... 39% 9.63M 31s
200200K .......... .......... .......... .......... .......... 39% 6.91M 31s
200250K .......... .......... .......... .......... .......... 39% 9.10M 31s
200300K .......... .......... .......... .......... .......... 39% 5.78M 31s
200350K .......... .......... .......... .......... .......... 39% 8.93M 31s
200400K .......... .......... .......... .......... .......... 39% 8.41M 31s
200450K .......... .......... .......... .......... .......... 39% 10.8M 31s
200500K .......... .......... .......... .......... .......... 39% 10.1M 31s
200550K .......... .......... .......... .......... .......... 39% 10.1M 31s
200600K .......... .......... .......... .......... .......... 39% 11.0M 31s
200650K .......... .......... .......... .......... .......... 39% 9.38M 31s
200700K .......... .......... .......... .......... .......... 39% 9.19M 31s
200750K .......... .......... .......... .......... .......... 39% 8.36M 31s
200800K .......... .......... .......... .......... .......... 39% 8.37M 31s
200850K .......... .......... .......... .......... .......... 39% 8.13M 31s
200900K .......... .......... .......... .......... .......... 39% 7.70M 31s
200950K .......... .......... .......... .......... .......... 39% 7.55M 31s
201000K .......... .......... .......... .......... .......... 39% 8.29M 31s
201050K .......... .......... .......... .......... .......... 39% 23.1M 31s
201100K .......... .......... .......... .......... .......... 39% 33.4M 31s
201150K .......... .......... .......... .......... .......... 39% 22.0M 31s
201200K .......... .......... .......... .......... .......... 39% 23.8M 31s
201250K .......... .......... .......... .......... .......... 39% 22.9M 31s
201300K .......... .......... .......... .......... .......... 39% 30.7M 31s
201350K .......... .......... .......... .......... .......... 39% 15.9M 31s
201400K .......... .......... .......... .......... .......... 39% 14.7M 31s
201450K .......... .......... .......... .......... .......... 39% 39.1M 31s
201500K .......... .......... .......... .......... .......... 39% 12.2M 31s
201550K .......... .......... .......... .......... .......... 39% 11.2M 31s
201600K .......... .......... .......... .......... .......... 39% 10.7M 31s
201650K .......... .......... .......... .......... .......... 39% 11.4M 31s
201700K .......... .......... .......... .......... .......... 39% 11.6M 31s
201750K .......... .......... .......... .......... .......... 39% 10.1M 31s
201800K .......... .......... .......... .......... .......... 39% 11.8M 31s
201850K .......... .......... .......... .......... .......... 39% 11.8M 31s
201900K .......... .......... .......... .......... .......... 39% 11.6M 31s
201950K .......... .......... .......... .......... .......... 40% 11.0M 31s
202000K .......... .......... .......... .......... .......... 40% 14.9M 31s
202050K .......... .......... .......... .......... .......... 40% 10.4M 31s
202100K .......... .......... .......... .......... .......... 40% 8.90M 31s
202150K .......... .......... .......... .......... .......... 40% 9.92M 31s
202200K .......... .......... .......... .......... .......... 40% 8.54M 30s
202250K .......... .......... .......... .......... .......... 40% 9.46M 30s
202300K .......... .......... .......... .......... .......... 40% 8.73M 30s
202350K .......... .......... .......... .......... .......... 40% 9.16M 30s
202400K .......... .......... .......... .......... .......... 40% 10.2M 30s
202450K .......... .......... .......... .......... .......... 40% 8.90M 30s
202500K .......... .......... .......... .......... .......... 40% 11.0M 30s
202550K .......... .......... .......... .......... .......... 40% 12.0M 30s
202600K .......... .......... .......... .......... .......... 40% 10.0M 30s
202650K .......... .......... .......... .......... .......... 40% 11.1M 30s
202700K .......... .......... .......... .......... .......... 40% 8.17M 30s
202750K .......... .......... .......... .......... .......... 40% 28.3M 30s
202800K .......... .......... .......... .......... .......... 40% 19.5M 30s
202850K .......... .......... .......... .......... .......... 40% 12.7M 30s
202900K .......... .......... .......... .......... .......... 40% 14.5M 30s
202950K .......... .......... .......... .......... .......... 40% 11.3M 30s
203000K .......... .......... .......... .......... .......... 40% 9.83M 30s
203050K .......... .......... .......... .......... .......... 40% 10.5M 30s
203100K .......... .......... .......... .......... .......... 40% 7.09M 30s
203150K .......... .......... .......... .......... .......... 40% 8.75M 30s
203200K .......... .......... .......... .......... .......... 40% 7.70M 30s
203250K .......... .......... .......... .......... .......... 40% 7.91M 30s
203300K .......... .......... .......... .......... .......... 40% 10.2M 30s
203350K .......... .......... .......... .......... .......... 40% 9.50M 30s
203400K .......... .......... .......... .......... .......... 40% 8.73M 30s
203450K .......... .......... .......... .......... .......... 40% 7.19M 30s
203500K .......... .......... .......... .......... .......... 40% 11.6M 30s
203550K .......... .......... .......... .......... .......... 40% 10.3M 30s
203600K .......... .......... .......... .......... .......... 40% 8.77M 30s
203650K .......... .......... .......... .......... .......... 40% 8.36M 30s
203700K .......... .......... .......... .......... .......... 40% 6.92M 30s
203750K .......... .......... .......... .......... .......... 40% 9.84M 30s
203800K .......... .......... .......... .......... .......... 40% 10.7M 30s
203850K .......... .......... .......... .......... .......... 40% 8.92M 30s
203900K .......... .......... .......... .......... .......... 40% 10.9M 30s
203950K .......... .......... .......... .......... .......... 40% 7.37M 30s
204000K .......... .......... .......... .......... .......... 40% 8.25M 30s
204050K .......... .......... .......... .......... .......... 40% 7.26M 30s
204100K .......... .......... .......... .......... .......... 40% 5.69M 30s
204150K .......... .......... .......... .......... .......... 40% 7.55M 30s
204200K .......... .......... .......... .......... .......... 40% 6.09M 30s
204250K .......... .......... .......... .......... .......... 40% 9.70M 30s
204300K .......... .......... .......... .......... .......... 40% 12.4M 30s
204350K .......... .......... .......... .......... .......... 40% 9.59M 30s
204400K .......... .......... .......... .......... .......... 40% 13.8M 30s
204450K .......... .......... .......... .......... .......... 40% 6.98M 30s
204500K .......... .......... .......... .......... .......... 40% 8.65M 30s
204550K .......... .......... .......... .......... .......... 40% 7.27M 30s
204600K .......... .......... .......... .......... .......... 40% 3.42M 30s
204650K .......... .......... .......... .......... .......... 40% 3.98M 30s
204700K .......... .......... .......... .......... .......... 40% 3.10M 30s
204750K .......... .......... .......... .......... .......... 40% 11.6M 30s
204800K .......... .......... .......... .......... .......... 40% 16.7M 30s
204850K .......... .......... .......... .......... .......... 40% 30.9M 30s
204900K .......... .......... .......... .......... .......... 40% 16.2M 30s
204950K .......... .......... .......... .......... .......... 40% 13.0M 30s
205000K .......... .......... .......... .......... .......... 40% 20.9M 30s
205050K .......... .......... .......... .......... .......... 40% 10.3M 30s
205100K .......... .......... .......... .......... .......... 40% 6.42M 30s
205150K .......... .......... .......... .......... .......... 40% 9.15M 30s
205200K .......... .......... .......... .......... .......... 40% 6.42M 30s
205250K .......... .......... .......... .......... .......... 40% 6.39M 30s
205300K .......... .......... .......... .......... .......... 40% 8.66M 30s
205350K .......... .......... .......... .......... .......... 40% 5.94M 30s
205400K .......... .......... .......... .......... .......... 40% 5.08M 30s
205450K .......... .......... .......... .......... .......... 40% 7.20M 30s
205500K .......... .......... .......... .......... .......... 40% 9.29M 30s
205550K .......... .......... .......... .......... .......... 40% 9.50M 30s
205600K .......... .......... .......... .......... .......... 40% 4.95M 30s
205650K .......... .......... .......... .......... .......... 40% 5.51M 30s
205700K .......... .......... .......... .......... .......... 40% 4.63M 30s
205750K .......... .......... .......... .......... .......... 40% 5.16M 30s
205800K .......... .......... .......... .......... .......... 40% 9.92M 30s
205850K .......... .......... .......... .......... .......... 40% 19.0M 30s
205900K .......... .......... .......... .......... .......... 40% 34.7M 30s
205950K .......... .......... .......... .......... .......... 40% 32.4M 30s
206000K .......... .......... .......... .......... .......... 40% 23.6M 30s
206050K .......... .......... .......... .......... .......... 40% 89.4M 30s
206100K .......... .......... .......... .......... .......... 40% 22.7M 30s
206150K .......... .......... .......... .......... .......... 40% 24.1M 30s
206200K .......... .......... .......... .......... .......... 40% 19.3M 30s
206250K .......... .......... .......... .......... .......... 40% 24.9M 30s
206300K .......... .......... .......... .......... .......... 40% 27.6M 30s
206350K .......... .......... .......... .......... .......... 40% 16.8M 30s
206400K .......... .......... .......... .......... .......... 40% 18.0M 30s
206450K .......... .......... .......... .......... .......... 40% 18.3M 30s
206500K .......... .......... .......... .......... .......... 40% 16.6M 30s
206550K .......... .......... .......... .......... .......... 40% 16.0M 30s
206600K .......... .......... .......... .......... .......... 40% 15.7M 30s
206650K .......... .......... .......... .......... .......... 40% 21.2M 30s
206700K .......... .......... .......... .......... .......... 40% 15.4M 30s
206750K .......... .......... .......... .......... .......... 40% 17.6M 30s
206800K .......... .......... .......... .......... .......... 40% 22.9M 30s
206850K .......... .......... .......... .......... .......... 40% 12.7M 30s
206900K .......... .......... .......... .......... .......... 40% 12.3M 30s
206950K .......... .......... .......... .......... .......... 40% 12.1M 30s
207000K .......... .......... .......... .......... .......... 41% 18.6M 30s
207050K .......... .......... .......... .......... .......... 41% 10.5M 30s
207100K .......... .......... .......... .......... .......... 41% 9.77M 30s
207150K .......... .......... .......... .......... .......... 41% 11.8M 30s
207200K .......... .......... .......... .......... .......... 41% 9.64M 30s
207250K .......... .......... .......... .......... .......... 41% 11.2M 30s
207300K .......... .......... .......... .......... .......... 41% 12.5M 30s
207350K .......... .......... .......... .......... .......... 41% 6.97M 30s
207400K .......... .......... .......... .......... .......... 41% 10.4M 30s
207450K .......... .......... .......... .......... .......... 41% 6.74M 30s
207500K .......... .......... .......... .......... .......... 41% 9.76M 30s
207550K .......... .......... .......... .......... .......... 41% 10.3M 30s
207600K .......... .......... .......... .......... .......... 41% 8.67M 30s
207650K .......... .......... .......... .......... .......... 41% 10.9M 30s
207700K .......... .......... .......... .......... .......... 41% 10.7M 30s
207750K .......... .......... .......... .......... .......... 41% 15.2M 30s
207800K .......... .......... .......... .......... .......... 41% 15.6M 30s
207850K .......... .......... .......... .......... .......... 41% 11.3M 30s
207900K .......... .......... .......... .......... .......... 41% 7.79M 30s
207950K .......... .......... .......... .......... .......... 41% 8.76M 30s
208000K .......... .......... .......... .......... .......... 41% 9.14M 30s
208050K .......... .......... .......... .......... .......... 41% 9.59M 30s
208100K .......... .......... .......... .......... .......... 41% 10.0M 30s
208150K .......... .......... .......... .......... .......... 41% 9.80M 30s
208200K .......... .......... .......... .......... .......... 41% 5.59M 30s
208250K .......... .......... .......... .......... .......... 41% 4.93M 30s
208300K .......... .......... .......... .......... .......... 41% 5.34M 30s
208350K .......... .......... .......... .......... .......... 41% 5.93M 30s
208400K .......... .......... .......... .......... .......... 41% 7.17M 30s
208450K .......... .......... .......... .......... .......... 41% 5.38M 30s
208500K .......... .......... .......... .......... .......... 41% 6.55M 30s
208550K .......... .......... .......... .......... .......... 41% 5.97M 30s
208600K .......... .......... .......... .......... .......... 41% 3.39M 30s
208650K .......... .......... .......... .......... .......... 41% 10.6M 30s
208700K .......... .......... .......... .......... .......... 41% 13.5M 30s
208750K .......... .......... .......... .......... .......... 41% 22.0M 30s
208800K .......... .......... .......... .......... .......... 41% 19.6M 30s
208850K .......... .......... .......... .......... .......... 41% 19.2M 30s
208900K .......... .......... .......... .......... .......... 41% 21.8M 30s
208950K .......... .......... .......... .......... .......... 41% 27.0M 30s
209000K .......... .......... .......... .......... .......... 41% 21.4M 30s
209050K .......... .......... .......... .......... .......... 41% 16.1M 30s
209100K .......... .......... .......... .......... .......... 41% 13.2M 30s
209150K .......... .......... .......... .......... .......... 41% 17.7M 30s
209200K .......... .......... .......... .......... .......... 41% 19.8M 30s
209250K .......... .......... .......... .......... .......... 41% 15.2M 30s
209300K .......... .......... .......... .......... .......... 41% 13.9M 30s
209350K .......... .......... .......... .......... .......... 41% 10.3M 30s
209400K .......... .......... .......... .......... .......... 41% 11.9M 30s
209450K .......... .......... .......... .......... .......... 41% 11.4M 30s
209500K .......... .......... .......... .......... .......... 41% 13.9M 30s
209550K .......... .......... .......... .......... .......... 41% 16.5M 30s
209600K .......... .......... .......... .......... .......... 41% 11.4M 30s
209650K .......... .......... .......... .......... .......... 41% 14.0M 30s
209700K .......... .......... .......... .......... .......... 41% 12.4M 30s
209750K .......... .......... .......... .......... .......... 41% 12.9M 30s
209800K .......... .......... .......... .......... .......... 41% 18.7M 30s
209850K .......... .......... .......... .......... .......... 41% 15.3M 30s
209900K .......... .......... .......... .......... .......... 41%  190M 30s
209950K .......... .......... .......... .......... .......... 41% 14.4M 30s
210000K .......... .......... .......... .......... .......... 41% 22.3M 30s
210050K .......... .......... .......... .......... .......... 41% 30.2M 30s
210100K .......... .......... .......... .......... .......... 41% 15.7M 30s
210150K .......... .......... .......... .......... .......... 41% 18.4M 30s
210200K .......... .......... .......... .......... .......... 41% 14.1M 30s
210250K .......... .......... .......... .......... .......... 41% 12.9M 30s
210300K .......... .......... .......... .......... .......... 41% 14.0M 30s
210350K .......... .......... .......... .......... .......... 41% 13.9M 30s
210400K .......... .......... .......... .......... .......... 41% 15.2M 30s
210450K .......... .......... .......... .......... .......... 41% 10.4M 30s
210500K .......... .......... .......... .......... .......... 41% 11.4M 30s
210550K .......... .......... .......... .......... .......... 41% 10.5M 30s
210600K .......... .......... .......... .......... .......... 41% 8.81M 30s
210650K .......... .......... .......... .......... .......... 41% 13.7M 30s
210700K .......... .......... .......... .......... .......... 41% 7.54M 30s
210750K .......... .......... .......... .......... .......... 41% 5.23M 30s
210800K .......... .......... .......... .......... .......... 41% 5.00M 30s
210850K .......... .......... .......... .......... .......... 41% 5.05M 30s
210900K .......... .......... .......... .......... .......... 41% 8.05M 30s
210950K .......... .......... .......... .......... .......... 41% 7.45M 30s
211000K .......... .......... .......... .......... .......... 41% 7.45M 30s
211050K .......... .......... .......... .......... .......... 41% 6.72M 30s
211100K .......... .......... .......... .......... .......... 41% 5.68M 30s
211150K .......... .......... .......... .......... .......... 41% 5.28M 30s
211200K .......... .......... .......... .......... .......... 41% 5.14M 30s
211250K .......... .......... .......... .......... .......... 41% 8.50M 30s
211300K .......... .......... .......... .......... .......... 41% 7.79M 30s
211350K .......... .......... .......... .......... .......... 41% 6.60M 30s
211400K .......... .......... .......... .......... .......... 41% 6.36M 30s
211450K .......... .......... .......... .......... .......... 41% 6.02M 30s
211500K .......... .......... .......... .......... .......... 41% 6.37M 30s
211550K .......... .......... .......... .......... .......... 41% 7.16M 30s
211600K .......... .......... .......... .......... .......... 41% 6.08M 30s
211650K .......... .......... .......... .......... .......... 41% 15.2M 30s
211700K .......... .......... .......... .......... .......... 41% 14.5M 30s
211750K .......... .......... .......... .......... .......... 41% 20.5M 30s
211800K .......... .......... .......... .......... .......... 41% 15.3M 30s
211850K .......... .......... .......... .......... .......... 41% 14.0M 30s
211900K .......... .......... .......... .......... .......... 41% 16.5M 30s
211950K .......... .......... .......... .......... .......... 41% 18.3M 30s
212000K .......... .......... .......... .......... .......... 41% 12.1M 30s
212050K .......... .......... .......... .......... .......... 42% 13.5M 30s
212100K .......... .......... .......... .......... .......... 42% 7.82M 30s
212150K .......... .......... .......... .......... .......... 42% 6.95M 30s
212200K .......... .......... .......... .......... .......... 42% 7.12M 29s
212250K .......... .......... .......... .......... .......... 42% 6.23M 29s
212300K .......... .......... .......... .......... .......... 42% 5.16M 29s
212350K .......... .......... .......... .......... .......... 42% 5.11M 30s
212400K .......... .......... .......... .......... .......... 42% 7.40M 29s
212450K .......... .......... .......... .......... .......... 42% 6.90M 29s
212500K .......... .......... .......... .......... .......... 42% 8.71M 29s
212550K .......... .......... .......... .......... .......... 42% 9.86M 29s
212600K .......... .......... .......... .......... .......... 42% 6.76M 29s
212650K .......... .......... .......... .......... .......... 42% 29.1M 29s
212700K .......... .......... .......... .......... .......... 42% 20.6M 29s
212750K .......... .......... .......... .......... .......... 42% 17.5M 29s
212800K .......... .......... .......... .......... .......... 42% 10.4M 29s
212850K .......... .......... .......... .......... .......... 42% 10.5M 29s
212900K .......... .......... .......... .......... .......... 42% 10.9M 29s
212950K .......... .......... .......... .......... .......... 42% 9.61M 29s
213000K .......... .......... .......... .......... .......... 42% 15.5M 29s
213050K .......... .......... .......... .......... .......... 42% 12.6M 29s
213100K .......... .......... .......... .......... .......... 42% 9.47M 29s
213150K .......... .......... .......... .......... .......... 42% 14.1M 29s
213200K .......... .......... .......... .......... .......... 42% 9.28M 29s
213250K .......... .......... .......... .......... .......... 42% 9.29M 29s
213300K .......... .......... .......... .......... .......... 42% 13.5M 29s
213350K .......... .......... .......... .......... .......... 42% 13.2M 29s
213400K .......... .......... .......... .......... .......... 42% 7.17M 29s
213450K .......... .......... .......... .......... .......... 42% 5.77M 29s
213500K .......... .......... .......... .......... .......... 42% 8.19M 29s
213550K .......... .......... .......... .......... .......... 42% 6.73M 29s
213600K .......... .......... .......... .......... .......... 42% 6.11M 29s
213650K .......... .......... .......... .......... .......... 42% 6.80M 29s
213700K .......... .......... .......... .......... .......... 42% 13.0M 29s
213750K .......... .......... .......... .......... .......... 42% 25.2M 29s
213800K .......... .......... .......... .......... .......... 42% 14.6M 29s
213850K .......... .......... .......... .......... .......... 42% 21.0M 29s
213900K .......... .......... .......... .......... .......... 42% 13.7M 29s
213950K .......... .......... .......... .......... .......... 42% 13.5M 29s
214000K .......... .......... .......... .......... .......... 42% 14.3M 29s
214050K .......... .......... .......... .......... .......... 42% 16.0M 29s
214100K .......... .......... .......... .......... .......... 42% 11.4M 29s
214150K .......... .......... .......... .......... .......... 42% 10.1M 29s
214200K .......... .......... .......... .......... .......... 42% 9.84M 29s
214250K .......... .......... .......... .......... .......... 42% 11.8M 29s
214300K .......... .......... .......... .......... .......... 42% 11.2M 29s
214350K .......... .......... .......... .......... .......... 42% 8.89M 29s
214400K .......... .......... .......... .......... .......... 42% 8.49M 29s
214450K .......... .......... .......... .......... .......... 42% 7.05M 29s
214500K .......... .......... .......... .......... .......... 42% 7.54M 29s
214550K .......... .......... .......... .......... .......... 42% 8.24M 29s
214600K .......... .......... .......... .......... .......... 42% 6.31M 29s
214650K .......... .......... .......... .......... .......... 42% 9.07M 29s
214700K .......... .......... .......... .......... .......... 42% 9.24M 29s
214750K .......... .......... .......... .......... .......... 42% 10.9M 29s
214800K .......... .......... .......... .......... .......... 42% 7.55M 29s
214850K .......... .......... .......... .......... .......... 42% 7.02M 29s
214900K .......... .......... .......... .......... .......... 42% 6.83M 29s
214950K .......... .......... .......... .......... .......... 42% 6.61M 29s
215000K .......... .......... .......... .......... .......... 42% 6.71M 29s
215050K .......... .......... .......... .......... .......... 42% 10.8M 29s
215100K .......... .......... .......... .......... .......... 42% 10.1M 29s
215150K .......... .......... .......... .......... .......... 42% 10.9M 29s
215200K .......... .......... .......... .......... .......... 42% 10.0M 29s
215250K .......... .......... .......... .......... .......... 42% 8.40M 29s
215300K .......... .......... .......... .......... .......... 42% 7.01M 29s
215350K .......... .......... .......... .......... .......... 42% 6.83M 29s
215400K .......... .......... .......... .......... .......... 42% 6.89M 29s
215450K .......... .......... .......... .......... .......... 42% 7.77M 29s
215500K .......... .......... .......... .......... .......... 42% 8.57M 29s
215550K .......... .......... .......... .......... .......... 42% 14.6M 29s
215600K .......... .......... .......... .......... .......... 42% 22.1M 29s
215650K .......... .......... .......... .......... .......... 42% 15.3M 29s
215700K .......... .......... .......... .......... .......... 42% 16.4M 29s
215750K .......... .......... .......... .......... .......... 42% 12.4M 29s
215800K .......... .......... .......... .......... .......... 42% 12.8M 29s
215850K .......... .......... .......... .......... .......... 42% 7.52M 29s
215900K .......... .......... .......... .......... .......... 42% 13.0M 29s
215950K .......... .......... .......... .......... .......... 42% 7.35M 29s
216000K .......... .......... .......... .......... .......... 42% 7.76M 29s
216050K .......... .......... .......... .......... .......... 42% 5.14M 29s
216100K .......... .......... .......... .......... .......... 42% 5.77M 29s
216150K .......... .......... .......... .......... .......... 42% 5.82M 29s
216200K .......... .......... .......... .......... .......... 42% 3.64M 29s
216250K .......... .......... .......... .......... .......... 42% 4.25M 29s
216300K .......... .......... .......... .......... .......... 42% 3.72M 29s
216350K .......... .......... .......... .......... .......... 42% 9.05M 29s
216400K .......... .......... .......... .......... .......... 42% 40.3M 29s
216450K .......... .......... .......... .......... .......... 42% 37.2M 29s
216500K .......... .......... .......... .......... .......... 42% 30.2M 29s
216550K .......... .......... .......... .......... .......... 42% 63.5M 29s
216600K .......... .......... .......... .......... .......... 42% 41.7M 29s
216650K .......... .......... .......... .......... .......... 42% 51.5M 29s
216700K .......... .......... .......... .......... .......... 42% 20.4M 29s
216750K .......... .......... .......... .......... .......... 42% 24.1M 29s
216800K .......... .......... .......... .......... .......... 42% 23.9M 29s
216850K .......... .......... .......... .......... .......... 42% 10.8M 29s
216900K .......... .......... .......... .......... .......... 42% 15.0M 29s
216950K .......... .......... .......... .......... .......... 42% 6.50M 29s
217000K .......... .......... .......... .......... .......... 42% 6.08M 29s
217050K .......... .......... .......... .......... .......... 42% 7.20M 29s
217100K .......... .......... .......... .......... .......... 43% 5.78M 29s
217150K .......... .......... .......... .......... .......... 43% 6.47M 29s
217200K .......... .......... .......... .......... .......... 43% 10.7M 29s
217250K .......... .......... .......... .......... .......... 43% 39.3M 29s
217300K .......... .......... .......... .......... .......... 43% 22.1M 29s
217350K .......... .......... .......... .......... .......... 43% 13.4M 29s
217400K .......... .......... .......... .......... .......... 43% 13.4M 29s
217450K .......... .......... .......... .......... .......... 43% 14.0M 29s
217500K .......... .......... .......... .......... .......... 43% 10.4M 29s
217550K .......... .......... .......... .......... .......... 43% 11.4M 29s
217600K .......... .......... .......... .......... .......... 43% 8.80M 29s
217650K .......... .......... .......... .......... .......... 43% 8.59M 29s
217700K .......... .......... .......... .......... .......... 43% 11.2M 29s
217750K .......... .......... .......... .......... .......... 43% 10.4M 29s
217800K .......... .......... .......... .......... .......... 43% 7.89M 29s
217850K .......... .......... .......... .......... .......... 43% 6.33M 29s
217900K .......... .......... .......... .......... .......... 43% 6.37M 29s
217950K .......... .......... .......... .......... .......... 43% 5.94M 29s
218000K .......... .......... .......... .......... .......... 43% 8.19M 29s
218050K .......... .......... .......... .......... .......... 43% 7.05M 29s
218100K .......... .......... .......... .......... .......... 43% 8.17M 29s
218150K .......... .......... .......... .......... .......... 43% 5.52M 29s
218200K .......... .......... .......... .......... .......... 43% 7.28M 29s
218250K .......... .......... .......... .......... .......... 43% 7.82M 29s
218300K .......... .......... .......... .......... .......... 43% 5.52M 29s
218350K .......... .......... .......... .......... .......... 43% 4.64M 29s
218400K .......... .......... .......... .......... .......... 43% 5.64M 29s
218450K .......... .......... .......... .......... .......... 43% 4.95M 29s
218500K .......... .......... .......... .......... .......... 43% 4.44M 29s
218550K .......... .......... .......... .......... .......... 43% 8.10M 29s
218600K .......... .......... .......... .......... .......... 43% 8.25M 29s
218650K .......... .......... .......... .......... .......... 43% 7.94M 29s
218700K .......... .......... .......... .......... .......... 43% 7.10M 29s
218750K .......... .......... .......... .......... .......... 43% 9.33M 29s
218800K .......... .......... .......... .......... .......... 43% 15.3M 29s
218850K .......... .......... .......... .......... .......... 43% 22.3M 29s
218900K .......... .......... .......... .......... .......... 43% 19.3M 29s
218950K .......... .......... .......... .......... .......... 43% 46.5M 29s
219000K .......... .......... .......... .......... .......... 43% 20.1M 29s
219050K .......... .......... .......... .......... .......... 43% 13.9M 29s
219100K .......... .......... .......... .......... .......... 43% 10.8M 29s
219150K .......... .......... .......... .......... .......... 43% 14.5M 29s
219200K .......... .......... .......... .......... .......... 43% 13.2M 29s
219250K .......... .......... .......... .......... .......... 43% 15.4M 29s
219300K .......... .......... .......... .......... .......... 43% 18.7M 29s
219350K .......... .......... .......... .......... .......... 43% 10.8M 29s
219400K .......... .......... .......... .......... .......... 43% 14.3M 29s
219450K .......... .......... .......... .......... .......... 43% 13.3M 29s
219500K .......... .......... .......... .......... .......... 43% 15.5M 29s
219550K .......... .......... .......... .......... .......... 43% 22.1M 29s
219600K .......... .......... .......... .......... .......... 43% 15.8M 29s
219650K .......... .......... .......... .......... .......... 43% 18.2M 29s
219700K .......... .......... .......... .......... .......... 43% 16.1M 29s
219750K .......... .......... .......... .......... .......... 43% 18.9M 29s
219800K .......... .......... .......... .......... .......... 43% 16.0M 29s
219850K .......... .......... .......... .......... .......... 43% 15.6M 29s
219900K .......... .......... .......... .......... .......... 43% 18.0M 29s
219950K .......... .......... .......... .......... .......... 43% 12.0M 29s
220000K .......... .......... .......... .......... .......... 43% 16.9M 29s
220050K .......... .......... .......... .......... .......... 43% 36.5M 29s
220100K .......... .......... .......... .......... .......... 43% 29.3M 29s
220150K .......... .......... .......... .......... .......... 43% 36.4M 29s
220200K .......... .......... .......... .......... .......... 43% 15.6M 29s
220250K .......... .......... .......... .......... .......... 43% 43.6M 29s
220300K .......... .......... .......... .......... .......... 43% 32.4M 29s
220350K .......... .......... .......... .......... .......... 43% 16.5M 29s
220400K .......... .......... .......... .......... .......... 43% 23.1M 29s
220450K .......... .......... .......... .......... .......... 43% 20.5M 29s
220500K .......... .......... .......... .......... .......... 43% 22.5M 29s
220550K .......... .......... .......... .......... .......... 43% 24.0M 29s
220600K .......... .......... .......... .......... .......... 43% 17.7M 29s
220650K .......... .......... .......... .......... .......... 43% 19.7M 29s
220700K .......... .......... .......... .......... .......... 43% 22.0M 29s
220750K .......... .......... .......... .......... .......... 43% 22.8M 29s
220800K .......... .......... .......... .......... .......... 43% 21.3M 29s
220850K .......... .......... .......... .......... .......... 43% 15.2M 29s
220900K .......... .......... .......... .......... .......... 43% 21.0M 29s
220950K .......... .......... .......... .......... .......... 43% 12.9M 29s
221000K .......... .......... .......... .......... .......... 43% 16.3M 29s
221050K .......... .......... .......... .......... .......... 43% 14.0M 29s
221100K .......... .......... .......... .......... .......... 43% 11.8M 29s
221150K .......... .......... .......... .......... .......... 43% 13.8M 29s
221200K .......... .......... .......... .......... .......... 43% 12.8M 29s
221250K .......... .......... .......... .......... .......... 43% 15.7M 29s
221300K .......... .......... .......... .......... .......... 43% 11.7M 29s
221350K .......... .......... .......... .......... .......... 43% 6.66M 29s
221400K .......... .......... .......... .......... .......... 43% 7.66M 29s
221450K .......... .......... .......... .......... .......... 43% 7.00M 29s
221500K .......... .......... .......... .......... .......... 43% 8.35M 29s
221550K .......... .......... .......... .......... .......... 43% 8.70M 29s
221600K .......... .......... .......... .......... .......... 43% 5.80M 29s
221650K .......... .......... .......... .......... .......... 43% 6.65M 29s
221700K .......... .......... .......... .......... .......... 43% 5.02M 29s
221750K .......... .......... .......... .......... .......... 43% 6.71M 29s
221800K .......... .......... .......... .......... .......... 43% 5.95M 28s
221850K .......... .......... .......... .......... .......... 43% 11.2M 28s
221900K .......... .......... .......... .......... .......... 43% 8.63M 28s
221950K .......... .......... .......... .......... .......... 43% 9.12M 28s
222000K .......... .......... .......... .......... .......... 43% 9.54M 28s
222050K .......... .......... .......... .......... .......... 43% 7.99M 28s
222100K .......... .......... .......... .......... .......... 43% 7.48M 28s
222150K .......... .......... .......... .......... .......... 44% 7.10M 28s
222200K .......... .......... .......... .......... .......... 44% 5.20M 28s
222250K .......... .......... .......... .......... .......... 44% 8.70M 28s
222300K .......... .......... .......... .......... .......... 44% 6.75M 28s
222350K .......... .......... .......... .......... .......... 44% 5.80M 28s
222400K .......... .......... .......... .......... .......... 44% 4.79M 28s
222450K .......... .......... .......... .......... .......... 44% 3.97M 28s
222500K .......... .......... .......... .......... .......... 44% 4.75M 28s
222550K .......... .......... .......... .......... .......... 44% 5.44M 28s
222600K .......... .......... .......... .......... .......... 44% 4.88M 28s
222650K .......... .......... .......... .......... .......... 44% 5.26M 28s
222700K .......... .......... .......... .......... .......... 44% 7.61M 28s
222750K .......... .......... .......... .......... .......... 44% 21.8M 28s
222800K .......... .......... .......... .......... .......... 44% 23.1M 28s
222850K .......... .......... .......... .......... .......... 44% 14.2M 28s
222900K .......... .......... .......... .......... .......... 44% 17.2M 28s
222950K .......... .......... .......... .......... .......... 44% 15.8M 28s
223000K .......... .......... .......... .......... .......... 44% 16.8M 28s
223050K .......... .......... .......... .......... .......... 44% 13.3M 28s
223100K .......... .......... .......... .......... .......... 44% 14.1M 28s
223150K .......... .......... .......... .......... .......... 44% 10.7M 28s
223200K .......... .......... .......... .......... .......... 44% 11.5M 28s
223250K .......... .......... .......... .......... .......... 44% 12.8M 28s
223300K .......... .......... .......... .......... .......... 44% 9.94M 28s
223350K .......... .......... .......... .......... .......... 44% 12.1M 28s
223400K .......... .......... .......... .......... .......... 44% 10.8M 28s
223450K .......... .......... .......... .......... .......... 44% 8.85M 28s
223500K .......... .......... .......... .......... .......... 44% 12.0M 28s
223550K .......... .......... .......... .......... .......... 44% 8.80M 28s
223600K .......... .......... .......... .......... .......... 44% 6.96M 28s
223650K .......... .......... .......... .......... .......... 44% 7.57M 28s
223700K .......... .......... .......... .......... .......... 44% 7.66M 28s
223750K .......... .......... .......... .......... .......... 44% 11.2M 28s
223800K .......... .......... .......... .......... .......... 44% 9.87M 28s
223850K .......... .......... .......... .......... .......... 44% 7.66M 28s
223900K .......... .......... .......... .......... .......... 44% 12.0M 28s
223950K .......... .......... .......... .......... .......... 44% 9.47M 28s
224000K .......... .......... .......... .......... .......... 44% 7.79M 28s
224050K .......... .......... .......... .......... .......... 44% 8.46M 28s
224100K .......... .......... .......... .......... .......... 44% 5.54M 28s
224150K .......... .......... .......... .......... .......... 44% 6.12M 28s
224200K .......... .......... .......... .......... .......... 44% 4.74M 28s
224250K .......... .......... .......... .......... .......... 44% 6.08M 28s
224300K .......... .......... .......... .......... .......... 44% 5.70M 28s
224350K .......... .......... .......... .......... .......... 44% 3.92M 28s
224400K .......... .......... .......... .......... .......... 44% 7.35M 28s
224450K .......... .......... .......... .......... .......... 44% 5.72M 28s
224500K .......... .......... .......... .......... .......... 44% 6.26M 28s
224550K .......... .......... .......... .......... .......... 44% 6.06M 28s
224600K .......... .......... .......... .......... .......... 44% 10.5M 28s
224650K .......... .......... .......... .......... .......... 44% 30.8M 28s
224700K .......... .......... .......... .......... .......... 44% 21.4M 28s
224750K .......... .......... .......... .......... .......... 44% 16.1M 28s
224800K .......... .......... .......... .......... .......... 44% 15.9M 28s
224850K .......... .......... .......... .......... .......... 44% 12.0M 28s
224900K .......... .......... .......... .......... .......... 44% 14.3M 28s
224950K .......... .......... .......... .......... .......... 44% 11.6M 28s
225000K .......... .......... .......... .......... .......... 44% 10.6M 28s
225050K .......... .......... .......... .......... .......... 44% 11.1M 28s
225100K .......... .......... .......... .......... .......... 44% 11.2M 28s
225150K .......... .......... .......... .......... .......... 44% 11.6M 28s
225200K .......... .......... .......... .......... .......... 44% 9.06M 28s
225250K .......... .......... .......... .......... .......... 44% 8.83M 28s
225300K .......... .......... .......... .......... .......... 44% 8.04M 28s
225350K .......... .......... .......... .......... .......... 44% 4.92M 28s
225400K .......... .......... .......... .......... .......... 44% 6.14M 28s
225450K .......... .......... .......... .......... .......... 44% 5.54M 28s
225500K .......... .......... .......... .......... .......... 44% 9.18M 28s
225550K .......... .......... .......... .......... .......... 44% 16.1M 28s
225600K .......... .......... .......... .......... .......... 44% 7.68M 28s
225650K .......... .......... .......... .......... .......... 44% 7.42M 28s
225700K .......... .......... .......... .......... .......... 44% 5.85M 28s
225750K .......... .......... .......... .......... .......... 44% 7.74M 28s
225800K .......... .......... .......... .......... .......... 44% 8.91M 28s
225850K .......... .......... .......... .......... .......... 44% 7.55M 28s
225900K .......... .......... .......... .......... .......... 44% 6.60M 28s
225950K .......... .......... .......... .......... .......... 44% 11.2M 28s
226000K .......... .......... .......... .......... .......... 44% 10.2M 28s
226050K .......... .......... .......... .......... .......... 44% 10.1M 28s
226100K .......... .......... .......... .......... .......... 44% 6.49M 28s
226150K .......... .......... .......... .......... .......... 44% 9.02M 28s
226200K .......... .......... .......... .......... .......... 44% 6.05M 28s
226250K .......... .......... .......... .......... .......... 44% 9.89M 28s
226300K .......... .......... .......... .......... .......... 44% 12.0M 28s
226350K .......... .......... .......... .......... .......... 44% 8.59M 28s
226400K .......... .......... .......... .......... .......... 44% 10.2M 28s
226450K .......... .......... .......... .......... .......... 44% 8.04M 28s
226500K .......... .......... .......... .......... .......... 44% 7.23M 28s
226550K .......... .......... .......... .......... .......... 44% 11.0M 28s
226600K .......... .......... .......... .......... .......... 44% 10.5M 28s
226650K .......... .......... .......... .......... .......... 44% 7.77M 28s
226700K .......... .......... .......... .......... .......... 44% 8.74M 28s
226750K .......... .......... .......... .......... .......... 44% 6.69M 28s
226800K .......... .......... .......... .......... .......... 44% 6.53M 28s
226850K .......... .......... .......... .......... .......... 44% 4.41M 28s
226900K .......... .......... .......... .......... .......... 44% 7.71M 28s
226950K .......... .......... .......... .......... .......... 44% 9.24M 28s
227000K .......... .......... .......... .......... .......... 44% 9.63M 28s
227050K .......... .......... .......... .......... .......... 44% 9.65M 28s
227100K .......... .......... .......... .......... .......... 44% 7.73M 28s
227150K .......... .......... .......... .......... .......... 44% 8.34M 28s
227200K .......... .......... .......... .......... .......... 45% 5.94M 28s
227250K .......... .......... .......... .......... .......... 45% 8.26M 28s
227300K .......... .......... .......... .......... .......... 45% 6.68M 28s
227350K .......... .......... .......... .......... .......... 45% 5.58M 28s
227400K .......... .......... .......... .......... .......... 45% 7.44M 28s
227450K .......... .......... .......... .......... .......... 45% 7.54M 28s
227500K .......... .......... .......... .......... .......... 45% 7.76M 28s
227550K .......... .......... .......... .......... .......... 45% 9.15M 28s
227600K .......... .......... .......... .......... .......... 45% 6.61M 28s
227650K .......... .......... .......... .......... .......... 45% 8.25M 28s
227700K .......... .......... .......... .......... .......... 45% 8.09M 28s
227750K .......... .......... .......... .......... .......... 45% 9.45M 28s
227800K .......... .......... .......... .......... .......... 45% 7.10M 28s
227850K .......... .......... .......... .......... .......... 45% 5.85M 28s
227900K .......... .......... .......... .......... .......... 45% 5.40M 28s
227950K .......... .......... .......... .......... .......... 45% 4.06M 28s
228000K .......... .......... .......... .......... .......... 45% 4.43M 28s
228050K .......... .......... .......... .......... .......... 45% 13.9M 28s
228100K .......... .......... .......... .......... .......... 45% 14.8M 28s
228150K .......... .......... .......... .......... .......... 45% 16.8M 28s
228200K .......... .......... .......... .......... .......... 45% 11.6M 28s
228250K .......... .......... .......... .......... .......... 45% 20.4M 28s
228300K .......... .......... .......... .......... .......... 45% 15.6M 28s
228350K .......... .......... .......... .......... .......... 45% 11.5M 28s
228400K .......... .......... .......... .......... .......... 45% 10.9M 28s
228450K .......... .......... .......... .......... .......... 45% 6.20M 28s
228500K .......... .......... .......... .......... .......... 45% 8.39M 28s
228550K .......... .......... .......... .......... .......... 45% 9.78M 28s
228600K .......... .......... .......... .......... .......... 45% 7.07M 28s
228650K .......... .......... .......... .......... .......... 45% 6.70M 28s
228700K .......... .......... .......... .......... .......... 45% 5.61M 28s
228750K .......... .......... .......... .......... .......... 45% 6.57M 28s
228800K .......... .......... .......... .......... .......... 45% 6.65M 28s
228850K .......... .......... .......... .......... .......... 45% 4.23M 28s
228900K .......... .......... .......... .......... .......... 45% 6.13M 28s
228950K .......... .......... .......... .......... .......... 45% 4.68M 28s
229000K .......... .......... .......... .......... .......... 45% 8.62M 28s
229050K .......... .......... .......... .......... .......... 45% 6.34M 28s
229100K .......... .......... .......... .......... .......... 45% 6.79M 28s
229150K .......... .......... .......... .......... .......... 45% 7.55M 28s
229200K .......... .......... .......... .......... .......... 45% 5.46M 28s
229250K .......... .......... .......... .......... .......... 45% 5.08M 28s
229300K .......... .......... .......... .......... .......... 45% 5.92M 28s
229350K .......... .......... .......... .......... .......... 45% 8.79M 28s
229400K .......... .......... .......... .......... .......... 45% 9.61M 28s
229450K .......... .......... .......... .......... .......... 45% 7.67M 28s
229500K .......... .......... .......... .......... .......... 45% 9.82M 28s
229550K .......... .......... .......... .......... .......... 45% 10.1M 28s
229600K .......... .......... .......... .......... .......... 45% 7.46M 28s
229650K .......... .......... .......... .......... .......... 45% 8.80M 28s
229700K .......... .......... .......... .......... .......... 45% 6.46M 28s
229750K .......... .......... .......... .......... .......... 45% 8.04M 28s
229800K .......... .......... .......... .......... .......... 45% 14.0M 28s
229850K .......... .......... .......... .......... .......... 45% 14.5M 28s
229900K .......... .......... .......... .......... .......... 45%  196M 28s
229950K .......... .......... .......... .......... .......... 45% 22.1M 28s
230000K .......... .......... .......... .......... .......... 45% 33.4M 28s
230050K .......... .......... .......... .......... .......... 45% 32.7M 28s
230100K .......... .......... .......... .......... .......... 45% 23.0M 28s
230150K .......... .......... .......... .......... .......... 45% 19.9M 28s
230200K .......... .......... .......... .......... .......... 45% 30.3M 28s
230250K .......... .......... .......... .......... .......... 45% 36.4M 28s
230300K .......... .......... .......... .......... .......... 45% 27.9M 28s
230350K .......... .......... .......... .......... .......... 45% 36.3M 28s
230400K .......... .......... .......... .......... .......... 45% 24.8M 28s
230450K .......... .......... .......... .......... .......... 45% 18.7M 28s
230500K .......... .......... .......... .......... .......... 45% 17.8M 28s
230550K .......... .......... .......... .......... .......... 45% 11.2M 28s
230600K .......... .......... .......... .......... .......... 45% 8.79M 28s
230650K .......... .......... .......... .......... .......... 45% 11.3M 28s
230700K .......... .......... .......... .......... .......... 45% 9.40M 28s
230750K .......... .......... .......... .......... .......... 45% 9.19M 28s
230800K .......... .......... .......... .......... .......... 45% 8.28M 28s
230850K .......... .......... .......... .......... .......... 45% 6.95M 28s
230900K .......... .......... .......... .......... .......... 45% 7.48M 28s
230950K .......... .......... .......... .......... .......... 45% 6.11M 28s
231000K .......... .......... .......... .......... .......... 45% 5.54M 28s
231050K .......... .......... .......... .......... .......... 45% 6.00M 28s
231100K .......... .......... .......... .......... .......... 45% 6.05M 28s
231150K .......... .......... .......... .......... .......... 45% 7.48M 28s
231200K .......... .......... .......... .......... .......... 45% 5.70M 28s
231250K .......... .......... .......... .......... .......... 45% 20.2M 28s
231300K .......... .......... .......... .......... .......... 45% 23.5M 28s
231350K .......... .......... .......... .......... .......... 45% 26.3M 28s
231400K .......... .......... .......... .......... .......... 45% 26.2M 28s
231450K .......... .......... .......... .......... .......... 45% 21.0M 28s
231500K .......... .......... .......... .......... .......... 45% 17.0M 28s
231550K .......... .......... .......... .......... .......... 45% 11.6M 28s
231600K .......... .......... .......... .......... .......... 45% 11.8M 28s
231650K .......... .......... .......... .......... .......... 45% 13.7M 28s
231700K .......... .......... .......... .......... .......... 45% 11.8M 28s
231750K .......... .......... .......... .......... .......... 45% 12.1M 28s
231800K .......... .......... .......... .......... .......... 45% 8.58M 28s
231850K .......... .......... .......... .......... .......... 45% 14.7M 28s
231900K .......... .......... .......... .......... .......... 45% 14.0M 28s
231950K .......... .......... .......... .......... .......... 45% 9.85M 28s
232000K .......... .......... .......... .......... .......... 45% 14.9M 28s
232050K .......... .......... .......... .......... .......... 45% 14.8M 28s
232100K .......... .......... .......... .......... .......... 45% 11.7M 28s
232150K .......... .......... .......... .......... .......... 45% 11.4M 28s
232200K .......... .......... .......... .......... .......... 45% 14.0M 28s
232250K .......... .......... .......... .......... .......... 46% 13.8M 28s
232300K .......... .......... .......... .......... .......... 46% 13.5M 28s
232350K .......... .......... .......... .......... .......... 46% 25.2M 28s
232400K .......... .......... .......... .......... .......... 46% 17.2M 28s
232450K .......... .......... .......... .......... .......... 46%  107M 28s
232500K .......... .......... .......... .......... .......... 46% 21.2M 28s
232550K .......... .......... .......... .......... .......... 46% 24.4M 28s
232600K .......... .......... .......... .......... .......... 46% 16.4M 28s
232650K .......... .......... .......... .......... .......... 46% 14.0M 28s
232700K .......... .......... .......... .......... .......... 46% 8.89M 28s
232750K .......... .......... .......... .......... .......... 46% 14.8M 28s
232800K .......... .......... .......... .......... .......... 46% 14.8M 28s
232850K .......... .......... .......... .......... .......... 46% 10.4M 28s
232900K .......... .......... .......... .......... .......... 46% 15.0M 28s
232950K .......... .......... .......... .......... .......... 46% 10.2M 27s
233000K .......... .......... .......... .......... .......... 46% 11.1M 27s
233050K .......... .......... .......... .......... .......... 46% 7.70M 27s
233100K .......... .......... .......... .......... .......... 46% 8.24M 27s
233150K .......... .......... .......... .......... .......... 46% 6.31M 27s
233200K .......... .......... .......... .......... .......... 46% 6.06M 27s
233250K .......... .......... .......... .......... .......... 46% 6.63M 27s
233300K .......... .......... .......... .......... .......... 46% 6.97M 27s
233350K .......... .......... .......... .......... .......... 46% 6.15M 27s
233400K .......... .......... .......... .......... .......... 46% 10.2M 27s
233450K .......... .......... .......... .......... .......... 46% 6.20M 27s
233500K .......... .......... .......... .......... .......... 46% 11.1M 27s
233550K .......... .......... .......... .......... .......... 46% 11.2M 27s
233600K .......... .......... .......... .......... .......... 46% 11.2M 27s
233650K .......... .......... .......... .......... .......... 46% 9.88M 27s
233700K .......... .......... .......... .......... .......... 46% 7.09M 27s
233750K .......... .......... .......... .......... .......... 46% 8.18M 27s
233800K .......... .......... .......... .......... .......... 46% 5.94M 27s
233850K .......... .......... .......... .......... .......... 46% 4.44M 27s
233900K .......... .......... .......... .......... .......... 46% 5.09M 27s
233950K .......... .......... .......... .......... .......... 46% 4.76M 27s
234000K .......... .......... .......... .......... .......... 46% 7.51M 27s
234050K .......... .......... .......... .......... .......... 46% 6.14M 27s
234100K .......... .......... .......... .......... .......... 46% 6.34M 27s
234150K .......... .......... .......... .......... .......... 46% 6.20M 27s
234200K .......... .......... .......... .......... .......... 46% 4.41M 27s
234250K .......... .......... .......... .......... .......... 46% 5.27M 27s
234300K .......... .......... .......... .......... .......... 46% 8.14M 27s
234350K .......... .......... .......... .......... .......... 46% 7.69M 27s
234400K .......... .......... .......... .......... .......... 46% 9.03M 27s
234450K .......... .......... .......... .......... .......... 46% 5.95M 27s
234500K .......... .......... .......... .......... .......... 46% 7.79M 27s
234550K .......... .......... .......... .......... .......... 46% 6.03M 27s
234600K .......... .......... .......... .......... .......... 46% 4.20M 27s
234650K .......... .......... .......... .......... .......... 46% 4.51M 27s
234700K .......... .......... .......... .......... .......... 46% 3.43M 27s
234750K .......... .......... .......... .......... .......... 46% 3.61M 27s
234800K .......... .......... .......... .......... .......... 46% 8.64M 27s
234850K .......... .......... .......... .......... .......... 46% 12.8M 27s
234900K .......... .......... .......... .......... .......... 46% 38.6M 27s
234950K .......... .......... .......... .......... .......... 46% 12.2M 27s
235000K .......... .......... .......... .......... .......... 46% 20.9M 27s
235050K .......... .......... .......... .......... .......... 46% 11.9M 27s
235100K .......... .......... .......... .......... .......... 46% 9.08M 27s
235150K .......... .......... .......... .......... .......... 46% 12.7M 27s
235200K .......... .......... .......... .......... .......... 46% 7.71M 27s
235250K .......... .......... .......... .......... .......... 46% 8.19M 27s
235300K .......... .......... .......... .......... .......... 46% 12.2M 27s
235350K .......... .......... .......... .......... .......... 46% 11.3M 27s
235400K .......... .......... .......... .......... .......... 46% 10.3M 27s
235450K .......... .......... .......... .......... .......... 46% 8.72M 27s
235500K .......... .......... .......... .......... .......... 46% 11.6M 27s
235550K .......... .......... .......... .......... .......... 46% 9.68M 27s
235600K .......... .......... .......... .......... .......... 46% 4.87M 27s
235650K .......... .......... .......... .......... .......... 46% 4.33M 27s
235700K .......... .......... .......... .......... .......... 46% 5.02M 27s
235750K .......... .......... .......... .......... .......... 46% 6.85M 27s
235800K .......... .......... .......... .......... .......... 46% 10.2M 27s
235850K .......... .......... .......... .......... .......... 46% 21.5M 27s
235900K .......... .......... .......... .......... .......... 46% 21.5M 27s
235950K .......... .......... .......... .......... .......... 46% 13.2M 27s
236000K .......... .......... .......... .......... .......... 46% 14.5M 27s
236050K .......... .......... .......... .......... .......... 46% 8.25M 27s
236100K .......... .......... .......... .......... .......... 46% 8.76M 27s
236150K .......... .......... .......... .......... .......... 46% 14.4M 27s
236200K .......... .......... .......... .......... .......... 46% 11.8M 27s
236250K .......... .......... .......... .......... .......... 46% 12.6M 27s
236300K .......... .......... .......... .......... .......... 46% 17.3M 27s
236350K .......... .......... .......... .......... .......... 46% 8.94M 27s
236400K .......... .......... .......... .......... .......... 46% 10.4M 27s
236450K .......... .......... .......... .......... .......... 46% 8.11M 27s
236500K .......... .......... .......... .......... .......... 46% 8.49M 27s
236550K .......... .......... .......... .......... .......... 46% 7.52M 27s
236600K .......... .......... .......... .......... .......... 46% 6.92M 27s
236650K .......... .......... .......... .......... .......... 46% 7.95M 27s
236700K .......... .......... .......... .......... .......... 46% 7.97M 27s
236750K .......... .......... .......... .......... .......... 46% 7.92M 27s
236800K .......... .......... .......... .......... .......... 46% 19.2M 27s
236850K .......... .......... .......... .......... .......... 46% 20.6M 27s
236900K .......... .......... .......... .......... .......... 46% 33.1M 27s
236950K .......... .......... .......... .......... .......... 46% 11.6M 27s
237000K .......... .......... .......... .......... .......... 46% 20.6M 27s
237050K .......... .......... .......... .......... .......... 46% 11.7M 27s
237100K .......... .......... .......... .......... .......... 46% 9.57M 27s
237150K .......... .......... .......... .......... .......... 46% 8.46M 27s
237200K .......... .......... .......... .......... .......... 46% 8.12M 27s
237250K .......... .......... .......... .......... .......... 46% 6.20M 27s
237300K .......... .......... .......... .......... .......... 47% 8.14M 27s
237350K .......... .......... .......... .......... .......... 47% 7.38M 27s
237400K .......... .......... .......... .......... .......... 47% 9.38M 27s
237450K .......... .......... .......... .......... .......... 47% 7.37M 27s
237500K .......... .......... .......... .......... .......... 47% 7.39M 27s
237550K .......... .......... .......... .......... .......... 47% 6.09M 27s
237600K .......... .......... .......... .......... .......... 47% 3.29M 27s
237650K .......... .......... .......... .......... .......... 47% 4.02M 27s
237700K .......... .......... .......... .......... .......... 47% 3.24M 27s
237750K .......... .......... .......... .......... .......... 47% 3.77M 27s
237800K .......... .......... .......... .......... .......... 47% 3.51M 27s
237850K .......... .......... .......... .......... .......... 47% 5.28M 27s
237900K .......... .......... .......... .......... .......... 47% 30.7M 27s
237950K .......... .......... .......... .......... .......... 47% 15.5M 27s
238000K .......... .......... .......... .......... .......... 47%  201M 27s
238050K .......... .......... .......... .......... .......... 47% 28.9M 27s
238100K .......... .......... .......... .......... .......... 47% 24.4M 27s
238150K .......... .......... .......... .......... .......... 47% 49.5M 27s
238200K .......... .......... .......... .......... .......... 47% 15.0M 27s
238250K .......... .......... .......... .......... .......... 47% 21.5M 27s
238300K .......... .......... .......... .......... .......... 47% 17.4M 27s
238350K .......... .......... .......... .......... .......... 47% 20.2M 27s
238400K .......... .......... .......... .......... .......... 47% 17.4M 27s
238450K .......... .......... .......... .......... .......... 47% 19.8M 27s
238500K .......... .......... .......... .......... .......... 47% 19.7M 27s
238550K .......... .......... .......... .......... .......... 47% 20.2M 27s
238600K .......... .......... .......... .......... .......... 47% 13.9M 27s
238650K .......... .......... .......... .......... .......... 47% 20.1M 27s
238700K .......... .......... .......... .......... .......... 47% 10.9M 27s
238750K .......... .......... .......... .......... .......... 47% 13.9M 27s
238800K .......... .......... .......... .......... .......... 47% 13.0M 27s
238850K .......... .......... .......... .......... .......... 47% 8.69M 27s
238900K .......... .......... .......... .......... .......... 47% 11.9M 27s
238950K .......... .......... .......... .......... .......... 47% 10.9M 27s
239000K .......... .......... .......... .......... .......... 47% 11.4M 27s
239050K .......... .......... .......... .......... .......... 47% 13.2M 27s
239100K .......... .......... .......... .......... .......... 47% 6.84M 27s
239150K .......... .......... .......... .......... .......... 47% 7.31M 27s
239200K .......... .......... .......... .......... .......... 47% 7.78M 27s
239250K .......... .......... .......... .......... .......... 47% 8.91M 27s
239300K .......... .......... .......... .......... .......... 47% 8.50M 27s
239350K .......... .......... .......... .......... .......... 47% 8.18M 27s
239400K .......... .......... .......... .......... .......... 47% 5.76M 27s
239450K .......... .......... .......... .......... .......... 47% 5.52M 27s
239500K .......... .......... .......... .......... .......... 47% 8.10M 27s
239550K .......... .......... .......... .......... .......... 47% 8.78M 27s
239600K .......... .......... .......... .......... .......... 47% 8.34M 27s
239650K .......... .......... .......... .......... .......... 47% 9.07M 27s
239700K .......... .......... .......... .......... .......... 47% 7.99M 27s
239750K .......... .......... .......... .......... .......... 47% 14.2M 27s
239800K .......... .......... .......... .......... .......... 47% 34.4M 27s
239850K .......... .......... .......... .......... .......... 47% 21.9M 27s
239900K .......... .......... .......... .......... .......... 47% 32.7M 27s
239950K .......... .......... .......... .......... .......... 47% 19.8M 27s
240000K .......... .......... .......... .......... .......... 47% 30.4M 27s
240050K .......... .......... .......... .......... .......... 47% 22.7M 27s
240100K .......... .......... .......... .......... .......... 47% 16.8M 27s
240150K .......... .......... .......... .......... .......... 47% 20.1M 27s
240200K .......... .......... .......... .......... .......... 47% 21.8M 27s
240250K .......... .......... .......... .......... .......... 47% 20.2M 27s
240300K .......... .......... .......... .......... .......... 47% 17.7M 27s
240350K .......... .......... .......... .......... .......... 47% 14.5M 27s
240400K .......... .......... .......... .......... .......... 47% 15.1M 27s
240450K .......... .......... .......... .......... .......... 47% 11.3M 27s
240500K .......... .......... .......... .......... .......... 47% 11.0M 27s
240550K .......... .......... .......... .......... .......... 47% 12.3M 27s
240600K .......... .......... .......... .......... .......... 47% 9.04M 27s
240650K .......... .......... .......... .......... .......... 47% 12.5M 27s
240700K .......... .......... .......... .......... .......... 47% 7.24M 27s
240750K .......... .......... .......... .......... .......... 47% 10.6M 27s
240800K .......... .......... .......... .......... .......... 47% 11.7M 27s
240850K .......... .......... .......... .......... .......... 47% 8.09M 27s
240900K .......... .......... .......... .......... .......... 47% 9.91M 27s
240950K .......... .......... .......... .......... .......... 47% 8.21M 27s
241000K .......... .......... .......... .......... .......... 47% 11.2M 27s
241050K .......... .......... .......... .......... .......... 47% 10.1M 27s
241100K .......... .......... .......... .......... .......... 47% 10.8M 27s
241150K .......... .......... .......... .......... .......... 47% 18.9M 27s
241200K .......... .......... .......... .......... .......... 47% 20.8M 27s
241250K .......... .......... .......... .......... .......... 47% 15.3M 27s
241300K .......... .......... .......... .......... .......... 47% 24.6M 27s
241350K .......... .......... .......... .......... .......... 47% 14.4M 27s
241400K .......... .......... .......... .......... .......... 47% 16.4M 27s
241450K .......... .......... .......... .......... .......... 47% 11.4M 27s
241500K .......... .......... .......... .......... .......... 47% 13.9M 27s
241550K .......... .......... .......... .......... .......... 47% 13.2M 27s
241600K .......... .......... .......... .......... .......... 47% 11.3M 27s
241650K .......... .......... .......... .......... .......... 47% 11.6M 27s
241700K .......... .......... .......... .......... .......... 47% 5.75M 27s
241750K .......... .......... .......... .......... .......... 47% 6.34M 27s
241800K .......... .......... .......... .......... .......... 47% 7.63M 27s
241850K .......... .......... .......... .......... .......... 47% 5.29M 27s
241900K .......... .......... .......... .......... .......... 47% 7.31M 27s
241950K .......... .......... .......... .......... .......... 47% 10.1M 27s
242000K .......... .......... .......... .......... .......... 47% 19.3M 27s
242050K .......... .......... .......... .......... .......... 47% 17.8M 27s
242100K .......... .......... .......... .......... .......... 47% 16.3M 27s
242150K .......... .......... .......... .......... .......... 47% 17.7M 27s
242200K .......... .......... .......... .......... .......... 47% 16.9M 27s
242250K .......... .......... .......... .......... .......... 47% 17.3M 27s
242300K .......... .......... .......... .......... .......... 47% 25.0M 27s
242350K .......... .......... .......... .......... .......... 48% 16.0M 27s
242400K .......... .......... .......... .......... .......... 48% 25.3M 27s
242450K .......... .......... .......... .......... .......... 48% 18.4M 27s
242500K .......... .......... .......... .......... .......... 48% 19.7M 27s
242550K .......... .......... .......... .......... .......... 48% 17.7M 27s
242600K .......... .......... .......... .......... .......... 48% 22.7M 27s
242650K .......... .......... .......... .......... .......... 48% 14.3M 27s
242700K .......... .......... .......... .......... .......... 48% 26.3M 27s
242750K .......... .......... .......... .......... .......... 48% 15.7M 27s
242800K .......... .......... .......... .......... .......... 48% 11.9M 27s
242850K .......... .......... .......... .......... .......... 48% 10.6M 27s
242900K .......... .......... .......... .......... .......... 48% 12.3M 27s
242950K .......... .......... .......... .......... .......... 48% 8.13M 27s
243000K .......... .......... .......... .......... .......... 48% 9.45M 27s
243050K .......... .......... .......... .......... .......... 48% 6.82M 27s
243100K .......... .......... .......... .......... .......... 48% 4.96M 27s
243150K .......... .......... .......... .......... .......... 48% 6.67M 27s
243200K .......... .......... .......... .......... .......... 48% 4.60M 27s
243250K .......... .......... .......... .......... .......... 48% 6.78M 27s
243300K .......... .......... .......... .......... .......... 48% 6.53M 27s
243350K .......... .......... .......... .......... .......... 48% 5.38M 27s
243400K .......... .......... .......... .......... .......... 48% 7.27M 26s
243450K .......... .......... .......... .......... .......... 48% 6.01M 26s
243500K .......... .......... .......... .......... .......... 48% 6.90M 26s
243550K .......... .......... .......... .......... .......... 48% 6.84M 26s
243600K .......... .......... .......... .......... .......... 48% 9.56M 26s
243650K .......... .......... .......... .......... .......... 48% 18.1M 26s
243700K .......... .......... .......... .......... .......... 48% 17.5M 26s
243750K .......... .......... .......... .......... .......... 48% 21.7M 26s
243800K .......... .......... .......... .......... .......... 48% 11.6M 26s
243850K .......... .......... .......... .......... .......... 48% 8.46M 26s
243900K .......... .......... .......... .......... .......... 48% 8.23M 26s
243950K .......... .......... .......... .......... .......... 48% 7.92M 26s
244000K .......... .......... .......... .......... .......... 48% 13.5M 26s
244050K .......... .......... .......... .......... .......... 48% 10.6M 26s
244100K .......... .......... .......... .......... .......... 48% 5.94M 26s
244150K .......... .......... .......... .......... .......... 48% 5.69M 26s
244200K .......... .......... .......... .......... .......... 48% 4.37M 26s
244250K .......... .......... .......... .......... .......... 48% 5.45M 26s
244300K .......... .......... .......... .......... .......... 48% 9.83M 26s
244350K .......... .......... .......... .......... .......... 48% 17.4M 26s
244400K .......... .......... .......... .......... .......... 48% 19.5M 26s
244450K .......... .......... .......... .......... .......... 48% 37.2M 26s
244500K .......... .......... .......... .......... .......... 48% 41.9M 26s
244550K .......... .......... .......... .......... .......... 48% 39.4M 26s
244600K .......... .......... .......... .......... .......... 48% 15.1M 26s
244650K .......... .......... .......... .......... .......... 48% 16.7M 26s
244700K .......... .......... .......... .......... .......... 48% 13.3M 26s
244750K .......... .......... .......... .......... .......... 48% 30.5M 26s
244800K .......... .......... .......... .......... .......... 48% 14.3M 26s
244850K .......... .......... .......... .......... .......... 48% 11.8M 26s
244900K .......... .......... .......... .......... .......... 48% 14.7M 26s
244950K .......... .......... .......... .......... .......... 48% 9.60M 26s
245000K .......... .......... .......... .......... .......... 48% 9.16M 26s
245050K .......... .......... .......... .......... .......... 48% 8.33M 26s
245100K .......... .......... .......... .......... .......... 48% 6.99M 26s
245150K .......... .......... .......... .......... .......... 48% 7.47M 26s
245200K .......... .......... .......... .......... .......... 48% 7.59M 26s
245250K .......... .......... .......... .......... .......... 48% 7.73M 26s
245300K .......... .......... .......... .......... .......... 48% 17.6M 26s
245350K .......... .......... .......... .......... .......... 48% 20.9M 26s
245400K .......... .......... .......... .......... .......... 48% 33.4M 26s
245450K .......... .......... .......... .......... .......... 48% 17.7M 26s
245500K .......... .......... .......... .......... .......... 48% 21.5M 26s
245550K .......... .......... .......... .......... .......... 48% 17.8M 26s
245600K .......... .......... .......... .......... .......... 48% 11.9M 26s
245650K .......... .......... .......... .......... .......... 48% 10.7M 26s
245700K .......... .......... .......... .......... .......... 48% 9.13M 26s
245750K .......... .......... .......... .......... .......... 48% 10.4M 26s
245800K .......... .......... .......... .......... .......... 48% 7.77M 26s
245850K .......... .......... .......... .......... .......... 48% 7.83M 26s
245900K .......... .......... .......... .......... .......... 48% 8.45M 26s
245950K .......... .......... .......... .......... .......... 48% 8.57M 26s
246000K .......... .......... .......... .......... .......... 48% 9.27M 26s
246050K .......... .......... .......... .......... .......... 48% 8.52M 26s
246100K .......... .......... .......... .......... .......... 48% 5.39M 26s
246150K .......... .......... .......... .......... .......... 48% 8.41M 26s
246200K .......... .......... .......... .......... .......... 48% 5.96M 26s
246250K .......... .......... .......... .......... .......... 48% 6.08M 26s
246300K .......... .......... .......... .......... .......... 48% 7.97M 26s
246350K .......... .......... .......... .......... .......... 48% 8.68M 26s
246400K .......... .......... .......... .......... .......... 48% 7.54M 26s
246450K .......... .......... .......... .......... .......... 48% 7.29M 26s
246500K .......... .......... .......... .......... .......... 48% 8.07M 26s
246550K .......... .......... .......... .......... .......... 48% 5.63M 26s
246600K .......... .......... .......... .......... .......... 48% 5.49M 26s
246650K .......... .......... .......... .......... .......... 48% 9.30M 26s
246700K .......... .......... .......... .......... .......... 48% 7.48M 26s
246750K .......... .......... .......... .......... .......... 48% 6.39M 26s
246800K .......... .......... .......... .......... .......... 48% 6.10M 26s
246850K .......... .......... .......... .......... .......... 48% 8.85M 26s
246900K .......... .......... .......... .......... .......... 48% 17.0M 26s
246950K .......... .......... .......... .......... .......... 48% 11.2M 26s
247000K .......... .......... .......... .......... .......... 48% 15.3M 26s
247050K .......... .......... .......... .......... .......... 48% 14.4M 26s
247100K .......... .......... .......... .......... .......... 48% 12.3M 26s
247150K .......... .......... .......... .......... .......... 48% 15.3M 26s
247200K .......... .......... .......... .......... .......... 48% 8.24M 26s
247250K .......... .......... .......... .......... .......... 48% 11.4M 26s
247300K .......... .......... .......... .......... .......... 48% 11.9M 26s
247350K .......... .......... .......... .......... .......... 48% 8.46M 26s
247400K .......... .......... .......... .......... .......... 49% 6.87M 26s
247450K .......... .......... .......... .......... .......... 49% 7.87M 26s
247500K .......... .......... .......... .......... .......... 49% 8.44M 26s
247550K .......... .......... .......... .......... .......... 49% 8.44M 26s
247600K .......... .......... .......... .......... .......... 49% 7.41M 26s
247650K .......... .......... .......... .......... .......... 49% 9.89M 26s
247700K .......... .......... .......... .......... .......... 49% 10.6M 26s
247750K .......... .......... .......... .......... .......... 49% 11.1M 26s
247800K .......... .......... .......... .......... .......... 49% 11.8M 26s
247850K .......... .......... .......... .......... .......... 49% 10.7M 26s
247900K .......... .......... .......... .......... .......... 49% 10.3M 26s
247950K .......... .......... .......... .......... .......... 49% 16.6M 26s
248000K .......... .......... .......... .......... .......... 49% 11.4M 26s
248050K .......... .......... .......... .......... .......... 49% 12.5M 26s
248100K .......... .......... .......... .......... .......... 49% 13.2M 26s
248150K .......... .......... .......... .......... .......... 49% 9.96M 26s
248200K .......... .......... .......... .......... .......... 49% 7.44M 26s
248250K .......... .......... .......... .......... .......... 49% 13.7M 26s
248300K .......... .......... .......... .......... .......... 49% 10.8M 26s
248350K .......... .......... .......... .......... .......... 49% 10.1M 26s
248400K .......... .......... .......... .......... .......... 49% 11.3M 26s
248450K .......... .......... .......... .......... .......... 49% 11.3M 26s
248500K .......... .......... .......... .......... .......... 49% 9.77M 26s
248550K .......... .......... .......... .......... .......... 49% 10.1M 26s
248600K .......... .......... .......... .......... .......... 49% 6.06M 26s
248650K .......... .......... .......... .......... .......... 49% 4.86M 26s
248700K .......... .......... .......... .......... .......... 49% 5.62M 26s
248750K .......... .......... .......... .......... .......... 49% 5.30M 26s
248800K .......... .......... .......... .......... .......... 49% 6.46M 26s
248850K .......... .......... .......... .......... .......... 49% 4.54M 26s
248900K .......... .......... .......... .......... .......... 49% 5.04M 26s
248950K .......... .......... .......... .......... .......... 49% 4.81M 26s
249000K .......... .......... .......... .......... .......... 49% 5.70M 26s
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249100K .......... .......... .......... .......... .......... 49% 5.49M 26s
249150K .......... .......... .......... .......... .......... 49% 8.29M 26s
249200K .......... .......... .......... .......... .......... 49% 10.1M 26s
249250K .......... .......... .......... .......... .......... 49% 10.0M 26s
249300K .......... .......... .......... .......... .......... 49% 13.8M 26s
249350K .......... .......... .......... .......... .......... 49% 9.05M 26s
249400K .......... .......... .......... .......... .......... 49% 13.0M 26s
249450K .......... .......... .......... .......... .......... 49% 7.75M 26s
249500K .......... .......... .......... .......... .......... 49% 14.1M 26s
249550K .......... .......... .......... .......... .......... 49% 10.6M 26s
249600K .......... .......... .......... .......... .......... 49% 6.24M 26s
249650K .......... .......... .......... .......... .......... 49% 13.7M 26s
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249850K .......... .......... .......... .......... .......... 49% 14.4M 26s
249900K .......... .......... .......... .......... .......... 49% 18.5M 26s
249950K .......... .......... .......... .......... .......... 49% 14.1M 26s
250000K .......... .......... .......... .......... .......... 49% 16.1M 26s
250050K .......... .......... .......... .......... .......... 49% 19.2M 26s
250100K .......... .......... .......... .......... .......... 49% 10.6M 26s
250150K .......... .......... .......... .......... .......... 49% 12.0M 26s
250200K .......... .......... .......... .......... .......... 49% 7.58M 26s
250250K .......... .......... .......... .......... .......... 49% 6.62M 26s
250300K .......... .......... .......... .......... .......... 49% 6.38M 26s
250350K .......... .......... .......... .......... .......... 49% 4.52M 26s
250400K .......... .......... .......... .......... .......... 49% 4.17M 26s
250450K .......... .......... .......... .......... .......... 49% 3.38M 26s
250500K .......... .......... .......... .......... .......... 49% 13.8M 26s
250550K .......... .......... .......... .......... .......... 49% 11.8M 26s
250600K .......... .......... .......... .......... .......... 49% 9.98M 26s
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250700K .......... .......... .......... .......... .......... 49% 5.58M 26s
250750K .......... .......... .......... .......... .......... 49% 4.87M 26s
250800K .......... .......... .......... .......... .......... 49% 5.64M 26s
250850K .......... .......... .......... .......... .......... 49% 3.98M 26s
250900K .......... .......... .......... .......... .......... 49% 3.26M 26s
250950K .......... .......... .......... .......... .......... 49% 3.25M 26s
251000K .......... .......... .......... .......... .......... 49% 17.4M 26s
251050K .......... .......... .......... .......... .......... 49% 15.7M 26s
251100K .......... .......... .......... .......... .......... 49% 17.3M 26s
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251200K .......... .......... .......... .......... .......... 49% 12.6M 26s
251250K .......... .......... .......... .......... .......... 49% 11.6M 26s
251300K .......... .......... .......... .......... .......... 49% 12.3M 26s
251350K .......... .......... .......... .......... .......... 49% 10.3M 26s
251400K .......... .......... .......... .......... .......... 49% 13.1M 26s
251450K .......... .......... .......... .......... .......... 49% 9.31M 26s
251500K .......... .......... .......... .......... .......... 49% 13.1M 26s
251550K .......... .......... .......... .......... .......... 49% 14.6M 26s
251600K .......... .......... .......... .......... .......... 49% 8.95M 26s
251650K .......... .......... .......... .......... .......... 49% 14.1M 26s
251700K .......... .......... .......... .......... .......... 49% 22.0M 26s
251750K .......... .......... .......... .......... .......... 49% 34.1M 26s
251800K .......... .......... .......... .......... .......... 49% 22.1M 26s
251850K .......... .......... .......... .......... .......... 49% 21.6M 26s
251900K .......... .......... .......... .......... .......... 49% 39.3M 26s
251950K .......... .......... .......... .......... .......... 49% 17.8M 26s
252000K .......... .......... .......... .......... .......... 49% 21.0M 26s
252050K .......... .......... .......... .......... .......... 49% 16.5M 26s
252100K .......... .......... .......... .......... .......... 49% 10.3M 26s
252150K .......... .......... .......... .......... .......... 49% 14.9M 26s
252200K .......... .......... .......... .......... .......... 49% 11.3M 26s
252250K .......... .......... .......... .......... .......... 49% 9.46M 26s
252300K .......... .......... .......... .......... .......... 49% 10.2M 26s
252350K .......... .......... .......... .......... .......... 49% 8.86M 26s
252400K .......... .......... .......... .......... .......... 49% 10.1M 26s
252450K .......... .......... .......... .......... .......... 50% 9.10M 26s
252500K .......... .......... .......... .......... .......... 50% 8.25M 26s
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252600K .......... .......... .......... .......... .......... 50% 7.18M 26s
252650K .......... .......... .......... .......... .......... 50% 6.74M 26s
252700K .......... .......... .......... .......... .......... 50% 5.41M 26s
252750K .......... .......... .......... .......... .......... 50% 7.13M 26s
252800K .......... .......... .......... .......... .......... 50% 7.12M 26s
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252900K .......... .......... .......... .......... .......... 50% 34.6M 26s
252950K .......... .......... .......... .......... .......... 50% 18.4M 26s
253000K .......... .......... .......... .......... .......... 50% 37.3M 26s
253050K .......... .......... .......... .......... .......... 50% 39.4M 26s
253100K .......... .......... .......... .......... .......... 50% 21.6M 26s
253150K .......... .......... .......... .......... .......... 50%  153M 26s
253200K .......... .......... .......... .......... .......... 50% 20.9M 26s
253250K .......... .......... .......... .......... .......... 50% 26.1M 26s
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253400K .......... .......... .......... .......... .......... 50% 14.5M 26s
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253500K .......... .......... .......... .......... .......... 50% 15.8M 25s
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253700K .......... .......... .......... .......... .......... 50% 10.2M 25s
253750K .......... .......... .......... .......... .......... 50% 15.0M 25s
253800K .......... .......... .......... .......... .......... 50% 15.0M 25s
253850K .......... .......... .......... .......... .......... 50% 11.0M 25s
253900K .......... .......... .......... .......... .......... 50% 9.57M 25s
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254000K .......... .......... .......... .......... .......... 50% 7.85M 25s
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254100K .......... .......... .......... .......... .......... 50% 6.02M 25s
254150K .......... .......... .......... .......... .......... 50% 6.91M 25s
254200K .......... .......... .......... .......... .......... 50% 6.22M 25s
254250K .......... .......... .......... .......... .......... 50% 7.67M 25s
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254350K .......... .......... .......... .......... .......... 50% 21.6M 25s
254400K .......... .......... .......... .......... .......... 50% 35.0M 25s
254450K .......... .......... .......... .......... .......... 50% 18.3M 25s
254500K .......... .......... .......... .......... .......... 50% 28.9M 25s
254550K .......... .......... .......... .......... .......... 50% 12.9M 25s
254600K .......... .......... .......... .......... .......... 50% 23.8M 25s
254650K .......... .......... .......... .......... .......... 50% 12.0M 25s
254700K .......... .......... .......... .......... .......... 50% 11.5M 25s
254750K .......... .......... .......... .......... .......... 50% 13.1M 25s
254800K .......... .......... .......... .......... .......... 50% 9.50M 25s
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254900K .......... .......... .......... .......... .......... 50% 9.60M 25s
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255000K .......... .......... .......... .......... .......... 50% 11.4M 25s
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255100K .......... .......... .......... .......... .......... 50% 7.49M 25s
255150K .......... .......... .......... .......... .......... 50% 10.0M 25s
255200K .......... .......... .......... .......... .......... 50% 11.5M 25s
255250K .......... .......... .......... .......... .......... 50% 17.6M 25s
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255400K .......... .......... .......... .......... .......... 50% 7.79M 25s
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255800K .......... .......... .......... .......... .......... 50% 14.7M 25s
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256000K .......... .......... .......... .......... .......... 50% 11.1M 25s
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256100K .......... .......... .......... .......... .......... 50% 10.7M 25s
256150K .......... .......... .......... .......... .......... 50% 14.4M 25s
256200K .......... .......... .......... .......... .......... 50% 12.2M 25s
256250K .......... .......... .......... .......... .......... 50% 14.0M 25s
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256500K .......... .......... .......... .......... .......... 50% 17.9M 25s
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256650K .......... .......... .......... .......... .......... 50% 20.9M 25s
256700K .......... .......... .......... .......... .......... 50% 14.0M 25s
256750K .......... .......... .......... .......... .......... 50% 20.0M 25s
256800K .......... .......... .......... .......... .......... 50% 14.8M 25s
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256900K .......... .......... .......... .......... .......... 50% 14.4M 25s
256950K .......... .......... .......... .......... .......... 50% 12.1M 25s
257000K .......... .......... .......... .......... .......... 50% 14.0M 25s
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257100K .......... .......... .......... .......... .......... 50% 12.1M 25s
257150K .......... .......... .......... .......... .......... 50% 13.2M 25s
257200K .......... .......... .......... .......... .......... 50% 11.9M 25s
257250K .......... .......... .......... .......... .......... 50% 12.2M 25s
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257350K .......... .......... .......... .......... .......... 50% 9.39M 25s
257400K .......... .......... .......... .......... .......... 50% 9.74M 25s
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257500K .......... .......... .......... .......... .......... 51% 8.38M 25s
257550K .......... .......... .......... .......... .......... 51% 10.8M 25s
257600K .......... .......... .......... .......... .......... 51% 6.45M 25s
257650K .......... .......... .......... .......... .......... 51% 7.39M 25s
257700K .......... .......... .......... .......... .......... 51% 6.86M 25s
257750K .......... .......... .......... .......... .......... 51% 7.12M 25s
257800K .......... .......... .......... .......... .......... 51% 10.2M 25s
257850K .......... .......... .......... .......... .......... 51% 10.1M 25s
257900K .......... .......... .......... .......... .......... 51% 8.59M 25s
257950K .......... .......... .......... .......... .......... 51% 7.57M 25s
258000K .......... .......... .......... .......... .......... 51% 9.61M 25s
258050K .......... .......... .......... .......... .......... 51% 8.69M 25s
258100K .......... .......... .......... .......... .......... 51% 5.28M 25s
258150K .......... .......... .......... .......... .......... 51% 9.03M 25s
258200K .......... .......... .......... .......... .......... 51% 9.41M 25s
258250K .......... .......... .......... .......... .......... 51% 7.67M 25s
258300K .......... .......... .......... .......... .......... 51% 8.91M 25s
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258400K .......... .......... .......... .......... .......... 51% 10.0M 25s
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258500K .......... .......... .......... .......... .......... 51% 7.96M 25s
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258750K .......... .......... .......... .......... .......... 51% 11.1M 25s
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258900K .......... .......... .......... .......... .......... 51% 17.6M 25s
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259000K .......... .......... .......... .......... .......... 51% 37.4M 25s
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259100K .......... .......... .......... .......... .......... 51% 19.4M 25s
259150K .......... .......... .......... .......... .......... 51% 22.8M 25s
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259250K .......... .......... .......... .......... .......... 51% 16.6M 25s
259300K .......... .......... .......... .......... .......... 51% 36.5M 25s
259350K .......... .......... .......... .......... .......... 51% 22.9M 25s
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259650K .......... .......... .......... .......... .......... 51% 19.7M 25s
259700K .......... .......... .......... .......... .......... 51% 17.3M 25s
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259800K .......... .......... .......... .......... .......... 51% 13.8M 25s
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260000K .......... .......... .......... .......... .......... 51% 49.1M 25s
260050K .......... .......... .......... .......... .......... 51% 43.1M 25s
260100K .......... .......... .......... .......... .......... 51% 20.3M 25s
260150K .......... .......... .......... .......... .......... 51%  131M 25s
260200K .......... .......... .......... .......... .......... 51%  118M 25s
260250K .......... .......... .......... .......... .......... 51% 23.1M 25s
260300K .......... .......... .......... .......... .......... 51% 40.0M 25s
260350K .......... .......... .......... .......... .......... 51% 15.1M 25s
260400K .......... .......... .......... .......... .......... 51% 16.7M 25s
260450K .......... .......... .......... .......... .......... 51% 9.44M 25s
260500K .......... .......... .......... .......... .......... 51% 23.3M 25s
260550K .......... .......... .......... .......... .......... 51% 7.35M 25s
260600K .......... .......... .......... .......... .......... 51% 6.31M 25s
260650K .......... .......... .......... .......... .......... 51% 5.53M 25s
260700K .......... .......... .......... .......... .......... 51% 5.93M 25s
260750K .......... .......... .......... .......... .......... 51% 6.40M 25s
260800K .......... .......... .......... .......... .......... 51% 6.79M 25s
260850K .......... .......... .......... .......... .......... 51% 6.15M 25s
260900K .......... .......... .......... .......... .......... 51% 7.73M 25s
260950K .......... .......... .......... .......... .......... 51% 19.0M 25s
261000K .......... .......... .......... .......... .......... 51% 32.7M 25s
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261100K .......... .......... .......... .......... .......... 51% 11.6M 25s
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261200K .......... .......... .......... .......... .......... 51% 10.7M 25s
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261300K .......... .......... .......... .......... .......... 51% 11.5M 25s
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261400K .......... .......... .......... .......... .......... 51% 9.91M 25s
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261500K .......... .......... .......... .......... .......... 51% 11.2M 25s
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261600K .......... .......... .......... .......... .......... 51% 7.73M 25s
261650K .......... .......... .......... .......... .......... 51% 6.59M 25s
261700K .......... .......... .......... .......... .......... 51% 7.61M 25s
261750K .......... .......... .......... .......... .......... 51% 7.91M 25s
261800K .......... .......... .......... .......... .......... 51% 7.14M 25s
261850K .......... .......... .......... .......... .......... 51% 8.10M 25s
261900K .......... .......... .......... .......... .......... 51% 9.40M 25s
261950K .......... .......... .......... .......... .......... 51% 8.72M 25s
262000K .......... .......... .......... .......... .......... 51% 11.4M 25s
262050K .......... .......... .......... .......... .......... 51% 9.60M 25s
262100K .......... .......... .......... .......... .......... 51% 10.9M 25s
262150K .......... .......... .......... .......... .......... 51% 9.02M 25s
262200K .......... .......... .......... .......... .......... 51% 12.1M 24s
262250K .......... .......... .......... .......... .......... 51% 15.7M 24s
262300K .......... .......... .......... .......... .......... 51% 10.7M 24s
262350K .......... .......... .......... .......... .......... 51% 12.0M 24s
262400K .......... .......... .......... .......... .......... 51% 12.3M 24s
262450K .......... .......... .......... .......... .......... 51% 12.4M 24s
262500K .......... .......... .......... .......... .......... 52% 12.6M 24s
262550K .......... .......... .......... .......... .......... 52% 12.8M 24s
262600K .......... .......... .......... .......... .......... 52% 12.9M 24s
262650K .......... .......... .......... .......... .......... 52% 13.0M 24s
262700K .......... .......... .......... .......... .......... 52% 9.48M 24s
262750K .......... .......... .......... .......... .......... 52% 16.1M 24s
262800K .......... .......... .......... .......... .......... 52% 14.4M 24s
262850K .......... .......... .......... .......... .......... 52% 35.1M 24s
262900K .......... .......... .......... .......... .......... 52% 20.2M 24s
262950K .......... .......... .......... .......... .......... 52% 10.2M 24s
263000K .......... .......... .......... .......... .......... 52% 13.8M 24s
263050K .......... .......... .......... .......... .......... 52% 8.81M 24s
263100K .......... .......... .......... .......... .......... 52% 8.35M 24s
263150K .......... .......... .......... .......... .......... 52% 11.0M 24s
263200K .......... .......... .......... .......... .......... 52% 7.83M 24s
263250K .......... .......... .......... .......... .......... 52% 9.18M 24s
263300K .......... .......... .......... .......... .......... 52% 10.5M 24s
263350K .......... .......... .......... .......... .......... 52% 8.38M 24s
263400K .......... .......... .......... .......... .......... 52% 10.2M 24s
263450K .......... .......... .......... .......... .......... 52% 8.70M 24s
263500K .......... .......... .......... .......... .......... 52% 8.02M 24s
263550K .......... .......... .......... .......... .......... 52% 11.1M 24s
263600K .......... .......... .......... .......... .......... 52% 6.68M 24s
263650K .......... .......... .......... .......... .......... 52% 6.65M 24s
263700K .......... .......... .......... .......... .......... 52% 6.44M 24s
263750K .......... .......... .......... .......... .......... 52% 8.48M 24s
263800K .......... .......... .......... .......... .......... 52% 7.56M 24s
263850K .......... .......... .......... .......... .......... 52% 5.84M 24s
263900K .......... .......... .......... .......... .......... 52% 12.2M 24s
263950K .......... .......... .......... .......... .......... 52% 25.3M 24s
264000K .......... .......... .......... .......... .......... 52% 16.8M 24s
264050K .......... .......... .......... .......... .......... 52% 19.2M 24s
264100K .......... .......... .......... .......... .......... 52% 15.2M 24s
264150K .......... .......... .......... .......... .......... 52% 10.2M 24s
264200K .......... .......... .......... .......... .......... 52% 5.82M 24s
264250K .......... .......... .......... .......... .......... 52% 10.6M 24s
264300K .......... .......... .......... .......... .......... 52% 15.3M 24s
264350K .......... .......... .......... .......... .......... 52% 13.1M 24s
264400K .......... .......... .......... .......... .......... 52% 14.0M 24s
264450K .......... .......... .......... .......... .......... 52% 15.1M 24s
264500K .......... .......... .......... .......... .......... 52% 11.9M 24s
264550K .......... .......... .......... .......... .......... 52% 13.3M 24s
264600K .......... .......... .......... .......... .......... 52% 14.5M 24s
264650K .......... .......... .......... .......... .......... 52% 13.6M 24s
264700K .......... .......... .......... .......... .......... 52% 11.9M 24s
264750K .......... .......... .......... .......... .......... 52% 17.3M 24s
264800K .......... .......... .......... .......... .......... 52% 5.73M 24s
264850K .......... .......... .......... .......... .......... 52% 15.6M 24s
264900K .......... .......... .......... .......... .......... 52% 19.2M 24s
264950K .......... .......... .......... .......... .......... 52% 22.9M 24s
265000K .......... .......... .......... .......... .......... 52% 13.0M 24s
265050K .......... .......... .......... .......... .......... 52% 76.8M 24s
265100K .......... .......... .......... .......... .......... 52% 11.0M 24s
265150K .......... .......... .......... .......... .......... 52% 18.9M 24s
265200K .......... .......... .......... .......... .......... 52% 13.9M 24s
265250K .......... .......... .......... .......... .......... 52% 21.1M 24s
265300K .......... .......... .......... .......... .......... 52% 22.1M 24s
265350K .......... .......... .......... .......... .......... 52% 14.6M 24s
265400K .......... .......... .......... .......... .......... 52% 15.7M 24s
265450K .......... .......... .......... .......... .......... 52% 21.8M 24s
265500K .......... .......... .......... .......... .......... 52% 15.4M 24s
265550K .......... .......... .......... .......... .......... 52% 20.2M 24s
265600K .......... .......... .......... .......... .......... 52% 18.2M 24s
265650K .......... .......... .......... .......... .......... 52% 19.1M 24s
265700K .......... .......... .......... .......... .......... 52% 18.0M 24s
265750K .......... .......... .......... .......... .......... 52% 17.5M 24s
265800K .......... .......... .......... .......... .......... 52% 23.3M 24s
265850K .......... .......... .......... .......... .......... 52% 23.1M 24s
265900K .......... .......... .......... .......... .......... 52% 10.0M 24s
265950K .......... .......... .......... .......... .......... 52%  122M 24s
266000K .......... .......... .......... .......... .......... 52% 18.9M 24s
266050K .......... .......... .......... .......... .......... 52% 20.2M 24s
266100K .......... .......... .......... .......... .......... 52% 19.0M 24s
266150K .......... .......... .......... .......... .......... 52% 15.5M 24s
266200K .......... .......... .......... .......... .......... 52% 16.4M 24s
266250K .......... .......... .......... .......... .......... 52% 18.2M 24s
266300K .......... .......... .......... .......... .......... 52% 22.9M 24s
266350K .......... .......... .......... .......... .......... 52% 15.6M 24s
266400K .......... .......... .......... .......... .......... 52% 22.2M 24s
266450K .......... .......... .......... .......... .......... 52% 16.3M 24s
266500K .......... .......... .......... .......... .......... 52% 24.4M 24s
266550K .......... .......... .......... .......... .......... 52% 18.6M 24s
266600K .......... .......... .......... .......... .......... 52% 16.5M 24s
266650K .......... .......... .......... .......... .......... 52% 16.6M 24s
266700K .......... .......... .......... .......... .......... 52% 17.3M 24s
266750K .......... .......... .......... .......... .......... 52% 14.7M 24s
266800K .......... .......... .......... .......... .......... 52% 14.4M 24s
266850K .......... .......... .......... .......... .......... 52% 22.6M 24s
266900K .......... .......... .......... .......... .......... 52% 43.4M 24s
266950K .......... .......... .......... .......... .......... 52% 20.2M 24s
267000K .......... .......... .......... .......... .......... 52% 24.9M 24s
267050K .......... .......... .......... .......... .......... 52% 55.0M 24s
267100K .......... .......... .......... .......... .......... 52% 11.6M 24s
267150K .......... .......... .......... .......... .......... 52% 27.4M 24s
267200K .......... .......... .......... .......... .......... 52% 26.3M 24s
267250K .......... .......... .......... .......... .......... 52% 29.2M 24s
267300K .......... .......... .......... .......... .......... 52% 29.7M 24s
267350K .......... .......... .......... .......... .......... 52% 26.4M 24s
267400K .......... .......... .......... .......... .......... 52% 35.5M 24s
267450K .......... .......... .......... .......... .......... 52% 20.8M 24s
267500K .......... .......... .......... .......... .......... 52% 19.7M 24s
267550K .......... .......... .......... .......... .......... 53% 14.0M 24s
267600K .......... .......... .......... .......... .......... 53% 18.0M 24s
267650K .......... .......... .......... .......... .......... 53% 14.5M 24s
267700K .......... .......... .......... .......... .......... 53% 13.9M 24s
267750K .......... .......... .......... .......... .......... 53% 18.0M 24s
267800K .......... .......... .......... .......... .......... 53% 17.1M 24s
267850K .......... .......... .......... .......... .......... 53% 8.75M 24s
267900K .......... .......... .......... .......... .......... 53% 25.9M 24s
267950K .......... .......... .......... .......... .......... 53% 9.81M 24s
268000K .......... .......... .......... .......... .......... 53% 17.8M 24s
268050K .......... .......... .......... .......... .......... 53% 11.4M 24s
268100K .......... .......... .......... .......... .......... 53% 11.8M 24s
268150K .......... .......... .......... .......... .......... 53% 17.5M 24s
268200K .......... .......... .......... .......... .......... 53% 8.70M 24s
268250K .......... .......... .......... .......... .......... 53% 11.9M 24s
268300K .......... .......... .......... .......... .......... 53% 8.67M 24s
268350K .......... .......... .......... .......... .......... 53% 7.58M 24s
268400K .......... .......... .......... .......... .......... 53% 12.0M 24s
268450K .......... .......... .......... .......... .......... 53% 9.42M 24s
268500K .......... .......... .......... .......... .......... 53% 11.0M 24s
268550K .......... .......... .......... .......... .......... 53% 12.5M 24s
268600K .......... .......... .......... .......... .......... 53% 12.0M 24s
268650K .......... .......... .......... .......... .......... 53% 14.7M 24s
268700K .......... .......... .......... .......... .......... 53% 10.9M 24s
268750K .......... .......... .......... .......... .......... 53% 11.8M 24s
268800K .......... .......... .......... .......... .......... 53% 12.1M 24s
268850K .......... .......... .......... .......... .......... 53% 10.5M 24s
268900K .......... .......... .......... .......... .......... 53% 15.9M 24s
268950K .......... .......... .......... .......... .......... 53% 12.9M 24s
269000K .......... .......... .......... .......... .......... 53% 14.2M 24s
269050K .......... .......... .......... .......... .......... 53% 18.2M 24s
269100K .......... .......... .......... .......... .......... 53% 12.1M 24s
269150K .......... .......... .......... .......... .......... 53% 18.9M 24s
269200K .......... .......... .......... .......... .......... 53% 29.4M 24s
269250K .......... .......... .......... .......... .......... 53% 37.5M 24s
269300K .......... .......... .......... .......... .......... 53% 24.0M 24s
269350K .......... .......... .......... .......... .......... 53%  142M 24s
269400K .......... .......... .......... .......... .......... 53% 43.6M 24s
269450K .......... .......... .......... .......... .......... 53% 31.7M 24s
269500K .......... .......... .......... .......... .......... 53% 29.5M 24s
269550K .......... .......... .......... .......... .......... 53% 23.8M 24s
269600K .......... .......... .......... .......... .......... 53% 27.2M 24s
269650K .......... .......... .......... .......... .......... 53% 16.2M 24s
269700K .......... .......... .......... .......... .......... 53% 23.6M 24s
269750K .......... .......... .......... .......... .......... 53% 18.3M 24s
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269850K .......... .......... .......... .......... .......... 53% 18.5M 24s
269900K .......... .......... .......... .......... .......... 53% 17.0M 24s
269950K .......... .......... .......... .......... .......... 53% 16.5M 23s
270000K .......... .......... .......... .......... .......... 53% 20.7M 23s
270050K .......... .......... .......... .......... .......... 53% 19.1M 23s
270100K .......... .......... .......... .......... .......... 53% 14.2M 23s
270150K .......... .......... .......... .......... .......... 53% 17.3M 23s
270200K .......... .......... .......... .......... .......... 53% 14.1M 23s
270250K .......... .......... .......... .......... .......... 53% 21.7M 23s
270300K .......... .......... .......... .......... .......... 53% 17.2M 23s
270350K .......... .......... .......... .......... .......... 53% 14.5M 23s
270400K .......... .......... .......... .......... .......... 53% 16.4M 23s
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270550K .......... .......... .......... .......... .......... 53% 10.3M 23s
270600K .......... .......... .......... .......... .......... 53% 8.17M 23s
270650K .......... .......... .......... .......... .......... 53% 10.5M 23s
270700K .......... .......... .......... .......... .......... 53% 8.55M 23s
270750K .......... .......... .......... .......... .......... 53% 11.2M 23s
270800K .......... .......... .......... .......... .......... 53% 13.1M 23s
270850K .......... .......... .......... .......... .......... 53% 9.21M 23s
270900K .......... .......... .......... .......... .......... 53% 8.12M 23s
270950K .......... .......... .......... .......... .......... 53% 8.94M 23s
271000K .......... .......... .......... .......... .......... 53% 8.78M 23s
271050K .......... .......... .......... .......... .......... 53% 8.23M 23s
271100K .......... .......... .......... .......... .......... 53% 6.86M 23s
271150K .......... .......... .......... .......... .......... 53% 12.1M 23s
271200K .......... .......... .......... .......... .......... 53% 8.34M 23s
271250K .......... .......... .......... .......... .......... 53% 16.0M 23s
271300K .......... .......... .......... .......... .......... 53% 41.8M 23s
271350K .......... .......... .......... .......... .......... 53% 20.0M 23s
271400K .......... .......... .......... .......... .......... 53% 58.4M 23s
271450K .......... .......... .......... .......... .......... 53% 20.1M 23s
271500K .......... .......... .......... .......... .......... 53% 17.6M 23s
271550K .......... .......... .......... .......... .......... 53% 18.3M 23s
271600K .......... .......... .......... .......... .......... 53% 14.1M 23s
271650K .......... .......... .......... .......... .......... 53% 21.2M 23s
271700K .......... .......... .......... .......... .......... 53% 13.4M 23s
271750K .......... .......... .......... .......... .......... 53% 16.0M 23s
271800K .......... .......... .......... .......... .......... 53% 17.1M 23s
271850K .......... .......... .......... .......... .......... 53% 14.2M 23s
271900K .......... .......... .......... .......... .......... 53% 17.3M 23s
271950K .......... .......... .......... .......... .......... 53% 11.0M 23s
272000K .......... .......... .......... .......... .......... 53% 15.2M 23s
272050K .......... .......... .......... .......... .......... 53% 12.1M 23s
272100K .......... .......... .......... .......... .......... 53% 13.8M 23s
272150K .......... .......... .......... .......... .......... 53% 18.0M 23s
272200K .......... .......... .......... .......... .......... 53% 15.5M 23s
272250K .......... .......... .......... .......... .......... 53% 32.9M 23s
272300K .......... .......... .......... .......... .......... 53% 23.1M 23s
272350K .......... .......... .......... .......... .......... 53% 13.2M 23s
272400K .......... .......... .......... .......... .......... 53% 15.9M 23s
272450K .......... .......... .......... .......... .......... 53% 11.9M 23s
272500K .......... .......... .......... .......... .......... 53% 10.8M 23s
272550K .......... .......... .......... .......... .......... 53% 14.3M 23s
272600K .......... .......... .......... .......... .......... 54% 11.1M 23s
272650K .......... .......... .......... .......... .......... 54% 17.8M 23s
272700K .......... .......... .......... .......... .......... 54% 15.2M 23s
272750K .......... .......... .......... .......... .......... 54% 15.0M 23s
272800K .......... .......... .......... .......... .......... 54% 11.0M 23s
272850K .......... .......... .......... .......... .......... 54% 7.01M 23s
272900K .......... .......... .......... .......... .......... 54% 8.72M 23s
272950K .......... .......... .......... .......... .......... 54% 11.1M 23s
273000K .......... .......... .......... .......... .......... 54% 9.21M 23s
273050K .......... .......... .......... .......... .......... 54% 10.6M 23s
273100K .......... .......... .......... .......... .......... 54% 11.0M 23s
273150K .......... .......... .......... .......... .......... 54% 13.9M 23s
273200K .......... .......... .......... .......... .......... 54% 8.90M 23s
273250K .......... .......... .......... .......... .......... 54% 12.1M 23s
273300K .......... .......... .......... .......... .......... 54% 16.1M 23s
273350K .......... .......... .......... .......... .......... 54% 27.1M 23s
273400K .......... .......... .......... .......... .......... 54% 19.1M 23s
273450K .......... .......... .......... .......... .......... 54% 23.0M 23s
273500K .......... .......... .......... .......... .......... 54% 19.2M 23s
273550K .......... .......... .......... .......... .......... 54% 14.8M 23s
273600K .......... .......... .......... .......... .......... 54% 12.6M 23s
273650K .......... .......... .......... .......... .......... 54% 16.2M 23s
273700K .......... .......... .......... .......... .......... 54% 13.2M 23s
273750K .......... .......... .......... .......... .......... 54% 8.94M 23s
273800K .......... .......... .......... .......... .......... 54% 10.6M 23s
273850K .......... .......... .......... .......... .......... 54% 10.6M 23s
273900K .......... .......... .......... .......... .......... 54% 12.8M 23s
273950K .......... .......... .......... .......... .......... 54% 7.14M 23s
274000K .......... .......... .......... .......... .......... 54% 9.05M 23s
274050K .......... .......... .......... .......... .......... 54% 8.69M 23s
274100K .......... .......... .......... .......... .......... 54% 17.3M 23s
274150K .......... .......... .......... .......... .......... 54% 32.6M 23s
274200K .......... .......... .......... .......... .......... 54% 17.5M 23s
274250K .......... .......... .......... .......... .......... 54% 22.3M 23s
274300K .......... .......... .......... .......... .......... 54% 19.7M 23s
274350K .......... .......... .......... .......... .......... 54% 13.6M 23s
274400K .......... .......... .......... .......... .......... 54% 15.4M 23s
274450K .......... .......... .......... .......... .......... 54% 11.8M 23s
274500K .......... .......... .......... .......... .......... 54% 9.09M 23s
274550K .......... .......... .......... .......... .......... 54% 3.37M 23s
274600K .......... .......... .......... .......... .......... 54% 8.37M 23s
274650K .......... .......... .......... .......... .......... 54% 18.5M 23s
274700K .......... .......... .......... .......... .......... 54% 12.7M 23s
274750K .......... .......... .......... .......... .......... 54% 16.0M 23s
274800K .......... .......... .......... .......... .......... 54% 32.5M 23s
274850K .......... .......... .......... .......... .......... 54% 16.9M 23s
274900K .......... .......... .......... .......... .......... 54% 23.3M 23s
274950K .......... .......... .......... .......... .......... 54% 20.7M 23s
275000K .......... .......... .......... .......... .......... 54% 13.6M 23s
275050K .......... .......... .......... .......... .......... 54% 14.0M 23s
275100K .......... .......... .......... .......... .......... 54% 12.3M 23s
275150K .......... .......... .......... .......... .......... 54% 14.4M 23s
275200K .......... .......... .......... .......... .......... 54% 13.4M 23s
275250K .......... .......... .......... .......... .......... 54% 14.8M 23s
275300K .......... .......... .......... .......... .......... 54% 13.4M 23s
275350K .......... .......... .......... .......... .......... 54% 12.7M 23s
275400K .......... .......... .......... .......... .......... 54% 14.1M 23s
275450K .......... .......... .......... .......... .......... 54% 6.20M 23s
275500K .......... .......... .......... .......... .......... 54% 7.91M 23s
275550K .......... .......... .......... .......... .......... 54% 12.7M 23s
275600K .......... .......... .......... .......... .......... 54% 9.20M 23s
275650K .......... .......... .......... .......... .......... 54% 9.63M 23s
275700K .......... .......... .......... .......... .......... 54% 9.93M 23s
275750K .......... .......... .......... .......... .......... 54% 9.50M 23s
275800K .......... .......... .......... .......... .......... 54% 12.0M 23s
275850K .......... .......... .......... .......... .......... 54% 9.01M 23s
275900K .......... .......... .......... .......... .......... 54% 15.2M 23s
275950K .......... .......... .......... .......... .......... 54% 12.5M 23s
276000K .......... .......... .......... .......... .......... 54% 21.2M 23s
276050K .......... .......... .......... .......... .......... 54% 13.8M 23s
276100K .......... .......... .......... .......... .......... 54% 16.2M 23s
276150K .......... .......... .......... .......... .......... 54% 15.7M 23s
276200K .......... .......... .......... .......... .......... 54% 11.3M 23s
276250K .......... .......... .......... .......... .......... 54% 11.8M 23s
276300K .......... .......... .......... .......... .......... 54% 16.3M 23s
276350K .......... .......... .......... .......... .......... 54% 11.2M 23s
276400K .......... .......... .......... .......... .......... 54% 15.7M 23s
276450K .......... .......... .......... .......... .......... 54% 14.3M 23s
276500K .......... .......... .......... .......... .......... 54% 14.3M 23s
276550K .......... .......... .......... .......... .......... 54% 13.1M 23s
276600K .......... .......... .......... .......... .......... 54% 19.2M 23s
276650K .......... .......... .......... .......... .......... 54% 45.2M 23s
276700K .......... .......... .......... .......... .......... 54% 24.7M 23s
276750K .......... .......... .......... .......... .......... 54% 45.6M 23s
276800K .......... .......... .......... .......... .......... 54% 17.7M 23s
276850K .......... .......... .......... .......... .......... 54% 38.8M 23s
276900K .......... .......... .......... .......... .......... 54% 37.2M 23s
276950K .......... .......... .......... .......... .......... 54% 20.0M 23s
277000K .......... .......... .......... .......... .......... 54% 23.6M 23s
277050K .......... .......... .......... .......... .......... 54% 17.7M 23s
277100K .......... .......... .......... .......... .......... 54% 12.9M 23s
277150K .......... .......... .......... .......... .......... 54% 10.5M 23s
277200K .......... .......... .......... .......... .......... 54% 21.7M 23s
277250K .......... .......... .......... .......... .......... 54% 14.5M 23s
277300K .......... .......... .......... .......... .......... 54% 11.8M 23s
277350K .......... .......... .......... .......... .......... 54% 8.79M 23s
277400K .......... .......... .......... .......... .......... 54% 10.6M 23s
277450K .......... .......... .......... .......... .......... 54% 8.49M 23s
277500K .......... .......... .......... .......... .......... 54% 9.83M 23s
277550K .......... .......... .......... .......... .......... 54% 8.72M 23s
277600K .......... .......... .......... .......... .......... 54% 7.58M 23s
277650K .......... .......... .......... .......... .......... 55% 11.2M 23s
277700K .......... .......... .......... .......... .......... 55% 13.4M 23s
277750K .......... .......... .......... .......... .......... 55% 14.8M 23s
277800K .......... .......... .......... .......... .......... 55% 14.0M 23s
277850K .......... .......... .......... .......... .......... 55% 21.9M 23s
277900K .......... .......... .......... .......... .......... 55% 15.0M 23s
277950K .......... .......... .......... .......... .......... 55% 17.8M 23s
278000K .......... .......... .......... .......... .......... 55% 16.5M 23s
278050K .......... .......... .......... .......... .......... 55% 15.9M 23s
278100K .......... .......... .......... .......... .......... 55% 13.3M 23s
278150K .......... .......... .......... .......... .......... 55% 18.7M 23s
278200K .......... .......... .......... .......... .......... 55% 11.4M 23s
278250K .......... .......... .......... .......... .......... 55% 14.1M 22s
278300K .......... .......... .......... .......... .......... 55% 14.1M 22s
278350K .......... .......... .......... .......... .......... 55% 9.99M 22s
278400K .......... .......... .......... .......... .......... 55% 12.8M 22s
278450K .......... .......... .......... .......... .......... 55% 12.6M 22s
278500K .......... .......... .......... .......... .......... 55% 10.3M 22s
278550K .......... .......... .......... .......... .......... 55% 7.42M 22s
278600K .......... .......... .......... .......... .......... 55% 6.23M 22s
278650K .......... .......... .......... .......... .......... 55% 8.15M 22s
278700K .......... .......... .......... .......... .......... 55% 5.98M 22s
278750K .......... .......... .......... .......... .......... 55% 5.25M 22s
278800K .......... .......... .......... .......... .......... 55% 11.1M 22s
278850K .......... .......... .......... .......... .......... 55% 7.57M 22s
278900K .......... .......... .......... .......... .......... 55% 7.59M 22s
278950K .......... .......... .......... .......... .......... 55% 4.90M 22s
279000K .......... .......... .......... .......... .......... 55% 4.54M 22s
279050K .......... .......... .......... .......... .......... 55% 17.1M 22s
279100K .......... .......... .......... .......... .......... 55% 17.1M 22s
279150K .......... .......... .......... .......... .......... 55% 12.7M 22s
279200K .......... .......... .......... .......... .......... 55% 10.1M 22s
279250K .......... .......... .......... .......... .......... 55% 14.6M 22s
279300K .......... .......... .......... .......... .......... 55% 16.3M 22s
279350K .......... .......... .......... .......... .......... 55% 16.4M 22s
279400K .......... .......... .......... .......... .......... 55% 17.5M 22s
279450K .......... .......... .......... .......... .......... 55% 11.0M 22s
279500K .......... .......... .......... .......... .......... 55% 13.1M 22s
279550K .......... .......... .......... .......... .......... 55% 17.1M 22s
279600K .......... .......... .......... .......... .......... 55% 12.3M 22s
279650K .......... .......... .......... .......... .......... 55% 14.5M 22s
279700K .......... .......... .......... .......... .......... 55% 12.1M 22s
279750K .......... .......... .......... .......... .......... 55% 15.9M 22s
279800K .......... .......... .......... .......... .......... 55% 10.6M 22s
279850K .......... .......... .......... .......... .......... 55% 11.3M 22s
279900K .......... .......... .......... .......... .......... 55% 22.8M 22s
279950K .......... .......... .......... .......... .......... 55% 30.7M 22s
280000K .......... .......... .......... .......... .......... 55% 20.9M 22s
280050K .......... .......... .......... .......... .......... 55%  178M 22s
280100K .......... .......... .......... .......... .......... 55% 24.7M 22s
280150K .......... .......... .......... .......... .......... 55% 39.8M 22s
280200K .......... .......... .......... .......... .......... 55% 28.7M 22s
280250K .......... .......... .......... .......... .......... 55% 25.1M 22s
280300K .......... .......... .......... .......... .......... 55% 24.6M 22s
280350K .......... .......... .......... .......... .......... 55% 22.6M 22s
280400K .......... .......... .......... .......... .......... 55% 51.8M 22s
280450K .......... .......... .......... .......... .......... 55% 17.4M 22s
280500K .......... .......... .......... .......... .......... 55% 24.5M 22s
280550K .......... .......... .......... .......... .......... 55% 24.8M 22s
280600K .......... .......... .......... .......... .......... 55% 24.5M 22s
280650K .......... .......... .......... .......... .......... 55% 17.5M 22s
280700K .......... .......... .......... .......... .......... 55% 17.6M 22s
280750K .......... .......... .......... .......... .......... 55% 18.1M 22s
280800K .......... .......... .......... .......... .......... 55% 23.4M 22s
280850K .......... .......... .......... .......... .......... 55% 13.6M 22s
280900K .......... .......... .......... .......... .......... 55% 23.7M 22s
280950K .......... .......... .......... .......... .......... 55% 13.7M 22s
281000K .......... .......... .......... .......... .......... 55% 23.4M 22s
281050K .......... .......... .......... .......... .......... 55% 19.7M 22s
281100K .......... .......... .......... .......... .......... 55% 13.9M 22s
281150K .......... .......... .......... .......... .......... 55% 17.4M 22s
281200K .......... .......... .......... .......... .......... 55% 7.14M 22s
281250K .......... .......... .......... .......... .......... 55% 14.9M 22s
281300K .......... .......... .......... .......... .......... 55% 21.9M 22s
281350K .......... .......... .......... .......... .......... 55% 15.3M 22s
281400K .......... .......... .......... .......... .......... 55% 8.29M 22s
281450K .......... .......... .......... .......... .......... 55% 9.87M 22s
281500K .......... .......... .......... .......... .......... 55% 10.6M 22s
281550K .......... .......... .......... .......... .......... 55% 11.0M 22s
281600K .......... .......... .......... .......... .......... 55% 10.4M 22s
281650K .......... .......... .......... .......... .......... 55% 8.02M 22s
281700K .......... .......... .......... .......... .......... 55% 7.00M 22s
281750K .......... .......... .......... .......... .......... 55% 9.42M 22s
281800K .......... .......... .......... .......... .......... 55% 8.16M 22s
281850K .......... .......... .......... .......... .......... 55% 5.86M 22s
281900K .......... .......... .......... .......... .......... 55% 8.57M 22s
281950K .......... .......... .......... .......... .......... 55% 6.24M 22s
282000K .......... .......... .......... .......... .......... 55% 12.6M 22s
282050K .......... .......... .......... .......... .......... 55% 34.2M 22s
282100K .......... .......... .......... .......... .......... 55% 21.0M 22s
282150K .......... .......... .......... .......... .......... 55% 42.0M 22s
282200K .......... .......... .......... .......... .......... 55% 30.5M 22s
282250K .......... .......... .......... .......... .......... 55% 23.2M 22s
282300K .......... .......... .......... .......... .......... 55% 24.9M 22s
282350K .......... .......... .......... .......... .......... 55% 16.9M 22s
282400K .......... .......... .......... .......... .......... 55% 17.2M 22s
282450K .......... .......... .......... .......... .......... 55% 15.6M 22s
282500K .......... .......... .......... .......... .......... 55% 18.5M 22s
282550K .......... .......... .......... .......... .......... 55% 18.1M 22s
282600K .......... .......... .......... .......... .......... 55% 15.7M 22s
282650K .......... .......... .......... .......... .......... 55% 24.0M 22s
282700K .......... .......... .......... .......... .......... 56% 15.3M 22s
282750K .......... .......... .......... .......... .......... 56% 18.6M 22s
282800K .......... .......... .......... .......... .......... 56% 28.0M 22s
282850K .......... .......... .......... .......... .......... 56% 16.2M 22s
282900K .......... .......... .......... .......... .......... 56% 12.6M 22s
282950K .......... .......... .......... .......... .......... 56% 13.1M 22s
283000K .......... .......... .......... .......... .......... 56% 20.3M 22s
283050K .......... .......... .......... .......... .......... 56% 15.3M 22s
283100K .......... .......... .......... .......... .......... 56% 15.2M 22s
283150K .......... .......... .......... .......... .......... 56% 13.1M 22s
283200K .......... .......... .......... .......... .......... 56% 13.7M 22s
283250K .......... .......... .......... .......... .......... 56% 15.4M 22s
283300K .......... .......... .......... .......... .......... 56% 23.4M 22s
283350K .......... .......... .......... .......... .......... 56% 9.53M 22s
283400K .......... .......... .......... .......... .......... 56% 16.0M 22s
283450K .......... .......... .......... .......... .......... 56% 6.85M 22s
283500K .......... .......... .......... .......... .......... 56% 14.3M 22s
283550K .......... .......... .......... .......... .......... 56% 8.78M 22s
283600K .......... .......... .......... .......... .......... 56% 10.7M 22s
283650K .......... .......... .......... .......... .......... 56% 22.9M 22s
283700K .......... .......... .......... .......... .......... 56% 11.8M 22s
283750K .......... .......... .......... .......... .......... 56% 21.0M 22s
283800K .......... .......... .......... .......... .......... 56% 19.3M 22s
283850K .......... .......... .......... .......... .......... 56% 13.2M 22s
283900K .......... .......... .......... .......... .......... 56% 22.6M 22s
283950K .......... .......... .......... .......... .......... 56% 14.6M 22s
284000K .......... .......... .......... .......... .......... 56% 15.1M 22s
284050K .......... .......... .......... .......... .......... 56% 15.5M 22s
284100K .......... .......... .......... .......... .......... 56% 16.2M 22s
284150K .......... .......... .......... .......... .......... 56% 17.9M 22s
284200K .......... .......... .......... .......... .......... 56% 12.8M 22s
284250K .......... .......... .......... .......... .......... 56% 16.3M 22s
284300K .......... .......... .......... .......... .......... 56% 22.6M 22s
284350K .......... .......... .......... .......... .......... 56% 13.2M 22s
284400K .......... .......... .......... .......... .......... 56% 9.17M 22s
284450K .......... .......... .......... .......... .......... 56% 37.3M 22s
284500K .......... .......... .......... .......... .......... 56% 20.0M 22s
284550K .......... .......... .......... .......... .......... 56% 24.3M 22s
284600K .......... .......... .......... .......... .......... 56% 18.8M 22s
284650K .......... .......... .......... .......... .......... 56% 14.6M 22s
284700K .......... .......... .......... .......... .......... 56% 16.0M 22s
284750K .......... .......... .......... .......... .......... 56% 23.3M 22s
284800K .......... .......... .......... .......... .......... 56% 15.2M 22s
284850K .......... .......... .......... .......... .......... 56% 18.8M 22s
284900K .......... .......... .......... .......... .......... 56% 19.4M 22s
284950K .......... .......... .......... .......... .......... 56% 12.4M 22s
285000K .......... .......... .......... .......... .......... 56% 17.2M 22s
285050K .......... .......... .......... .......... .......... 56% 23.3M 22s
285100K .......... .......... .......... .......... .......... 56% 13.4M 22s
285150K .......... .......... .......... .......... .......... 56% 13.6M 22s
285200K .......... .......... .......... .......... .......... 56% 8.48M 22s
285250K .......... .......... .......... .......... .......... 56% 9.83M 22s
285300K .......... .......... .......... .......... .......... 56% 10.2M 22s
285350K .......... .......... .......... .......... .......... 56% 7.08M 22s
285400K .......... .......... .......... .......... .......... 56% 7.85M 22s
285450K .......... .......... .......... .......... .......... 56% 7.20M 22s
285500K .......... .......... .......... .......... .......... 56% 8.35M 22s
285550K .......... .......... .......... .......... .......... 56% 8.59M 22s
285600K .......... .......... .......... .......... .......... 56% 11.2M 22s
285650K .......... .......... .......... .......... .......... 56% 72.1M 22s
285700K .......... .......... .......... .......... .......... 56% 15.0M 22s
285750K .......... .......... .......... .......... .......... 56% 15.8M 22s
285800K .......... .......... .......... .......... .......... 56% 24.1M 22s
285850K .......... .......... .......... .......... .......... 56% 22.5M 22s
285900K .......... .......... .......... .......... .......... 56% 26.5M 22s
285950K .......... .......... .......... .......... .......... 56% 19.1M 22s
286000K .......... .......... .......... .......... .......... 56% 25.9M 22s
286050K .......... .......... .......... .......... .......... 56% 27.1M 22s
286100K .......... .......... .......... .......... .......... 56% 18.6M 22s
286150K .......... .......... .......... .......... .......... 56% 20.5M 22s
286200K .......... .......... .......... .......... .......... 56% 17.4M 22s
286250K .......... .......... .......... .......... .......... 56% 21.1M 22s
286300K .......... .......... .......... .......... .......... 56% 21.9M 22s
286350K .......... .......... .......... .......... .......... 56% 22.5M 22s
286400K .......... .......... .......... .......... .......... 56% 16.7M 22s
286450K .......... .......... .......... .......... .......... 56% 12.5M 22s
286500K .......... .......... .......... .......... .......... 56% 13.5M 22s
286550K .......... .......... .......... .......... .......... 56% 10.3M 21s
286600K .......... .......... .......... .......... .......... 56% 13.8M 21s
286650K .......... .......... .......... .......... .......... 56% 15.2M 21s
286700K .......... .......... .......... .......... .......... 56% 14.0M 21s
286750K .......... .......... .......... .......... .......... 56% 11.3M 21s
286800K .......... .......... .......... .......... .......... 56% 16.8M 21s
286850K .......... .......... .......... .......... .......... 56% 13.9M 21s
286900K .......... .......... .......... .......... .......... 56% 14.9M 21s
286950K .......... .......... .......... .......... .......... 56% 13.2M 21s
287000K .......... .......... .......... .......... .......... 56% 15.3M 21s
287050K .......... .......... .......... .......... .......... 56% 11.1M 21s
287100K .......... .......... .......... .......... .......... 56% 10.3M 21s
287150K .......... .......... .......... .......... .......... 56% 12.2M 21s
287200K .......... .......... .......... .......... .......... 56% 11.5M 21s
287250K .......... .......... .......... .......... .......... 56% 12.6M 21s
287300K .......... .......... .......... .......... .......... 56% 14.5M 21s
287350K .......... .......... .......... .......... .......... 56% 10.5M 21s
287400K .......... .......... .......... .......... .......... 56% 14.1M 21s
287450K .......... .......... .......... .......... .......... 56% 10.3M 21s
287500K .......... .......... .......... .......... .......... 56% 16.9M 21s
287550K .......... .......... .......... .......... .......... 56% 17.3M 21s
287600K .......... .......... .......... .......... .......... 56% 23.0M 21s
287650K .......... .......... .......... .......... .......... 56% 76.7M 21s
287700K .......... .......... .......... .......... .......... 56% 16.6M 21s
287750K .......... .......... .......... .......... .......... 57% 23.7M 21s
287800K .......... .......... .......... .......... .......... 57% 20.9M 21s
287850K .......... .......... .......... .......... .......... 57% 18.6M 21s
287900K .......... .......... .......... .......... .......... 57% 21.0M 21s
287950K .......... .......... .......... .......... .......... 57% 13.2M 21s
288000K .......... .......... .......... .......... .......... 57% 15.7M 21s
288050K .......... .......... .......... .......... .......... 57% 13.6M 21s
288100K .......... .......... .......... .......... .......... 57% 11.9M 21s
288150K .......... .......... .......... .......... .......... 57% 11.4M 21s
288200K .......... .......... .......... .......... .......... 57% 12.5M 21s
288250K .......... .......... .......... .......... .......... 57% 11.0M 21s
288300K .......... .......... .......... .......... .......... 57% 10.8M 21s
288350K .......... .......... .......... .......... .......... 57% 9.12M 21s
288400K .......... .......... .......... .......... .......... 57% 11.2M 21s
288450K .......... .......... .......... .......... .......... 57% 7.83M 21s
288500K .......... .......... .......... .......... .......... 57% 7.01M 21s
288550K .......... .......... .......... .......... .......... 57% 9.45M 21s
288600K .......... .......... .......... .......... .......... 57% 8.39M 21s
288650K .......... .......... .......... .......... .......... 57% 8.85M 21s
288700K .......... .......... .......... .......... .......... 57% 8.77M 21s
288750K .......... .......... .......... .......... .......... 57% 8.49M 21s
288800K .......... .......... .......... .......... .......... 57% 20.1M 21s
288850K .......... .......... .......... .......... .......... 57% 21.5M 21s
288900K .......... .......... .......... .......... .......... 57% 31.5M 21s
288950K .......... .......... .......... .......... .......... 57% 20.0M 21s
289000K .......... .......... .......... .......... .......... 57% 17.1M 21s
289050K .......... .......... .......... .......... .......... 57% 17.8M 21s
289100K .......... .......... .......... .......... .......... 57% 14.4M 21s
289150K .......... .......... .......... .......... .......... 57% 14.5M 21s
289200K .......... .......... .......... .......... .......... 57% 12.5M 21s
289250K .......... .......... .......... .......... .......... 57% 17.4M 21s
289300K .......... .......... .......... .......... .......... 57% 11.5M 21s
289350K .......... .......... .......... .......... .......... 57% 12.1M 21s
289400K .......... .......... .......... .......... .......... 57% 12.4M 21s
289450K .......... .......... .......... .......... .......... 57% 14.6M 21s
289500K .......... .......... .......... .......... .......... 57% 15.5M 21s
289550K .......... .......... .......... .......... .......... 57% 19.9M 21s
289600K .......... .......... .......... .......... .......... 57% 15.5M 21s
289650K .......... .......... .......... .......... .......... 57% 18.5M 21s
289700K .......... .......... .......... .......... .......... 57% 14.8M 21s
289750K .......... .......... .......... .......... .......... 57% 15.7M 21s
289800K .......... .......... .......... .......... .......... 57% 18.3M 21s
289850K .......... .......... .......... .......... .......... 57% 15.4M 21s
289900K .......... .......... .......... .......... .......... 57% 18.2M 21s
289950K .......... .......... .......... .......... .......... 57% 15.3M 21s
290000K .......... .......... .......... .......... .......... 57% 16.0M 21s
290050K .......... .......... .......... .......... .......... 57% 18.4M 21s
290100K .......... .......... .......... .......... .......... 57% 24.9M 21s
290150K .......... .......... .......... .......... .......... 57% 13.4M 21s
290200K .......... .......... .......... .......... .......... 57% 20.2M 21s
290250K .......... .......... .......... .......... .......... 57%  205M 21s
290300K .......... .......... .......... .......... .......... 57% 33.1M 21s
290350K .......... .......... .......... .......... .......... 57% 16.8M 21s
290400K .......... .......... .......... .......... .......... 57% 22.3M 21s
290450K .......... .......... .......... .......... .......... 57% 16.5M 21s
290500K .......... .......... .......... .......... .......... 57% 15.0M 21s
290550K .......... .......... .......... .......... .......... 57% 19.5M 21s
290600K .......... .......... .......... .......... .......... 57% 11.6M 21s
290650K .......... .......... .......... .......... .......... 57% 23.0M 21s
290700K .......... .......... .......... .......... .......... 57% 13.9M 21s
290750K .......... .......... .......... .......... .......... 57% 14.3M 21s
290800K .......... .......... .......... .......... .......... 57% 19.6M 21s
290850K .......... .......... .......... .......... .......... 57% 12.3M 21s
290900K .......... .......... .......... .......... .......... 57% 18.6M 21s
290950K .......... .......... .......... .......... .......... 57% 14.4M 21s
291000K .......... .......... .......... .......... .......... 57% 29.3M 21s
291050K .......... .......... .......... .......... .......... 57% 50.3M 21s
291100K .......... .......... .......... .......... .......... 57% 33.0M 21s
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291200K .......... .......... .......... .......... .......... 57% 50.1M 21s
291250K .......... .......... .......... .......... .......... 57% 26.3M 21s
291300K .......... .......... .......... .......... .......... 57% 24.1M 21s
291350K .......... .......... .......... .......... .......... 57% 17.6M 21s
291400K .......... .......... .......... .......... .......... 57% 24.1M 21s
291450K .......... .......... .......... .......... .......... 57% 14.5M 21s
291500K .......... .......... .......... .......... .......... 57% 51.1M 21s
291550K .......... .......... .......... .......... .......... 57% 24.0M 21s
291600K .......... .......... .......... .......... .......... 57% 16.1M 21s
291650K .......... .......... .......... .......... .......... 57% 25.8M 21s
291700K .......... .......... .......... .......... .......... 57% 20.0M 21s
291750K .......... .......... .......... .......... .......... 57% 19.4M 21s
291800K .......... .......... .......... .......... .......... 57% 18.4M 21s
291850K .......... .......... .......... .......... .......... 57% 14.2M 21s
291900K .......... .......... .......... .......... .......... 57% 12.9M 21s
291950K .......... .......... .......... .......... .......... 57% 5.99M 21s
292000K .......... .......... .......... .......... .......... 57% 7.28M 21s
292050K .......... .......... .......... .......... .......... 57% 9.44M 21s
292100K .......... .......... .......... .......... .......... 57% 6.15M 21s
292150K .......... .......... .......... .......... .......... 57% 7.27M 21s
292200K .......... .......... .......... .......... .......... 57% 5.92M 21s
292250K .......... .......... .......... .......... .......... 57% 7.54M 21s
292300K .......... .......... .......... .......... .......... 57% 4.11M 21s
292350K .......... .......... .......... .......... .......... 57% 4.06M 21s
292400K .......... .......... .......... .......... .......... 57% 14.5M 21s
292450K .......... .......... .......... .......... .......... 57% 15.8M 21s
292500K .......... .......... .......... .......... .......... 57% 25.5M 21s
292550K .......... .......... .......... .......... .......... 57% 20.1M 21s
292600K .......... .......... .......... .......... .......... 57% 9.01M 21s
292650K .......... .......... .......... .......... .......... 57% 14.9M 21s
292700K .......... .......... .......... .......... .......... 57% 11.7M 21s
292750K .......... .......... .......... .......... .......... 57% 13.5M 21s
292800K .......... .......... .......... .......... .......... 58% 16.1M 21s
292850K .......... .......... .......... .......... .......... 58% 14.4M 21s
292900K .......... .......... .......... .......... .......... 58% 11.4M 21s
292950K .......... .......... .......... .......... .......... 58% 10.6M 21s
293000K .......... .......... .......... .......... .......... 58% 16.8M 21s
293050K .......... .......... .......... .......... .......... 58% 15.7M 21s
293100K .......... .......... .......... .......... .......... 58% 15.6M 21s
293150K .......... .......... .......... .......... .......... 58% 16.1M 21s
293200K .......... .......... .......... .......... .......... 58% 13.1M 21s
293250K .......... .......... .......... .......... .......... 58% 13.4M 21s
293300K .......... .......... .......... .......... .......... 58% 14.3M 21s
293350K .......... .......... .......... .......... .......... 58% 10.7M 21s
293400K .......... .......... .......... .......... .......... 58% 15.9M 21s
293450K .......... .......... .......... .......... .......... 58% 12.8M 21s
293500K .......... .......... .......... .......... .......... 58%  121M 21s
293550K .......... .......... .......... .......... .......... 58% 22.1M 21s
293600K .......... .......... .......... .......... .......... 58% 21.4M 21s
293650K .......... .......... .......... .......... .......... 58% 15.3M 21s
293700K .......... .......... .......... .......... .......... 58% 9.91M 21s
293750K .......... .......... .......... .......... .......... 58% 15.6M 21s
293800K .......... .......... .......... .......... .......... 58% 14.5M 21s
293850K .......... .......... .......... .......... .......... 58% 14.8M 21s
293900K .......... .......... .......... .......... .......... 58% 15.2M 21s
293950K .......... .......... .......... .......... .......... 58% 9.81M 21s
294000K .......... .......... .......... .......... .......... 58% 14.2M 21s
294050K .......... .......... .......... .......... .......... 58% 13.5M 21s
294100K .......... .......... .......... .......... .......... 58% 7.30M 21s
294150K .......... .......... .......... .......... .......... 58% 13.2M 21s
294200K .......... .......... .......... .......... .......... 58% 14.9M 21s
294250K .......... .......... .......... .......... .......... 58% 15.1M 21s
294300K .......... .......... .......... .......... .......... 58% 16.4M 21s
294350K .......... .......... .......... .......... .......... 58% 7.59M 21s
294400K .......... .......... .......... .......... .......... 58% 8.76M 21s
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294500K .......... .......... .......... .......... .......... 58% 6.70M 21s
294550K .......... .......... .......... .......... .......... 58% 9.03M 21s
294600K .......... .......... .......... .......... .......... 58% 9.11M 21s
294650K .......... .......... .......... .......... .......... 58% 9.20M 21s
294700K .......... .......... .......... .......... .......... 58% 8.41M 21s
294750K .......... .......... .......... .......... .......... 58% 8.35M 21s
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294850K .......... .......... .......... .......... .......... 58% 12.0M 21s
294900K .......... .......... .......... .......... .......... 58% 11.1M 21s
294950K .......... .......... .......... .......... .......... 58% 9.20M 21s
295000K .......... .......... .......... .......... .......... 58% 10.6M 21s
295050K .......... .......... .......... .......... .......... 58% 12.2M 21s
295100K .......... .......... .......... .......... .......... 58% 7.25M 21s
295150K .......... .......... .......... .......... .......... 58% 10.5M 21s
295200K .......... .......... .......... .......... .......... 58% 7.64M 21s
295250K .......... .......... .......... .......... .......... 58% 7.80M 20s
295300K .......... .......... .......... .......... .......... 58% 6.88M 20s
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295400K .......... .......... .......... .......... .......... 58% 7.18M 20s
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295500K .......... .......... .......... .......... .......... 58% 6.83M 20s
295550K .......... .......... .......... .......... .......... 58% 20.9M 20s
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295700K .......... .......... .......... .......... .......... 58% 21.6M 20s
295750K .......... .......... .......... .......... .......... 58% 37.8M 20s
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295900K .......... .......... .......... .......... .......... 58% 40.4M 20s
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296000K .......... .......... .......... .......... .......... 58% 23.9M 20s
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296100K .......... .......... .......... .......... .......... 58% 17.4M 20s
296150K .......... .......... .......... .......... .......... 58% 32.8M 20s
296200K .......... .......... .......... .......... .......... 58% 17.9M 20s
296250K .......... .......... .......... .......... .......... 58% 15.6M 20s
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296400K .......... .......... .......... .......... .......... 58% 11.8M 20s
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296900K .......... .......... .......... .......... .......... 58% 8.89M 20s
296950K .......... .......... .......... .......... .......... 58% 6.82M 20s
297000K .......... .......... .......... .......... .......... 58% 8.27M 20s
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297100K .......... .......... .......... .......... .......... 58% 6.04M 20s
297150K .......... .......... .......... .......... .......... 58% 4.30M 20s
297200K .......... .......... .......... .......... .......... 58% 8.23M 20s
297250K .......... .......... .......... .......... .......... 58% 11.4M 20s
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298000K .......... .......... .......... .......... .......... 59% 18.2M 20s
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298100K .......... .......... .......... .......... .......... 59% 30.7M 20s
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298250K .......... .......... .......... .......... .......... 59% 42.6M 20s
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299000K .......... .......... .......... .......... .......... 59% 23.9M 20s
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299100K .......... .......... .......... .......... .......... 59% 26.6M 20s
299150K .......... .......... .......... .......... .......... 59% 17.9M 20s
299200K .......... .......... .......... .......... .......... 59% 14.0M 20s
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299300K .......... .......... .......... .......... .......... 59% 19.9M 20s
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299500K .......... .......... .......... .......... .......... 59% 23.0M 20s
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299750K .......... .......... .......... .......... .......... 59% 20.9M 20s
299800K .......... .......... .......... .......... .......... 59% 41.3M 20s
299850K .......... .......... .......... .......... .......... 59% 19.9M 20s
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300000K .......... .......... .......... .......... .......... 59% 27.4M 20s
300050K .......... .......... .......... .......... .......... 59% 30.7M 20s
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300500K .......... .......... .......... .......... .......... 59% 35.5M 20s
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301000K .......... .......... .......... .......... .......... 59% 34.9M 20s
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301100K .......... .......... .......... .......... .......... 59% 19.9M 20s
301150K .......... .......... .......... .......... .......... 59% 29.6M 20s
301200K .......... .......... .......... .......... .......... 59% 21.8M 20s
301250K .......... .......... .......... .......... .......... 59% 38.7M 20s
301300K .......... .......... .......... .......... .......... 59% 32.1M 20s
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301400K .......... .......... .......... .......... .......... 59% 27.9M 20s
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301500K .......... .......... .......... .......... .......... 59% 33.8M 20s
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301600K .......... .......... .......... .......... .......... 59% 24.2M 20s
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301750K .......... .......... .......... .......... .......... 59%  198M 20s
301800K .......... .......... .......... .......... .......... 59% 19.5M 20s
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302000K .......... .......... .......... .......... .......... 59% 16.1M 20s
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302150K .......... .......... .......... .......... .......... 59% 14.5M 20s
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302250K .......... .......... .......... .......... .......... 59% 17.5M 20s
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302450K .......... .......... .......... .......... .......... 59% 27.8M 20s
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302800K .......... .......... .......... .......... .......... 59% 22.6M 20s
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303000K .......... .......... .......... .......... .......... 60% 28.2M 20s
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303100K .......... .......... .......... .......... .......... 60% 22.0M 20s
303150K .......... .......... .......... .......... .......... 60% 28.7M 20s
303200K .......... .......... .......... .......... .......... 60% 22.1M 20s
303250K .......... .......... .......... .......... .......... 60% 30.4M 19s
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303350K .......... .......... .......... .......... .......... 60% 26.4M 19s
303400K .......... .......... .......... .......... .......... 60% 24.0M 19s
303450K .......... .......... .......... .......... .......... 60% 24.3M 19s
303500K .......... .......... .......... .......... .......... 60% 35.7M 19s
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303600K .......... .......... .......... .......... .......... 60% 45.3M 19s
303650K .......... .......... .......... .......... .......... 60% 65.7M 19s
303700K .......... .......... .......... .......... .......... 60% 40.4M 19s
303750K .......... .......... .......... .......... .......... 60%  105M 19s
303800K .......... .......... .......... .......... .......... 60% 54.3M 19s
303850K .......... .......... .......... .......... .......... 60% 90.6M 19s
303900K .......... .......... .......... .......... .......... 60% 64.6M 19s
303950K .......... .......... .......... .......... .......... 60% 41.8M 19s
304000K .......... .......... .......... .......... .......... 60% 19.4M 19s
304050K .......... .......... .......... .......... .......... 60% 49.3M 19s
304100K .......... .......... .......... .......... .......... 60%  111M 19s
304150K .......... .......... .......... .......... .......... 60% 59.4M 19s
304200K .......... .......... .......... .......... .......... 60% 44.0M 19s
304250K .......... .......... .......... .......... .......... 60% 27.0M 19s
304300K .......... .......... .......... .......... .......... 60%  167M 19s
304350K .......... .......... .......... .......... .......... 60%  117M 19s
304400K .......... .......... .......... .......... .......... 60% 47.9M 19s
304450K .......... .......... .......... .......... .......... 60% 30.4M 19s
304500K .......... .......... .......... .......... .......... 60% 35.1M 19s
304550K .......... .......... .......... .......... .......... 60% 43.3M 19s
304600K .......... .......... .......... .......... .......... 60% 30.7M 19s
304650K .......... .......... .......... .......... .......... 60% 38.8M 19s
304700K .......... .......... .......... .......... .......... 60% 36.2M 19s
304750K .......... .......... .......... .......... .......... 60% 41.1M 19s
304800K .......... .......... .......... .......... .......... 60% 29.9M 19s
304850K .......... .......... .......... .......... .......... 60% 40.8M 19s
304900K .......... .......... .......... .......... .......... 60% 38.9M 19s
304950K .......... .......... .......... .......... .......... 60% 28.2M 19s
305000K .......... .......... .......... .......... .......... 60% 40.0M 19s
305050K .......... .......... .......... .......... .......... 60% 41.4M 19s
305100K .......... .......... .......... .......... .......... 60% 27.2M 19s
305150K .......... .......... .......... .......... .......... 60% 41.3M 19s
305200K .......... .......... .......... .......... .......... 60% 42.9M 19s
305250K .......... .......... .......... .......... .......... 60% 30.0M 19s
305300K .......... .......... .......... .......... .......... 60% 36.1M 19s
305350K .......... .......... .......... .......... .......... 60% 40.3M 19s
305400K .......... .......... .......... .......... .......... 60% 40.4M 19s
305450K .......... .......... .......... .......... .......... 60% 26.3M 19s
305500K .......... .......... .......... .......... .......... 60% 54.0M 19s
305550K .......... .......... .......... .......... .......... 60% 29.9M 19s
305600K .......... .......... .......... .......... .......... 60% 75.5M 19s
305650K .......... .......... .......... .......... .......... 60% 29.0M 19s
305700K .......... .......... .......... .......... .......... 60% 36.1M 19s
305750K .......... .......... .......... .......... .......... 60% 73.5M 19s
305800K .......... .......... .......... .......... .......... 60% 14.2M 19s
305850K .......... .......... .......... .......... .......... 60%  166M 19s
305900K .......... .......... .......... .......... .......... 60%  245M 19s
305950K .......... .......... .......... .......... .......... 60% 27.8M 19s
306000K .......... .......... .......... .......... .......... 60% 52.0M 19s
306050K .......... .......... .......... .......... .......... 60% 51.7M 19s
306100K .......... .......... .......... .......... .......... 60%  130M 19s
306150K .......... .......... .......... .......... .......... 60% 30.4M 19s
306200K .......... .......... .......... .......... .......... 60% 40.4M 19s
306250K .......... .......... .......... .......... .......... 60% 25.6M 19s
306300K .......... .......... .......... .......... .......... 60% 36.9M 19s
306350K .......... .......... .......... .......... .......... 60% 27.9M 19s
306400K .......... .......... .......... .......... .......... 60% 27.7M 19s
306450K .......... .......... .......... .......... .......... 60% 29.8M 19s
306500K .......... .......... .......... .......... .......... 60% 35.5M 19s
306550K .......... .......... .......... .......... .......... 60% 33.1M 19s
306600K .......... .......... .......... .......... .......... 60% 28.4M 19s
306650K .......... .......... .......... .......... .......... 60% 35.6M 19s
306700K .......... .......... .......... .......... .......... 60% 27.2M 19s
306750K .......... .......... .......... .......... .......... 60% 35.6M 19s
306800K .......... .......... .......... .......... .......... 60% 28.5M 19s
306850K .......... .......... .......... .......... .......... 60% 30.4M 19s
306900K .......... .......... .......... .......... .......... 60% 29.0M 19s
306950K .......... .......... .......... .......... .......... 60% 26.9M 19s
307000K .......... .......... .......... .......... .......... 60% 38.3M 19s
307050K .......... .......... .......... .......... .......... 60% 42.2M 19s
307100K .......... .......... .......... .......... .......... 60% 26.3M 19s
307150K .......... .......... .......... .......... .......... 60% 22.6M 19s
307200K .......... .......... .......... .......... .......... 60% 24.8M 19s
307250K .......... .......... .......... .......... .......... 60% 42.1M 19s
307300K .......... .......... .......... .......... .......... 60% 22.3M 19s
307350K .......... .......... .......... .......... .......... 60% 22.1M 19s
307400K .......... .......... .......... .......... .......... 60% 65.9M 19s
307450K .......... .......... .......... .......... .......... 60% 19.8M 19s
307500K .......... .......... .......... .......... .......... 60% 19.8M 19s
307550K .......... .......... .......... .......... .......... 60% 23.6M 19s
307600K .......... .......... .......... .......... .......... 60%  119M 19s
307650K .......... .......... .......... .......... .......... 60% 26.0M 19s
307700K .......... .......... .......... .......... .......... 60% 25.5M 19s
307750K .......... .......... .......... .......... .......... 60% 25.3M 19s
307800K .......... .......... .......... .......... .......... 60% 27.9M 19s
307850K .......... .......... .......... .......... .......... 60% 19.5M 19s
307900K .......... .......... .......... .......... .......... 60% 30.0M 19s
307950K .......... .......... .......... .......... .......... 61% 23.0M 19s
308000K .......... .......... .......... .......... .......... 61% 26.8M 19s
308050K .......... .......... .......... .......... .......... 61% 29.4M 19s
308100K .......... .......... .......... .......... .......... 61% 18.5M 19s
308150K .......... .......... .......... .......... .......... 61% 41.8M 19s
308200K .......... .......... .......... .......... .......... 61% 16.8M 19s
308250K .......... .......... .......... .......... .......... 61% 26.4M 19s
308300K .......... .......... .......... .......... .......... 61% 26.6M 19s
308350K .......... .......... .......... .......... .......... 61% 21.2M 19s
308400K .......... .......... .......... .......... .......... 61% 26.4M 19s
308450K .......... .......... .......... .......... .......... 61% 20.9M 19s
308500K .......... .......... .......... .......... .......... 61% 33.1M 19s
308550K .......... .......... .......... .......... .......... 61% 38.6M 19s
308600K .......... .......... .......... .......... .......... 61% 11.4M 19s
308650K .......... .......... .......... .......... .......... 61% 40.5M 19s
308700K .......... .......... .......... .......... .......... 61% 26.4M 19s
308750K .......... .......... .......... .......... .......... 61%  136M 19s
308800K .......... .......... .......... .......... .......... 61% 25.9M 19s
308850K .......... .......... .......... .......... .......... 61% 23.1M 19s
308900K .......... .......... .......... .......... .......... 61% 19.2M 19s
308950K .......... .......... .......... .......... .......... 61% 17.3M 19s
309000K .......... .......... .......... .......... .......... 61% 24.5M 19s
309050K .......... .......... .......... .......... .......... 61% 21.4M 19s
309100K .......... .......... .......... .......... .......... 61% 15.9M 19s
309150K .......... .......... .......... .......... .......... 61% 20.1M 19s
309200K .......... .......... .......... .......... .......... 61% 18.7M 19s
309250K .......... .......... .......... .......... .......... 61% 21.4M 19s
309300K .......... .......... .......... .......... .......... 61% 19.3M 19s
309350K .......... .......... .......... .......... .......... 61% 20.5M 19s
309400K .......... .......... .......... .......... .......... 61% 16.6M 19s
309450K .......... .......... .......... .......... .......... 61% 19.4M 19s
309500K .......... .......... .......... .......... .......... 61% 19.9M 19s
309550K .......... .......... .......... .......... .......... 61% 29.0M 19s
309600K .......... .......... .......... .......... .......... 61% 19.8M 19s
309650K .......... .......... .......... .......... .......... 61% 33.2M 19s
309700K .......... .......... .......... .......... .......... 61% 26.1M 19s
309750K .......... .......... .......... .......... .......... 61% 25.5M 19s
309800K .......... .......... .......... .......... .......... 61% 28.7M 19s
309850K .......... .......... .......... .......... .......... 61% 5.64M 19s
309900K .......... .......... .......... .......... .......... 61%  179M 19s
309950K .......... .......... .......... .......... .......... 61%  121M 19s
310000K .......... .......... .......... .......... .......... 61%  194M 19s
310050K .......... .......... .......... .......... .......... 61% 48.7M 19s
310100K .......... .......... .......... .......... .......... 61% 25.4M 19s
310150K .......... .......... .......... .......... .......... 61% 15.4M 19s
310200K .......... .......... .......... .......... .......... 61% 14.1M 19s
310250K .......... .......... .......... .......... .......... 61% 19.7M 19s
310300K .......... .......... .......... .......... .......... 61% 17.3M 19s
310350K .......... .......... .......... .......... .......... 61% 18.6M 19s
310400K .......... .......... .......... .......... .......... 61% 14.5M 19s
310450K .......... .......... .......... .......... .......... 61% 20.8M 19s
310500K .......... .......... .......... .......... .......... 61% 14.4M 19s
310550K .......... .......... .......... .......... .......... 61% 22.5M 19s
310600K .......... .......... .......... .......... .......... 61% 15.9M 18s
310650K .......... .......... .......... .......... .......... 61% 16.0M 18s
310700K .......... .......... .......... .......... .......... 61% 13.9M 18s
310750K .......... .......... .......... .......... .......... 61% 14.3M 18s
310800K .......... .......... .......... .......... .......... 61%  173M 18s
310850K .......... .......... .......... .......... .......... 61% 25.9M 18s
310900K .......... .......... .......... .......... .......... 61% 21.2M 18s
310950K .......... .......... .......... .......... .......... 61% 34.0M 18s
311000K .......... .......... .......... .......... .......... 61% 22.4M 18s
311050K .......... .......... .......... .......... .......... 61% 26.1M 18s
311100K .......... .......... .......... .......... .......... 61% 19.3M 18s
311150K .......... .......... .......... .......... .......... 61% 21.3M 18s
311200K .......... .......... .......... .......... .......... 61% 23.3M 18s
311250K .......... .......... .......... .......... .......... 61% 20.1M 18s
311300K .......... .......... .......... .......... .......... 61% 23.5M 18s
311350K .......... .......... .......... .......... .......... 61% 25.1M 18s
311400K .......... .......... .......... .......... .......... 61% 20.5M 18s
311450K .......... .......... .......... .......... .......... 61% 19.1M 18s
311500K .......... .......... .......... .......... .......... 61% 20.6M 18s
311550K .......... .......... .......... .......... .......... 61% 24.5M 18s
311600K .......... .......... .......... .......... .......... 61% 18.7M 18s
311650K .......... .......... .......... .......... .......... 61% 21.6M 18s
311700K .......... .......... .......... .......... .......... 61% 21.0M 18s
311750K .......... .......... .......... .......... .......... 61% 15.2M 18s
311800K .......... .......... .......... .......... .......... 61% 41.2M 18s
311850K .......... .......... .......... .......... .......... 61% 22.1M 18s
311900K .......... .......... .......... .......... .......... 61% 16.6M 18s
311950K .......... .......... .......... .......... .......... 61%  144M 18s
312000K .......... .......... .......... .......... .......... 61% 19.5M 18s
312050K .......... .......... .......... .......... .......... 61% 31.1M 18s
312100K .......... .......... .......... .......... .......... 61% 34.4M 18s
312150K .......... .......... .......... .......... .......... 61% 23.3M 18s
312200K .......... .......... .......... .......... .......... 61% 20.0M 18s
312250K .......... .......... .......... .......... .......... 61% 21.6M 18s
312300K .......... .......... .......... .......... .......... 61% 40.0M 18s
312350K .......... .......... .......... .......... .......... 61% 21.3M 18s
312400K .......... .......... .......... .......... .......... 61% 21.6M 18s
312450K .......... .......... .......... .......... .......... 61% 23.4M 18s
312500K .......... .......... .......... .......... .......... 61% 38.0M 18s
312550K .......... .......... .......... .......... .......... 61% 28.1M 18s
312600K .......... .......... .......... .......... .......... 61% 21.9M 18s
312650K .......... .......... .......... .......... .......... 61% 25.1M 18s
312700K .......... .......... .......... .......... .......... 61% 19.5M 18s
312750K .......... .......... .......... .......... .......... 61% 21.2M 18s
312800K .......... .......... .......... .......... .......... 61% 34.3M 18s
312850K .......... .......... .......... .......... .......... 61% 16.8M 18s
312900K .......... .......... .......... .......... .......... 61% 23.3M 18s
312950K .......... .......... .......... .......... .......... 61% 22.6M 18s
313000K .......... .......... .......... .......... .......... 62% 32.4M 18s
313050K .......... .......... .......... .......... .......... 62% 63.9M 18s
313100K .......... .......... .......... .......... .......... 62% 31.3M 18s
313150K .......... .......... .......... .......... .......... 62% 14.7M 18s
313200K .......... .......... .......... .......... .......... 62%  178M 18s
313250K .......... .......... .......... .......... .......... 62%  264M 18s
313300K .......... .......... .......... .......... .......... 62% 61.7M 18s
313350K .......... .......... .......... .......... .......... 62% 18.5M 18s
313400K .......... .......... .......... .......... .......... 62% 67.7M 18s
313450K .......... .......... .......... .......... .......... 62% 39.1M 18s
313500K .......... .......... .......... .......... .......... 62% 73.5M 18s
313550K .......... .......... .......... .......... .......... 62% 40.1M 18s
313600K .......... .......... .......... .......... .......... 62% 29.7M 18s
313650K .......... .......... .......... .......... .......... 62% 39.2M 18s
313700K .......... .......... .......... .......... .......... 62% 27.7M 18s
313750K .......... .......... .......... .......... .......... 62% 41.2M 18s
313800K .......... .......... .......... .......... .......... 62% 43.7M 18s
313850K .......... .......... .......... .......... .......... 62% 26.4M 18s
313900K .......... .......... .......... .......... .......... 62% 35.0M 18s
313950K .......... .......... .......... .......... .......... 62% 22.9M 18s
314000K .......... .......... .......... .......... .......... 62% 47.3M 18s
314050K .......... .......... .......... .......... .......... 62% 41.7M 18s
314100K .......... .......... .......... .......... .......... 62% 27.5M 18s
314150K .......... .......... .......... .......... .......... 62% 40.7M 18s
314200K .......... .......... .......... .......... .......... 62% 23.2M 18s
314250K .......... .......... .......... .......... .......... 62% 40.8M 18s
314300K .......... .......... .......... .......... .......... 62% 39.6M 18s
314350K .......... .......... .......... .......... .......... 62% 28.9M 18s
314400K .......... .......... .......... .......... .......... 62% 36.0M 18s
314450K .......... .......... .......... .......... .......... 62% 23.9M 18s
314500K .......... .......... .......... .......... .......... 62% 40.3M 18s
314550K .......... .......... .......... .......... .......... 62% 39.4M 18s
314600K .......... .......... .......... .......... .......... 62% 34.6M 18s
314650K .......... .......... .......... .......... .......... 62% 32.6M 18s
314700K .......... .......... .......... .......... .......... 62% 34.8M 18s
314750K .......... .......... .......... .......... .......... 62% 36.8M 18s
314800K .......... .......... .......... .......... .......... 62% 63.1M 18s
314850K .......... .......... .......... .......... .......... 62% 20.0M 18s
314900K .......... .......... .......... .......... .......... 62% 31.2M 18s
314950K .......... .......... .......... .......... .......... 62% 81.8M 18s
315000K .......... .......... .......... .......... .......... 62% 23.5M 18s
315050K .......... .......... .......... .......... .......... 62%  116M 18s
315100K .......... .......... .......... .......... .......... 62% 46.2M 18s
315150K .......... .......... .......... .......... .......... 62% 33.9M 18s
315200K .......... .......... .......... .......... .......... 62% 32.8M 18s
315250K .......... .......... .......... .......... .......... 62% 21.0M 18s
315300K .......... .......... .......... .......... .......... 62% 40.4M 18s
315350K .......... .......... .......... .......... .......... 62% 22.9M 18s
315400K .......... .......... .......... .......... .......... 62% 23.7M 18s
315450K .......... .......... .......... .......... .......... 62% 24.4M 18s
315500K .......... .......... .......... .......... .......... 62% 21.3M 18s
315550K .......... .......... .......... .......... .......... 62% 35.8M 18s
315600K .......... .......... .......... .......... .......... 62% 21.2M 18s
315650K .......... .......... .......... .......... .......... 62% 25.3M 18s
315700K .......... .......... .......... .......... .......... 62% 20.5M 18s
315750K .......... .......... .......... .......... .......... 62% 29.7M 18s
315800K .......... .......... .......... .......... .......... 62% 25.1M 18s
315850K .......... .......... .......... .......... .......... 62% 21.1M 18s
315900K .......... .......... .......... .......... .......... 62% 33.3M 18s
315950K .......... .......... .......... .......... .......... 62% 26.4M 18s
316000K .......... .......... .......... .......... .......... 62% 21.5M 18s
316050K .......... .......... .......... .......... .......... 62% 29.4M 18s
316100K .......... .......... .......... .......... .......... 62% 26.4M 18s
316150K .......... .......... .......... .......... .......... 62% 30.0M 18s
316200K .......... .......... .......... .......... .......... 62% 16.3M 18s
316250K .......... .......... .......... .......... .......... 62%  171M 18s
316300K .......... .......... .......... .......... .......... 62% 20.3M 18s
316350K .......... .......... .......... .......... .......... 62% 27.6M 18s
316400K .......... .......... .......... .......... .......... 62% 39.4M 18s
316450K .......... .......... .......... .......... .......... 62% 19.9M 18s
316500K .......... .......... .......... .......... .......... 62% 17.6M 18s
316550K .......... .......... .......... .......... .......... 62% 18.2M 18s
316600K .......... .......... .......... .......... .......... 62% 16.0M 18s
316650K .......... .......... .......... .......... .......... 62% 13.1M 18s
316700K .......... .......... .......... .......... .......... 62% 13.6M 18s
316750K .......... .......... .......... .......... .......... 62% 16.1M 18s
316800K .......... .......... .......... .......... .......... 62% 18.4M 18s
316850K .......... .......... .......... .......... .......... 62% 16.4M 18s
316900K .......... .......... .......... .......... .......... 62% 16.4M 18s
316950K .......... .......... .......... .......... .......... 62% 15.5M 18s
317000K .......... .......... .......... .......... .......... 62% 15.7M 18s
317050K .......... .......... .......... .......... .......... 62% 15.7M 18s
317100K .......... .......... .......... .......... .......... 62% 9.57M 18s
317150K .......... .......... .......... .......... .......... 62% 40.4M 18s
317200K .......... .......... .......... .......... .......... 62% 16.5M 18s
317250K .......... .......... .......... .......... .......... 62% 21.3M 18s
317300K .......... .......... .......... .......... .......... 62% 34.3M 18s
317350K .......... .......... .......... .......... .......... 62% 12.3M 18s
317400K .......... .......... .......... .......... .......... 62% 14.4M 18s
317450K .......... .......... .......... .......... .......... 62% 15.6M 18s
317500K .......... .......... .......... .......... .......... 62% 17.3M 18s
317550K .......... .......... .......... .......... .......... 62% 14.5M 18s
317600K .......... .......... .......... .......... .......... 62% 14.1M 18s
317650K .......... .......... .......... .......... .......... 62% 16.5M 18s
317700K .......... .......... .......... .......... .......... 62% 17.5M 18s
317750K .......... .......... .......... .......... .......... 62% 17.5M 18s
317800K .......... .......... .......... .......... .......... 62% 19.6M 18s
317850K .......... .......... .......... .......... .......... 62% 10.7M 18s
317900K .......... .......... .......... .......... .......... 62% 11.8M 18s
317950K .......... .......... .......... .......... .......... 62% 11.8M 18s
318000K .......... .......... .......... .......... .......... 62% 17.8M 18s
318050K .......... .......... .......... .......... .......... 63% 21.5M 18s
318100K .......... .......... .......... .......... .......... 63% 13.3M 18s
318150K .......... .......... .......... .......... .......... 63% 15.5M 18s
318200K .......... .......... .......... .......... .......... 63% 15.4M 18s
318250K .......... .......... .......... .......... .......... 63% 14.9M 18s
318300K .......... .......... .......... .......... .......... 63% 15.4M 18s
318350K .......... .......... .......... .......... .......... 63% 12.8M 18s
318400K .......... .......... .......... .......... .......... 63% 12.9M 18s
318450K .......... .......... .......... .......... .......... 63% 14.7M 18s
318500K .......... .......... .......... .......... .......... 63% 13.2M 18s
318550K .......... .......... .......... .......... .......... 63% 15.0M 17s
318600K .......... .......... .......... .......... .......... 63% 10.0M 17s
318650K .......... .......... .......... .......... .......... 63% 36.0M 17s
318700K .......... .......... .......... .......... .......... 63% 15.9M 17s
318750K .......... .......... .......... .......... .......... 63% 17.4M 17s
318800K .......... .......... .......... .......... .......... 63% 24.5M 17s
318850K .......... .......... .......... .......... .......... 63% 25.0M 17s
318900K .......... .......... .......... .......... .......... 63% 18.3M 17s
318950K .......... .......... .......... .......... .......... 63% 12.8M 17s
319000K .......... .......... .......... .......... .......... 63% 23.9M 17s
319050K .......... .......... .......... .......... .......... 63% 13.9M 17s
319100K .......... .......... .......... .......... .......... 63% 15.9M 17s
319150K .......... .......... .......... .......... .......... 63% 14.1M 17s
319200K .......... .......... .......... .......... .......... 63% 15.5M 17s
319250K .......... .......... .......... .......... .......... 63% 15.1M 17s
319300K .......... .......... .......... .......... .......... 63% 23.5M 17s
319350K .......... .......... .......... .......... .......... 63% 10.8M 17s
319400K .......... .......... .......... .......... .......... 63% 22.9M 17s
319450K .......... .......... .......... .......... .......... 63% 30.4M 17s
319500K .......... .......... .......... .......... .......... 63% 44.6M 17s
319550K .......... .......... .......... .......... .......... 63% 24.5M 17s
319600K .......... .......... .......... .......... .......... 63% 36.8M 17s
319650K .......... .......... .......... .......... .......... 63% 36.2M 17s
319700K .......... .......... .......... .......... .......... 63% 57.6M 17s
319750K .......... .......... .......... .......... .......... 63% 31.1M 17s
319800K .......... .......... .......... .......... .......... 63% 32.6M 17s
319850K .......... .......... .......... .......... .......... 63% 27.7M 17s
319900K .......... .......... .......... .......... .......... 63% 29.2M 17s
319950K .......... .......... .......... .......... .......... 63% 27.6M 17s
320000K .......... .......... .......... .......... .......... 63% 34.1M 17s
320050K .......... .......... .......... .......... .......... 63% 29.5M 17s
320100K .......... .......... .......... .......... .......... 63% 30.0M 17s
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320200K .......... .......... .......... .......... .......... 63% 30.4M 17s
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320300K .......... .......... .......... .......... .......... 63% 38.4M 17s
320350K .......... .......... .......... .......... .......... 63% 41.3M 17s
320400K .......... .......... .......... .......... .......... 63% 20.5M 17s
320450K .......... .......... .......... .......... .......... 63% 34.7M 17s
320500K .......... .......... .......... .......... .......... 63% 36.3M 17s
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320600K .......... .......... .......... .......... .......... 63% 29.8M 17s
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320700K .......... .......... .......... .......... .......... 63% 30.6M 17s
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320800K .......... .......... .......... .......... .......... 63% 30.8M 17s
320850K .......... .......... .......... .......... .......... 63% 14.7M 17s
320900K .......... .......... .......... .......... .......... 63% 31.8M 17s
320950K .......... .......... .......... .......... .......... 63% 26.5M 17s
321000K .......... .......... .......... .......... .......... 63% 21.2M 17s
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321100K .......... .......... .......... .......... .......... 63% 24.1M 17s
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321200K .......... .......... .......... .......... .......... 63% 22.2M 17s
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321500K .......... .......... .......... .......... .......... 63% 23.2M 17s
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321600K .......... .......... .......... .......... .......... 63% 20.8M 17s
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321800K .......... .......... .......... .......... .......... 63% 32.2M 17s
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321900K .......... .......... .......... .......... .......... 63% 80.6M 17s
321950K .......... .......... .......... .......... .......... 63% 39.4M 17s
322000K .......... .......... .......... .......... .......... 63% 97.5M 17s
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322100K .......... .......... .......... .......... .......... 63%  161M 17s
322150K .......... .......... .......... .......... .......... 63% 68.4M 17s
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322250K .......... .......... .......... .......... .......... 63%  126M 17s
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322350K .......... .......... .......... .......... .......... 63% 75.9M 17s
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322450K .......... .......... .......... .......... .......... 63% 27.4M 17s
322500K .......... .......... .......... .......... .......... 63% 24.6M 17s
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322600K .......... .......... .......... .......... .......... 63% 22.9M 17s
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322700K .......... .......... .......... .......... .......... 63% 22.3M 17s
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322800K .......... .......... .......... .......... .......... 63% 29.6M 17s
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322900K .......... .......... .......... .......... .......... 63% 29.9M 17s
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323000K .......... .......... .......... .......... .......... 63% 35.1M 17s
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323100K .......... .......... .......... .......... .......... 64% 25.5M 17s
323150K .......... .......... .......... .......... .......... 64% 31.5M 17s
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323250K .......... .......... .......... .......... .......... 64% 34.8M 17s
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324000K .......... .......... .......... .......... .......... 64%  103M 17s
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324100K .......... .......... .......... .......... .......... 64% 23.8M 17s
324150K .......... .......... .......... .......... .......... 64% 36.8M 17s
324200K .......... .......... .......... .......... .......... 64% 21.4M 17s
324250K .......... .......... .......... .......... .......... 64% 35.6M 17s
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325400K .......... .......... .......... .......... .......... 64% 71.7M 17s
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325700K .......... .......... .......... .......... .......... 64% 38.9M 17s
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332000K .......... .......... .......... .......... .......... 65% 92.3M 16s
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332200K .......... .......... .......... .......... .......... 65% 14.9M 16s
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332300K .......... .......... .......... .......... .......... 65% 22.3M 16s
332350K .......... .......... .......... .......... .......... 65% 19.6M 16s
332400K .......... .......... .......... .......... .......... 65% 13.8M 16s
332450K .......... .......... .......... .......... .......... 65% 19.0M 16s
332500K .......... .......... .......... .......... .......... 65% 19.7M 16s
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332600K .......... .......... .......... .......... .......... 65% 16.8M 16s
332650K .......... .......... .......... .......... .......... 65% 21.4M 16s
332700K .......... .......... .......... .......... .......... 65% 17.6M 16s
332750K .......... .......... .......... .......... .......... 65% 18.6M 16s
332800K .......... .......... .......... .......... .......... 65% 22.0M 16s
332850K .......... .......... .......... .......... .......... 65% 25.2M 16s
332900K .......... .......... .......... .......... .......... 65% 29.3M 16s
332950K .......... .......... .......... .......... .......... 65% 26.7M 16s
333000K .......... .......... .......... .......... .......... 65% 17.5M 16s
333050K .......... .......... .......... .......... .......... 65%  154M 16s
333100K .......... .......... .......... .......... .......... 65% 18.8M 16s
333150K .......... .......... .......... .......... .......... 65% 52.1M 16s
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333250K .......... .......... .......... .......... .......... 66% 25.9M 16s
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333350K .......... .......... .......... .......... .......... 66% 26.4M 16s
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333900K .......... .......... .......... .......... .......... 66% 15.2M 16s
333950K .......... .......... .......... .......... .......... 66% 9.30M 16s
334000K .......... .......... .......... .......... .......... 66% 15.1M 16s
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334250K .......... .......... .......... .......... .......... 66% 15.6M 16s
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345900K .......... .......... .......... .......... .......... 68%  230M 14s
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346750K .......... .......... .......... .......... .......... 68% 26.7M 14s
346800K .......... .......... .......... .......... .......... 68% 22.7M 14s
346850K .......... .......... .......... .......... .......... 68% 27.1M 14s
346900K .......... .......... .......... .......... .......... 68% 19.1M 14s
346950K .......... .......... .......... .......... .......... 68% 36.7M 14s
347000K .......... .......... .......... .......... .......... 68%  226M 14s
347050K .......... .......... .......... .......... .......... 68% 21.4M 14s
347100K .......... .......... .......... .......... .......... 68% 46.1M 14s
347150K .......... .......... .......... .......... .......... 68% 24.0M 14s
347200K .......... .......... .......... .......... .......... 68% 15.1M 14s
347250K .......... .......... .......... .......... .......... 68% 38.4M 14s
347300K .......... .......... .......... .......... .......... 68% 20.4M 14s
347350K .......... .......... .......... .......... .......... 68% 14.3M 14s
347400K .......... .......... .......... .......... .......... 68% 21.0M 14s
347450K .......... .......... .......... .......... .......... 68% 17.4M 14s
347500K .......... .......... .......... .......... .......... 68% 21.8M 14s
347550K .......... .......... .......... .......... .......... 68% 25.0M 14s
347600K .......... .......... .......... .......... .......... 68% 24.8M 14s
347650K .......... .......... .......... .......... .......... 68% 17.7M 14s
347700K .......... .......... .......... .......... .......... 68% 19.8M 14s
347750K .......... .......... .......... .......... .......... 68% 20.1M 14s
347800K .......... .......... .......... .......... .......... 68% 22.2M 14s
347850K .......... .......... .......... .......... .......... 68% 23.6M 14s
347900K .......... .......... .......... .......... .......... 68% 21.6M 14s
347950K .......... .......... .......... .......... .......... 68% 21.8M 14s
348000K .......... .......... .......... .......... .......... 68% 13.0M 14s
348050K .......... .......... .......... .......... .......... 68% 32.0M 14s
348100K .......... .......... .......... .......... .......... 68% 56.2M 14s
348150K .......... .......... .......... .......... .......... 68% 18.2M 14s
348200K .......... .......... .......... .......... .......... 68% 43.1M 14s
348250K .......... .......... .......... .......... .......... 68% 22.1M 14s
348300K .......... .......... .......... .......... .......... 68% 24.9M 14s
348350K .......... .......... .......... .......... .......... 69% 22.9M 14s
348400K .......... .......... .......... .......... .......... 69% 26.6M 14s
348450K .......... .......... .......... .......... .......... 69% 27.7M 14s
348500K .......... .......... .......... .......... .......... 69% 25.5M 14s
348550K .......... .......... .......... .......... .......... 69% 25.5M 14s
348600K .......... .......... .......... .......... .......... 69% 22.8M 14s
348650K .......... .......... .......... .......... .......... 69% 24.0M 14s
348700K .......... .......... .......... .......... .......... 69% 23.5M 14s
348750K .......... .......... .......... .......... .......... 69% 37.2M 14s
348800K .......... .......... .......... .......... .......... 69% 22.3M 14s
348850K .......... .......... .......... .......... .......... 69% 19.2M 14s
348900K .......... .......... .......... .......... .......... 69% 22.3M 14s
348950K .......... .......... .......... .......... .......... 69% 19.9M 14s
349000K .......... .......... .......... .......... .......... 69% 29.2M 14s
349050K .......... .......... .......... .......... .......... 69% 26.0M 14s
349100K .......... .......... .......... .......... .......... 69% 24.5M 14s
349150K .......... .......... .......... .......... .......... 69% 26.3M 14s
349200K .......... .......... .......... .......... .......... 69% 57.0M 14s
349250K .......... .......... .......... .......... .......... 69% 28.7M 14s
349300K .......... .......... .......... .......... .......... 69% 14.1M 14s
349350K .......... .......... .......... .......... .......... 69%  145M 14s
349400K .......... .......... .......... .......... .......... 69% 27.7M 14s
349450K .......... .......... .......... .......... .......... 69% 91.8M 14s
349500K .......... .......... .......... .......... .......... 69% 84.3M 14s
349550K .......... .......... .......... .......... .......... 69% 29.3M 14s
349600K .......... .......... .......... .......... .......... 69% 38.0M 14s
349650K .......... .......... .......... .......... .......... 69% 31.2M 14s
349700K .......... .......... .......... .......... .......... 69% 26.1M 14s
349750K .......... .......... .......... .......... .......... 69% 29.1M 14s
349800K .......... .......... .......... .......... .......... 69% 19.3M 14s
349850K .......... .......... .......... .......... .......... 69% 27.0M 14s
349900K .......... .......... .......... .......... .......... 69% 36.1M 14s
349950K .......... .......... .......... .......... .......... 69% 24.2M 14s
350000K .......... .......... .......... .......... .......... 69% 44.7M 14s
350050K .......... .......... .......... .......... .......... 69% 22.8M 14s
350100K .......... .......... .......... .......... .......... 69% 19.4M 14s
350150K .......... .......... .......... .......... .......... 69% 39.2M 14s
350200K .......... .......... .......... .......... .......... 69% 20.1M 14s
350250K .......... .......... .......... .......... .......... 69% 36.5M 14s
350300K .......... .......... .......... .......... .......... 69% 17.6M 14s
350350K .......... .......... .......... .......... .......... 69% 28.0M 14s
350400K .......... .......... .......... .......... .......... 69% 31.5M 14s
350450K .......... .......... .......... .......... .......... 69% 26.7M 14s
350500K .......... .......... .......... .......... .......... 69% 25.3M 14s
350550K .......... .......... .......... .......... .......... 69% 43.2M 14s
350600K .......... .......... .......... .......... .......... 69% 12.5M 14s
350650K .......... .......... .......... .......... .......... 69% 43.1M 14s
350700K .......... .......... .......... .......... .......... 69%  142M 14s
350750K .......... .......... .......... .......... .......... 69% 21.8M 14s
350800K .......... .......... .......... .......... .......... 69%  111M 14s
350850K .......... .......... .......... .......... .......... 69% 25.0M 14s
350900K .......... .......... .......... .......... .......... 69% 33.4M 14s
350950K .......... .......... .......... .......... .......... 69% 35.2M 14s
351000K .......... .......... .......... .......... .......... 69% 19.2M 14s
351050K .......... .......... .......... .......... .......... 69% 23.4M 14s
351100K .......... .......... .......... .......... .......... 69% 19.4M 14s
351150K .......... .......... .......... .......... .......... 69% 22.4M 14s
351200K .......... .......... .......... .......... .......... 69% 14.7M 14s
351250K .......... .......... .......... .......... .......... 69% 23.4M 14s
351300K .......... .......... .......... .......... .......... 69% 23.5M 14s
351350K .......... .......... .......... .......... .......... 69% 18.5M 14s
351400K .......... .......... .......... .......... .......... 69% 21.7M 14s
351450K .......... .......... .......... .......... .......... 69% 21.7M 14s
351500K .......... .......... .......... .......... .......... 69% 16.0M 14s
351550K .......... .......... .......... .......... .......... 69% 18.2M 14s
351600K .......... .......... .......... .......... .......... 69% 19.5M 14s
351650K .......... .......... .......... .......... .......... 69% 23.0M 14s
351700K .......... .......... .......... .......... .......... 69% 23.9M 14s
351750K .......... .......... .......... .......... .......... 69% 24.3M 14s
351800K .......... .......... .......... .......... .......... 69% 16.8M 14s
351850K .......... .......... .......... .......... .......... 69% 33.9M 14s
351900K .......... .......... .......... .......... .......... 69% 56.1M 14s
351950K .......... .......... .......... .......... .......... 69% 39.2M 14s
352000K .......... .......... .......... .......... .......... 69% 30.9M 14s
352050K .......... .......... .......... .......... .......... 69% 23.7M 14s
352100K .......... .......... .......... .......... .......... 69% 24.1M 14s
352150K .......... .......... .......... .......... .......... 69% 21.9M 14s
352200K .......... .......... .......... .......... .......... 69% 14.8M 14s
352250K .......... .......... .......... .......... .......... 69% 21.5M 14s
352300K .......... .......... .......... .......... .......... 69% 20.0M 14s
352350K .......... .......... .......... .......... .......... 69% 18.1M 14s
352400K .......... .......... .......... .......... .......... 69% 14.9M 14s
352450K .......... .......... .......... .......... .......... 69% 18.2M 14s
352500K .......... .......... .......... .......... .......... 69% 26.5M 14s
352550K .......... .......... .......... .......... .......... 69% 23.4M 14s
352600K .......... .......... .......... .......... .......... 69% 16.6M 14s
352650K .......... .......... .......... .......... .......... 69% 27.2M 13s
352700K .......... .......... .......... .......... .......... 69% 16.2M 13s
352750K .......... .......... .......... .......... .......... 69% 19.9M 13s
352800K .......... .......... .......... .......... .......... 69% 14.4M 13s
352850K .......... .......... .......... .......... .......... 69% 9.84M 13s
352900K .......... .......... .......... .......... .......... 69% 25.1M 13s
352950K .......... .......... .......... .......... .......... 69% 24.1M 13s
353000K .......... .......... .......... .......... .......... 69% 16.5M 13s
353050K .......... .......... .......... .......... .......... 69% 54.0M 13s
353100K .......... .......... .......... .......... .......... 69% 13.8M 13s
353150K .......... .......... .......... .......... .......... 69% 22.0M 13s
353200K .......... .......... .......... .......... .......... 69% 21.6M 13s
353250K .......... .......... .......... .......... .......... 69% 16.9M 13s
353300K .......... .......... .......... .......... .......... 69% 24.4M 13s
353350K .......... .......... .......... .......... .......... 69% 15.4M 13s
353400K .......... .......... .......... .......... .......... 70% 20.4M 13s
353450K .......... .......... .......... .......... .......... 70% 13.6M 13s
353500K .......... .......... .......... .......... .......... 70% 18.2M 13s
353550K .......... .......... .......... .......... .......... 70% 24.3M 13s
353600K .......... .......... .......... .......... .......... 70% 16.9M 13s
353650K .......... .......... .......... .......... .......... 70% 16.7M 13s
353700K .......... .......... .......... .......... .......... 70% 14.6M 13s
353750K .......... .......... .......... .......... .......... 70% 23.3M 13s
353800K .......... .......... .......... .......... .......... 70% 13.1M 13s
353850K .......... .......... .......... .......... .......... 70% 24.3M 13s
353900K .......... .......... .......... .......... .......... 70% 33.0M 13s
353950K .......... .......... .......... .......... .......... 70% 20.9M 13s
354000K .......... .......... .......... .......... .......... 70% 19.2M 13s
354050K .......... .......... .......... .......... .......... 70% 16.0M 13s
354100K .......... .......... .......... .......... .......... 70% 15.1M 13s
354150K .......... .......... .......... .......... .......... 70% 22.3M 13s
354200K .......... .......... .......... .......... .......... 70% 14.7M 13s
354250K .......... .......... .......... .......... .......... 70% 21.0M 13s
354300K .......... .......... .......... .......... .......... 70% 18.8M 13s
354350K .......... .......... .......... .......... .......... 70% 12.8M 13s
354400K .......... .......... .......... .......... .......... 70% 14.5M 13s
354450K .......... .......... .......... .......... .......... 70% 21.5M 13s
354500K .......... .......... .......... .......... .......... 70% 17.4M 13s
354550K .......... .......... .......... .......... .......... 70% 19.8M 13s
354600K .......... .......... .......... .......... .......... 70% 15.7M 13s
354650K .......... .......... .......... .......... .......... 70% 14.3M 13s
354700K .......... .......... .......... .......... .......... 70% 41.0M 13s
354750K .......... .......... .......... .......... .......... 70% 14.9M 13s
354800K .......... .......... .......... .......... .......... 70% 72.9M 13s
354850K .......... .......... .......... .......... .......... 70% 31.4M 13s
354900K .......... .......... .......... .......... .......... 70%  103M 13s
354950K .......... .......... .......... .......... .......... 70% 19.5M 13s
355000K .......... .......... .......... .......... .......... 70% 24.5M 13s
355050K .......... .......... .......... .......... .......... 70% 28.2M 13s
355100K .......... .......... .......... .......... .......... 70% 20.6M 13s
355150K .......... .......... .......... .......... .......... 70% 18.3M 13s
355200K .......... .......... .......... .......... .......... 70% 23.9M 13s
355250K .......... .......... .......... .......... .......... 70% 24.6M 13s
355300K .......... .......... .......... .......... .......... 70% 21.9M 13s
355350K .......... .......... .......... .......... .......... 70% 21.3M 13s
355400K .......... .......... .......... .......... .......... 70% 19.2M 13s
355450K .......... .......... .......... .......... .......... 70% 18.9M 13s
355500K .......... .......... .......... .......... .......... 70% 22.2M 13s
355550K .......... .......... .......... .......... .......... 70% 25.4M 13s
355600K .......... .......... .......... .......... .......... 70% 23.6M 13s
355650K .......... .......... .......... .......... .......... 70% 21.4M 13s
355700K .......... .......... .......... .......... .......... 70% 20.5M 13s
355750K .......... .......... .......... .......... .......... 70% 28.3M 13s
355800K .......... .......... .......... .......... .......... 70% 26.4M 13s
355850K .......... .......... .......... .......... .......... 70% 18.9M 13s
355900K .......... .......... .......... .......... .......... 70% 13.9M 13s
355950K .......... .......... .......... .......... .......... 70%  147M 13s
356000K .......... .......... .......... .......... .......... 70% 44.1M 13s
356050K .......... .......... .......... .......... .......... 70% 36.5M 13s
356100K .......... .......... .......... .......... .......... 70% 20.4M 13s
356150K .......... .......... .......... .......... .......... 70% 27.5M 13s
356200K .......... .......... .......... .......... .......... 70% 18.2M 13s
356250K .......... .......... .......... .......... .......... 70% 19.3M 13s
356300K .......... .......... .......... .......... .......... 70% 24.6M 13s
356350K .......... .......... .......... .......... .......... 70% 18.1M 13s
356400K .......... .......... .......... .......... .......... 70% 28.0M 13s
356450K .......... .......... .......... .......... .......... 70% 18.2M 13s
356500K .......... .......... .......... .......... .......... 70% 21.1M 13s
356550K .......... .......... .......... .......... .......... 70% 23.7M 13s
356600K .......... .......... .......... .......... .......... 70% 17.8M 13s
356650K .......... .......... .......... .......... .......... 70% 20.9M 13s
356700K .......... .......... .......... .......... .......... 70% 16.4M 13s
356750K .......... .......... .......... .......... .......... 70% 20.2M 13s
356800K .......... .......... .......... .......... .......... 70% 19.9M 13s
356850K .......... .......... .......... .......... .......... 70% 24.0M 13s
356900K .......... .......... .......... .......... .......... 70% 20.3M 13s
356950K .......... .......... .......... .......... .......... 70% 8.13M 13s
357000K .......... .......... .......... .......... .......... 70%  127M 13s
357050K .......... .......... .......... .......... .......... 70% 31.9M 13s
357100K .......... .......... .......... .......... .......... 70% 29.6M 13s
357150K .......... .......... .......... .......... .......... 70% 21.8M 13s
357200K .......... .......... .......... .......... .......... 70% 19.9M 13s
357250K .......... .......... .......... .......... .......... 70% 23.0M 13s
357300K .......... .......... .......... .......... .......... 70% 22.7M 13s
357350K .......... .......... .......... .......... .......... 70% 22.4M 13s
357400K .......... .......... .......... .......... .......... 70% 14.1M 13s
357450K .......... .......... .......... .......... .......... 70% 23.3M 13s
357500K .......... .......... .......... .......... .......... 70% 24.1M 13s
357550K .......... .......... .......... .......... .......... 70% 25.9M 13s
357600K .......... .......... .......... .......... .......... 70% 19.2M 13s
357650K .......... .......... .......... .......... .......... 70% 27.1M 13s
357700K .......... .......... .......... .......... .......... 70% 18.1M 13s
357750K .......... .......... .......... .......... .......... 70% 22.5M 13s
357800K .......... .......... .......... .......... .......... 70% 24.9M 13s
357850K .......... .......... .......... .......... .......... 70% 17.6M 13s
357900K .......... .......... .......... .......... .......... 70% 25.6M 13s
357950K .......... .......... .......... .......... .......... 70% 11.6M 13s
358000K .......... .......... .......... .......... .......... 70%  161M 13s
358050K .......... .......... .......... .......... .......... 70% 11.6M 13s
358100K .......... .......... .......... .......... .......... 70% 36.9M 13s
358150K .......... .......... .......... .......... .......... 70% 21.1M 13s
358200K .......... .......... .......... .......... .......... 70% 17.9M 13s
358250K .......... .......... .......... .......... .......... 70% 36.2M 13s
358300K .......... .......... .......... .......... .......... 70% 22.2M 13s
358350K .......... .......... .......... .......... .......... 70% 18.5M 13s
358400K .......... .......... .......... .......... .......... 70% 28.3M 13s
358450K .......... .......... .......... .......... .......... 71% 18.6M 13s
358500K .......... .......... .......... .......... .......... 71% 13.6M 13s
358550K .......... .......... .......... .......... .......... 71% 39.3M 13s
358600K .......... .......... .......... .......... .......... 71% 18.4M 13s
358650K .......... .......... .......... .......... .......... 71% 21.9M 13s
358700K .......... .......... .......... .......... .......... 71% 17.8M 13s
358750K .......... .......... .......... .......... .......... 71% 26.0M 13s
358800K .......... .......... .......... .......... .......... 71% 12.8M 13s
358850K .......... .......... .......... .......... .......... 71% 19.3M 13s
358900K .......... .......... .......... .......... .......... 71% 14.1M 13s
358950K .......... .......... .......... .......... .......... 71% 11.3M 13s
359000K .......... .......... .......... .......... .......... 71% 21.6M 13s
359050K .......... .......... .......... .......... .......... 71% 16.2M 13s
359100K .......... .......... .......... .......... .......... 71% 21.4M 13s
359150K .......... .......... .......... .......... .......... 71% 20.4M 13s
359200K .......... .......... .......... .......... .......... 71% 19.3M 13s
359250K .......... .......... .......... .......... .......... 71% 16.1M 13s
359300K .......... .......... .......... .......... .......... 71% 24.9M 13s
359350K .......... .......... .......... .......... .......... 71% 12.6M 13s
359400K .......... .......... .......... .......... .......... 71% 19.3M 13s
359450K .......... .......... .......... .......... .......... 71% 14.9M 13s
359500K .......... .......... .......... .......... .......... 71% 28.0M 13s
359550K .......... .......... .......... .......... .......... 71% 50.9M 13s
359600K .......... .......... .......... .......... .......... 71% 26.1M 13s
359650K .......... .......... .......... .......... .......... 71% 42.7M 13s
359700K .......... .......... .......... .......... .......... 71% 52.4M 13s
359750K .......... .......... .......... .......... .......... 71% 43.3M 13s
359800K .......... .......... .......... .......... .......... 71% 49.3M 13s
359850K .......... .......... .......... .......... .......... 71% 24.9M 13s
359900K .......... .......... .......... .......... .......... 71% 35.9M 13s
359950K .......... .......... .......... .......... .......... 71% 28.6M 13s
360000K .......... .......... .......... .......... .......... 71% 45.2M 13s
360050K .......... .......... .......... .......... .......... 71% 39.1M 13s
360100K .......... .......... .......... .......... .......... 71% 26.5M 13s
360150K .......... .......... .......... .......... .......... 71% 33.0M 13s
360200K .......... .......... .......... .......... .......... 71% 30.1M 13s
360250K .......... .......... .......... .......... .......... 71% 26.4M 13s
360300K .......... .......... .......... .......... .......... 71% 43.8M 13s
360350K .......... .......... .......... .......... .......... 71% 31.0M 13s
360400K .......... .......... .......... .......... .......... 71% 32.5M 13s
360450K .......... .......... .......... .......... .......... 71% 32.7M 13s
360500K .......... .......... .......... .......... .......... 71% 31.9M 13s
360550K .......... .......... .......... .......... .......... 71% 34.8M 13s
360600K .......... .......... .......... .......... .......... 71% 32.3M 13s
360650K .......... .......... .......... .......... .......... 71% 31.0M 13s
360700K .......... .......... .......... .......... .......... 71% 24.3M 13s
360750K .......... .......... .......... .......... .......... 71% 33.4M 13s
360800K .......... .......... .......... .......... .......... 71% 37.4M 13s
360850K .......... .......... .......... .......... .......... 71% 38.5M 13s
360900K .......... .......... .......... .......... .......... 71% 31.5M 13s
360950K .......... .......... .......... .......... .......... 71% 18.2M 13s
361000K .......... .......... .......... .......... .......... 71%  233M 13s
361050K .......... .......... .......... .......... .......... 71% 48.1M 13s
361100K .......... .......... .......... .......... .......... 71% 32.5M 13s
361150K .......... .......... .......... .......... .......... 71%  271M 13s
361200K .......... .......... .......... .......... .......... 71% 23.0M 13s
361250K .......... .......... .......... .......... .......... 71%  152M 13s
361300K .......... .......... .......... .......... .......... 71% 39.7M 13s
361350K .......... .......... .......... .......... .......... 71% 32.9M 13s
361400K .......... .......... .......... .......... .......... 71% 35.2M 13s
361450K .......... .......... .......... .......... .......... 71% 32.9M 13s
361500K .......... .......... .......... .......... .......... 71% 42.5M 13s
361550K .......... .......... .......... .......... .......... 71% 36.7M 13s
361600K .......... .......... .......... .......... .......... 71% 24.8M 13s
361650K .......... .......... .......... .......... .......... 71% 36.3M 13s
361700K .......... .......... .......... .......... .......... 71% 36.2M 13s
361750K .......... .......... .......... .......... .......... 71% 47.1M 13s
361800K .......... .......... .......... .......... .......... 71% 35.2M 13s
361850K .......... .......... .......... .......... .......... 71% 27.2M 13s
361900K .......... .......... .......... .......... .......... 71% 38.6M 13s
361950K .......... .......... .......... .......... .......... 71% 34.2M 13s
362000K .......... .......... .......... .......... .......... 71% 37.1M 13s
362050K .......... .......... .......... .......... .......... 71% 23.7M 12s
362100K .......... .......... .......... .......... .......... 71% 31.6M 12s
362150K .......... .......... .......... .......... .......... 71% 45.6M 12s
362200K .......... .......... .......... .......... .......... 71% 38.1M 12s
362250K .......... .......... .......... .......... .......... 71% 38.5M 12s
362300K .......... .......... .......... .......... .......... 71% 31.9M 12s
362350K .......... .......... .......... .......... .......... 71% 26.2M 12s
362400K .......... .......... .......... .......... .......... 71% 39.0M 12s
362450K .......... .......... .......... .......... .......... 71% 40.2M 12s
362500K .......... .......... .......... .......... .......... 71% 59.7M 12s
362550K .......... .......... .......... .......... .......... 71% 33.2M 12s
362600K .......... .......... .......... .......... .......... 71% 18.3M 12s
362650K .......... .......... .......... .......... .......... 71%  182M 12s
362700K .......... .......... .......... .......... .......... 71% 32.2M 12s
362750K .......... .......... .......... .......... .......... 71% 53.0M 12s
362800K .......... .......... .......... .......... .......... 71% 39.7M 12s
362850K .......... .......... .......... .......... .......... 71% 38.9M 12s
362900K .......... .......... .......... .......... .......... 71% 63.2M 12s
362950K .......... .......... .......... .......... .......... 71% 26.6M 12s
363000K .......... .......... .......... .......... .......... 71% 30.5M 12s
363050K .......... .......... .......... .......... .......... 71% 26.9M 12s
363100K .......... .......... .......... .......... .......... 71% 20.2M 12s
363150K .......... .......... .......... .......... .......... 71% 24.9M 12s
363200K .......... .......... .......... .......... .......... 71% 24.8M 12s
363250K .......... .......... .......... .......... .......... 71% 25.1M 12s
363300K .......... .......... .......... .......... .......... 71% 30.9M 12s
363350K .......... .......... .......... .......... .......... 71% 22.3M 12s
363400K .......... .......... .......... .......... .......... 71% 23.2M 12s
363450K .......... .......... .......... .......... .......... 71% 18.6M 12s
363500K .......... .......... .......... .......... .......... 72% 20.8M 12s
363550K .......... .......... .......... .......... .......... 72% 38.3M 12s
363600K .......... .......... .......... .......... .......... 72% 24.1M 12s
363650K .......... .......... .......... .......... .......... 72% 20.7M 12s
363700K .......... .......... .......... .......... .......... 72% 20.1M 12s
363750K .......... .......... .......... .......... .......... 72% 44.6M 12s
363800K .......... .......... .......... .......... .......... 72% 50.1M 12s
363850K .......... .......... .......... .......... .......... 72% 60.5M 12s
363900K .......... .......... .......... .......... .......... 72% 26.1M 12s
363950K .......... .......... .......... .......... .......... 72% 42.9M 12s
364000K .......... .......... .......... .......... .......... 72% 46.2M 12s
364050K .......... .......... .......... .......... .......... 72%  239M 12s
364100K .......... .......... .......... .......... .......... 72% 24.1M 12s
364150K .......... .......... .......... .......... .......... 72%  155M 12s
364200K .......... .......... .......... .......... .......... 72% 25.8M 12s
364250K .......... .......... .......... .......... .......... 72% 41.2M 12s
364300K .......... .......... .......... .......... .......... 72% 24.0M 12s
364350K .......... .......... .......... .......... .......... 72% 21.0M 12s
364400K .......... .......... .......... .......... .......... 72% 69.4M 12s
364450K .......... .......... .......... .......... .......... 72% 20.5M 12s
364500K .......... .......... .......... .......... .......... 72% 22.2M 12s
364550K .......... .......... .......... .......... .......... 72% 37.4M 12s
364600K .......... .......... .......... .......... .......... 72% 22.0M 12s
364650K .......... .......... .......... .......... .......... 72% 27.9M 12s
364700K .......... .......... .......... .......... .......... 72% 21.8M 12s
364750K .......... .......... .......... .......... .......... 72% 27.4M 12s
364800K .......... .......... .......... .......... .......... 72% 22.2M 12s
364850K .......... .......... .......... .......... .......... 72% 18.1M 12s
364900K .......... .......... .......... .......... .......... 72% 28.6M 12s
364950K .......... .......... .......... .......... .......... 72% 30.4M 12s
365000K .......... .......... .......... .......... .......... 72% 20.1M 12s
365050K .......... .......... .......... .......... .......... 72% 22.8M 12s
365100K .......... .......... .......... .......... .......... 72% 21.6M 12s
365150K .......... .......... .......... .......... .......... 72% 14.1M 12s
365200K .......... .......... .......... .......... .......... 72% 20.5M 12s
365250K .......... .......... .......... .......... .......... 72% 29.3M 12s
365300K .......... .......... .......... .......... .......... 72% 30.9M 12s
365350K .......... .......... .......... .......... .......... 72% 37.6M 12s
365400K .......... .......... .......... .......... .......... 72% 18.0M 12s
365450K .......... .......... .......... .......... .......... 72%  138M 12s
365500K .......... .......... .......... .......... .......... 72% 21.1M 12s
365550K .......... .......... .......... .......... .......... 72%  103M 12s
365600K .......... .......... .......... .......... .......... 72% 33.4M 12s
365650K .......... .......... .......... .......... .......... 72% 38.9M 12s
365700K .......... .......... .......... .......... .......... 72% 23.4M 12s
365750K .......... .......... .......... .......... .......... 72% 33.7M 12s
365800K .......... .......... .......... .......... .......... 72% 23.2M 12s
365850K .......... .......... .......... .......... .......... 72% 29.8M 12s
365900K .......... .......... .......... .......... .......... 72% 33.2M 12s
365950K .......... .......... .......... .......... .......... 72% 26.2M 12s
366000K .......... .......... .......... .......... .......... 72% 25.1M 12s
366050K .......... .......... .......... .......... .......... 72% 42.9M 12s
366100K .......... .......... .......... .......... .......... 72% 21.8M 12s
366150K .......... .......... .......... .......... .......... 72% 34.3M 12s
366200K .......... .......... .......... .......... .......... 72% 23.9M 12s
366250K .......... .......... .......... .......... .......... 72% 28.8M 12s
366300K .......... .......... .......... .......... .......... 72% 27.0M 12s
366350K .......... .......... .......... .......... .......... 72% 24.1M 12s
366400K .......... .......... .......... .......... .......... 72% 30.4M 12s
366450K .......... .......... .......... .......... .......... 72% 33.4M 12s
366500K .......... .......... .......... .......... .......... 72% 23.0M 12s
366550K .......... .......... .......... .......... .......... 72% 30.6M 12s
366600K .......... .......... .......... .......... .......... 72% 32.4M 12s
366650K .......... .......... .......... .......... .......... 72% 18.0M 12s
366700K .......... .......... .......... .......... .......... 72% 26.1M 12s
366750K .......... .......... .......... .......... .......... 72%  138M 12s
366800K .......... .......... .......... .......... .......... 72% 27.0M 12s
366850K .......... .......... .......... .......... .......... 72% 16.6M 12s
366900K .......... .......... .......... .......... .......... 72%  206M 12s
366950K .......... .......... .......... .......... .......... 72% 37.2M 12s
367000K .......... .......... .......... .......... .......... 72% 48.1M 12s
367050K .......... .......... .......... .......... .......... 72% 17.8M 12s
367100K .......... .......... .......... .......... .......... 72%  163M 12s
367150K .......... .......... .......... .......... .......... 72% 27.5M 12s
367200K .......... .......... .......... .......... .......... 72% 37.6M 12s
367250K .......... .......... .......... .......... .......... 72% 20.8M 12s
367300K .......... .......... .......... .......... .......... 72% 39.3M 12s
367350K .......... .......... .......... .......... .......... 72% 20.3M 12s
367400K .......... .......... .......... .......... .......... 72% 32.6M 12s
367450K .......... .......... .......... .......... .......... 72% 28.3M 12s
367500K .......... .......... .......... .......... .......... 72% 23.0M 12s
367550K .......... .......... .......... .......... .......... 72% 36.5M 12s
367600K .......... .......... .......... .......... .......... 72% 23.2M 12s
367650K .......... .......... .......... .......... .......... 72% 24.4M 12s
367700K .......... .......... .......... .......... .......... 72% 23.8M 12s
367750K .......... .......... .......... .......... .......... 72% 38.7M 12s
367800K .......... .......... .......... .......... .......... 72% 25.5M 12s
367850K .......... .......... .......... .......... .......... 72% 31.5M 12s
367900K .......... .......... .......... .......... .......... 72% 30.5M 12s
367950K .......... .......... .......... .......... .......... 72% 21.4M 12s
368000K .......... .......... .......... .......... .......... 72% 32.6M 12s
368050K .......... .......... .......... .......... .......... 72% 20.5M 12s
368100K .......... .......... .......... .......... .......... 72% 29.0M 12s
368150K .......... .......... .......... .......... .......... 72% 15.1M 12s
368200K .......... .......... .......... .......... .......... 72%  101M 12s
368250K .......... .......... .......... .......... .......... 72% 39.5M 12s
368300K .......... .......... .......... .......... .......... 72% 14.9M 12s
368350K .......... .......... .......... .......... .......... 72% 29.2M 12s
368400K .......... .......... .......... .......... .......... 72% 48.1M 12s
368450K .......... .......... .......... .......... .......... 72% 22.0M 12s
368500K .......... .......... .......... .......... .......... 72% 25.1M 12s
368550K .......... .......... .......... .......... .......... 73% 24.0M 12s
368600K .......... .......... .......... .......... .......... 73% 18.3M 12s
368650K .......... .......... .......... .......... .......... 73% 28.2M 12s
368700K .......... .......... .......... .......... .......... 73% 22.2M 12s
368750K .......... .......... .......... .......... .......... 73% 20.5M 12s
368800K .......... .......... .......... .......... .......... 73% 24.9M 12s
368850K .......... .......... .......... .......... .......... 73% 17.8M 12s
368900K .......... .......... .......... .......... .......... 73% 26.9M 12s
368950K .......... .......... .......... .......... .......... 73% 21.1M 12s
369000K .......... .......... .......... .......... .......... 73% 22.5M 12s
369050K .......... .......... .......... .......... .......... 73% 23.8M 12s
369100K .......... .......... .......... .......... .......... 73% 21.2M 12s
369150K .......... .......... .......... .......... .......... 73% 21.2M 12s
369200K .......... .......... .......... .......... .......... 73% 22.2M 12s
369250K .......... .......... .......... .......... .......... 73% 19.8M 12s
369300K .......... .......... .......... .......... .......... 73% 11.1M 12s
369350K .......... .......... .......... .......... .......... 73% 23.6M 12s
369400K .......... .......... .......... .......... .......... 73% 13.9M 12s
369450K .......... .......... .......... .......... .......... 73% 18.5M 12s
369500K .......... .......... .......... .......... .......... 73% 18.1M 12s
369550K .......... .......... .......... .......... .......... 73% 15.9M 12s
369600K .......... .......... .......... .......... .......... 73% 11.6M 12s
369650K .......... .......... .......... .......... .......... 73% 15.9M 12s
369700K .......... .......... .......... .......... .......... 73% 14.3M 12s
369750K .......... .......... .......... .......... .......... 73% 20.0M 12s
369800K .......... .......... .......... .......... .......... 73% 15.7M 12s
369850K .......... .......... .......... .......... .......... 73% 13.4M 12s
369900K .......... .......... .......... .......... .......... 73% 15.6M 12s
369950K .......... .......... .......... .......... .......... 73% 15.2M 12s
370000K .......... .......... .......... .......... .......... 73% 18.3M 12s
370050K .......... .......... .......... .......... .......... 73% 22.3M 12s
370100K .......... .......... .......... .......... .......... 73% 20.9M 12s
370150K .......... .......... .......... .......... .......... 73% 13.4M 12s
370200K .......... .......... .......... .......... .......... 73% 43.1M 12s
370250K .......... .......... .......... .......... .......... 73% 6.03M 12s
370300K .......... .......... .......... .......... .......... 73%  182M 12s
370350K .......... .......... .......... .......... .......... 73%  123M 12s
370400K .......... .......... .......... .......... .......... 73%  118M 12s
370450K .......... .......... .......... .......... .......... 73%  156M 12s
370500K .......... .......... .......... .......... .......... 73% 31.5M 12s
370550K .......... .......... .......... .......... .......... 73% 23.1M 12s
370600K .......... .......... .......... .......... .......... 73% 24.0M 12s
370650K .......... .......... .......... .......... .......... 73% 21.5M 12s
370700K .......... .......... .......... .......... .......... 73% 20.8M 12s
370750K .......... .......... .......... .......... .......... 73% 24.6M 12s
370800K .......... .......... .......... .......... .......... 73% 25.5M 12s
370850K .......... .......... .......... .......... .......... 73% 17.5M 12s
370900K .......... .......... .......... .......... .......... 73% 30.3M 12s
370950K .......... .......... .......... .......... .......... 73% 17.4M 12s
371000K .......... .......... .......... .......... .......... 73% 34.1M 12s
371050K .......... .......... .......... .......... .......... 73% 32.7M 12s
371100K .......... .......... .......... .......... .......... 73% 17.0M 12s
371150K .......... .......... .......... .......... .......... 73% 29.3M 12s
371200K .......... .......... .......... .......... .......... 73% 31.0M 12s
371250K .......... .......... .......... .......... .......... 73% 15.9M 12s
371300K .......... .......... .......... .......... .......... 73% 27.4M 12s
371350K .......... .......... .......... .......... .......... 73% 17.6M 12s
371400K .......... .......... .......... .......... .......... 73%  258M 12s
371450K .......... .......... .......... .......... .......... 73% 26.1M 12s
371500K .......... .......... .......... .......... .......... 73% 27.9M 12s
371550K .......... .......... .......... .......... .......... 73% 20.6M 11s
371600K .......... .......... .......... .......... .......... 73% 13.8M 11s
371650K .......... .......... .......... .......... .......... 73% 19.8M 11s
371700K .......... .......... .......... .......... .......... 73% 15.0M 11s
371750K .......... .......... .......... .......... .......... 73% 16.7M 11s
371800K .......... .......... .......... .......... .......... 73% 15.6M 11s
371850K .......... .......... .......... .......... .......... 73% 15.9M 11s
371900K .......... .......... .......... .......... .......... 73% 17.5M 11s
371950K .......... .......... .......... .......... .......... 73% 15.0M 11s
372000K .......... .......... .......... .......... .......... 73% 22.1M 11s
372050K .......... .......... .......... .......... .......... 73% 14.1M 11s
372100K .......... .......... .......... .......... .......... 73% 16.2M 11s
372150K .......... .......... .......... .......... .......... 73% 19.1M 11s
372200K .......... .......... .......... .......... .......... 73% 18.8M 11s
372250K .......... .......... .......... .......... .......... 73% 16.5M 11s
372300K .......... .......... .......... .......... .......... 73% 26.5M 11s
372350K .......... .......... .......... .......... .......... 73% 17.2M 11s
372400K .......... .......... .......... .......... .......... 73% 18.6M 11s
372450K .......... .......... .......... .......... .......... 73% 16.0M 11s
372500K .......... .......... .......... .......... .......... 73% 22.6M 11s
372550K .......... .......... .......... .......... .......... 73% 17.1M 11s
372600K .......... .......... .......... .......... .......... 73% 19.3M 11s
372650K .......... .......... .......... .......... .......... 73% 17.4M 11s
372700K .......... .......... .......... .......... .......... 73% 17.9M 11s
372750K .......... .......... .......... .......... .......... 73% 19.5M 11s
372800K .......... .......... .......... .......... .......... 73% 19.0M 11s
372850K .......... .......... .......... .......... .......... 73% 20.2M 11s
372900K .......... .......... .......... .......... .......... 73% 15.9M 11s
372950K .......... .......... .......... .......... .......... 73% 21.0M 11s
373000K .......... .......... .......... .......... .......... 73% 13.8M 11s
373050K .......... .......... .......... .......... .......... 73% 15.7M 11s
373100K .......... .......... .......... .......... .......... 73% 18.7M 11s
373150K .......... .......... .......... .......... .......... 73% 17.8M 11s
373200K .......... .......... .......... .......... .......... 73% 27.0M 11s
373250K .......... .......... .......... .......... .......... 73% 19.3M 11s
373300K .......... .......... .......... .......... .......... 73% 84.3M 11s
373350K .......... .......... .......... .......... .......... 73% 25.2M 11s
373400K .......... .......... .......... .......... .......... 73% 28.7M 11s
373450K .......... .......... .......... .......... .......... 73% 30.4M 11s
373500K .......... .......... .......... .......... .......... 73% 28.0M 11s
373550K .......... .......... .......... .......... .......... 73% 45.4M 11s
373600K .......... .......... .......... .......... .......... 74% 26.9M 11s
373650K .......... .......... .......... .......... .......... 74% 32.9M 11s
373700K .......... .......... .......... .......... .......... 74% 26.1M 11s
373750K .......... .......... .......... .......... .......... 74% 38.2M 11s
373800K .......... .......... .......... .......... .......... 74% 33.2M 11s
373850K .......... .......... .......... .......... .......... 74% 34.8M 11s
373900K .......... .......... .......... .......... .......... 74% 31.4M 11s
373950K .......... .......... .......... .......... .......... 74% 23.1M 11s
374000K .......... .......... .......... .......... .......... 74% 36.3M 11s
374050K .......... .......... .......... .......... .......... 74% 22.6M 11s
374100K .......... .......... .......... .......... .......... 74% 40.7M 11s
374150K .......... .......... .......... .......... .......... 74% 26.1M 11s
374200K .......... .......... .......... .......... .......... 74% 29.9M 11s
374250K .......... .......... .......... .......... .......... 74% 38.3M 11s
374300K .......... .......... .......... .......... .......... 74% 29.1M 11s
374350K .......... .......... .......... .......... .......... 74% 19.3M 11s
374400K .......... .......... .......... .......... .......... 74% 22.4M 11s
374450K .......... .......... .......... .......... .......... 74% 50.9M 11s
374500K .......... .......... .......... .......... .......... 74% 68.8M 11s
374550K .......... .......... .......... .......... .......... 74% 49.4M 11s
374600K .......... .......... .......... .......... .......... 74% 95.4M 11s
374650K .......... .......... .......... .......... .......... 74% 19.7M 11s
374700K .......... .......... .......... .......... .......... 74%  191M 11s
374750K .......... .......... .......... .......... .......... 74%  125M 11s
374800K .......... .......... .......... .......... .......... 74% 39.9M 11s
374850K .......... .......... .......... .......... .......... 74% 51.9M 11s
374900K .......... .......... .......... .......... .......... 74% 49.6M 11s
374950K .......... .......... .......... .......... .......... 74%  159M 11s
375000K .......... .......... .......... .......... .......... 74% 55.5M 11s
375050K .......... .......... .......... .......... .......... 74% 32.0M 11s
375100K .......... .......... .......... .......... .......... 74% 39.3M 11s
375150K .......... .......... .......... .......... .......... 74% 38.3M 11s
375200K .......... .......... .......... .......... .......... 74% 34.2M 11s
375250K .......... .......... .......... .......... .......... 74% 47.2M 11s
375300K .......... .......... .......... .......... .......... 74% 27.8M 11s
375350K .......... .......... .......... .......... .......... 74% 29.2M 11s
375400K .......... .......... .......... .......... .......... 74% 51.9M 11s
375450K .......... .......... .......... .......... .......... 74% 24.9M 11s
375500K .......... .......... .......... .......... .......... 74% 43.9M 11s
375550K .......... .......... .......... .......... .......... 74% 32.5M 11s
375600K .......... .......... .......... .......... .......... 74% 45.7M 11s
375650K .......... .......... .......... .......... .......... 74% 39.4M 11s
375700K .......... .......... .......... .......... .......... 74% 25.5M 11s
375750K .......... .......... .......... .......... .......... 74% 47.2M 11s
375800K .......... .......... .......... .......... .......... 74% 35.9M 11s
375850K .......... .......... .......... .......... .......... 74% 36.4M 11s
375900K .......... .......... .......... .......... .......... 74% 38.1M 11s
375950K .......... .......... .......... .......... .......... 74% 34.3M 11s
376000K .......... .......... .......... .......... .......... 74% 35.9M 11s
376050K .......... .......... .......... .......... .......... 74% 35.4M 11s
376100K .......... .......... .......... .......... .......... 74% 38.5M 11s
376150K .......... .......... .......... .......... .......... 74% 47.8M 11s
376200K .......... .......... .......... .......... .......... 74% 28.0M 11s
376250K .......... .......... .......... .......... .......... 74% 81.0M 11s
376300K .......... .......... .......... .......... .......... 74% 44.8M 11s
376350K .......... .......... .......... .......... .......... 74% 70.1M 11s
376400K .......... .......... .......... .......... .......... 74% 13.9M 11s
376450K .......... .......... .......... .......... .......... 74%  164M 11s
376500K .......... .......... .......... .......... .......... 74%  187M 11s
376550K .......... .......... .......... .......... .......... 74%  229M 11s
376600K .......... .......... .......... .......... .......... 74% 19.4M 11s
376650K .......... .......... .......... .......... .......... 74%  115M 11s
376700K .......... .......... .......... .......... .......... 74% 35.6M 11s
376750K .......... .......... .......... .......... .......... 74% 32.4M 11s
376800K .......... .......... .......... .......... .......... 74%  235M 11s
376850K .......... .......... .......... .......... .......... 74% 57.5M 11s
376900K .......... .......... .......... .......... .......... 74% 30.2M 11s
376950K .......... .......... .......... .......... .......... 74% 26.7M 11s
377000K .......... .......... .......... .......... .......... 74% 42.5M 11s
377050K .......... .......... .......... .......... .......... 74% 33.5M 11s
377100K .......... .......... .......... .......... .......... 74% 25.8M 11s
377150K .......... .......... .......... .......... .......... 74% 34.3M 11s
377200K .......... .......... .......... .......... .......... 74% 30.4M 11s
377250K .......... .......... .......... .......... .......... 74% 30.5M 11s
377300K .......... .......... .......... .......... .......... 74% 36.3M 11s
377350K .......... .......... .......... .......... .......... 74% 23.2M 11s
377400K .......... .......... .......... .......... .......... 74% 43.6M 11s
377450K .......... .......... .......... .......... .......... 74% 19.5M 11s
377500K .......... .......... .......... .......... .......... 74% 29.1M 11s
377550K .......... .......... .......... .......... .......... 74% 48.2M 11s
377600K .......... .......... .......... .......... .......... 74% 20.1M 11s
377650K .......... .......... .......... .......... .......... 74% 43.2M 11s
377700K .......... .......... .......... .......... .......... 74% 22.4M 11s
377750K .......... .......... .......... .......... .......... 74% 40.8M 11s
377800K .......... .......... .......... .......... .......... 74% 19.9M 11s
377850K .......... .......... .......... .......... .......... 74% 18.6M 11s
377900K .......... .......... .......... .......... .......... 74% 30.8M 11s
377950K .......... .......... .......... .......... .......... 74% 22.0M 11s
378000K .......... .......... .......... .......... .......... 74%  108M 11s
378050K .......... .......... .......... .......... .......... 74% 13.9M 11s
378100K .......... .......... .......... .......... .......... 74% 92.8M 11s
378150K .......... .......... .......... .......... .......... 74% 31.1M 11s
378200K .......... .......... .......... .......... .......... 74% 30.5M 11s
378250K .......... .......... .......... .......... .......... 74% 20.6M 11s
378300K .......... .......... .......... .......... .......... 74%  265M 11s
378350K .......... .......... .......... .......... .......... 74% 24.4M 11s
378400K .......... .......... .......... .......... .......... 74% 57.1M 11s
378450K .......... .......... .......... .......... .......... 74% 12.6M 11s
378500K .......... .......... .......... .......... .......... 74% 37.6M 11s
378550K .......... .......... .......... .......... .......... 74% 27.2M 11s
378600K .......... .......... .......... .......... .......... 74% 20.6M 11s
378650K .......... .......... .......... .......... .......... 75% 38.9M 11s
378700K .......... .......... .......... .......... .......... 75% 23.7M 11s
378750K .......... .......... .......... .......... .......... 75% 22.2M 11s
378800K .......... .......... .......... .......... .......... 75% 41.8M 11s
378850K .......... .......... .......... .......... .......... 75% 24.7M 11s
378900K .......... .......... .......... .......... .......... 75% 21.6M 11s
378950K .......... .......... .......... .......... .......... 75% 21.9M 11s
379000K .......... .......... .......... .......... .......... 75% 28.0M 11s
379050K .......... .......... .......... .......... .......... 75% 34.6M 11s
379100K .......... .......... .......... .......... .......... 75% 20.3M 11s
379150K .......... .......... .......... .......... .......... 75% 36.5M 11s
379200K .......... .......... .......... .......... .......... 75% 16.6M 11s
379250K .......... .......... .......... .......... .......... 75% 18.4M 11s
379300K .......... .......... .......... .......... .......... 75% 29.9M 11s
379350K .......... .......... .......... .......... .......... 75% 13.9M 11s
379400K .......... .......... .......... .......... .......... 75%  169M 11s
379450K .......... .......... .......... .......... .......... 75% 24.5M 11s
379500K .......... .......... .......... .......... .......... 75% 25.4M 11s
379550K .......... .......... .......... .......... .......... 75% 56.6M 11s
379600K .......... .......... .......... .......... .......... 75% 25.1M 11s
379650K .......... .......... .......... .......... .......... 75% 23.2M 11s
379700K .......... .......... .......... .......... .......... 75% 22.9M 11s
379750K .......... .......... .......... .......... .......... 75% 23.9M 11s
379800K .......... .......... .......... .......... .......... 75% 20.5M 11s
379850K .......... .......... .......... .......... .......... 75% 20.1M 11s
379900K .......... .......... .......... .......... .......... 75% 30.9M 11s
379950K .......... .......... .......... .......... .......... 75% 22.3M 11s
380000K .......... .......... .......... .......... .......... 75% 24.9M 11s
380050K .......... .......... .......... .......... .......... 75% 19.2M 11s
380100K .......... .......... .......... .......... .......... 75% 21.9M 11s
380150K .......... .......... .......... .......... .......... 75% 21.9M 11s
380200K .......... .......... .......... .......... .......... 75% 23.7M 11s
380250K .......... .......... .......... .......... .......... 75% 32.8M 11s
380300K .......... .......... .......... .......... .......... 75% 25.8M 11s
380350K .......... .......... .......... .......... .......... 75% 25.9M 11s
380400K .......... .......... .......... .......... .......... 75% 24.7M 11s
380450K .......... .......... .......... .......... .......... 75% 27.5M 11s
380500K .......... .......... .......... .......... .......... 75% 16.6M 11s
380550K .......... .......... .......... .......... .......... 75%  211M 11s
380600K .......... .......... .......... .......... .......... 75% 19.6M 11s
380650K .......... .......... .......... .......... .......... 75% 46.5M 11s
380700K .......... .......... .......... .......... .......... 75% 30.5M 11s
380750K .......... .......... .......... .......... .......... 75% 23.8M 11s
380800K .......... .......... .......... .......... .......... 75% 19.2M 11s
380850K .......... .......... .......... .......... .......... 75% 20.1M 11s
380900K .......... .......... .......... .......... .......... 75% 22.5M 11s
380950K .......... .......... .......... .......... .......... 75% 26.4M 11s
381000K .......... .......... .......... .......... .......... 75% 18.3M 11s
381050K .......... .......... .......... .......... .......... 75% 23.7M 11s
381100K .......... .......... .......... .......... .......... 75% 23.0M 11s
381150K .......... .......... .......... .......... .......... 75% 23.6M 11s
381200K .......... .......... .......... .......... .......... 75% 20.1M 11s
381250K .......... .......... .......... .......... .......... 75% 21.6M 11s
381300K .......... .......... .......... .......... .......... 75% 23.7M 10s
381350K .......... .......... .......... .......... .......... 75% 20.0M 10s
381400K .......... .......... .......... .......... .......... 75% 24.7M 10s
381450K .......... .......... .......... .......... .......... 75% 19.1M 10s
381500K .......... .......... .......... .......... .......... 75% 27.7M 10s
381550K .......... .......... .......... .......... .......... 75% 25.2M 10s
381600K .......... .......... .......... .......... .......... 75% 15.5M 10s
381650K .......... .......... .......... .......... .......... 75% 17.9M 10s
381700K .......... .......... .......... .......... .......... 75% 67.5M 10s
381750K .......... .......... .......... .......... .......... 75% 18.2M 10s
381800K .......... .......... .......... .......... .......... 75% 25.6M 10s
381850K .......... .......... .......... .......... .......... 75% 19.8M 10s
381900K .......... .......... .......... .......... .......... 75% 34.2M 10s
381950K .......... .......... .......... .......... .......... 75% 17.7M 10s
382000K .......... .......... .......... .......... .......... 75% 23.2M 10s
382050K .......... .......... .......... .......... .......... 75% 23.6M 10s
382100K .......... .......... .......... .......... .......... 75% 23.3M 10s
382150K .......... .......... .......... .......... .......... 75% 19.9M 10s
382200K .......... .......... .......... .......... .......... 75% 18.6M 10s
382250K .......... .......... .......... .......... .......... 75% 20.4M 10s
382300K .......... .......... .......... .......... .......... 75% 21.1M 10s
382350K .......... .......... .......... .......... .......... 75% 20.9M 10s
382400K .......... .......... .......... .......... .......... 75% 26.9M 10s
382450K .......... .......... .......... .......... .......... 75% 21.7M 10s
382500K .......... .......... .......... .......... .......... 75% 19.3M 10s
382550K .......... .......... .......... .......... .......... 75% 26.5M 10s
382600K .......... .......... .......... .......... .......... 75% 29.8M 10s
382650K .......... .......... .......... .......... .......... 75% 29.9M 10s
382700K .......... .......... .......... .......... .......... 75% 41.9M 10s
382750K .......... .......... .......... .......... .......... 75%  216M 10s
382800K .......... .......... .......... .......... .......... 75% 19.6M 10s
382850K .......... .......... .......... .......... .......... 75% 66.4M 10s
382900K .......... .......... .......... .......... .......... 75% 36.7M 10s
382950K .......... .......... .......... .......... .......... 75% 23.9M 10s
383000K .......... .......... .......... .......... .......... 75% 18.9M 10s
383050K .......... .......... .......... .......... .......... 75% 24.7M 10s
383100K .......... .......... .......... .......... .......... 75% 19.5M 10s
383150K .......... .......... .......... .......... .......... 75% 22.3M 10s
383200K .......... .......... .......... .......... .......... 75% 20.8M 10s
383250K .......... .......... .......... .......... .......... 75% 23.0M 10s
383300K .......... .......... .......... .......... .......... 75% 43.2M 10s
383350K .......... .......... .......... .......... .......... 75% 20.0M 10s
383400K .......... .......... .......... .......... .......... 75% 22.0M 10s
383450K .......... .......... .......... .......... .......... 75% 25.8M 10s
383500K .......... .......... .......... .......... .......... 75% 21.8M 10s
383550K .......... .......... .......... .......... .......... 75% 20.2M 10s
383600K .......... .......... .......... .......... .......... 75% 20.6M 10s
383650K .......... .......... .......... .......... .......... 75% 21.2M 10s
383700K .......... .......... .......... .......... .......... 76% 27.1M 10s
383750K .......... .......... .......... .......... .......... 76% 29.9M 10s
383800K .......... .......... .......... .......... .......... 76% 10.4M 10s
383850K .......... .......... .......... .......... .......... 76%  126M 10s
383900K .......... .......... .......... .......... .......... 76% 20.1M 10s
383950K .......... .......... .......... .......... .......... 76% 30.5M 10s
384000K .......... .......... .......... .......... .......... 76% 55.9M 10s
384050K .......... .......... .......... .......... .......... 76% 22.2M 10s
384100K .......... .......... .......... .......... .......... 76% 25.0M 10s
384150K .......... .......... .......... .......... .......... 76% 21.4M 10s
384200K .......... .......... .......... .......... .......... 76% 17.7M 10s
384250K .......... .......... .......... .......... .......... 76% 17.5M 10s
384300K .......... .......... .......... .......... .......... 76% 22.6M 10s
384350K .......... .......... .......... .......... .......... 76% 17.3M 10s
384400K .......... .......... .......... .......... .......... 76% 22.0M 10s
384450K .......... .......... .......... .......... .......... 76% 15.4M 10s
384500K .......... .......... .......... .......... .......... 76% 24.5M 10s
384550K .......... .......... .......... .......... .......... 76% 24.5M 10s
384600K .......... .......... .......... .......... .......... 76% 15.9M 10s
384650K .......... .......... .......... .......... .......... 76% 28.7M 10s
384700K .......... .......... .......... .......... .......... 76% 18.4M 10s
384750K .......... .......... .......... .......... .......... 76% 20.4M 10s
384800K .......... .......... .......... .......... .......... 76% 30.7M 10s
384850K .......... .......... .......... .......... .......... 76% 31.4M 10s
384900K .......... .......... .......... .......... .......... 76%  100M 10s
384950K .......... .......... .......... .......... .......... 76% 20.5M 10s
385000K .......... .......... .......... .......... .......... 76% 19.8M 10s
385050K .......... .......... .......... .......... .......... 76% 42.3M 10s
385100K .......... .......... .......... .......... .......... 76% 26.2M 10s
385150K .......... .......... .......... .......... .......... 76% 24.0M 10s
385200K .......... .......... .......... .......... .......... 76% 23.3M 10s
385250K .......... .......... .......... .......... .......... 76% 28.7M 10s
385300K .......... .......... .......... .......... .......... 76% 25.7M 10s
385350K .......... .......... .......... .......... .......... 76% 20.7M 10s
385400K .......... .......... .......... .......... .......... 76% 24.1M 10s
385450K .......... .......... .......... .......... .......... 76% 23.0M 10s
385500K .......... .......... .......... .......... .......... 76% 30.9M 10s
385550K .......... .......... .......... .......... .......... 76% 23.4M 10s
385600K .......... .......... .......... .......... .......... 76% 19.2M 10s
385650K .......... .......... .......... .......... .......... 76% 21.1M 10s
385700K .......... .......... .......... .......... .......... 76% 20.2M 10s
385750K .......... .......... .......... .......... .......... 76% 22.1M 10s
385800K .......... .......... .......... .......... .......... 76% 30.2M 10s
385850K .......... .......... .......... .......... .......... 76% 23.9M 10s
385900K .......... .......... .......... .......... .......... 76% 20.7M 10s
385950K .......... .......... .......... .......... .......... 76% 22.9M 10s
386000K .......... .......... .......... .......... .......... 76% 12.8M 10s
386050K .......... .......... .......... .......... .......... 76% 17.8M 10s
386100K .......... .......... .......... .......... .......... 76% 70.2M 10s
386150K .......... .......... .......... .......... .......... 76% 25.2M 10s
386200K .......... .......... .......... .......... .......... 76% 15.3M 10s
386250K .......... .......... .......... .......... .......... 76% 20.3M 10s
386300K .......... .......... .......... .......... .......... 76% 15.9M 10s
386350K .......... .......... .......... .......... .......... 76% 17.2M 10s
386400K .......... .......... .......... .......... .......... 76% 20.6M 10s
386450K .......... .......... .......... .......... .......... 76% 15.4M 10s
386500K .......... .......... .......... .......... .......... 76% 21.1M 10s
386550K .......... .......... .......... .......... .......... 76% 15.2M 10s
386600K .......... .......... .......... .......... .......... 76% 22.3M 10s
386650K .......... .......... .......... .......... .......... 76% 13.7M 10s
386700K .......... .......... .......... .......... .......... 76% 21.2M 10s
386750K .......... .......... .......... .......... .......... 76% 16.9M 10s
386800K .......... .......... .......... .......... .......... 76% 24.3M 10s
386850K .......... .......... .......... .......... .......... 76% 28.1M 10s
386900K .......... .......... .......... .......... .......... 76% 24.6M 10s
386950K .......... .......... .......... .......... .......... 76% 65.9M 10s
387000K .......... .......... .......... .......... .......... 76% 14.7M 10s
387050K .......... .......... .......... .......... .......... 76%  156M 10s
387100K .......... .......... .......... .......... .......... 76% 20.7M 10s
387150K .......... .......... .......... .......... .......... 76% 69.4M 10s
387200K .......... .......... .......... .......... .......... 76% 26.7M 10s
387250K .......... .......... .......... .......... .......... 76% 24.4M 10s
387300K .......... .......... .......... .......... .......... 76% 40.3M 10s
387350K .......... .......... .......... .......... .......... 76% 23.0M 10s
387400K .......... .......... .......... .......... .......... 76% 22.3M 10s
387450K .......... .......... .......... .......... .......... 76% 26.1M 10s
387500K .......... .......... .......... .......... .......... 76% 30.5M 10s
387550K .......... .......... .......... .......... .......... 76% 32.1M 10s
387600K .......... .......... .......... .......... .......... 76% 22.8M 10s
387650K .......... .......... .......... .......... .......... 76% 29.6M 10s
387700K .......... .......... .......... .......... .......... 76% 26.5M 10s
387750K .......... .......... .......... .......... .......... 76% 42.9M 10s
387800K .......... .......... .......... .......... .......... 76% 22.3M 10s
387850K .......... .......... .......... .......... .......... 76% 24.5M 10s
387900K .......... .......... .......... .......... .......... 76% 45.3M 10s
387950K .......... .......... .......... .......... .......... 76% 21.0M 10s
388000K .......... .......... .......... .......... .......... 76% 18.7M 10s
388050K .......... .......... .......... .......... .......... 76% 36.0M 10s
388100K .......... .......... .......... .......... .......... 76% 23.2M 10s
388150K .......... .......... .......... .......... .......... 76% 32.3M 10s
388200K .......... .......... .......... .......... .......... 76% 21.3M 10s
388250K .......... .......... .......... .......... .......... 76% 9.11M 10s
388300K .......... .......... .......... .......... .......... 76%  110M 10s
388350K .......... .......... .......... .......... .......... 76%  103M 10s
388400K .......... .......... .......... .......... .......... 76% 26.7M 10s
388450K .......... .......... .......... .......... .......... 76% 18.7M 10s
388500K .......... .......... .......... .......... .......... 76%  179M 10s
388550K .......... .......... .......... .......... .......... 76% 50.9M 10s
388600K .......... .......... .......... .......... .......... 76% 26.9M 10s
388650K .......... .......... .......... .......... .......... 76% 28.7M 10s
388700K .......... .......... .......... .......... .......... 76% 23.0M 10s
388750K .......... .......... .......... .......... .......... 77% 28.3M 10s
388800K .......... .......... .......... .......... .......... 77% 40.6M 10s
388850K .......... .......... .......... .......... .......... 77% 28.0M 10s
388900K .......... .......... .......... .......... .......... 77% 26.1M 10s
388950K .......... .......... .......... .......... .......... 77% 23.2M 10s
389000K .......... .......... .......... .......... .......... 77% 39.9M 10s
389050K .......... .......... .......... .......... .......... 77% 26.6M 10s
389100K .......... .......... .......... .......... .......... 77% 33.3M 10s
389150K .......... .......... .......... .......... .......... 77% 28.9M 10s
389200K .......... .......... .......... .......... .......... 77% 27.7M 10s
389250K .......... .......... .......... .......... .......... 77% 37.2M 10s
389300K .......... .......... .......... .......... .......... 77% 27.3M 10s
389350K .......... .......... .......... .......... .......... 77% 24.0M 10s
389400K .......... .......... .......... .......... .......... 77% 25.2M 10s
389450K .......... .......... .......... .......... .......... 77% 22.0M 10s
389500K .......... .......... .......... .......... .......... 77% 32.9M 10s
389550K .......... .......... .......... .......... .......... 77% 29.2M 10s
389600K .......... .......... .......... .......... .......... 77% 12.6M 10s
389650K .......... .......... .......... .......... .......... 77%  105M 10s
389700K .......... .......... .......... .......... .......... 77% 15.0M 10s
389750K .......... .......... .......... .......... .......... 77%  233M 10s
389800K .......... .......... .......... .......... .......... 77% 29.8M 10s
389850K .......... .......... .......... .......... .......... 77% 26.7M 10s
389900K .......... .......... .......... .......... .......... 77% 26.2M 10s
389950K .......... .......... .......... .......... .......... 77% 23.0M 10s
390000K .......... .......... .......... .......... .......... 77% 42.8M 10s
390050K .......... .......... .......... .......... .......... 77% 22.3M 10s
390100K .......... .......... .......... .......... .......... 77% 25.6M 10s
390150K .......... .......... .......... .......... .......... 77% 22.1M 10s
390200K .......... .......... .......... .......... .......... 77% 44.6M 10s
390250K .......... .......... .......... .......... .......... 77% 26.5M 10s
390300K .......... .......... .......... .......... .......... 77% 30.6M 10s
390350K .......... .......... .......... .......... .......... 77% 31.1M 10s
390400K .......... .......... .......... .......... .......... 77% 24.2M 10s
390450K .......... .......... .......... .......... .......... 77% 29.1M 10s
390500K .......... .......... .......... .......... .......... 77% 32.8M 10s
390550K .......... .......... .......... .......... .......... 77% 34.2M 10s
390600K .......... .......... .......... .......... .......... 77% 28.5M 10s
390650K .......... .......... .......... .......... .......... 77% 33.7M 10s
390700K .......... .......... .......... .......... .......... 77% 18.5M 10s
390750K .......... .......... .......... .......... .......... 77% 30.7M 10s
390800K .......... .......... .......... .......... .......... 77% 38.0M 10s
390850K .......... .......... .......... .......... .......... 77% 22.2M 10s
390900K .......... .......... .......... .......... .......... 77% 40.8M 10s
390950K .......... .......... .......... .......... .......... 77% 19.9M 10s
391000K .......... .......... .......... .......... .......... 77% 37.8M 10s
391050K .......... .......... .......... .......... .......... 77% 30.8M 10s
391100K .......... .......... .......... .......... .......... 77% 25.1M 10s
391150K .......... .......... .......... .......... .......... 77% 22.1M 10s
391200K .......... .......... .......... .......... .......... 77% 30.6M 10s
391250K .......... .......... .......... .......... .......... 77% 39.3M 10s
391300K .......... .......... .......... .......... .......... 77% 30.6M 10s
391350K .......... .......... .......... .......... .......... 77% 16.5M 10s
391400K .......... .......... .......... .......... .......... 77% 29.0M 10s
391450K .......... .......... .......... .......... .......... 77%  140M 10s
391500K .......... .......... .......... .......... .......... 77%  147M 9s
391550K .......... .......... .......... .......... .......... 77% 38.0M 9s
391600K .......... .......... .......... .......... .......... 77% 18.0M 9s
391650K .......... .......... .......... .......... .......... 77% 39.4M 9s
391700K .......... .......... .......... .......... .......... 77% 50.3M 9s
391750K .......... .......... .......... .......... .......... 77% 35.1M 9s
391800K .......... .......... .......... .......... .......... 77% 40.6M 9s
391850K .......... .......... .......... .......... .......... 77% 23.9M 9s
391900K .......... .......... .......... .......... .......... 77% 26.1M 9s
391950K .......... .......... .......... .......... .......... 77% 29.3M 9s
392000K .......... .......... .......... .......... .......... 77% 27.2M 9s
392050K .......... .......... .......... .......... .......... 77% 38.6M 9s
392100K .......... .......... .......... .......... .......... 77% 24.4M 9s
392150K .......... .......... .......... .......... .......... 77% 29.8M 9s
392200K .......... .......... .......... .......... .......... 77% 28.4M 9s
392250K .......... .......... .......... .......... .......... 77% 34.8M 9s
392300K .......... .......... .......... .......... .......... 77% 27.6M 9s
392350K .......... .......... .......... .......... .......... 77% 27.3M 9s
392400K .......... .......... .......... .......... .......... 77% 32.8M 9s
392450K .......... .......... .......... .......... .......... 77% 23.1M 9s
392500K .......... .......... .......... .......... .......... 77% 31.1M 9s
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392650K .......... .......... .......... .......... .......... 77% 36.3M 9s
392700K .......... .......... .......... .......... .......... 77% 19.4M 9s
392750K .......... .......... .......... .......... .......... 77% 23.5M 9s
392800K .......... .......... .......... .......... .......... 77% 16.2M 9s
392850K .......... .......... .......... .......... .......... 77% 22.0M 9s
392900K .......... .......... .......... .......... .......... 77% 21.3M 9s
392950K .......... .......... .......... .......... .......... 77% 50.5M 9s
393000K .......... .......... .......... .......... .......... 77% 31.3M 9s
393050K .......... .......... .......... .......... .......... 77% 27.4M 9s
393100K .......... .......... .......... .......... .......... 77% 20.6M 9s
393150K .......... .......... .......... .......... .......... 77% 21.0M 9s
393200K .......... .......... .......... .......... .......... 77% 19.2M 9s
393250K .......... .......... .......... .......... .......... 77% 24.7M 9s
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393350K .......... .......... .......... .......... .......... 77% 21.0M 9s
393400K .......... .......... .......... .......... .......... 77% 23.5M 9s
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393550K .......... .......... .......... .......... .......... 77% 20.0M 9s
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393650K .......... .......... .......... .......... .......... 77% 20.0M 9s
393700K .......... .......... .......... .......... .......... 77% 18.8M 9s
393750K .......... .......... .......... .......... .......... 77% 26.9M 9s
393800K .......... .......... .......... .......... .......... 78% 24.4M 9s
393850K .......... .......... .......... .......... .......... 78% 6.63M 9s
393900K .......... .......... .......... .......... .......... 78% 42.2M 9s
393950K .......... .......... .......... .......... .......... 78% 26.4M 9s
394000K .......... .......... .......... .......... .......... 78% 13.6M 9s
394050K .......... .......... .......... .......... .......... 78% 57.5M 9s
394100K .......... .......... .......... .......... .......... 78% 20.8M 9s
394150K .......... .......... .......... .......... .......... 78% 24.9M 9s
394200K .......... .......... .......... .......... .......... 78% 25.0M 9s
394250K .......... .......... .......... .......... .......... 78% 22.7M 9s
394300K .......... .......... .......... .......... .......... 78% 20.2M 9s
394350K .......... .......... .......... .......... .......... 78% 33.2M 9s
394400K .......... .......... .......... .......... .......... 78% 20.8M 9s
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394550K .......... .......... .......... .......... .......... 78% 21.0M 9s
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394700K .......... .......... .......... .......... .......... 78% 28.7M 9s
394750K .......... .......... .......... .......... .......... 78% 22.5M 9s
394800K .......... .......... .......... .......... .......... 78% 21.9M 9s
394850K .......... .......... .......... .......... .......... 78% 19.8M 9s
394900K .......... .......... .......... .......... .......... 78% 24.9M 9s
394950K .......... .......... .......... .......... .......... 78% 12.0M 9s
395000K .......... .......... .......... .......... .......... 78% 21.2M 9s
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395100K .......... .......... .......... .......... .......... 78% 49.5M 9s
395150K .......... .......... .......... .......... .......... 78% 19.7M 9s
395200K .......... .......... .......... .......... .......... 78% 20.4M 9s
395250K .......... .......... .......... .......... .......... 78% 17.8M 9s
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395400K .......... .......... .......... .......... .......... 78% 16.8M 9s
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395500K .......... .......... .......... .......... .......... 78% 24.7M 9s
395550K .......... .......... .......... .......... .......... 78% 19.3M 9s
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395650K .......... .......... .......... .......... .......... 78% 19.1M 9s
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396000K .......... .......... .......... .......... .......... 78%  119M 9s
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396250K .......... .......... .......... .......... .......... 78% 31.3M 9s
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397000K .......... .......... .......... .......... .......... 78% 35.0M 9s
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397100K .......... .......... .......... .......... .......... 78% 51.5M 9s
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397250K .......... .......... .......... .......... .......... 78%  111M 9s
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397450K .......... .......... .......... .......... .......... 78% 78.1M 9s
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398000K .......... .......... .......... .......... .......... 78% 38.7M 9s
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398200K .......... .......... .......... .......... .......... 78% 35.6M 9s
398250K .......... .......... .......... .......... .......... 78% 32.3M 9s
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398850K .......... .......... .......... .......... .......... 79% 41.5M 9s
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399000K .......... .......... .......... .......... .......... 79% 43.0M 9s
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399100K .......... .......... .......... .......... .......... 79% 62.4M 9s
399150K .......... .......... .......... .......... .......... 79%  104M 9s
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399300K .......... .......... .......... .......... .......... 79%  142M 9s
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399400K .......... .......... .......... .......... .......... 79% 39.9M 9s
399450K .......... .......... .......... .......... .......... 79% 66.8M 9s
399500K .......... .......... .......... .......... .......... 79% 89.9M 9s
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399600K .......... .......... .......... .......... .......... 79%  136M 9s
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399700K .......... .......... .......... .......... .......... 79% 40.2M 9s
399750K .......... .......... .......... .......... .......... 79% 46.2M 9s
399800K .......... .......... .......... .......... .......... 79% 35.0M 9s
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400000K .......... .......... .......... .......... .......... 79% 43.2M 9s
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401300K .......... .......... .......... .......... .......... 79%  137M 9s
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401400K .......... .......... .......... .......... .......... 79% 32.5M 9s
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401500K .......... .......... .......... .......... .......... 79% 33.4M 9s
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401800K .......... .......... .......... .......... .......... 79% 33.0M 9s
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402000K .......... .......... .......... .......... .......... 79% 16.6M 8s
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402150K .......... .......... .......... .......... .......... 79% 33.6M 8s
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402250K .......... .......... .......... .......... .......... 79% 32.0M 8s
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402500K .......... .......... .......... .......... .......... 79% 34.1M 8s
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402750K .......... .......... .......... .......... .......... 79% 74.3M 8s
402800K .......... .......... .......... .......... .......... 79% 68.4M 8s
402850K .......... .......... .......... .......... .......... 79% 25.2M 8s
402900K .......... .......... .......... .......... .......... 79%  166M 8s
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403000K .......... .......... .......... .......... .......... 79% 91.8M 8s
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403150K .......... .......... .......... .......... .......... 79% 36.9M 8s
403200K .......... .......... .......... .......... .......... 79% 32.9M 8s
403250K .......... .......... .......... .......... .......... 79% 31.4M 8s
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403400K .......... .......... .......... .......... .......... 79% 37.2M 8s
403450K .......... .......... .......... .......... .......... 79% 27.6M 8s
403500K .......... .......... .......... .......... .......... 79% 34.2M 8s
403550K .......... .......... .......... .......... .......... 79% 36.2M 8s
403600K .......... .......... .......... .......... .......... 79% 22.6M 8s
403650K .......... .......... .......... .......... .......... 79% 33.6M 8s
403700K .......... .......... .......... .......... .......... 79% 30.9M 8s
403750K .......... .......... .......... .......... .......... 79% 42.3M 8s
403800K .......... .......... .......... .......... .......... 79% 25.8M 8s
403850K .......... .......... .......... .......... .......... 79% 35.0M 8s
403900K .......... .......... .......... .......... .......... 80% 42.0M 8s
403950K .......... .......... .......... .......... .......... 80% 30.0M 8s
404000K .......... .......... .......... .......... .......... 80% 40.2M 8s
404050K .......... .......... .......... .......... .......... 80% 33.4M 8s
404100K .......... .......... .......... .......... .......... 80% 32.1M 8s
404150K .......... .......... .......... .......... .......... 80% 35.4M 8s
404200K .......... .......... .......... .......... .......... 80% 22.7M 8s
404250K .......... .......... .......... .......... .......... 80%  117M 8s
404300K .......... .......... .......... .......... .......... 80% 15.1M 8s
404350K .......... .......... .......... .......... .......... 80% 18.4M 8s
404400K .......... .......... .......... .......... .......... 80%  195M 8s
404450K .......... .......... .......... .......... .......... 80% 27.2M 8s
404500K .......... .......... .......... .......... .......... 80% 20.2M 8s
404550K .......... .......... .......... .......... .......... 80% 22.8M 8s
404600K .......... .......... .......... .......... .......... 80% 19.9M 8s
404650K .......... .......... .......... .......... .......... 80% 21.6M 8s
404700K .......... .......... .......... .......... .......... 80% 18.8M 8s
404750K .......... .......... .......... .......... .......... 80% 23.7M 8s
404800K .......... .......... .......... .......... .......... 80% 26.5M 8s
404850K .......... .......... .......... .......... .......... 80% 21.6M 8s
404900K .......... .......... .......... .......... .......... 80% 23.5M 8s
404950K .......... .......... .......... .......... .......... 80% 16.9M 8s
405000K .......... .......... .......... .......... .......... 80% 29.4M 8s
405050K .......... .......... .......... .......... .......... 80% 20.0M 8s
405100K .......... .......... .......... .......... .......... 80% 18.7M 8s
405150K .......... .......... .......... .......... .......... 80% 30.5M 8s
405200K .......... .......... .......... .......... .......... 80% 20.3M 8s
405250K .......... .......... .......... .......... .......... 80% 21.5M 8s
405300K .......... .......... .......... .......... .......... 80% 22.2M 8s
405350K .......... .......... .......... .......... .......... 80% 21.2M 8s
405400K .......... .......... .......... .......... .......... 80% 22.5M 8s
405450K .......... .......... .......... .......... .......... 80% 17.1M 8s
405500K .......... .......... .......... .......... .......... 80% 36.8M 8s
405550K .......... .......... .......... .......... .......... 80% 18.3M 8s
405600K .......... .......... .......... .......... .......... 80% 19.1M 8s
405650K .......... .......... .......... .......... .......... 80% 59.0M 8s
405700K .......... .......... .......... .......... .......... 80% 17.4M 8s
405750K .......... .......... .......... .......... .......... 80% 27.1M 8s
405800K .......... .......... .......... .......... .......... 80% 26.4M 8s
405850K .......... .......... .......... .......... .......... 80% 18.9M 8s
405900K .......... .......... .......... .......... .......... 80% 24.1M 8s
405950K .......... .......... .......... .......... .......... 80% 19.2M 8s
406000K .......... .......... .......... .......... .......... 80% 31.6M 8s
406050K .......... .......... .......... .......... .......... 80% 20.1M 8s
406100K .......... .......... .......... .......... .......... 80% 20.0M 8s
406150K .......... .......... .......... .......... .......... 80% 20.1M 8s
406200K .......... .......... .......... .......... .......... 80% 21.2M 8s
406250K .......... .......... .......... .......... .......... 80% 23.6M 8s
406300K .......... .......... .......... .......... .......... 80% 18.9M 8s
406350K .......... .......... .......... .......... .......... 80% 17.5M 8s
406400K .......... .......... .......... .......... .......... 80% 16.6M 8s
406450K .......... .......... .......... .......... .......... 80% 26.9M 8s
406500K .......... .......... .......... .......... .......... 80% 32.3M 8s
406550K .......... .......... .......... .......... .......... 80% 87.8M 8s
406600K .......... .......... .......... .......... .......... 80% 37.2M 8s
406650K .......... .......... .......... .......... .......... 80% 39.7M 8s
406700K .......... .......... .......... .......... .......... 80% 25.4M 8s
406750K .......... .......... .......... .......... .......... 80% 75.0M 8s
406800K .......... .......... .......... .......... .......... 80% 50.3M 8s
406850K .......... .......... .......... .......... .......... 80% 31.9M 8s
406900K .......... .......... .......... .......... .......... 80% 36.8M 8s
406950K .......... .......... .......... .......... .......... 80% 18.9M 8s
407000K .......... .......... .......... .......... .......... 80% 17.4M 8s
407050K .......... .......... .......... .......... .......... 80% 20.4M 8s
407100K .......... .......... .......... .......... .......... 80% 38.4M 8s
407150K .......... .......... .......... .......... .......... 80% 17.8M 8s
407200K .......... .......... .......... .......... .......... 80% 18.3M 8s
407250K .......... .......... .......... .......... .......... 80% 16.8M 8s
407300K .......... .......... .......... .......... .......... 80% 20.0M 8s
407350K .......... .......... .......... .......... .......... 80% 14.9M 8s
407400K .......... .......... .......... .......... .......... 80% 21.7M 8s
407450K .......... .......... .......... .......... .......... 80% 16.5M 8s
407500K .......... .......... .......... .......... .......... 80% 22.2M 8s
407550K .......... .......... .......... .......... .......... 80% 21.5M 8s
407600K .......... .......... .......... .......... .......... 80% 14.6M 8s
407650K .......... .......... .......... .......... .......... 80% 19.5M 8s
407700K .......... .......... .......... .......... .......... 80% 21.0M 8s
407750K .......... .......... .......... .......... .......... 80% 22.7M 8s
407800K .......... .......... .......... .......... .......... 80% 31.4M 8s
407850K .......... .......... .......... .......... .......... 80% 70.4M 8s
407900K .......... .......... .......... .......... .......... 80% 19.9M 8s
407950K .......... .......... .......... .......... .......... 80% 38.7M 8s
408000K .......... .......... .......... .......... .......... 80%  110M 8s
408050K .......... .......... .......... .......... .......... 80% 48.7M 8s
408100K .......... .......... .......... .......... .......... 80% 36.4M 8s
408150K .......... .......... .......... .......... .......... 80% 48.6M 8s
408200K .......... .......... .......... .......... .......... 80% 26.8M 8s
408250K .......... .......... .......... .......... .......... 80% 43.4M 8s
408300K .......... .......... .......... .......... .......... 80% 44.7M 8s
408350K .......... .......... .......... .......... .......... 80% 35.7M 8s
408400K .......... .......... .......... .......... .......... 80% 39.9M 8s
408450K .......... .......... .......... .......... .......... 80% 28.9M 8s
408500K .......... .......... .......... .......... .......... 80% 38.7M 8s
408550K .......... .......... .......... .......... .......... 80% 42.9M 8s
408600K .......... .......... .......... .......... .......... 80% 27.6M 8s
408650K .......... .......... .......... .......... .......... 80% 43.9M 8s
408700K .......... .......... .......... .......... .......... 80% 30.2M 8s
408750K .......... .......... .......... .......... .......... 80% 38.2M 8s
408800K .......... .......... .......... .......... .......... 80% 49.8M 8s
408850K .......... .......... .......... .......... .......... 80% 34.9M 8s
408900K .......... .......... .......... .......... .......... 80% 53.4M 8s
408950K .......... .......... .......... .......... .......... 81% 28.9M 8s
409000K .......... .......... .......... .......... .......... 81% 41.3M 8s
409050K .......... .......... .......... .......... .......... 81% 47.0M 8s
409100K .......... .......... .......... .......... .......... 81% 29.2M 8s
409150K .......... .......... .......... .......... .......... 81% 56.4M 8s
409200K .......... .......... .......... .......... .......... 81% 8.09M 8s
409250K .......... .......... .......... .......... .......... 81% 39.3M 8s
409300K .......... .......... .......... .......... .......... 81%  129M 8s
409350K .......... .......... .......... .......... .......... 81% 29.7M 8s
409400K .......... .......... .......... .......... .......... 81% 14.9M 8s
409450K .......... .......... .......... .......... .......... 81%  173M 8s
409500K .......... .......... .......... .......... .......... 81% 17.4M 8s
409550K .......... .......... .......... .......... .......... 81%  179M 8s
409600K .......... .......... .......... .......... .......... 81%  155M 8s
409650K .......... .......... .......... .......... .......... 81%  146M 8s
409700K .......... .......... .......... .......... .......... 81% 39.7M 8s
409750K .......... .......... .......... .......... .......... 81% 50.5M 8s
409800K .......... .......... .......... .......... .......... 81%  158M 8s
409850K .......... .......... .......... .......... .......... 81% 30.4M 8s
409900K .......... .......... .......... .......... .......... 81%  105M 8s
409950K .......... .......... .......... .......... .......... 81% 26.7M 8s
410000K .......... .......... .......... .......... .......... 81% 31.1M 8s
410050K .......... .......... .......... .......... .......... 81% 31.9M 8s
410100K .......... .......... .......... .......... .......... 81% 26.7M 8s
410150K .......... .......... .......... .......... .......... 81% 33.7M 8s
410200K .......... .......... .......... .......... .......... 81% 23.5M 8s
410250K .......... .......... .......... .......... .......... 81% 41.7M 8s
410300K .......... .......... .......... .......... .......... 81% 23.9M 8s
410350K .......... .......... .......... .......... .......... 81% 23.6M 8s
410400K .......... .......... .......... .......... .......... 81% 39.8M 8s
410450K .......... .......... .......... .......... .......... 81% 22.9M 8s
410500K .......... .......... .......... .......... .......... 81% 41.8M 8s
410550K .......... .......... .......... .......... .......... 81% 27.3M 8s
410600K .......... .......... .......... .......... .......... 81% 31.1M 8s
410650K .......... .......... .......... .......... .......... 81% 26.2M 8s
410700K .......... .......... .......... .......... .......... 81% 34.3M 8s
410750K .......... .......... .......... .......... .......... 81% 24.5M 8s
410800K .......... .......... .......... .......... .......... 81% 37.2M 8s
410850K .......... .......... .......... .......... .......... 81% 22.8M 8s
410900K .......... .......... .......... .......... .......... 81% 34.3M 8s
410950K .......... .......... .......... .......... .......... 81% 41.2M 8s
411000K .......... .......... .......... .......... .......... 81% 72.8M 8s
411050K .......... .......... .......... .......... .......... 81% 54.1M 8s
411100K .......... .......... .......... .......... .......... 81%  101M 8s
411150K .......... .......... .......... .......... .......... 81% 46.4M 8s
411200K .......... .......... .......... .......... .......... 81% 21.6M 8s
411250K .......... .......... .......... .......... .......... 81% 89.3M 8s
411300K .......... .......... .......... .......... .......... 81% 81.1M 8s
411350K .......... .......... .......... .......... .......... 81% 73.3M 8s
411400K .......... .......... .......... .......... .......... 81% 76.8M 8s
411450K .......... .......... .......... .......... .......... 81% 29.8M 8s
411500K .......... .......... .......... .......... .......... 81%  233M 8s
411550K .......... .......... .......... .......... .......... 81%  271M 8s
411600K .......... .......... .......... .......... .......... 81% 36.3M 8s
411650K .......... .......... .......... .......... .......... 81% 39.1M 8s
411700K .......... .......... .......... .......... .......... 81% 31.0M 8s
411750K .......... .......... .......... .......... .......... 81% 33.4M 8s
411800K .......... .......... .......... .......... .......... 81% 41.2M 8s
411850K .......... .......... .......... .......... .......... 81% 26.7M 8s
411900K .......... .......... .......... .......... .......... 81% 28.8M 8s
411950K .......... .......... .......... .......... .......... 81% 29.8M 8s
412000K .......... .......... .......... .......... .......... 81% 19.4M 8s
412050K .......... .......... .......... .......... .......... 81% 50.4M 8s
412100K .......... .......... .......... .......... .......... 81% 26.5M 8s
412150K .......... .......... .......... .......... .......... 81% 35.3M 8s
412200K .......... .......... .......... .......... .......... 81% 30.4M 8s
412250K .......... .......... .......... .......... .......... 81% 28.2M 8s
412300K .......... .......... .......... .......... .......... 81% 41.1M 8s
412350K .......... .......... .......... .......... .......... 81% 28.9M 8s
412400K .......... .......... .......... .......... .......... 81% 43.1M 8s
412450K .......... .......... .......... .......... .......... 81% 26.6M 8s
412500K .......... .......... .......... .......... .......... 81% 42.6M 8s
412550K .......... .......... .......... .......... .......... 81% 26.9M 7s
412600K .......... .......... .......... .......... .......... 81% 20.1M 7s
412650K .......... .......... .......... .......... .......... 81% 21.9M 7s
412700K .......... .......... .......... .......... .......... 81% 13.4M 7s
412750K .......... .......... .......... .......... .......... 81% 62.5M 7s
412800K .......... .......... .......... .......... .......... 81% 41.0M 7s
412850K .......... .......... .......... .......... .......... 81% 34.4M 7s
412900K .......... .......... .......... .......... .......... 81% 27.6M 7s
412950K .......... .......... .......... .......... .......... 81% 23.6M 7s
413000K .......... .......... .......... .......... .......... 81% 26.8M 7s
413050K .......... .......... .......... .......... .......... 81% 26.4M 7s
413100K .......... .......... .......... .......... .......... 81% 29.0M 7s
413150K .......... .......... .......... .......... .......... 81% 31.8M 7s
413200K .......... .......... .......... .......... .......... 81% 18.6M 7s
413250K .......... .......... .......... .......... .......... 81% 34.4M 7s
413300K .......... .......... .......... .......... .......... 81% 24.8M 7s
413350K .......... .......... .......... .......... .......... 81% 22.0M 7s
413400K .......... .......... .......... .......... .......... 81% 34.0M 7s
413450K .......... .......... .......... .......... .......... 81% 18.8M 7s
413500K .......... .......... .......... .......... .......... 81% 37.9M 7s
413550K .......... .......... .......... .......... .......... 81% 25.5M 7s
413600K .......... .......... .......... .......... .......... 81% 24.6M 7s
413650K .......... .......... .......... .......... .......... 81% 30.9M 7s
413700K .......... .......... .......... .......... .......... 81% 25.0M 7s
413750K .......... .......... .......... .......... .......... 81% 21.0M 7s
413800K .......... .......... .......... .......... .......... 81% 39.2M 7s
413850K .......... .......... .......... .......... .......... 81% 22.6M 7s
413900K .......... .......... .......... .......... .......... 81% 8.51M 7s
413950K .......... .......... .......... .......... .......... 81%  117M 7s
414000K .......... .......... .......... .......... .......... 82%  157M 7s
414050K .......... .......... .......... .......... .......... 82% 35.1M 7s
414100K .......... .......... .......... .......... .......... 82% 39.1M 7s
414150K .......... .......... .......... .......... .......... 82% 17.9M 7s
414200K .......... .......... .......... .......... .......... 82% 20.3M 7s
414250K .......... .......... .......... .......... .......... 82% 19.9M 7s
414300K .......... .......... .......... .......... .......... 82% 19.8M 7s
414350K .......... .......... .......... .......... .......... 82% 19.0M 7s
414400K .......... .......... .......... .......... .......... 82% 17.8M 7s
414450K .......... .......... .......... .......... .......... 82% 20.8M 7s
414500K .......... .......... .......... .......... .......... 82% 22.6M 7s
414550K .......... .......... .......... .......... .......... 82% 16.7M 7s
414600K .......... .......... .......... .......... .......... 82% 18.9M 7s
414650K .......... .......... .......... .......... .......... 82% 19.1M 7s
414700K .......... .......... .......... .......... .......... 82% 17.4M 7s
414750K .......... .......... .......... .......... .......... 82% 20.2M 7s
414800K .......... .......... .......... .......... .......... 82% 20.4M 7s
414850K .......... .......... .......... .......... .......... 82% 16.0M 7s
414900K .......... .......... .......... .......... .......... 82% 26.8M 7s
414950K .......... .......... .......... .......... .......... 82% 14.9M 7s
415000K .......... .......... .......... .......... .......... 82% 21.2M 7s
415050K .......... .......... .......... .......... .......... 82% 36.3M 7s
415100K .......... .......... .......... .......... .......... 82% 20.5M 7s
415150K .......... .......... .......... .......... .......... 82% 21.0M 7s
415200K .......... .......... .......... .......... .......... 82% 21.9M 7s
415250K .......... .......... .......... .......... .......... 82% 24.5M 7s
415300K .......... .......... .......... .......... .......... 82% 24.2M 7s
415350K .......... .......... .......... .......... .......... 82% 14.0M 7s
415400K .......... .......... .......... .......... .......... 82% 24.3M 7s
415450K .......... .......... .......... .......... .......... 82% 23.5M 7s
415500K .......... .......... .......... .......... .......... 82% 23.9M 7s
415550K .......... .......... .......... .......... .......... 82% 24.3M 7s
415600K .......... .......... .......... .......... .......... 82% 17.2M 7s
415650K .......... .......... .......... .......... .......... 82% 27.9M 7s
415700K .......... .......... .......... .......... .......... 82% 16.6M 7s
415750K .......... .......... .......... .......... .......... 82% 37.7M 7s
415800K .......... .......... .......... .......... .......... 82% 22.6M 7s
415850K .......... .......... .......... .......... .......... 82% 20.5M 7s
415900K .......... .......... .......... .......... .......... 82% 17.6M 7s
415950K .......... .......... .......... .......... .......... 82% 28.9M 7s
416000K .......... .......... .......... .......... .......... 82% 16.9M 7s
416050K .......... .......... .......... .......... .......... 82% 31.0M 7s
416100K .......... .......... .......... .......... .......... 82% 17.1M 7s
416150K .......... .......... .......... .......... .......... 82% 16.5M 7s
416200K .......... .......... .......... .......... .......... 82% 24.1M 7s
416250K .......... .......... .......... .......... .......... 82% 21.2M 7s
416300K .......... .......... .......... .......... .......... 82% 20.6M 7s
416350K .......... .......... .......... .......... .......... 82% 16.2M 7s
416400K .......... .......... .......... .......... .......... 82% 19.5M 7s
416450K .......... .......... .......... .......... .......... 82% 19.6M 7s
416500K .......... .......... .......... .......... .......... 82% 17.5M 7s
416550K .......... .......... .......... .......... .......... 82% 20.7M 7s
416600K .......... .......... .......... .......... .......... 82% 16.1M 7s
416650K .......... .......... .......... .......... .......... 82% 24.9M 7s
416700K .......... .......... .......... .......... .......... 82% 14.6M 7s
416750K .......... .......... .......... .......... .......... 82% 26.3M 7s
416800K .......... .......... .......... .......... .......... 82% 17.7M 7s
416850K .......... .......... .......... .......... .......... 82% 17.5M 7s
416900K .......... .......... .......... .......... .......... 82% 19.3M 7s
416950K .......... .......... .......... .......... .......... 82% 22.6M 7s
417000K .......... .......... .......... .......... .......... 82% 23.4M 7s
417050K .......... .......... .......... .......... .......... 82% 25.6M 7s
417100K .......... .......... .......... .......... .......... 82% 23.1M 7s
417150K .......... .......... .......... .......... .......... 82% 17.8M 7s
417200K .......... .......... .......... .......... .......... 82% 47.4M 7s
417250K .......... .......... .......... .......... .......... 82% 27.6M 7s
417300K .......... .......... .......... .......... .......... 82% 25.1M 7s
417350K .......... .......... .......... .......... .......... 82% 13.7M 7s
417400K .......... .......... .......... .......... .......... 82% 21.3M 7s
417450K .......... .......... .......... .......... .......... 82% 14.5M 7s
417500K .......... .......... .......... .......... .......... 82% 25.7M 7s
417550K .......... .......... .......... .......... .......... 82% 24.4M 7s
417600K .......... .......... .......... .......... .......... 82% 21.1M 7s
417650K .......... .......... .......... .......... .......... 82% 22.9M 7s
417700K .......... .......... .......... .......... .......... 82% 20.1M 7s
417750K .......... .......... .......... .......... .......... 82% 24.9M 7s
417800K .......... .......... .......... .......... .......... 82% 20.5M 7s
417850K .......... .......... .......... .......... .......... 82% 18.3M 7s
417900K .......... .......... .......... .......... .......... 82% 19.9M 7s
417950K .......... .......... .......... .......... .......... 82% 20.1M 7s
418000K .......... .......... .......... .......... .......... 82% 14.7M 7s
418050K .......... .......... .......... .......... .......... 82% 61.3M 7s
418100K .......... .......... .......... .......... .......... 82% 11.2M 7s
418150K .......... .......... .......... .......... .......... 82% 11.9M 7s
418200K .......... .......... .......... .......... .......... 82% 29.4M 7s
418250K .......... .......... .......... .......... .......... 82% 18.9M 7s
418300K .......... .......... .......... .......... .......... 82% 17.0M 7s
418350K .......... .......... .......... .......... .......... 82% 13.4M 7s
418400K .......... .......... .......... .......... .......... 82% 19.2M 7s
418450K .......... .......... .......... .......... .......... 82% 14.3M 7s
418500K .......... .......... .......... .......... .......... 82% 18.6M 7s
418550K .......... .......... .......... .......... .......... 82% 16.4M 7s
418600K .......... .......... .......... .......... .......... 82% 20.8M 7s
418650K .......... .......... .......... .......... .......... 82% 15.2M 7s
418700K .......... .......... .......... .......... .......... 82% 15.2M 7s
418750K .......... .......... .......... .......... .......... 82% 16.8M 7s
418800K .......... .......... .......... .......... .......... 82% 19.3M 7s
418850K .......... .......... .......... .......... .......... 82% 28.3M 7s
418900K .......... .......... .......... .......... .......... 82% 43.6M 7s
418950K .......... .......... .......... .......... .......... 82% 27.8M 7s
419000K .......... .......... .......... .......... .......... 82% 81.7M 7s
419050K .......... .......... .......... .......... .......... 83% 12.8M 7s
419100K .......... .......... .......... .......... .......... 83% 20.1M 7s
419150K .......... .......... .......... .......... .......... 83% 43.0M 7s
419200K .......... .......... .......... .......... .......... 83% 28.6M 7s
419250K .......... .......... .......... .......... .......... 83% 18.6M 7s
419300K .......... .......... .......... .......... .......... 83% 31.7M 7s
419350K .......... .......... .......... .......... .......... 83% 22.1M 7s
419400K .......... .......... .......... .......... .......... 83% 24.1M 7s
419450K .......... .......... .......... .......... .......... 83% 25.3M 7s
419500K .......... .......... .......... .......... .......... 83% 23.9M 7s
419550K .......... .......... .......... .......... .......... 83% 19.8M 7s
419600K .......... .......... .......... .......... .......... 83% 19.5M 7s
419650K .......... .......... .......... .......... .......... 83% 25.1M 7s
419700K .......... .......... .......... .......... .......... 83% 16.6M 7s
419750K .......... .......... .......... .......... .......... 83% 26.1M 7s
419800K .......... .......... .......... .......... .......... 83% 22.8M 7s
419850K .......... .......... .......... .......... .......... 83% 17.2M 7s
419900K .......... .......... .......... .......... .......... 83% 24.2M 7s
419950K .......... .......... .......... .......... .......... 83% 20.3M 7s
420000K .......... .......... .......... .......... .......... 83% 21.8M 7s
420050K .......... .......... .......... .......... .......... 83% 18.1M 7s
420100K .......... .......... .......... .......... .......... 83% 22.7M 7s
420150K .......... .......... .......... .......... .......... 83% 56.5M 7s
420200K .......... .......... .......... .......... .......... 83% 15.4M 7s
420250K .......... .......... .......... .......... .......... 83% 39.8M 7s
420300K .......... .......... .......... .......... .......... 83% 26.3M 7s
420350K .......... .......... .......... .......... .......... 83% 29.3M 7s
420400K .......... .......... .......... .......... .......... 83% 16.0M 7s
420450K .......... .......... .......... .......... .......... 83% 15.8M 7s
420500K .......... .......... .......... .......... .......... 83% 20.2M 7s
420550K .......... .......... .......... .......... .......... 83% 22.6M 7s
420600K .......... .......... .......... .......... .......... 83% 19.7M 7s
420650K .......... .......... .......... .......... .......... 83% 22.8M 7s
420700K .......... .......... .......... .......... .......... 83% 15.5M 7s
420750K .......... .......... .......... .......... .......... 83% 19.6M 7s
420800K .......... .......... .......... .......... .......... 83% 27.2M 7s
420850K .......... .......... .......... .......... .......... 83% 17.2M 7s
420900K .......... .......... .......... .......... .......... 83% 23.1M 7s
420950K .......... .......... .......... .......... .......... 83% 20.4M 7s
421000K .......... .......... .......... .......... .......... 83% 19.0M 7s
421050K .......... .......... .......... .......... .......... 83% 22.2M 7s
421100K .......... .......... .......... .......... .......... 83% 19.3M 7s
421150K .......... .......... .......... .......... .......... 83% 17.1M 7s
421200K .......... .......... .......... .......... .......... 83% 20.0M 7s
421250K .......... .......... .......... .......... .......... 83% 32.9M 7s
421300K .......... .......... .......... .......... .......... 83% 30.7M 7s
421350K .......... .......... .......... .......... .......... 83% 38.8M 7s
421400K .......... .......... .......... .......... .......... 83% 13.6M 7s
421450K .......... .......... .......... .......... .......... 83% 24.3M 7s
421500K .......... .......... .......... .......... .......... 83% 82.3M 7s
421550K .......... .......... .......... .......... .......... 83% 35.7M 7s
421600K .......... .......... .......... .......... .......... 83% 65.2M 7s
421650K .......... .......... .......... .......... .......... 83% 33.9M 7s
421700K .......... .......... .......... .......... .......... 83% 25.0M 7s
421750K .......... .......... .......... .......... .......... 83% 43.7M 7s
421800K .......... .......... .......... .......... .......... 83% 28.2M 7s
421850K .......... .......... .......... .......... .......... 83% 28.0M 7s
421900K .......... .......... .......... .......... .......... 83% 32.9M 7s
421950K .......... .......... .......... .......... .......... 83% 21.8M 7s
422000K .......... .......... .......... .......... .......... 83% 43.7M 7s
422050K .......... .......... .......... .......... .......... 83% 39.4M 7s
422100K .......... .......... .......... .......... .......... 83% 27.5M 7s
422150K .......... .......... .......... .......... .......... 83% 32.2M 7s
422200K .......... .......... .......... .......... .......... 83% 30.9M 7s
422250K .......... .......... .......... .......... .......... 83% 40.0M 7s
422300K .......... .......... .......... .......... .......... 83% 27.3M 7s
422350K .......... .......... .......... .......... .......... 83% 28.6M 7s
422400K .......... .......... .......... .......... .......... 83% 31.9M 7s
422450K .......... .......... .......... .......... .......... 83% 39.3M 7s
422500K .......... .......... .......... .......... .......... 83% 25.2M 7s
422550K .......... .......... .......... .......... .......... 83% 52.6M 7s
422600K .......... .......... .......... .......... .......... 83% 25.8M 7s
422650K .......... .......... .......... .......... .......... 83% 33.6M 7s
422700K .......... .......... .......... .......... .......... 83% 21.8M 7s
422750K .......... .......... .......... .......... .......... 83% 15.5M 7s
422800K .......... .......... .......... .......... .......... 83% 22.4M 7s
422850K .......... .......... .......... .......... .......... 83% 19.9M 7s
422900K .......... .......... .......... .......... .......... 83% 43.9M 7s
422950K .......... .......... .......... .......... .......... 83% 23.8M 7s
423000K .......... .......... .......... .......... .......... 83% 23.2M 7s
423050K .......... .......... .......... .......... .......... 83% 27.3M 7s
423100K .......... .......... .......... .......... .......... 83% 27.6M 7s
423150K .......... .......... .......... .......... .......... 83% 32.2M 7s
423200K .......... .......... .......... .......... .......... 83% 22.7M 7s
423250K .......... .......... .......... .......... .......... 83% 22.0M 7s
423300K .......... .......... .......... .......... .......... 83% 24.2M 7s
423350K .......... .......... .......... .......... .......... 83% 19.3M 7s
423400K .......... .......... .......... .......... .......... 83% 19.9M 7s
423450K .......... .......... .......... .......... .......... 83% 19.4M 7s
423500K .......... .......... .......... .......... .......... 83% 21.9M 7s
423550K .......... .......... .......... .......... .......... 83% 24.5M 7s
423600K .......... .......... .......... .......... .......... 83% 24.1M 7s
423650K .......... .......... .......... .......... .......... 83% 25.6M 7s
423700K .......... .......... .......... .......... .......... 83% 17.6M 7s
423750K .......... .......... .......... .......... .......... 83% 18.2M 7s
423800K .......... .......... .......... .......... .......... 83% 20.7M 7s
423850K .......... .......... .......... .......... .......... 83% 25.4M 6s
423900K .......... .......... .......... .......... .......... 83% 23.8M 6s
423950K .......... .......... .......... .......... .......... 83% 20.8M 6s
424000K .......... .......... .......... .......... .......... 83% 17.9M 6s
424050K .......... .......... .......... .......... .......... 83%  178M 6s
424100K .......... .......... .......... .......... .......... 84% 34.1M 6s
424150K .......... .......... .......... .......... .......... 84% 40.0M 6s
424200K .......... .......... .......... .......... .......... 84% 18.9M 6s
424250K .......... .......... .......... .......... .......... 84% 46.4M 6s
424300K .......... .......... .......... .......... .......... 84% 25.2M 6s
424350K .......... .......... .......... .......... .......... 84% 21.7M 6s
424400K .......... .......... .......... .......... .......... 84% 37.5M 6s
424450K .......... .......... .......... .......... .......... 84% 18.8M 6s
424500K .......... .......... .......... .......... .......... 84% 28.0M 6s
424550K .......... .......... .......... .......... .......... 84% 16.4M 6s
424600K .......... .......... .......... .......... .......... 84% 19.1M 6s
424650K .......... .......... .......... .......... .......... 84% 38.3M 6s
424700K .......... .......... .......... .......... .......... 84% 20.9M 6s
424750K .......... .......... .......... .......... .......... 84% 29.7M 6s
424800K .......... .......... .......... .......... .......... 84% 22.9M 6s
424850K .......... .......... .......... .......... .......... 84% 28.0M 6s
424900K .......... .......... .......... .......... .......... 84% 28.5M 6s
424950K .......... .......... .......... .......... .......... 84% 27.5M 6s
425000K .......... .......... .......... .......... .......... 84% 22.0M 6s
425050K .......... .......... .......... .......... .......... 84% 59.9M 6s
425100K .......... .......... .......... .......... .......... 84% 28.4M 6s
425150K .......... .......... .......... .......... .......... 84% 17.8M 6s
425200K .......... .......... .......... .......... .......... 84%  127M 6s
425250K .......... .......... .......... .......... .......... 84% 56.6M 6s
425300K .......... .......... .......... .......... .......... 84%  257M 6s
425350K .......... .......... .......... .......... .......... 84% 26.3M 6s
425400K .......... .......... .......... .......... .......... 84%  236M 6s
425450K .......... .......... .......... .......... .......... 84% 25.1M 6s
425500K .......... .......... .......... .......... .......... 84% 52.4M 6s
425550K .......... .......... .......... .......... .......... 84% 36.0M 6s
425600K .......... .......... .......... .......... .......... 84% 26.1M 6s
425650K .......... .......... .......... .......... .......... 84% 37.3M 6s
425700K .......... .......... .......... .......... .......... 84% 26.6M 6s
425750K .......... .......... .......... .......... .......... 84% 40.0M 6s
425800K .......... .......... .......... .......... .......... 84% 32.1M 6s
425850K .......... .......... .......... .......... .......... 84% 35.9M 6s
425900K .......... .......... .......... .......... .......... 84% 24.9M 6s
425950K .......... .......... .......... .......... .......... 84% 37.0M 6s
426000K .......... .......... .......... .......... .......... 84% 33.6M 6s
426050K .......... .......... .......... .......... .......... 84% 31.4M 6s
426100K .......... .......... .......... .......... .......... 84% 24.3M 6s
426150K .......... .......... .......... .......... .......... 84% 35.4M 6s
426200K .......... .......... .......... .......... .......... 84% 41.1M 6s
426250K .......... .......... .......... .......... .......... 84% 26.0M 6s
426300K .......... .......... .......... .......... .......... 84% 37.7M 6s
426350K .......... .......... .......... .......... .......... 84% 26.2M 6s
426400K .......... .......... .......... .......... .......... 84% 40.7M 6s
426450K .......... .......... .......... .......... .......... 84% 27.1M 6s
426500K .......... .......... .......... .......... .......... 84% 39.9M 6s
426550K .......... .......... .......... .......... .......... 84% 35.7M 6s
426600K .......... .......... .......... .......... .......... 84% 34.0M 6s
426650K .......... .......... .......... .......... .......... 84% 8.95M 6s
426700K .......... .......... .......... .......... .......... 84%  142M 6s
426750K .......... .......... .......... .......... .......... 84%  249M 6s
426800K .......... .......... .......... .......... .......... 84%  279M 6s
426850K .......... .......... .......... .......... .......... 84% 24.5M 6s
426900K .......... .......... .......... .......... .......... 84%  237M 6s
426950K .......... .......... .......... .......... .......... 84%  226M 6s
427000K .......... .......... .......... .......... .......... 84% 75.6M 6s
427050K .......... .......... .......... .......... .......... 84% 46.1M 6s
427100K .......... .......... .......... .......... .......... 84% 39.6M 6s
427150K .......... .......... .......... .......... .......... 84% 66.7M 6s
427200K .......... .......... .......... .......... .......... 84% 43.8M 6s
427250K .......... .......... .......... .......... .......... 84% 51.5M 6s
427300K .......... .......... .......... .......... .......... 84% 50.7M 6s
427350K .......... .......... .......... .......... .......... 84% 45.6M 6s
427400K .......... .......... .......... .......... .......... 84% 49.9M 6s
427450K .......... .......... .......... .......... .......... 84% 43.7M 6s
427500K .......... .......... .......... .......... .......... 84% 51.6M 6s
427550K .......... .......... .......... .......... .......... 84% 58.7M 6s
427600K .......... .......... .......... .......... .......... 84% 50.8M 6s
427650K .......... .......... .......... .......... .......... 84% 50.8M 6s
427700K .......... .......... .......... .......... .......... 84% 47.2M 6s
427750K .......... .......... .......... .......... .......... 84% 64.5M 6s
427800K .......... .......... .......... .......... .......... 84% 45.3M 6s
427850K .......... .......... .......... .......... .......... 84% 50.3M 6s
427900K .......... .......... .......... .......... .......... 84% 55.3M 6s
427950K .......... .......... .......... .......... .......... 84% 52.8M 6s
428000K .......... .......... .......... .......... .......... 84% 49.3M 6s
428050K .......... .......... .......... .......... .......... 84% 51.0M 6s
428100K .......... .......... .......... .......... .......... 84% 43.8M 6s
428150K .......... .......... .......... .......... .......... 84% 80.6M 6s
428200K .......... .......... .......... .......... .......... 84% 33.1M 6s
428250K .......... .......... .......... .......... .......... 84% 78.9M 6s
428300K .......... .......... .......... .......... .......... 84% 43.0M 6s
428350K .......... .......... .......... .......... .......... 84% 35.8M 6s
428400K .......... .......... .......... .......... .......... 84% 39.2M 6s
428450K .......... .......... .......... .......... .......... 84% 64.0M 6s
428500K .......... .......... .......... .......... .......... 84% 39.9M 6s
428550K .......... .......... .......... .......... .......... 84% 58.6M 6s
428600K .......... .......... .......... .......... .......... 84% 41.7M 6s
428650K .......... .......... .......... .......... .......... 84% 46.9M 6s
428700K .......... .......... .......... .......... .......... 84% 72.4M 6s
428750K .......... .......... .......... .......... .......... 84% 55.9M 6s
428800K .......... .......... .......... .......... .......... 84% 86.0M 6s
428850K .......... .......... .......... .......... .......... 84% 19.2M 6s
428900K .......... .......... .......... .......... .......... 84%  190M 6s
428950K .......... .......... .......... .......... .......... 84% 23.4M 6s
429000K .......... .......... .......... .......... .......... 84%  152M 6s
429050K .......... .......... .......... .......... .......... 84%  191M 6s
429100K .......... .......... .......... .......... .......... 84%  180M 6s
429150K .......... .......... .......... .......... .......... 85%  162M 6s
429200K .......... .......... .......... .......... .......... 85%  117M 6s
429250K .......... .......... .......... .......... .......... 85%  162M 6s
429300K .......... .......... .......... .......... .......... 85% 32.1M 6s
429350K .......... .......... .......... .......... .......... 85% 41.7M 6s
429400K .......... .......... .......... .......... .......... 85% 64.7M 6s
429450K .......... .......... .......... .......... .......... 85%  109M 6s
429500K .......... .......... .......... .......... .......... 85% 45.0M 6s
429550K .......... .......... .......... .......... .......... 85% 32.6M 6s
429600K .......... .......... .......... .......... .......... 85% 41.9M 6s
429650K .......... .......... .......... .......... .......... 85% 42.7M 6s
429700K .......... .......... .......... .......... .......... 85% 38.6M 6s
429750K .......... .......... .......... .......... .......... 85% 48.2M 6s
429800K .......... .......... .......... .......... .......... 85% 39.1M 6s
429850K .......... .......... .......... .......... .......... 85% 31.3M 6s
429900K .......... .......... .......... .......... .......... 85% 39.1M 6s
429950K .......... .......... .......... .......... .......... 85% 34.2M 6s
430000K .......... .......... .......... .......... .......... 85% 36.9M 6s
430050K .......... .......... .......... .......... .......... 85% 45.8M 6s
430100K .......... .......... .......... .......... .......... 85% 34.2M 6s
430150K .......... .......... .......... .......... .......... 85% 41.7M 6s
430200K .......... .......... .......... .......... .......... 85% 36.3M 6s
430250K .......... .......... .......... .......... .......... 85% 30.0M 6s
430300K .......... .......... .......... .......... .......... 85% 48.9M 6s
430350K .......... .......... .......... .......... .......... 85% 46.4M 6s
430400K .......... .......... .......... .......... .......... 85% 36.9M 6s
430450K .......... .......... .......... .......... .......... 85% 39.3M 6s
430500K .......... .......... .......... .......... .......... 85% 38.1M 6s
430550K .......... .......... .......... .......... .......... 85% 41.2M 6s
430600K .......... .......... .......... .......... .......... 85% 38.4M 6s
430650K .......... .......... .......... .......... .......... 85% 45.7M 6s
430700K .......... .......... .......... .......... .......... 85% 35.0M 6s
430750K .......... .......... .......... .......... .......... 85% 38.9M 6s
430800K .......... .......... .......... .......... .......... 85% 47.7M 6s
430850K .......... .......... .......... .......... .......... 85% 27.6M 6s
430900K .......... .......... .......... .......... .......... 85% 44.6M 6s
430950K .......... .......... .......... .......... .......... 85% 26.5M 6s
431000K .......... .......... .......... .......... .......... 85% 18.8M 6s
431050K .......... .......... .......... .......... .......... 85%  178M 6s
431100K .......... .......... .......... .......... .......... 85%  116M 6s
431150K .......... .......... .......... .......... .......... 85% 17.2M 6s
431200K .......... .......... .......... .......... .......... 85%  104M 6s
431250K .......... .......... .......... .......... .......... 85%  103M 6s
431300K .......... .......... .......... .......... .......... 85% 29.9M 6s
431350K .......... .......... .......... .......... .......... 85% 56.2M 6s
431400K .......... .......... .......... .......... .......... 85% 25.4M 6s
431450K .......... .......... .......... .......... .......... 85% 22.1M 6s
431500K .......... .......... .......... .......... .......... 85% 32.1M 6s
431550K .......... .......... .......... .......... .......... 85% 24.3M 6s
431600K .......... .......... .......... .......... .......... 85% 24.6M 6s
431650K .......... .......... .......... .......... .......... 85% 21.6M 6s
431700K .......... .......... .......... .......... .......... 85% 22.3M 6s
431750K .......... .......... .......... .......... .......... 85% 40.3M 6s
431800K .......... .......... .......... .......... .......... 85% 20.8M 6s
431850K .......... .......... .......... .......... .......... 85% 18.5M 6s
431900K .......... .......... .......... .......... .......... 85% 27.7M 6s
431950K .......... .......... .......... .......... .......... 85% 24.2M 6s
432000K .......... .......... .......... .......... .......... 85% 23.4M 6s
432050K .......... .......... .......... .......... .......... 85% 31.6M 6s
432100K .......... .......... .......... .......... .......... 85% 27.8M 6s
432150K .......... .......... .......... .......... .......... 85% 23.4M 6s
432200K .......... .......... .......... .......... .......... 85% 19.4M 6s
432250K .......... .......... .......... .......... .......... 85% 42.0M 6s
432300K .......... .......... .......... .......... .......... 85% 31.7M 6s
432350K .......... .......... .......... .......... .......... 85% 11.3M 6s
432400K .......... .......... .......... .......... .......... 85% 43.6M 6s
432450K .......... .......... .......... .......... .......... 85% 38.3M 6s
432500K .......... .......... .......... .......... .......... 85% 66.4M 6s
432550K .......... .......... .......... .......... .......... 85% 42.9M 6s
432600K .......... .......... .......... .......... .......... 85% 38.2M 6s
432650K .......... .......... .......... .......... .......... 85% 31.9M 6s
432700K .......... .......... .......... .......... .......... 85% 41.0M 6s
432750K .......... .......... .......... .......... .......... 85% 16.6M 6s
432800K .......... .......... .......... .......... .......... 85% 36.9M 6s
432850K .......... .......... .......... .......... .......... 85% 27.4M 6s
432900K .......... .......... .......... .......... .......... 85% 43.0M 6s
432950K .......... .......... .......... .......... .......... 85% 33.0M 6s
433000K .......... .......... .......... .......... .......... 85% 39.3M 6s
433050K .......... .......... .......... .......... .......... 85% 26.0M 6s
433100K .......... .......... .......... .......... .......... 85% 35.3M 6s
433150K .......... .......... .......... .......... .......... 85% 43.7M 6s
433200K .......... .......... .......... .......... .......... 85% 30.7M 6s
433250K .......... .......... .......... .......... .......... 85% 43.1M 6s
433300K .......... .......... .......... .......... .......... 85% 33.0M 6s
433350K .......... .......... .......... .......... .......... 85% 38.9M 6s
433400K .......... .......... .......... .......... .......... 85% 25.1M 6s
433450K .......... .......... .......... .......... .......... 85% 40.9M 6s
433500K .......... .......... .......... .......... .......... 85% 41.1M 6s
433550K .......... .......... .......... .......... .......... 85% 39.4M 6s
433600K .......... .......... .......... .......... .......... 85% 35.2M 6s
433650K .......... .......... .......... .......... .......... 85% 35.4M 6s
433700K .......... .......... .......... .......... .......... 85% 29.2M 6s
433750K .......... .......... .......... .......... .......... 85% 51.4M 6s
433800K .......... .......... .......... .......... .......... 85% 47.5M 6s
433850K .......... .......... .......... .......... .......... 85% 52.2M 6s
433900K .......... .......... .......... .......... .......... 85% 17.1M 6s
433950K .......... .......... .......... .......... .......... 85%  215M 6s
434000K .......... .......... .......... .......... .......... 85% 41.9M 6s
434050K .......... .......... .......... .......... .......... 85%  218M 6s
434100K .......... .......... .......... .......... .......... 85%  168M 6s
434150K .......... .......... .......... .......... .......... 85% 28.6M 6s
434200K .......... .......... .......... .......... .......... 86% 74.7M 6s
434250K .......... .......... .......... .......... .......... 86% 62.5M 6s
434300K .......... .......... .......... .......... .......... 86% 73.5M 6s
434350K .......... .......... .......... .......... .......... 86% 47.5M 6s
434400K .......... .......... .......... .......... .......... 86% 44.6M 6s
434450K .......... .......... .......... .......... .......... 86% 42.6M 6s
434500K .......... .......... .......... .......... .......... 86% 46.7M 6s
434550K .......... .......... .......... .......... .......... 86% 41.5M 6s
434600K .......... .......... .......... .......... .......... 86% 48.2M 6s
434650K .......... .......... .......... .......... .......... 86% 41.3M 6s
434700K .......... .......... .......... .......... .......... 86% 42.2M 6s
434750K .......... .......... .......... .......... .......... 86% 46.2M 6s
434800K .......... .......... .......... .......... .......... 86% 44.0M 6s
434850K .......... .......... .......... .......... .......... 86% 51.2M 6s
434900K .......... .......... .......... .......... .......... 86% 45.2M 6s
434950K .......... .......... .......... .......... .......... 86% 34.5M 6s
435000K .......... .......... .......... .......... .......... 86% 49.0M 6s
435050K .......... .......... .......... .......... .......... 86% 35.5M 6s
435100K .......... .......... .......... .......... .......... 86% 44.1M 5s
435150K .......... .......... .......... .......... .......... 86% 56.2M 5s
435200K .......... .......... .......... .......... .......... 86% 34.1M 5s
435250K .......... .......... .......... .......... .......... 86% 53.9M 5s
435300K .......... .......... .......... .......... .......... 86% 41.9M 5s
435350K .......... .......... .......... .......... .......... 86% 35.6M 5s
435400K .......... .......... .......... .......... .......... 86% 48.9M 5s
435450K .......... .......... .......... .......... .......... 86% 38.8M 5s
435500K .......... .......... .......... .......... .......... 86% 49.1M 5s
435550K .......... .......... .......... .......... .......... 86% 45.7M 5s
435600K .......... .......... .......... .......... .......... 86% 34.8M 5s
435650K .......... .......... .......... .......... .......... 86% 38.1M 5s
435700K .......... .......... .......... .......... .......... 86% 43.6M 5s
435750K .......... .......... .......... .......... .......... 86% 38.1M 5s
435800K .......... .......... .......... .......... .......... 86% 37.1M 5s
435850K .......... .......... .......... .......... .......... 86% 36.2M 5s
435900K .......... .......... .......... .......... .......... 86% 13.9M 5s
435950K .......... .......... .......... .......... .......... 86% 27.0M 5s
436000K .......... .......... .......... .......... .......... 86% 80.7M 5s
436050K .......... .......... .......... .......... .......... 86% 46.2M 5s
436100K .......... .......... .......... .......... .......... 86% 23.6M 5s
436150K .......... .......... .......... .......... .......... 86% 22.9M 5s
436200K .......... .......... .......... .......... .......... 86% 16.7M 5s
436250K .......... .......... .......... .......... .......... 86% 23.6M 5s
436300K .......... .......... .......... .......... .......... 86% 19.9M 5s
436350K .......... .......... .......... .......... .......... 86% 14.4M 5s
436400K .......... .......... .......... .......... .......... 86% 24.3M 5s
436450K .......... .......... .......... .......... .......... 86% 14.2M 5s
436500K .......... .......... .......... .......... .......... 86% 24.4M 5s
436550K .......... .......... .......... .......... .......... 86% 16.9M 5s
436600K .......... .......... .......... .......... .......... 86% 20.0M 5s
436650K .......... .......... .......... .......... .......... 86% 16.2M 5s
436700K .......... .......... .......... .......... .......... 86% 17.1M 5s
436750K .......... .......... .......... .......... .......... 86% 15.5M 5s
436800K .......... .......... .......... .......... .......... 86% 22.6M 5s
436850K .......... .......... .......... .......... .......... 86% 30.1M 5s
436900K .......... .......... .......... .......... .......... 86% 14.9M 5s
436950K .......... .......... .......... .......... .......... 86% 20.0M 5s
437000K .......... .......... .......... .......... .......... 86% 52.8M 5s
437050K .......... .......... .......... .......... .......... 86% 15.8M 5s
437100K .......... .......... .......... .......... .......... 86% 18.7M 5s
437150K .......... .......... .......... .......... .......... 86% 13.8M 5s
437200K .......... .......... .......... .......... .......... 86% 17.0M 5s
437250K .......... .......... .......... .......... .......... 86% 14.5M 5s
437300K .......... .......... .......... .......... .......... 86% 16.7M 5s
437350K .......... .......... .......... .......... .......... 86% 10.9M 5s
437400K .......... .......... .......... .......... .......... 86% 23.5M 5s
437450K .......... .......... .......... .......... .......... 86% 10.9M 5s
437500K .......... .......... .......... .......... .......... 86% 13.7M 5s
437550K .......... .......... .......... .......... .......... 86% 19.2M 5s
437600K .......... .......... .......... .......... .......... 86% 14.2M 5s
437650K .......... .......... .......... .......... .......... 86% 26.0M 5s
437700K .......... .......... .......... .......... .......... 86% 12.0M 5s
437750K .......... .......... .......... .......... .......... 86% 25.6M 5s
437800K .......... .......... .......... .......... .......... 86% 19.7M 5s
437850K .......... .......... .......... .......... .......... 86% 14.5M 5s
437900K .......... .......... .......... .......... .......... 86% 13.8M 5s
437950K .......... .......... .......... .......... .......... 86% 15.2M 5s
438000K .......... .......... .......... .......... .......... 86% 15.8M 5s
438050K .......... .......... .......... .......... .......... 86% 14.3M 5s
438100K .......... .......... .......... .......... .......... 86% 12.8M 5s
438150K .......... .......... .......... .......... .......... 86% 11.4M 5s
438200K .......... .......... .......... .......... .......... 86% 14.2M 5s
438250K .......... .......... .......... .......... .......... 86% 14.4M 5s
438300K .......... .......... .......... .......... .......... 86% 15.8M 5s
438350K .......... .......... .......... .......... .......... 86% 10.2M 5s
438400K .......... .......... .......... .......... .......... 86% 17.8M 5s
438450K .......... .......... .......... .......... .......... 86% 17.5M 5s
438500K .......... .......... .......... .......... .......... 86% 18.9M 5s
438550K .......... .......... .......... .......... .......... 86% 34.2M 5s
438600K .......... .......... .......... .......... .......... 86% 19.4M 5s
438650K .......... .......... .......... .......... .......... 86% 39.2M 5s
438700K .......... .......... .......... .......... .......... 86% 21.1M 5s
438750K .......... .......... .......... .......... .......... 86% 28.1M 5s
438800K .......... .......... .......... .......... .......... 86% 29.9M 5s
438850K .......... .......... .......... .......... .......... 86% 20.1M 5s
438900K .......... .......... .......... .......... .......... 86% 23.9M 5s
438950K .......... .......... .......... .......... .......... 86% 26.0M 5s
439000K .......... .......... .......... .......... .......... 86% 23.3M 5s
439050K .......... .......... .......... .......... .......... 86% 21.3M 5s
439100K .......... .......... .......... .......... .......... 86% 21.7M 5s
439150K .......... .......... .......... .......... .......... 86% 32.8M 5s
439200K .......... .......... .......... .......... .......... 86% 18.4M 5s
439250K .......... .......... .......... .......... .......... 87% 22.8M 5s
439300K .......... .......... .......... .......... .......... 87% 23.6M 5s
439350K .......... .......... .......... .......... .......... 87% 23.2M 5s
439400K .......... .......... .......... .......... .......... 87% 38.9M 5s
439450K .......... .......... .......... .......... .......... 87% 32.9M 5s
439500K .......... .......... .......... .......... .......... 87% 86.3M 5s
439550K .......... .......... .......... .......... .......... 87% 32.8M 5s
439600K .......... .......... .......... .......... .......... 87% 14.2M 5s
439650K .......... .......... .......... .......... .......... 87%  198M 5s
439700K .......... .......... .......... .......... .......... 87%  160M 5s
439750K .......... .......... .......... .......... .......... 87% 36.4M 5s
439800K .......... .......... .......... .......... .......... 87% 43.3M 5s
439850K .......... .......... .......... .......... .......... 87% 37.3M 5s
439900K .......... .......... .......... .......... .......... 87%  109M 5s
439950K .......... .......... .......... .......... .......... 87% 21.5M 5s
440000K .......... .......... .......... .......... .......... 87%  153M 5s
440050K .......... .......... .......... .......... .......... 87% 41.9M 5s
440100K .......... .......... .......... .......... .......... 87% 29.1M 5s
440150K .......... .......... .......... .......... .......... 87% 44.1M 5s
440200K .......... .......... .......... .......... .......... 87% 35.5M 5s
440250K .......... .......... .......... .......... .......... 87% 45.1M 5s
440300K .......... .......... .......... .......... .......... 87% 32.3M 5s
440350K .......... .......... .......... .......... .......... 87% 46.4M 5s
440400K .......... .......... .......... .......... .......... 87% 46.1M 5s
440450K .......... .......... .......... .......... .......... 87% 26.0M 5s
440500K .......... .......... .......... .......... .......... 87% 50.8M 5s
440550K .......... .......... .......... .......... .......... 87% 45.0M 5s
440600K .......... .......... .......... .......... .......... 87% 31.3M 5s
440650K .......... .......... .......... .......... .......... 87% 40.6M 5s
440700K .......... .......... .......... .......... .......... 87% 34.2M 5s
440750K .......... .......... .......... .......... .......... 87% 37.1M 5s
440800K .......... .......... .......... .......... .......... 87% 52.3M 5s
440850K .......... .......... .......... .......... .......... 87% 37.3M 5s
440900K .......... .......... .......... .......... .......... 87% 29.7M 5s
440950K .......... .......... .......... .......... .......... 87% 23.0M 5s
441000K .......... .......... .......... .......... .......... 87% 43.8M 5s
441050K .......... .......... .......... .......... .......... 87% 48.6M 5s
441100K .......... .......... .......... .......... .......... 87% 37.6M 5s
441150K .......... .......... .......... .......... .......... 87% 35.7M 5s
441200K .......... .......... .......... .......... .......... 87% 36.1M 5s
441250K .......... .......... .......... .......... .......... 87% 37.1M 5s
441300K .......... .......... .......... .......... .......... 87% 38.4M 5s
441350K .......... .......... .......... .......... .......... 87% 35.9M 5s
441400K .......... .......... .......... .......... .......... 87% 70.9M 5s
441450K .......... .......... .......... .......... .......... 87% 39.9M 5s
441500K .......... .......... .......... .......... .......... 87%  112M 5s
441550K .......... .......... .......... .......... .......... 87% 19.9M 5s
441600K .......... .......... .......... .......... .......... 87% 88.6M 5s
441650K .......... .......... .......... .......... .......... 87% 80.0M 5s
441700K .......... .......... .......... .......... .......... 87% 54.2M 5s
441750K .......... .......... .......... .......... .......... 87% 62.4M 5s
441800K .......... .......... .......... .......... .......... 87%  109M 5s
441850K .......... .......... .......... .......... .......... 87% 47.6M 5s
441900K .......... .......... .......... .......... .......... 87%  144M 5s
441950K .......... .......... .......... .......... .......... 87% 22.2M 5s
442000K .......... .......... .......... .......... .......... 87%  151M 5s
442050K .......... .......... .......... .......... .......... 87% 38.5M 5s
442100K .......... .......... .......... .......... .......... 87% 18.9M 5s
442150K .......... .......... .......... .......... .......... 87% 41.0M 5s
442200K .......... .......... .......... .......... .......... 87% 31.1M 5s
442250K .......... .......... .......... .......... .......... 87% 28.6M 5s
442300K .......... .......... .......... .......... .......... 87% 35.1M 5s
442350K .......... .......... .......... .......... .......... 87% 21.9M 5s
442400K .......... .......... .......... .......... .......... 87% 40.5M 5s
442450K .......... .......... .......... .......... .......... 87% 16.4M 5s
442500K .......... .......... .......... .......... .......... 87% 35.5M 5s
442550K .......... .......... .......... .......... .......... 87% 38.7M 5s
442600K .......... .......... .......... .......... .......... 87% 20.3M 5s
442650K .......... .......... .......... .......... .......... 87% 32.2M 5s
442700K .......... .......... .......... .......... .......... 87% 31.4M 5s
442750K .......... .......... .......... .......... .......... 87% 21.8M 5s
442800K .......... .......... .......... .......... .......... 87% 37.5M 5s
442850K .......... .......... .......... .......... .......... 87% 34.2M 5s
442900K .......... .......... .......... .......... .......... 87% 22.3M 5s
442950K .......... .......... .......... .......... .......... 87% 36.7M 5s
443000K .......... .......... .......... .......... .......... 87% 24.2M 5s
443050K .......... .......... .......... .......... .......... 87% 41.4M 5s
443100K .......... .......... .......... .......... .......... 87% 35.9M 5s
443150K .......... .......... .......... .......... .......... 87% 38.1M 5s
443200K .......... .......... .......... .......... .......... 87% 18.6M 5s
443250K .......... .......... .......... .......... .......... 87%  138M 5s
443300K .......... .......... .......... .......... .......... 87% 23.8M 5s
443350K .......... .......... .......... .......... .......... 87%  161M 5s
443400K .......... .......... .......... .......... .......... 87%  139M 5s
443450K .......... .......... .......... .......... .......... 87% 75.0M 5s
443500K .......... .......... .......... .......... .......... 87% 80.2M 5s
443550K .......... .......... .......... .......... .......... 87% 79.9M 5s
443600K .......... .......... .......... .......... .......... 87% 71.1M 5s
443650K .......... .......... .......... .......... .......... 87% 94.3M 5s
443700K .......... .......... .......... .......... .......... 87% 29.0M 5s
443750K .......... .......... .......... .......... .......... 87% 28.2M 5s
443800K .......... .......... .......... .......... .......... 87% 32.4M 5s
443850K .......... .......... .......... .......... .......... 87% 35.8M 5s
443900K .......... .......... .......... .......... .......... 87% 33.0M 5s
443950K .......... .......... .......... .......... .......... 87% 27.7M 5s
444000K .......... .......... .......... .......... .......... 87% 39.4M 5s
444050K .......... .......... .......... .......... .......... 87% 25.8M 5s
444100K .......... .......... .......... .......... .......... 87% 25.6M 5s
444150K .......... .......... .......... .......... .......... 87% 38.7M 5s
444200K .......... .......... .......... .......... .......... 87% 28.7M 5s
444250K .......... .......... .......... .......... .......... 87% 30.6M 5s
444300K .......... .......... .......... .......... .......... 88% 35.0M 5s
444350K .......... .......... .......... .......... .......... 88% 26.3M 5s
444400K .......... .......... .......... .......... .......... 88% 40.6M 5s
444450K .......... .......... .......... .......... .......... 88% 23.7M 5s
444500K .......... .......... .......... .......... .......... 88% 34.4M 5s
444550K .......... .......... .......... .......... .......... 88% 27.5M 5s
444600K .......... .......... .......... .......... .......... 88% 35.2M 5s
444650K .......... .......... .......... .......... .......... 88% 24.3M 5s
444700K .......... .......... .......... .......... .......... 88% 31.0M 5s
444750K .......... .......... .......... .......... .......... 88% 32.4M 5s
444800K .......... .......... .......... .......... .......... 88% 38.3M 5s
444850K .......... .......... .......... .......... .......... 88% 32.7M 5s
444900K .......... .......... .......... .......... .......... 88% 30.5M 5s
444950K .......... .......... .......... .......... .......... 88% 39.8M 5s
445000K .......... .......... .......... .......... .......... 88% 19.8M 5s
445050K .......... .......... .......... .......... .......... 88%  125M 5s
445100K .......... .......... .......... .......... .......... 88% 27.6M 5s
445150K .......... .......... .......... .......... .......... 88% 88.1M 5s
445200K .......... .......... .......... .......... .......... 88% 23.9M 5s
445250K .......... .......... .......... .......... .......... 88%  109M 5s
445300K .......... .......... .......... .......... .......... 88% 28.8M 5s
445350K .......... .......... .......... .......... .......... 88% 30.5M 5s
445400K .......... .......... .......... .......... .......... 88% 33.6M 5s
445450K .......... .......... .......... .......... .......... 88% 29.1M 5s
445500K .......... .......... .......... .......... .......... 88% 41.4M 5s
445550K .......... .......... .......... .......... .......... 88% 29.0M 5s
445600K .......... .......... .......... .......... .......... 88% 34.6M 5s
445650K .......... .......... .......... .......... .......... 88% 40.2M 5s
445700K .......... .......... .......... .......... .......... 88% 23.3M 5s
445750K .......... .......... .......... .......... .......... 88% 42.1M 5s
445800K .......... .......... .......... .......... .......... 88% 37.7M 5s
445850K .......... .......... .......... .......... .......... 88% 25.0M 5s
445900K .......... .......... .......... .......... .......... 88% 36.5M 5s
445950K .......... .......... .......... .......... .......... 88% 33.4M 5s
446000K .......... .......... .......... .......... .......... 88% 28.3M 5s
446050K .......... .......... .......... .......... .......... 88% 25.0M 5s
446100K .......... .......... .......... .......... .......... 88% 41.7M 5s
446150K .......... .......... .......... .......... .......... 88% 29.2M 5s
446200K .......... .......... .......... .......... .......... 88% 31.7M 5s
446250K .......... .......... .......... .......... .......... 88% 22.8M 5s
446300K .......... .......... .......... .......... .......... 88% 36.8M 5s
446350K .......... .......... .......... .......... .......... 88% 38.7M 5s
446400K .......... .......... .......... .......... .......... 88% 29.5M 5s
446450K .......... .......... .......... .......... .......... 88% 22.3M 5s
446500K .......... .......... .......... .......... .......... 88% 93.5M 5s
446550K .......... .......... .......... .......... .......... 88% 12.7M 5s
446600K .......... .......... .......... .......... .......... 88%  100M 5s
446650K .......... .......... .......... .......... .......... 88% 36.2M 5s
446700K .......... .......... .......... .......... .......... 88% 39.8M 5s
446750K .......... .......... .......... .......... .......... 88% 29.3M 5s
446800K .......... .......... .......... .......... .......... 88% 80.0M 5s
446850K .......... .......... .......... .......... .......... 88% 23.6M 5s
446900K .......... .......... .......... .......... .......... 88% 27.3M 5s
446950K .......... .......... .......... .......... .......... 88% 25.7M 4s
447000K .......... .......... .......... .......... .......... 88% 19.7M 4s
447050K .......... .......... .......... .......... .......... 88% 23.2M 4s
447100K .......... .......... .......... .......... .......... 88% 17.1M 4s
447150K .......... .......... .......... .......... .......... 88% 19.6M 4s
447200K .......... .......... .......... .......... .......... 88% 22.2M 4s
447250K .......... .......... .......... .......... .......... 88% 20.9M 4s
447300K .......... .......... .......... .......... .......... 88% 24.3M 4s
447350K .......... .......... .......... .......... .......... 88% 16.0M 4s
447400K .......... .......... .......... .......... .......... 88% 21.6M 4s
447450K .......... .......... .......... .......... .......... 88% 21.1M 4s
447500K .......... .......... .......... .......... .......... 88% 23.1M 4s
447550K .......... .......... .......... .......... .......... 88% 25.2M 4s
447600K .......... .......... .......... .......... .......... 88% 14.1M 4s
447650K .......... .......... .......... .......... .......... 88% 20.8M 4s
447700K .......... .......... .......... .......... .......... 88% 19.6M 4s
447750K .......... .......... .......... .......... .......... 88% 28.3M 4s
447800K .......... .......... .......... .......... .......... 88% 20.8M 4s
447850K .......... .......... .......... .......... .......... 88% 59.1M 4s
447900K .......... .......... .......... .......... .......... 88% 15.3M 4s
447950K .......... .......... .......... .......... .......... 88% 21.1M 4s
448000K .......... .......... .......... .......... .......... 88% 24.0M 4s
448050K .......... .......... .......... .......... .......... 88% 17.2M 4s
448100K .......... .......... .......... .......... .......... 88% 4.74M 4s
448150K .......... .......... .......... .......... .......... 88% 11.5M 4s
448200K .......... .......... .......... .......... .......... 88% 10.9M 4s
448250K .......... .......... .......... .......... .......... 88% 13.0M 4s
448300K .......... .......... .......... .......... .......... 88% 13.1M 4s
448350K .......... .......... .......... .......... .......... 88% 9.46M 4s
448400K .......... .......... .......... .......... .......... 88% 17.6M 4s
448450K .......... .......... .......... .......... .......... 88% 26.0M 4s
448500K .......... .......... .......... .......... .......... 88% 20.9M 4s
448550K .......... .......... .......... .......... .......... 88% 18.8M 4s
448600K .......... .......... .......... .......... .......... 88% 20.5M 4s
448650K .......... .......... .......... .......... .......... 88% 26.4M 4s
448700K .......... .......... .......... .......... .......... 88% 19.4M 4s
448750K .......... .......... .......... .......... .......... 88% 23.6M 4s
448800K .......... .......... .......... .......... .......... 88% 21.6M 4s
448850K .......... .......... .......... .......... .......... 88% 18.3M 4s
448900K .......... .......... .......... .......... .......... 88% 23.0M 4s
448950K .......... .......... .......... .......... .......... 88% 20.8M 4s
449000K .......... .......... .......... .......... .......... 88% 23.6M 4s
449050K .......... .......... .......... .......... .......... 88% 19.4M 4s
449100K .......... .......... .......... .......... .......... 88% 17.5M 4s
449150K .......... .......... .......... .......... .......... 88% 23.7M 4s
449200K .......... .......... .......... .......... .......... 88% 15.4M 4s
449250K .......... .......... .......... .......... .......... 88% 25.1M 4s
449300K .......... .......... .......... .......... .......... 88% 19.1M 4s
449350K .......... .......... .......... .......... .......... 89% 22.4M 4s
449400K .......... .......... .......... .......... .......... 89% 28.6M 4s
449450K .......... .......... .......... .......... .......... 89% 20.8M 4s
449500K .......... .......... .......... .......... .......... 89% 9.30M 4s
449550K .......... .......... .......... .......... .......... 89% 20.9M 4s
449600K .......... .......... .......... .......... .......... 89%  173M 4s
449650K .......... .......... .......... .......... .......... 89% 29.5M 4s
449700K .......... .......... .......... .......... .......... 89% 18.3M 4s
449750K .......... .......... .......... .......... .......... 89% 15.8M 4s
449800K .......... .......... .......... .......... .......... 89% 18.1M 4s
449850K .......... .......... .......... .......... .......... 89% 16.8M 4s
449900K .......... .......... .......... .......... .......... 89% 14.1M 4s
449950K .......... .......... .......... .......... .......... 89% 15.5M 4s
450000K .......... .......... .......... .......... .......... 89% 18.3M 4s
450050K .......... .......... .......... .......... .......... 89% 27.0M 4s
450100K .......... .......... .......... .......... .......... 89% 13.0M 4s
450150K .......... .......... .......... .......... .......... 89% 15.8M 4s
450200K .......... .......... .......... .......... .......... 89% 16.3M 4s
450250K .......... .......... .......... .......... .......... 89% 15.9M 4s
450300K .......... .......... .......... .......... .......... 89% 22.5M 4s
450350K .......... .......... .......... .......... .......... 89% 15.7M 4s
450400K .......... .......... .......... .......... .......... 89% 37.3M 4s
450450K .......... .......... .......... .......... .......... 89% 12.6M 4s
450500K .......... .......... .......... .......... .......... 89% 18.5M 4s
450550K .......... .......... .......... .......... .......... 89% 34.6M 4s
450600K .......... .......... .......... .......... .......... 89% 15.4M 4s
450650K .......... .......... .......... .......... .......... 89% 21.8M 4s
450700K .......... .......... .......... .......... .......... 89% 14.1M 4s
450750K .......... .......... .......... .......... .......... 89% 15.4M 4s
450800K .......... .......... .......... .......... .......... 89% 13.7M 4s
450850K .......... .......... .......... .......... .......... 89% 13.8M 4s
450900K .......... .......... .......... .......... .......... 89% 23.1M 4s
450950K .......... .......... .......... .......... .......... 89% 14.6M 4s
451000K .......... .......... .......... .......... .......... 89% 16.5M 4s
451050K .......... .......... .......... .......... .......... 89% 21.3M 4s
451100K .......... .......... .......... .......... .......... 89% 14.9M 4s
451150K .......... .......... .......... .......... .......... 89% 13.8M 4s
451200K .......... .......... .......... .......... .......... 89% 14.7M 4s
451250K .......... .......... .......... .......... .......... 89% 16.1M 4s
451300K .......... .......... .......... .......... .......... 89% 22.0M 4s
451350K .......... .......... .......... .......... .......... 89% 19.7M 4s
451400K .......... .......... .......... .......... .......... 89% 34.3M 4s
451450K .......... .......... .......... .......... .......... 89% 22.2M 4s
451500K .......... .......... .......... .......... .......... 89% 10.4M 4s
451550K .......... .......... .......... .......... .......... 89%  151M 4s
451600K .......... .......... .......... .......... .......... 89% 35.7M 4s
451650K .......... .......... .......... .......... .......... 89% 21.3M 4s
451700K .......... .......... .......... .......... .......... 89% 23.4M 4s
451750K .......... .......... .......... .......... .......... 89% 21.4M 4s
451800K .......... .......... .......... .......... .......... 89% 23.2M 4s
451850K .......... .......... .......... .......... .......... 89% 14.9M 4s
451900K .......... .......... .......... .......... .......... 89% 21.7M 4s
451950K .......... .......... .......... .......... .......... 89% 22.6M 4s
452000K .......... .......... .......... .......... .......... 89% 18.1M 4s
452050K .......... .......... .......... .......... .......... 89% 25.9M 4s
452100K .......... .......... .......... .......... .......... 89% 19.4M 4s
452150K .......... .......... .......... .......... .......... 89% 18.4M 4s
452200K .......... .......... .......... .......... .......... 89% 16.0M 4s
452250K .......... .......... .......... .......... .......... 89% 24.4M 4s
452300K .......... .......... .......... .......... .......... 89% 22.5M 4s
452350K .......... .......... .......... .......... .......... 89% 19.4M 4s
452400K .......... .......... .......... .......... .......... 89% 18.8M 4s
452450K .......... .......... .......... .......... .......... 89% 17.0M 4s
452500K .......... .......... .......... .......... .......... 89% 56.4M 4s
452550K .......... .......... .......... .......... .......... 89% 22.6M 4s
452600K .......... .......... .......... .......... .......... 89% 20.7M 4s
452650K .......... .......... .......... .......... .......... 89% 41.1M 4s
452700K .......... .......... .......... .......... .......... 89% 16.4M 4s
452750K .......... .......... .......... .......... .......... 89% 26.5M 4s
452800K .......... .......... .......... .......... .......... 89% 26.1M 4s
452850K .......... .......... .......... .......... .......... 89% 18.6M 4s
452900K .......... .......... .......... .......... .......... 89% 20.4M 4s
452950K .......... .......... .......... .......... .......... 89% 19.9M 4s
453000K .......... .......... .......... .......... .......... 89% 22.6M 4s
453050K .......... .......... .......... .......... .......... 89% 18.8M 4s
453100K .......... .......... .......... .......... .......... 89% 24.2M 4s
453150K .......... .......... .......... .......... .......... 89% 15.0M 4s
453200K .......... .......... .......... .......... .......... 89% 21.6M 4s
453250K .......... .......... .......... .......... .......... 89% 20.2M 4s
453300K .......... .......... .......... .......... .......... 89% 24.1M 4s
453350K .......... .......... .......... .......... .......... 89% 18.1M 4s
453400K .......... .......... .......... .......... .......... 89% 19.8M 4s
453450K .......... .......... .......... .......... .......... 89% 18.1M 4s
453500K .......... .......... .......... .......... .......... 89% 21.5M 4s
453550K .......... .......... .......... .......... .......... 89% 19.1M 4s
453600K .......... .......... .......... .......... .......... 89% 20.9M 4s
453650K .......... .......... .......... .......... .......... 89% 43.9M 4s
453700K .......... .......... .......... .......... .......... 89% 19.4M 4s
453750K .......... .......... .......... .......... .......... 89% 26.9M 4s
453800K .......... .......... .......... .......... .......... 89%  171M 4s
453850K .......... .......... .......... .......... .......... 89%  132M 4s
453900K .......... .......... .......... .......... .......... 89% 31.0M 4s
453950K .......... .......... .......... .......... .......... 89% 23.1M 4s
454000K .......... .......... .......... .......... .......... 89% 28.2M 4s
454050K .......... .......... .......... .......... .......... 89% 24.9M 4s
454100K .......... .......... .......... .......... .......... 89% 24.6M 4s
454150K .......... .......... .......... .......... .......... 89% 25.0M 4s
454200K .......... .......... .......... .......... .......... 89% 24.5M 4s
454250K .......... .......... .......... .......... .......... 89% 21.8M 4s
454300K .......... .......... .......... .......... .......... 89% 23.4M 4s
454350K .......... .......... .......... .......... .......... 89% 25.1M 4s
454400K .......... .......... .......... .......... .......... 90% 28.6M 4s
454450K .......... .......... .......... .......... .......... 90% 25.6M 4s
454500K .......... .......... .......... .......... .......... 90% 25.6M 4s
454550K .......... .......... .......... .......... .......... 90% 26.6M 4s
454600K .......... .......... .......... .......... .......... 90% 24.7M 4s
454650K .......... .......... .......... .......... .......... 90% 27.4M 4s
454700K .......... .......... .......... .......... .......... 90% 19.9M 4s
454750K .......... .......... .......... .......... .......... 90% 23.6M 4s
454800K .......... .......... .......... .......... .......... 90% 41.1M 4s
454850K .......... .......... .......... .......... .......... 90% 27.3M 4s
454900K .......... .......... .......... .......... .......... 90% 27.5M 4s
454950K .......... .......... .......... .......... .......... 90% 12.2M 4s
455000K .......... .......... .......... .......... .......... 90%  191M 4s
455050K .......... .......... .......... .......... .......... 90%  247M 4s
455100K .......... .......... .......... .......... .......... 90% 26.0M 4s
455150K .......... .......... .......... .......... .......... 90% 48.7M 4s
455200K .......... .......... .......... .......... .......... 90% 32.3M 4s
455250K .......... .......... .......... .......... .......... 90% 25.3M 4s
455300K .......... .......... .......... .......... .......... 90% 21.2M 4s
455350K .......... .......... .......... .......... .......... 90% 23.0M 4s
455400K .......... .......... .......... .......... .......... 90% 38.8M 4s
455450K .......... .......... .......... .......... .......... 90% 17.9M 4s
455500K .......... .......... .......... .......... .......... 90% 32.9M 4s
455550K .......... .......... .......... .......... .......... 90% 23.9M 4s
455600K .......... .......... .......... .......... .......... 90% 16.9M 4s
455650K .......... .......... .......... .......... .......... 90% 21.9M 4s
455700K .......... .......... .......... .......... .......... 90% 20.4M 4s
455750K .......... .......... .......... .......... .......... 90% 30.3M 4s
455800K .......... .......... .......... .......... .......... 90% 38.8M 4s
455850K .......... .......... .......... .......... .......... 90% 23.0M 4s
455900K .......... .......... .......... .......... .......... 90% 23.8M 4s
455950K .......... .......... .......... .......... .......... 90% 21.3M 4s
456000K .......... .......... .......... .......... .......... 90% 22.8M 4s
456050K .......... .......... .......... .......... .......... 90% 43.6M 4s
456100K .......... .......... .......... .......... .......... 90% 14.5M 4s
456150K .......... .......... .......... .......... .......... 90%  125M 4s
456200K .......... .......... .......... .......... .......... 90% 13.6M 4s
456250K .......... .......... .......... .......... .......... 90% 23.1M 4s
456300K .......... .......... .......... .......... .......... 90% 22.5M 4s
456350K .......... .......... .......... .......... .......... 90% 27.7M 4s
456400K .......... .......... .......... .......... .......... 90% 23.9M 4s
456450K .......... .......... .......... .......... .......... 90% 21.7M 4s
456500K .......... .......... .......... .......... .......... 90% 20.9M 4s
456550K .......... .......... .......... .......... .......... 90% 28.4M 4s
456600K .......... .......... .......... .......... .......... 90% 21.9M 4s
456650K .......... .......... .......... .......... .......... 90% 19.0M 4s
456700K .......... .......... .......... .......... .......... 90% 14.4M 4s
456750K .......... .......... .......... .......... .......... 90% 23.1M 4s
456800K .......... .......... .......... .......... .......... 90% 39.6M 4s
456850K .......... .......... .......... .......... .......... 90% 19.2M 4s
456900K .......... .......... .......... .......... .......... 90% 21.4M 4s
456950K .......... .......... .......... .......... .......... 90% 17.4M 4s
457000K .......... .......... .......... .......... .......... 90% 22.8M 4s
457050K .......... .......... .......... .......... .......... 90% 24.0M 4s
457100K .......... .......... .......... .......... .......... 90% 18.5M 4s
457150K .......... .......... .......... .......... .......... 90% 31.9M 4s
457200K .......... .......... .......... .......... .......... 90% 16.1M 4s
457250K .......... .......... .......... .......... .......... 90% 57.8M 4s
457300K .......... .......... .......... .......... .......... 90% 18.1M 4s
457350K .......... .......... .......... .......... .......... 90% 55.9M 4s
457400K .......... .......... .......... .......... .......... 90% 30.8M 4s
457450K .......... .......... .......... .......... .......... 90% 47.3M 4s
457500K .......... .......... .......... .......... .......... 90% 19.7M 4s
457550K .......... .......... .......... .......... .......... 90% 28.5M 4s
457600K .......... .......... .......... .......... .......... 90% 28.1M 4s
457650K .......... .......... .......... .......... .......... 90% 24.6M 4s
457700K .......... .......... .......... .......... .......... 90% 19.9M 4s
457750K .......... .......... .......... .......... .......... 90% 26.2M 4s
457800K .......... .......... .......... .......... .......... 90% 19.4M 4s
457850K .......... .......... .......... .......... .......... 90% 19.7M 4s
457900K .......... .......... .......... .......... .......... 90% 27.2M 4s
457950K .......... .......... .......... .......... .......... 90% 15.6M 4s
458000K .......... .......... .......... .......... .......... 90% 19.4M 4s
458050K .......... .......... .......... .......... .......... 90% 19.0M 4s
458100K .......... .......... .......... .......... .......... 90% 26.0M 4s
458150K .......... .......... .......... .......... .......... 90% 24.1M 4s
458200K .......... .......... .......... .......... .......... 90% 25.1M 4s
458250K .......... .......... .......... .......... .......... 90% 21.7M 4s
458300K .......... .......... .......... .......... .......... 90% 21.6M 4s
458350K .......... .......... .......... .......... .......... 90% 20.8M 4s
458400K .......... .......... .......... .......... .......... 90% 31.4M 4s
458450K .......... .......... .......... .......... .......... 90% 28.9M 4s
458500K .......... .......... .......... .......... .......... 90% 22.6M 4s
458550K .......... .......... .......... .......... .......... 90% 37.1M 4s
458600K .......... .......... .......... .......... .......... 90% 24.0M 4s
458650K .......... .......... .......... .......... .......... 90%  183M 4s
458700K .......... .......... .......... .......... .......... 90% 25.1M 4s
458750K .......... .......... .......... .......... .......... 90% 25.4M 4s
458800K .......... .......... .......... .......... .......... 90%  168M 4s
458850K .......... .......... .......... .......... .......... 90% 23.9M 4s
458900K .......... .......... .......... .......... .......... 90% 28.6M 4s
458950K .......... .......... .......... .......... .......... 90% 23.8M 4s
459000K .......... .......... .......... .......... .......... 90% 34.7M 4s
459050K .......... .......... .......... .......... .......... 90% 27.8M 4s
459100K .......... .......... .......... .......... .......... 90% 22.4M 4s
459150K .......... .......... .......... .......... .......... 90% 33.4M 4s
459200K .......... .......... .......... .......... .......... 90% 21.8M 4s
459250K .......... .......... .......... .......... .......... 90% 29.6M 4s
459300K .......... .......... .......... .......... .......... 90% 28.0M 3s
459350K .......... .......... .......... .......... .......... 90% 22.8M 3s
459400K .......... .......... .......... .......... .......... 90% 22.1M 3s
459450K .......... .......... .......... .......... .......... 91% 39.7M 3s
459500K .......... .......... .......... .......... .......... 91% 22.2M 3s
459550K .......... .......... .......... .......... .......... 91% 21.8M 3s
459600K .......... .......... .......... .......... .......... 91% 20.8M 3s
459650K .......... .......... .......... .......... .......... 91% 21.6M 3s
459700K .......... .......... .......... .......... .......... 91% 37.5M 3s
459750K .......... .......... .......... .......... .......... 91% 25.4M 3s
459800K .......... .......... .......... .......... .......... 91% 30.0M 3s
459850K .......... .......... .......... .......... .......... 91% 31.2M 3s
459900K .......... .......... .......... .......... .......... 91% 50.7M 3s
459950K .......... .......... .......... .......... .......... 91% 19.9M 3s
460000K .......... .......... .......... .......... .......... 91%  163M 3s
460050K .......... .......... .......... .......... .......... 91% 19.3M 3s
460100K .......... .......... .......... .......... .......... 91% 49.2M 3s
460150K .......... .......... .......... .......... .......... 91% 39.3M 3s
460200K .......... .......... .......... .......... .......... 91% 45.4M 3s
460250K .......... .......... .......... .......... .......... 91% 26.3M 3s
460300K .......... .......... .......... .......... .......... 91% 21.4M 3s
460350K .......... .......... .......... .......... .......... 91% 26.3M 3s
460400K .......... .......... .......... .......... .......... 91% 21.3M 3s
460450K .......... .......... .......... .......... .......... 91% 20.3M 3s
460500K .......... .......... .......... .......... .......... 91% 21.0M 3s
460550K .......... .......... .......... .......... .......... 91% 22.5M 3s
460600K .......... .......... .......... .......... .......... 91% 17.1M 3s
460650K .......... .......... .......... .......... .......... 91% 21.5M 3s
460700K .......... .......... .......... .......... .......... 91% 19.2M 3s
460750K .......... .......... .......... .......... .......... 91% 33.7M 3s
460800K .......... .......... .......... .......... .......... 91% 19.6M 3s
460850K .......... .......... .......... .......... .......... 91% 22.5M 3s
460900K .......... .......... .......... .......... .......... 91% 20.4M 3s
460950K .......... .......... .......... .......... .......... 91% 17.0M 3s
461000K .......... .......... .......... .......... .......... 91% 34.7M 3s
461050K .......... .......... .......... .......... .......... 91% 31.8M 3s
461100K .......... .......... .......... .......... .......... 91% 7.86M 3s
461150K .......... .......... .......... .......... .......... 91%  143M 3s
461200K .......... .......... .......... .......... .......... 91%  121M 3s
461250K .......... .......... .......... .......... .......... 91% 44.1M 3s
461300K .......... .......... .......... .......... .......... 91% 31.2M 3s
461350K .......... .......... .......... .......... .......... 91% 19.1M 3s
461400K .......... .......... .......... .......... .......... 91% 27.6M 3s
461450K .......... .......... .......... .......... .......... 91% 16.1M 3s
461500K .......... .......... .......... .......... .......... 91% 21.0M 3s
461550K .......... .......... .......... .......... .......... 91% 22.0M 3s
461600K .......... .......... .......... .......... .......... 91% 18.4M 3s
461650K .......... .......... .......... .......... .......... 91% 22.8M 3s
461700K .......... .......... .......... .......... .......... 91% 19.8M 3s
461750K .......... .......... .......... .......... .......... 91% 25.2M 3s
461800K .......... .......... .......... .......... .......... 91% 19.6M 3s
461850K .......... .......... .......... .......... .......... 91% 21.8M 3s
461900K .......... .......... .......... .......... .......... 91% 18.7M 3s
461950K .......... .......... .......... .......... .......... 91% 18.9M 3s
462000K .......... .......... .......... .......... .......... 91% 24.4M 3s
462050K .......... .......... .......... .......... .......... 91% 19.8M 3s
462100K .......... .......... .......... .......... .......... 91% 24.3M 3s
462150K .......... .......... .......... .......... .......... 91% 32.8M 3s
462200K .......... .......... .......... .......... .......... 91% 40.4M 3s
462250K .......... .......... .......... .......... .......... 91% 15.2M 3s
462300K .......... .......... .......... .......... .......... 91%  132M 3s
462350K .......... .......... .......... .......... .......... 91% 22.6M 3s
462400K .......... .......... .......... .......... .......... 91% 47.9M 3s
462450K .......... .......... .......... .......... .......... 91% 44.9M 3s
462500K .......... .......... .......... .......... .......... 91% 22.0M 3s
462550K .......... .......... .......... .......... .......... 91% 26.8M 3s
462600K .......... .......... .......... .......... .......... 91% 22.9M 3s
462650K .......... .......... .......... .......... .......... 91% 27.1M 3s
462700K .......... .......... .......... .......... .......... 91% 19.0M 3s
462750K .......... .......... .......... .......... .......... 91% 24.1M 3s
462800K .......... .......... .......... .......... .......... 91% 23.3M 3s
462850K .......... .......... .......... .......... .......... 91% 19.3M 3s
462900K .......... .......... .......... .......... .......... 91% 23.2M 3s
462950K .......... .......... .......... .......... .......... 91% 20.3M 3s
463000K .......... .......... .......... .......... .......... 91% 21.1M 3s
463050K .......... .......... .......... .......... .......... 91% 21.4M 3s
463100K .......... .......... .......... .......... .......... 91% 21.6M 3s
463150K .......... .......... .......... .......... .......... 91% 24.9M 3s
463200K .......... .......... .......... .......... .......... 91% 27.0M 3s
463250K .......... .......... .......... .......... .......... 91% 22.3M 3s
463300K .......... .......... .......... .......... .......... 91% 86.7M 3s
463350K .......... .......... .......... .......... .......... 91% 11.9M 3s
463400K .......... .......... .......... .......... .......... 91% 26.0M 3s
463450K .......... .......... .......... .......... .......... 91% 15.3M 3s
463500K .......... .......... .......... .......... .......... 91%  152M 3s
463550K .......... .......... .......... .......... .......... 91%  121M 3s
463600K .......... .......... .......... .......... .......... 91%  103M 3s
463650K .......... .......... .......... .......... .......... 91% 43.2M 3s
463700K .......... .......... .......... .......... .......... 91% 26.4M 3s
463750K .......... .......... .......... .......... .......... 91% 34.8M 3s
463800K .......... .......... .......... .......... .......... 91% 29.0M 3s
463850K .......... .......... .......... .......... .......... 91% 21.1M 3s
463900K .......... .......... .......... .......... .......... 91% 37.9M 3s
463950K .......... .......... .......... .......... .......... 91% 25.9M 3s
464000K .......... .......... .......... .......... .......... 91% 36.4M 3s
464050K .......... .......... .......... .......... .......... 91% 24.3M 3s
464100K .......... .......... .......... .......... .......... 91% 25.3M 3s
464150K .......... .......... .......... .......... .......... 91% 36.5M 3s
464200K .......... .......... .......... .......... .......... 91% 24.9M 3s
464250K .......... .......... .......... .......... .......... 91% 36.8M 3s
464300K .......... .......... .......... .......... .......... 91% 28.8M 3s
464350K .......... .......... .......... .......... .......... 91% 21.9M 3s
464400K .......... .......... .......... .......... .......... 91% 33.7M 3s
464450K .......... .......... .......... .......... .......... 91% 23.8M 3s
464500K .......... .......... .......... .......... .......... 92% 36.0M 3s
464550K .......... .......... .......... .......... .......... 92% 23.7M 3s
464600K .......... .......... .......... .......... .......... 92% 23.9M 3s
464650K .......... .......... .......... .......... .......... 92% 10.4M 3s
464700K .......... .......... .......... .......... .......... 92%  186M 3s
464750K .......... .......... .......... .......... .......... 92% 19.3M 3s
464800K .......... .......... .......... .......... .......... 92% 25.5M 3s
464850K .......... .......... .......... .......... .......... 92% 23.9M 3s
464900K .......... .......... .......... .......... .......... 92% 24.9M 3s
464950K .......... .......... .......... .......... .......... 92% 21.0M 3s
465000K .......... .......... .......... .......... .......... 92% 18.4M 3s
465050K .......... .......... .......... .......... .......... 92% 25.7M 3s
465100K .......... .......... .......... .......... .......... 92% 19.4M 3s
465150K .......... .......... .......... .......... .......... 92% 21.1M 3s
465200K .......... .......... .......... .......... .......... 92% 19.9M 3s
465250K .......... .......... .......... .......... .......... 92% 20.4M 3s
465300K .......... .......... .......... .......... .......... 92% 29.3M 3s
465350K .......... .......... .......... .......... .......... 92% 16.8M 3s
465400K .......... .......... .......... .......... .......... 92% 21.6M 3s
465450K .......... .......... .......... .......... .......... 92% 20.5M 3s
465500K .......... .......... .......... .......... .......... 92% 23.8M 3s
465550K .......... .......... .......... .......... .......... 92% 21.3M 3s
465600K .......... .......... .......... .......... .......... 92% 20.6M 3s
465650K .......... .......... .......... .......... .......... 92% 29.9M 3s
465700K .......... .......... .......... .......... .......... 92% 44.5M 3s
465750K .......... .......... .......... .......... .......... 92% 19.8M 3s
465800K .......... .......... .......... .......... .......... 92% 15.3M 3s
465850K .......... .......... .......... .......... .......... 92%  178M 3s
465900K .......... .......... .......... .......... .......... 92% 22.1M 3s
465950K .......... .......... .......... .......... .......... 92% 25.6M 3s
466000K .......... .......... .......... .......... .......... 92% 21.3M 3s
466050K .......... .......... .......... .......... .......... 92% 24.5M 3s
466100K .......... .......... .......... .......... .......... 92% 17.8M 3s
466150K .......... .......... .......... .......... .......... 92% 17.8M 3s
466200K .......... .......... .......... .......... .......... 92% 21.7M 3s
466250K .......... .......... .......... .......... .......... 92% 21.1M 3s
466300K .......... .......... .......... .......... .......... 92% 22.9M 3s
466350K .......... .......... .......... .......... .......... 92% 22.4M 3s
466400K .......... .......... .......... .......... .......... 92% 19.9M 3s
466450K .......... .......... .......... .......... .......... 92% 13.9M 3s
466500K .......... .......... .......... .......... .......... 92% 23.3M 3s
466550K .......... .......... .......... .......... .......... 92% 20.6M 3s
466600K .......... .......... .......... .......... .......... 92% 20.1M 3s
466650K .......... .......... .......... .......... .......... 92% 19.5M 3s
466700K .......... .......... .......... .......... .......... 92% 26.6M 3s
466750K .......... .......... .......... .......... .......... 92% 24.4M 3s
466800K .......... .......... .......... .......... .......... 92% 17.5M 3s
466850K .......... .......... .......... .......... .......... 92% 26.1M 3s
466900K .......... .......... .......... .......... .......... 92%  254M 3s
466950K .......... .......... .......... .......... .......... 92% 27.4M 3s
467000K .......... .......... .......... .......... .......... 92% 20.1M 3s
467050K .......... .......... .......... .......... .......... 92% 32.9M 3s
467100K .......... .......... .......... .......... .......... 92% 19.7M 3s
467150K .......... .......... .......... .......... .......... 92% 15.3M 3s
467200K .......... .......... .......... .......... .......... 92% 19.6M 3s
467250K .......... .......... .......... .......... .......... 92% 25.0M 3s
467300K .......... .......... .......... .......... .......... 92% 18.9M 3s
467350K .......... .......... .......... .......... .......... 92% 15.5M 3s
467400K .......... .......... .......... .......... .......... 92% 17.9M 3s
467450K .......... .......... .......... .......... .......... 92% 15.4M 3s
467500K .......... .......... .......... .......... .......... 92% 21.5M 3s
467550K .......... .......... .......... .......... .......... 92% 21.3M 3s
467600K .......... .......... .......... .......... .......... 92% 18.9M 3s
467650K .......... .......... .......... .......... .......... 92% 19.8M 3s
467700K .......... .......... .......... .......... .......... 92% 20.1M 3s
467750K .......... .......... .......... .......... .......... 92% 12.6M 3s
467800K .......... .......... .......... .......... .......... 92% 10.4M 3s
467850K .......... .......... .......... .......... .......... 92% 45.3M 3s
467900K .......... .......... .......... .......... .......... 92% 11.9M 3s
467950K .......... .......... .......... .......... .......... 92% 8.91M 3s
468000K .......... .......... .......... .......... .......... 92% 10.6M 3s
468050K .......... .......... .......... .......... .......... 92% 13.0M 3s
468100K .......... .......... .......... .......... .......... 92% 8.79M 3s
468150K .......... .......... .......... .......... .......... 92% 11.5M 3s
468200K .......... .......... .......... .......... .......... 92% 9.23M 3s
468250K .......... .......... .......... .......... .......... 92% 11.7M 3s
468300K .......... .......... .......... .......... .......... 92% 10.6M 3s
468350K .......... .......... .......... .......... .......... 92% 9.65M 3s
468400K .......... .......... .......... .......... .......... 92% 20.8M 3s
468450K .......... .......... .......... .......... .......... 92% 17.6M 3s
468500K .......... .......... .......... .......... .......... 92% 21.8M 3s
468550K .......... .......... .......... .......... .......... 92% 22.4M 3s
468600K .......... .......... .......... .......... .......... 92% 15.7M 3s
468650K .......... .......... .......... .......... .......... 92% 23.4M 3s
468700K .......... .......... .......... .......... .......... 92% 15.9M 3s
468750K .......... .......... .......... .......... .......... 92% 21.0M 3s
468800K .......... .......... .......... .......... .......... 92% 22.2M 3s
468850K .......... .......... .......... .......... .......... 92% 15.6M 3s
468900K .......... .......... .......... .......... .......... 92% 22.1M 3s
468950K .......... .......... .......... .......... .......... 92% 17.9M 3s
469000K .......... .......... .......... .......... .......... 92% 18.1M 3s
469050K .......... .......... .......... .......... .......... 92% 21.5M 3s
469100K .......... .......... .......... .......... .......... 92% 39.5M 3s
469150K .......... .......... .......... .......... .......... 92% 34.8M 3s
469200K .......... .......... .......... .......... .......... 92% 64.0M 3s
469250K .......... .......... .......... .......... .......... 92% 29.9M 3s
469300K .......... .......... .......... .......... .......... 92% 50.6M 3s
469350K .......... .......... .......... .......... .......... 92% 95.4M 3s
469400K .......... .......... .......... .......... .......... 92% 40.7M 3s
469450K .......... .......... .......... .......... .......... 92% 31.5M 3s
469500K .......... .......... .......... .......... .......... 92% 43.1M 3s
469550K .......... .......... .......... .......... .......... 93% 28.0M 3s
469600K .......... .......... .......... .......... .......... 93% 41.6M 3s
469650K .......... .......... .......... .......... .......... 93% 49.0M 3s
469700K .......... .......... .......... .......... .......... 93% 21.8M 3s
469750K .......... .......... .......... .......... .......... 93% 35.2M 3s
469800K .......... .......... .......... .......... .......... 93% 44.0M 3s
469850K .......... .......... .......... .......... .......... 93% 25.7M 3s
469900K .......... .......... .......... .......... .......... 93% 38.9M 3s
469950K .......... .......... .......... .......... .......... 93% 24.2M 3s
470000K .......... .......... .......... .......... .......... 93% 30.3M 3s
470050K .......... .......... .......... .......... .......... 93% 49.3M 3s
470100K .......... .......... .......... .......... .......... 93% 28.2M 3s
470150K .......... .......... .......... .......... .......... 93% 45.3M 3s
470200K .......... .......... .......... .......... .......... 93% 24.2M 3s
470250K .......... .......... .......... .......... .......... 93% 26.7M 3s
470300K .......... .......... .......... .......... .......... 93% 56.6M 3s
470350K .......... .......... .......... .......... .......... 93% 24.8M 3s
470400K .......... .......... .......... .......... .......... 93% 43.9M 3s
470450K .......... .......... .......... .......... .......... 93% 31.0M 3s
470500K .......... .......... .......... .......... .......... 93% 36.2M 3s
470550K .......... .......... .......... .......... .......... 93% 40.9M 3s
470600K .......... .......... .......... .......... .......... 93% 40.0M 3s
470650K .......... .......... .......... .......... .......... 93% 21.0M 3s
470700K .......... .......... .......... .......... .......... 93% 77.8M 3s
470750K .......... .......... .......... .......... .......... 93%  218M 3s
470800K .......... .......... .......... .......... .......... 93% 24.4M 3s
470850K .......... .......... .......... .......... .......... 93% 38.2M 3s
470900K .......... .......... .......... .......... .......... 93% 99.4M 3s
470950K .......... .......... .......... .......... .......... 93% 40.9M 3s
471000K .......... .......... .......... .......... .......... 93% 35.4M 3s
471050K .......... .......... .......... .......... .......... 93% 24.5M 3s
471100K .......... .......... .......... .......... .......... 93% 35.4M 3s
471150K .......... .......... .......... .......... .......... 93% 30.8M 3s
471200K .......... .......... .......... .......... .......... 93% 25.4M 3s
471250K .......... .......... .......... .......... .......... 93% 43.4M 3s
471300K .......... .......... .......... .......... .......... 93% 25.6M 3s
471350K .......... .......... .......... .......... .......... 93% 33.3M 3s
471400K .......... .......... .......... .......... .......... 93% 40.8M 3s
471450K .......... .......... .......... .......... .......... 93% 28.2M 3s
471500K .......... .......... .......... .......... .......... 93% 28.3M 3s
471550K .......... .......... .......... .......... .......... 93% 48.9M 3s
471600K .......... .......... .......... .......... .......... 93% 25.7M 3s
471650K .......... .......... .......... .......... .......... 93% 23.9M 3s
471700K .......... .......... .......... .......... .......... 93% 34.5M 3s
471750K .......... .......... .......... .......... .......... 93% 27.1M 3s
471800K .......... .......... .......... .......... .......... 93% 30.2M 3s
471850K .......... .......... .......... .......... .......... 93% 31.7M 3s
471900K .......... .......... .......... .......... .......... 93% 27.1M 3s
471950K .......... .......... .......... .......... .......... 93% 37.1M 2s
472000K .......... .......... .......... .......... .......... 93% 25.2M 2s
472050K .......... .......... .......... .......... .......... 93% 42.4M 2s
472100K .......... .......... .......... .......... .......... 93% 15.4M 2s
472150K .......... .......... .......... .......... .......... 93% 21.3M 2s
472200K .......... .......... .......... .......... .......... 93% 43.3M 2s
472250K .......... .......... .......... .......... .......... 93% 30.5M 2s
472300K .......... .......... .......... .......... .......... 93% 43.2M 2s
472350K .......... .......... .......... .......... .......... 93% 36.1M 2s
472400K .......... .......... .......... .......... .......... 93% 34.4M 2s
472450K .......... .......... .......... .......... .......... 93% 31.1M 2s
472500K .......... .......... .......... .......... .......... 93% 38.2M 2s
472550K .......... .......... .......... .......... .......... 93% 37.9M 2s
472600K .......... .......... .......... .......... .......... 93% 38.6M 2s
472650K .......... .......... .......... .......... .......... 93% 32.9M 2s
472700K .......... .......... .......... .......... .......... 93% 24.9M 2s
472750K .......... .......... .......... .......... .......... 93% 49.1M 2s
472800K .......... .......... .......... .......... .......... 93% 41.5M 2s
472850K .......... .......... .......... .......... .......... 93% 50.3M 2s
472900K .......... .......... .......... .......... .......... 93% 36.5M 2s
472950K .......... .......... .......... .......... .......... 93% 28.2M 2s
473000K .......... .......... .......... .......... .......... 93% 48.7M 2s
473050K .......... .......... .......... .......... .......... 93% 37.3M 2s
473100K .......... .......... .......... .......... .......... 93% 42.0M 2s
473150K .......... .......... .......... .......... .......... 93% 37.0M 2s
473200K .......... .......... .......... .......... .......... 93% 27.5M 2s
473250K .......... .......... .......... .......... .......... 93% 42.6M 2s
473300K .......... .......... .......... .......... .......... 93% 34.1M 2s
473350K .......... .......... .......... .......... .......... 93% 46.0M 2s
473400K .......... .......... .......... .......... .......... 93% 39.9M 2s
473450K .......... .......... .......... .......... .......... 93% 29.7M 2s
473500K .......... .......... .......... .......... .......... 93% 33.3M 2s
473550K .......... .......... .......... .......... .......... 93% 62.8M 2s
473600K .......... .......... .......... .......... .......... 93% 37.9M 2s
473650K .......... .......... .......... .......... .......... 93% 66.2M 2s
473700K .......... .......... .......... .......... .......... 93% 70.9M 2s
473750K .......... .......... .......... .......... .......... 93% 64.4M 2s
473800K .......... .......... .......... .......... .......... 93% 23.9M 2s
473850K .......... .......... .......... .......... .......... 93% 77.8M 2s
473900K .......... .......... .......... .......... .......... 93%  144M 2s
473950K .......... .......... .......... .......... .......... 93% 30.5M 2s
474000K .......... .......... .......... .......... .......... 93% 62.9M 2s
474050K .......... .......... .......... .......... .......... 93% 27.9M 2s
474100K .......... .......... .......... .......... .......... 93% 59.4M 2s
474150K .......... .......... .......... .......... .......... 93%  126M 2s
474200K .......... .......... .......... .......... .......... 93% 28.1M 2s
474250K .......... .......... .......... .......... .......... 93% 34.8M 2s
474300K .......... .......... .......... .......... .......... 93% 27.8M 2s
474350K .......... .......... .......... .......... .......... 93% 28.1M 2s
474400K .......... .......... .......... .......... .......... 93% 32.6M 2s
474450K .......... .......... .......... .......... .......... 93% 27.5M 2s
474500K .......... .......... .......... .......... .......... 93% 26.1M 2s
474550K .......... .......... .......... .......... .......... 93% 36.8M 2s
474600K .......... .......... .......... .......... .......... 94% 23.5M 2s
474650K .......... .......... .......... .......... .......... 94% 32.9M 2s
474700K .......... .......... .......... .......... .......... 94% 26.6M 2s
474750K .......... .......... .......... .......... .......... 94% 33.7M 2s
474800K .......... .......... .......... .......... .......... 94% 30.5M 2s
474850K .......... .......... .......... .......... .......... 94% 32.0M 2s
474900K .......... .......... .......... .......... .......... 94% 37.6M 2s
474950K .......... .......... .......... .......... .......... 94% 30.0M 2s
475000K .......... .......... .......... .......... .......... 94% 38.0M 2s
475050K .......... .......... .......... .......... .......... 94% 30.2M 2s
475100K .......... .......... .......... .......... .......... 94% 36.2M 2s
475150K .......... .......... .......... .......... .......... 94% 28.8M 2s
475200K .......... .......... .......... .......... .......... 94% 38.8M 2s
475250K .......... .......... .......... .......... .......... 94% 33.7M 2s
475300K .......... .......... .......... .......... .......... 94% 36.1M 2s
475350K .......... .......... .......... .......... .......... 94% 23.8M 2s
475400K .......... .......... .......... .......... .......... 94% 19.8M 2s
475450K .......... .......... .......... .......... .......... 94%  157M 2s
475500K .......... .......... .......... .......... .......... 94% 27.0M 2s
475550K .......... .......... .......... .......... .......... 94% 39.9M 2s
475600K .......... .......... .......... .......... .......... 94% 31.4M 2s
475650K .......... .......... .......... .......... .......... 94% 43.0M 2s
475700K .......... .......... .......... .......... .......... 94% 28.1M 2s
475750K .......... .......... .......... .......... .......... 94% 39.7M 2s
475800K .......... .......... .......... .......... .......... 94% 40.6M 2s
475850K .......... .......... .......... .......... .......... 94% 23.7M 2s
475900K .......... .......... .......... .......... .......... 94% 44.1M 2s
475950K .......... .......... .......... .......... .......... 94% 26.0M 2s
476000K .......... .......... .......... .......... .......... 94% 31.2M 2s
476050K .......... .......... .......... .......... .......... 94% 28.3M 2s
476100K .......... .......... .......... .......... .......... 94% 25.3M 2s
476150K .......... .......... .......... .......... .......... 94% 28.1M 2s
476200K .......... .......... .......... .......... .......... 94% 37.7M 2s
476250K .......... .......... .......... .......... .......... 94% 21.5M 2s
476300K .......... .......... .......... .......... .......... 94% 35.8M 2s
476350K .......... .......... .......... .......... .......... 94% 24.4M 2s
476400K .......... .......... .......... .......... .......... 94% 39.8M 2s
476450K .......... .......... .......... .......... .......... 94% 23.3M 2s
476500K .......... .......... .......... .......... .......... 94% 44.6M 2s
476550K .......... .......... .......... .......... .......... 94% 29.2M 2s
476600K .......... .......... .......... .......... .......... 94% 28.8M 2s
476650K .......... .......... .......... .......... .......... 94% 34.6M 2s
476700K .......... .......... .......... .......... .......... 94% 31.2M 2s
476750K .......... .......... .......... .......... .......... 94% 36.1M 2s
476800K .......... .......... .......... .......... .......... 94% 91.8M 2s
476850K .......... .......... .......... .......... .......... 94% 29.3M 2s
476900K .......... .......... .......... .......... .......... 94% 21.1M 2s
476950K .......... .......... .......... .......... .......... 94%  101M 2s
477000K .......... .......... .......... .......... .......... 94% 38.7M 2s
477050K .......... .......... .......... .......... .......... 94% 35.7M 2s
477100K .......... .......... .......... .......... .......... 94%  169M 2s
477150K .......... .......... .......... .......... .......... 94% 43.8M 2s
477200K .......... .......... .......... .......... .......... 94% 28.9M 2s
477250K .......... .......... .......... .......... .......... 94%  127M 2s
477300K .......... .......... .......... .......... .......... 94% 35.1M 2s
477350K .......... .......... .......... .......... .......... 94% 25.9M 2s
477400K .......... .......... .......... .......... .......... 94% 33.0M 2s
477450K .......... .......... .......... .......... .......... 94% 25.7M 2s
477500K .......... .......... .......... .......... .......... 94% 36.1M 2s
477550K .......... .......... .......... .......... .......... 94% 22.9M 2s
477600K .......... .......... .......... .......... .......... 94% 27.2M 2s
477650K .......... .......... .......... .......... .......... 94% 37.9M 2s
477700K .......... .......... .......... .......... .......... 94% 23.2M 2s
477750K .......... .......... .......... .......... .......... 94% 31.0M 2s
477800K .......... .......... .......... .......... .......... 94% 21.6M 2s
477850K .......... .......... .......... .......... .......... 94% 24.5M 2s
477900K .......... .......... .......... .......... .......... 94% 30.1M 2s
477950K .......... .......... .......... .......... .......... 94% 27.9M 2s
478000K .......... .......... .......... .......... .......... 94% 33.2M 2s
478050K .......... .......... .......... .......... .......... 94% 41.9M 2s
478100K .......... .......... .......... .......... .......... 94% 27.5M 2s
478150K .......... .......... .......... .......... .......... 94% 26.4M 2s
478200K .......... .......... .......... .......... .......... 94% 23.2M 2s
478250K .......... .......... .......... .......... .......... 94% 36.5M 2s
478300K .......... .......... .......... .......... .......... 94% 41.2M 2s
478350K .......... .......... .......... .......... .......... 94% 26.1M 2s
478400K .......... .......... .......... .......... .......... 94% 14.6M 2s
478450K .......... .......... .......... .......... .......... 94% 89.9M 2s
478500K .......... .......... .......... .......... .......... 94%  162M 2s
478550K .......... .......... .......... .......... .......... 94% 16.9M 2s
478600K .......... .......... .......... .......... .......... 94% 81.4M 2s
478650K .......... .......... .......... .......... .......... 94% 72.8M 2s
478700K .......... .......... .......... .......... .......... 94% 19.6M 2s
478750K .......... .......... .......... .......... .......... 94% 30.4M 2s
478800K .......... .......... .......... .......... .......... 94% 21.9M 2s
478850K .......... .......... .......... .......... .......... 94% 27.9M 2s
478900K .......... .......... .......... .......... .......... 94% 22.6M 2s
478950K .......... .......... .......... .......... .......... 94% 25.9M 2s
479000K .......... .......... .......... .......... .......... 94% 23.0M 2s
479050K .......... .......... .......... .......... .......... 94% 26.7M 2s
479100K .......... .......... .......... .......... .......... 94% 22.1M 2s
479150K .......... .......... .......... .......... .......... 94% 25.0M 2s
479200K .......... .......... .......... .......... .......... 94% 20.2M 2s
479250K .......... .......... .......... .......... .......... 94% 26.9M 2s
479300K .......... .......... .......... .......... .......... 94% 21.0M 2s
479350K .......... .......... .......... .......... .......... 94% 19.1M 2s
479400K .......... .......... .......... .......... .......... 94% 26.0M 2s
479450K .......... .......... .......... .......... .......... 94% 15.9M 2s
479500K .......... .......... .......... .......... .......... 94% 25.5M 2s
479550K .......... .......... .......... .......... .......... 94%  104M 2s
479600K .......... .......... .......... .......... .......... 94% 17.5M 2s
479650K .......... .......... .......... .......... .......... 95% 21.6M 2s
479700K .......... .......... .......... .......... .......... 95% 22.5M 2s
479750K .......... .......... .......... .......... .......... 95% 30.5M 2s
479800K .......... .......... .......... .......... .......... 95% 23.5M 2s
479850K .......... .......... .......... .......... .......... 95% 21.1M 2s
479900K .......... .......... .......... .......... .......... 95% 25.7M 2s
479950K .......... .......... .......... .......... .......... 95% 21.1M 2s
480000K .......... .......... .......... .......... .......... 95% 26.0M 2s
480050K .......... .......... .......... .......... .......... 95% 28.4M 2s
480100K .......... .......... .......... .......... .......... 95% 20.3M 2s
480150K .......... .......... .......... .......... .......... 95% 21.0M 2s
480200K .......... .......... .......... .......... .......... 95% 19.7M 2s
480250K .......... .......... .......... .......... .......... 95% 24.7M 2s
480300K .......... .......... .......... .......... .......... 95% 29.7M 2s
480350K .......... .......... .......... .......... .......... 95% 19.4M 2s
480400K .......... .......... .......... .......... .......... 95% 20.4M 2s
480450K .......... .......... .......... .......... .......... 95% 22.5M 2s
480500K .......... .......... .......... .......... .......... 95% 20.1M 2s
480550K .......... .......... .......... .......... .......... 95% 18.6M 2s
480600K .......... .......... .......... .......... .......... 95% 29.5M 2s
480650K .......... .......... .......... .......... .......... 95% 11.9M 2s
480700K .......... .......... .......... .......... .......... 95% 26.8M 2s
480750K .......... .......... .......... .......... .......... 95% 24.1M 2s
480800K .......... .......... .......... .......... .......... 95% 21.7M 2s
480850K .......... .......... .......... .......... .......... 95% 17.6M 2s
480900K .......... .......... .......... .......... .......... 95% 27.9M 2s
480950K .......... .......... .......... .......... .......... 95% 16.4M 2s
481000K .......... .......... .......... .......... .......... 95% 23.2M 2s
481050K .......... .......... .......... .......... .......... 95% 21.3M 2s
481100K .......... .......... .......... .......... .......... 95% 18.2M 2s
481150K .......... .......... .......... .......... .......... 95% 21.5M 2s
481200K .......... .......... .......... .......... .......... 95% 20.0M 2s
481250K .......... .......... .......... .......... .......... 95% 18.3M 2s
481300K .......... .......... .......... .......... .......... 95% 23.4M 2s
481350K .......... .......... .......... .......... .......... 95% 20.2M 2s
481400K .......... .......... .......... .......... .......... 95% 18.7M 2s
481450K .......... .......... .......... .......... .......... 95% 22.9M 2s
481500K .......... .......... .......... .......... .......... 95% 19.0M 2s
481550K .......... .......... .......... .......... .......... 95% 16.1M 2s
481600K .......... .......... .......... .......... .......... 95% 24.1M 2s
481650K .......... .......... .......... .......... .......... 95% 21.5M 2s
481700K .......... .......... .......... .......... .......... 95% 31.3M 2s
481750K .......... .......... .......... .......... .......... 95% 62.7M 2s
481800K .......... .......... .......... .......... .......... 95% 16.6M 2s
481850K .......... .......... .......... .......... .......... 95% 50.4M 2s
481900K .......... .......... .......... .......... .......... 95% 17.4M 2s
481950K .......... .......... .......... .......... .......... 95%  137M 2s
482000K .......... .......... .......... .......... .......... 95% 44.5M 2s
482050K .......... .......... .......... .......... .......... 95% 39.4M 2s
482100K .......... .......... .......... .......... .......... 95% 20.8M 2s
482150K .......... .......... .......... .......... .......... 95% 32.0M 2s
482200K .......... .......... .......... .......... .......... 95% 21.1M 2s
482250K .......... .......... .......... .......... .......... 95% 33.7M 2s
482300K .......... .......... .......... .......... .......... 95% 24.4M 2s
482350K .......... .......... .......... .......... .......... 95% 18.1M 2s
482400K .......... .......... .......... .......... .......... 95% 27.0M 2s
482450K .......... .......... .......... .......... .......... 95% 29.2M 2s
482500K .......... .......... .......... .......... .......... 95% 20.7M 2s
482550K .......... .......... .......... .......... .......... 95% 27.2M 2s
482600K .......... .......... .......... .......... .......... 95% 20.5M 2s
482650K .......... .......... .......... .......... .......... 95% 31.5M 2s
482700K .......... .......... .......... .......... .......... 95% 22.0M 2s
482750K .......... .......... .......... .......... .......... 95% 24.6M 2s
482800K .......... .......... .......... .......... .......... 95% 22.7M 2s
482850K .......... .......... .......... .......... .......... 95% 28.6M 2s
482900K .......... .......... .......... .......... .......... 95% 27.5M 2s
482950K .......... .......... .......... .......... .......... 95% 22.2M 2s
483000K .......... .......... .......... .......... .......... 95% 16.5M 2s
483050K .......... .......... .......... .......... .......... 95%  156M 2s
483100K .......... .......... .......... .......... .......... 95% 12.0M 2s
483150K .......... .......... .......... .......... .......... 95%  172M 2s
483200K .......... .......... .......... .......... .......... 95% 25.1M 2s
483250K .......... .......... .......... .......... .......... 95% 46.0M 2s
483300K .......... .......... .......... .......... .......... 95% 24.8M 2s
483350K .......... .......... .......... .......... .......... 95% 21.2M 2s
483400K .......... .......... .......... .......... .......... 95% 23.6M 2s
483450K .......... .......... .......... .......... .......... 95% 24.6M 2s
483500K .......... .......... .......... .......... .......... 95% 36.0M 2s
483550K .......... .......... .......... .......... .......... 95% 28.3M 2s
483600K .......... .......... .......... .......... .......... 95% 22.5M 2s
483650K .......... .......... .......... .......... .......... 95% 35.2M 2s
483700K .......... .......... .......... .......... .......... 95% 26.2M 2s
483750K .......... .......... .......... .......... .......... 95% 23.4M 2s
483800K .......... .......... .......... .......... .......... 95% 42.9M 2s
483850K .......... .......... .......... .......... .......... 95% 21.6M 2s
483900K .......... .......... .......... .......... .......... 95% 23.3M 2s
483950K .......... .......... .......... .......... .......... 95% 25.6M 2s
484000K .......... .......... .......... .......... .......... 95% 39.6M 2s
484050K .......... .......... .......... .......... .......... 95% 24.3M 2s
484100K .......... .......... .......... .......... .......... 95% 23.3M 2s
484150K .......... .......... .......... .......... .......... 95% 23.4M 2s
484200K .......... .......... .......... .......... .......... 95% 22.7M 2s
484250K .......... .......... .......... .......... .......... 95% 23.3M 2s
484300K .......... .......... .......... .......... .......... 95% 32.2M 2s
484350K .......... .......... .......... .......... .......... 95% 19.4M 2s
484400K .......... .......... .......... .......... .......... 95% 17.9M 2s
484450K .......... .......... .......... .......... .......... 95%  221M 2s
484500K .......... .......... .......... .......... .......... 95% 19.0M 2s
484550K .......... .......... .......... .......... .......... 95%  213M 2s
484600K .......... .......... .......... .......... .......... 95% 20.8M 2s
484650K .......... .......... .......... .......... .......... 95% 28.5M 2s
484700K .......... .......... .......... .......... .......... 96% 20.5M 2s
484750K .......... .......... .......... .......... .......... 96% 25.0M 2s
484800K .......... .......... .......... .......... .......... 96% 19.6M 1s
484850K .......... .......... .......... .......... .......... 96% 19.5M 1s
484900K .......... .......... .......... .......... .......... 96% 18.9M 1s
484950K .......... .......... .......... .......... .......... 96% 16.7M 1s
485000K .......... .......... .......... .......... .......... 96% 19.5M 1s
485050K .......... .......... .......... .......... .......... 96% 17.5M 1s
485100K .......... .......... .......... .......... .......... 96% 19.6M 1s
485150K .......... .......... .......... .......... .......... 96% 23.3M 1s
485200K .......... .......... .......... .......... .......... 96% 17.4M 1s
485250K .......... .......... .......... .......... .......... 96% 17.6M 1s
485300K .......... .......... .......... .......... .......... 96% 25.1M 1s
485350K .......... .......... .......... .......... .......... 96% 21.3M 1s
485400K .......... .......... .......... .......... .......... 96% 28.0M 1s
485450K .......... .......... .......... .......... .......... 96% 20.4M 1s
485500K .......... .......... .......... .......... .......... 96% 46.2M 1s
485550K .......... .......... .......... .......... .......... 96% 24.2M 1s
485600K .......... .......... .......... .......... .......... 96% 26.5M 1s
485650K .......... .......... .......... .......... .......... 96% 18.1M 1s
485700K .......... .......... .......... .......... .......... 96% 14.2M 1s
485750K .......... .......... .......... .......... .......... 96% 19.2M 1s
485800K .......... .......... .......... .......... .......... 96% 20.6M 1s
485850K .......... .......... .......... .......... .......... 96% 15.2M 1s
485900K .......... .......... .......... .......... .......... 96% 19.2M 1s
485950K .......... .......... .......... .......... .......... 96% 16.7M 1s
486000K .......... .......... .......... .......... .......... 96% 9.96M 1s
486050K .......... .......... .......... .......... .......... 96% 14.9M 1s
486100K .......... .......... .......... .......... .......... 96% 15.4M 1s
486150K .......... .......... .......... .......... .......... 96% 16.3M 1s
486200K .......... .......... .......... .......... .......... 96% 9.02M 1s
486250K .......... .......... .......... .......... .......... 96% 9.54M 1s
486300K .......... .......... .......... .......... .......... 96% 18.9M 1s
486350K .......... .......... .......... .......... .......... 96% 11.2M 1s
486400K .......... .......... .......... .......... .......... 96% 11.9M 1s
486450K .......... .......... .......... .......... .......... 96% 11.0M 1s
486500K .......... .......... .......... .......... .......... 96% 14.0M 1s
486550K .......... .......... .......... .......... .......... 96% 10.6M 1s
486600K .......... .......... .......... .......... .......... 96% 12.2M 1s
486650K .......... .......... .......... .......... .......... 96% 14.0M 1s
486700K .......... .......... .......... .......... .......... 96% 15.2M 1s
486750K .......... .......... .......... .......... .......... 96% 15.5M 1s
486800K .......... .......... .......... .......... .......... 96% 14.9M 1s
486850K .......... .......... .......... .......... .......... 96% 7.19M 1s
486900K .......... .......... .......... .......... .......... 96% 10.8M 1s
486950K .......... .......... .......... .......... .......... 96% 19.8M 1s
487000K .......... .......... .......... .......... .......... 96% 31.2M 1s
487050K .......... .......... .......... .......... .......... 96% 20.1M 1s
487100K .......... .......... .......... .......... .......... 96% 16.6M 1s
487150K .......... .......... .......... .......... .......... 96% 16.3M 1s
487200K .......... .......... .......... .......... .......... 96% 16.1M 1s
487250K .......... .......... .......... .......... .......... 96% 24.3M 1s
487300K .......... .......... .......... .......... .......... 96% 14.2M 1s
487350K .......... .......... .......... .......... .......... 96% 15.6M 1s
487400K .......... .......... .......... .......... .......... 96% 18.6M 1s
487450K .......... .......... .......... .......... .......... 96% 14.2M 1s
487500K .......... .......... .......... .......... .......... 96% 18.8M 1s
487550K .......... .......... .......... .......... .......... 96% 15.4M 1s
487600K .......... .......... .......... .......... .......... 96% 21.4M 1s
487650K .......... .......... .......... .......... .......... 96% 22.5M 1s
487700K .......... .......... .......... .......... .......... 96% 11.0M 1s
487750K .......... .......... .......... .......... .......... 96%  250M 1s
487800K .......... .......... .......... .......... .......... 96% 16.9M 1s
487850K .......... .......... .......... .......... .......... 96% 19.8M 1s
487900K .......... .......... .......... .......... .......... 96% 21.4M 1s
487950K .......... .......... .......... .......... .......... 96% 18.2M 1s
488000K .......... .......... .......... .......... .......... 96% 22.2M 1s
488050K .......... .......... .......... .......... .......... 96% 18.6M 1s
488100K .......... .......... .......... .......... .......... 96% 18.3M 1s
488150K .......... .......... .......... .......... .......... 96% 23.1M 1s
488200K .......... .......... .......... .......... .......... 96% 19.7M 1s
488250K .......... .......... .......... .......... .......... 96% 20.2M 1s
488300K .......... .......... .......... .......... .......... 96% 24.4M 1s
488350K .......... .......... .......... .......... .......... 96% 15.5M 1s
488400K .......... .......... .......... .......... .......... 96% 23.9M 1s
488450K .......... .......... .......... .......... .......... 96% 17.7M 1s
488500K .......... .......... .......... .......... .......... 96% 16.4M 1s
488550K .......... .......... .......... .......... .......... 96% 19.5M 1s
488600K .......... .......... .......... .......... .......... 96% 25.8M 1s
488650K .......... .......... .......... .......... .......... 96% 11.4M 1s
488700K .......... .......... .......... .......... .......... 96%  180M 1s
488750K .......... .......... .......... .......... .......... 96% 17.2M 1s
488800K .......... .......... .......... .......... .......... 96% 71.6M 1s
488850K .......... .......... .......... .......... .......... 96% 19.9M 1s
488900K .......... .......... .......... .......... .......... 96% 22.1M 1s
488950K .......... .......... .......... .......... .......... 96% 14.8M 1s
489000K .......... .......... .......... .......... .......... 96% 37.9M 1s
489050K .......... .......... .......... .......... .......... 96% 18.2M 1s
489100K .......... .......... .......... .......... .......... 96% 27.1M 1s
489150K .......... .......... .......... .......... .......... 96% 21.4M 1s
489200K .......... .......... .......... .......... .......... 96% 15.5M 1s
489250K .......... .......... .......... .......... .......... 96% 38.8M 1s
489300K .......... .......... .......... .......... .......... 96% 21.6M 1s
489350K .......... .......... .......... .......... .......... 96% 23.6M 1s
489400K .......... .......... .......... .......... .......... 96% 24.8M 1s
489450K .......... .......... .......... .......... .......... 96% 19.0M 1s
489500K .......... .......... .......... .......... .......... 96% 23.8M 1s
489550K .......... .......... .......... .......... .......... 96% 24.5M 1s
489600K .......... .......... .......... .......... .......... 96% 18.9M 1s
489650K .......... .......... .......... .......... .......... 96% 25.7M 1s
489700K .......... .......... .......... .......... .......... 96% 23.9M 1s
489750K .......... .......... .......... .......... .......... 97% 33.5M 1s
489800K .......... .......... .......... .......... .......... 97% 15.1M 1s
489850K .......... .......... .......... .......... .......... 97% 26.8M 1s
489900K .......... .......... .......... .......... .......... 97% 43.1M 1s
489950K .......... .......... .......... .......... .......... 97% 29.4M 1s
490000K .......... .......... .......... .......... .......... 97% 20.5M 1s
490050K .......... .......... .......... .......... .......... 97% 27.6M 1s
490100K .......... .......... .......... .......... .......... 97% 22.7M 1s
490150K .......... .......... .......... .......... .......... 97% 29.8M 1s
490200K .......... .......... .......... .......... .......... 97% 24.9M 1s
490250K .......... .......... .......... .......... .......... 97% 29.7M 1s
490300K .......... .......... .......... .......... .......... 97% 22.0M 1s
490350K .......... .......... .......... .......... .......... 97% 31.9M 1s
490400K .......... .......... .......... .......... .......... 97% 24.7M 1s
490450K .......... .......... .......... .......... .......... 97% 25.5M 1s
490500K .......... .......... .......... .......... .......... 97% 22.6M 1s
490550K .......... .......... .......... .......... .......... 97% 47.2M 1s
490600K .......... .......... .......... .......... .......... 97% 22.4M 1s
490650K .......... .......... .......... .......... .......... 97% 25.9M 1s
490700K .......... .......... .......... .......... .......... 97% 19.8M 1s
490750K .......... .......... .......... .......... .......... 97% 32.1M 1s
490800K .......... .......... .......... .......... .......... 97% 21.8M 1s
490850K .......... .......... .......... .......... .......... 97% 23.6M 1s
490900K .......... .......... .......... .......... .......... 97% 30.5M 1s
490950K .......... .......... .......... .......... .......... 97% 22.7M 1s
491000K .......... .......... .......... .......... .......... 97% 28.7M 1s
491050K .......... .......... .......... .......... .......... 97% 13.9M 1s
491100K .......... .......... .......... .......... .......... 97%  104M 1s
491150K .......... .......... .......... .......... .......... 97%  184M 1s
491200K .......... .......... .......... .......... .......... 97% 16.8M 1s
491250K .......... .......... .......... .......... .......... 97% 36.4M 1s
491300K .......... .......... .......... .......... .......... 97% 53.5M 1s
491350K .......... .......... .......... .......... .......... 97% 22.1M 1s
491400K .......... .......... .......... .......... .......... 97% 36.0M 1s
491450K .......... .......... .......... .......... .......... 97% 21.1M 1s
491500K .......... .......... .......... .......... .......... 97% 33.0M 1s
491550K .......... .......... .......... .......... .......... 97% 26.9M 1s
491600K .......... .......... .......... .......... .......... 97% 29.1M 1s
491650K .......... .......... .......... .......... .......... 97% 24.6M 1s
491700K .......... .......... .......... .......... .......... 97% 22.4M 1s
491750K .......... .......... .......... .......... .......... 97% 33.4M 1s
491800K .......... .......... .......... .......... .......... 97% 44.6M 1s
491850K .......... .......... .......... .......... .......... 97% 22.8M 1s
491900K .......... .......... .......... .......... .......... 97% 32.3M 1s
491950K .......... .......... .......... .......... .......... 97% 22.6M 1s
492000K .......... .......... .......... .......... .......... 97% 31.0M 1s
492050K .......... .......... .......... .......... .......... 97% 34.9M 1s
492100K .......... .......... .......... .......... .......... 97% 26.7M 1s
492150K .......... .......... .......... .......... .......... 97% 28.1M 1s
492200K .......... .......... .......... .......... .......... 97% 43.6M 1s
492250K .......... .......... .......... .......... .......... 97% 23.2M 1s
492300K .......... .......... .......... .......... .......... 97% 29.9M 1s
492350K .......... .......... .......... .......... .......... 97% 26.4M 1s
492400K .......... .......... .......... .......... .......... 97% 26.9M 1s
492450K .......... .......... .......... .......... .......... 97% 14.9M 1s
492500K .......... .......... .......... .......... .......... 97% 25.5M 1s
492550K .......... .......... .......... .......... .......... 97%  133M 1s
492600K .......... .......... .......... .......... .......... 97% 16.9M 1s
492650K .......... .......... .......... .......... .......... 97% 26.8M 1s
492700K .......... .......... .......... .......... .......... 97% 41.5M 1s
492750K .......... .......... .......... .......... .......... 97% 18.5M 1s
492800K .......... .......... .......... .......... .......... 97% 20.8M 1s
492850K .......... .......... .......... .......... .......... 97% 14.1M 1s
492900K .......... .......... .......... .......... .......... 97% 20.4M 1s
492950K .......... .......... .......... .......... .......... 97% 14.6M 1s
493000K .......... .......... .......... .......... .......... 97% 23.4M 1s
493050K .......... .......... .......... .......... .......... 97% 15.4M 1s
493100K .......... .......... .......... .......... .......... 97% 14.4M 1s
493150K .......... .......... .......... .......... .......... 97% 21.8M 1s
493200K .......... .......... .......... .......... .......... 97% 14.0M 1s
493250K .......... .......... .......... .......... .......... 97% 19.9M 1s
493300K .......... .......... .......... .......... .......... 97% 18.3M 1s
493350K .......... .......... .......... .......... .......... 97% 27.9M 1s
493400K .......... .......... .......... .......... .......... 97% 15.3M 1s
493450K .......... .......... .......... .......... .......... 97% 93.9M 1s
493500K .......... .......... .......... .......... .......... 97% 50.7M 1s
493550K .......... .......... .......... .......... .......... 97% 37.2M 1s
493600K .......... .......... .......... .......... .......... 97% 67.7M 1s
493650K .......... .......... .......... .......... .......... 97% 25.1M 1s
493700K .......... .......... .......... .......... .......... 97% 23.0M 1s
493750K .......... .......... .......... .......... .......... 97% 24.4M 1s
493800K .......... .......... .......... .......... .......... 97% 33.0M 1s
493850K .......... .......... .......... .......... .......... 97% 20.6M 1s
493900K .......... .......... .......... .......... .......... 97% 22.2M 1s
493950K .......... .......... .......... .......... .......... 97% 26.0M 1s
494000K .......... .......... .......... .......... .......... 97% 25.4M 1s
494050K .......... .......... .......... .......... .......... 97% 29.3M 1s
494100K .......... .......... .......... .......... .......... 97% 20.8M 1s
494150K .......... .......... .......... .......... .......... 97% 36.0M 1s
494200K .......... .......... .......... .......... .......... 97% 14.8M 1s
494250K .......... .......... .......... .......... .......... 97% 42.1M 1s
494300K .......... .......... .......... .......... .......... 97% 22.4M 1s
494350K .......... .......... .......... .......... .......... 97% 19.7M 1s
494400K .......... .......... .......... .......... .......... 97% 27.1M 1s
494450K .......... .......... .......... .......... .......... 97% 19.5M 1s
494500K .......... .......... .......... .......... .......... 97% 23.8M 1s
494550K .......... .......... .......... .......... .......... 97% 89.6M 1s
494600K .......... .......... .......... .......... .......... 97% 11.6M 1s
494650K .......... .......... .......... .......... .......... 97%  175M 1s
494700K .......... .......... .......... .......... .......... 97% 18.9M 1s
494750K .......... .......... .......... .......... .......... 97%  129M 1s
494800K .......... .......... .......... .......... .......... 98% 46.1M 1s
494850K .......... .......... .......... .......... .......... 98% 40.7M 1s
494900K .......... .......... .......... .......... .......... 98% 38.7M 1s
494950K .......... .......... .......... .......... .......... 98% 29.9M 1s
495000K .......... .......... .......... .......... .......... 98% 33.2M 1s
495050K .......... .......... .......... .......... .......... 98% 29.8M 1s
495100K .......... .......... .......... .......... .......... 98% 21.0M 1s
495150K .......... .......... .......... .......... .......... 98% 37.2M 1s
495200K .......... .......... .......... .......... .......... 98% 23.7M 1s
495250K .......... .......... .......... .......... .......... 98% 34.6M 1s
495300K .......... .......... .......... .......... .......... 98% 26.9M 1s
495350K .......... .......... .......... .......... .......... 98% 37.8M 1s
495400K .......... .......... .......... .......... .......... 98% 29.3M 1s
495450K .......... .......... .......... .......... .......... 98% 24.0M 1s
495500K .......... .......... .......... .......... .......... 98% 31.2M 1s
495550K .......... .......... .......... .......... .......... 98% 26.3M 1s
495600K .......... .......... .......... .......... .......... 98% 24.6M 1s
495650K .......... .......... .......... .......... .......... 98% 33.1M 1s
495700K .......... .......... .......... .......... .......... 98% 28.1M 1s
495750K .......... .......... .......... .......... .......... 98% 28.7M 1s
495800K .......... .......... .......... .......... .......... 98% 22.3M 1s
495850K .......... .......... .......... .......... .......... 98% 35.2M 1s
495900K .......... .......... .......... .......... .......... 98% 21.7M 1s
495950K .......... .......... .......... .......... .......... 98% 31.5M 1s
496000K .......... .......... .......... .......... .......... 98% 16.2M 1s
496050K .......... .......... .......... .......... .......... 98% 32.0M 1s
496100K .......... .......... .......... .......... .......... 98% 20.8M 1s
496150K .......... .......... .......... .......... .......... 98% 31.1M 1s
496200K .......... .......... .......... .......... .......... 98% 60.4M 1s
496250K .......... .......... .......... .......... .......... 98% 21.3M 1s
496300K .......... .......... .......... .......... .......... 98% 25.0M 1s
496350K .......... .......... .......... .......... .......... 98% 23.3M 1s
496400K .......... .......... .......... .......... .......... 98% 19.8M 1s
496450K .......... .......... .......... .......... .......... 98% 22.8M 1s
496500K .......... .......... .......... .......... .......... 98% 24.2M 1s
496550K .......... .......... .......... .......... .......... 98% 26.3M 1s
496600K .......... .......... .......... .......... .......... 98% 20.1M 1s
496650K .......... .......... .......... .......... .......... 98% 24.1M 1s
496700K .......... .......... .......... .......... .......... 98% 19.4M 1s
496750K .......... .......... .......... .......... .......... 98% 20.5M 1s
496800K .......... .......... .......... .......... .......... 98% 23.7M 1s
496850K .......... .......... .......... .......... .......... 98% 21.3M 1s
496900K .......... .......... .......... .......... .......... 98% 25.0M 1s
496950K .......... .......... .......... .......... .......... 98% 19.5M 1s
497000K .......... .......... .......... .......... .......... 98% 25.1M 1s
497050K .......... .......... .......... .......... .......... 98% 33.9M 1s
497100K .......... .......... .......... .......... .......... 98% 17.8M 1s
497150K .......... .......... .......... .......... .......... 98% 21.8M 1s
497200K .......... .......... .......... .......... .......... 98% 14.4M 1s
497250K .......... .......... .......... .......... .......... 98%  159M 1s
497300K .......... .......... .......... .......... .......... 98% 21.9M 1s
497350K .......... .......... .......... .......... .......... 98% 22.2M 1s
497400K .......... .......... .......... .......... .......... 98%  202M 1s
497450K .......... .......... .......... .......... .......... 98% 21.3M 1s
497500K .......... .......... .......... .......... .......... 98% 22.9M 1s
497550K .......... .......... .......... .......... .......... 98% 18.5M 1s
497600K .......... .......... .......... .......... .......... 98% 21.0M 1s
497650K .......... .......... .......... .......... .......... 98% 18.8M 1s
497700K .......... .......... .......... .......... .......... 98% 18.6M 1s
497750K .......... .......... .......... .......... .......... 98% 25.7M 1s
497800K .......... .......... .......... .......... .......... 98% 18.9M 1s
497850K .......... .......... .......... .......... .......... 98% 19.0M 1s
497900K .......... .......... .......... .......... .......... 98% 17.2M 1s
497950K .......... .......... .......... .......... .......... 98% 19.9M 1s
498000K .......... .......... .......... .......... .......... 98% 24.9M 1s
498050K .......... .......... .......... .......... .......... 98% 14.0M 1s
498100K .......... .......... .......... .......... .......... 98% 18.7M 0s
498150K .......... .......... .......... .......... .......... 98% 26.2M 0s
498200K .......... .......... .......... .......... .......... 98% 39.6M 0s
498250K .......... .......... .......... .......... .......... 98% 14.6M 0s
498300K .......... .......... .......... .......... .......... 98%  176M 0s
498350K .......... .......... .......... .......... .......... 98% 51.4M 0s
498400K .......... .......... .......... .......... .......... 98% 27.6M 0s
498450K .......... .......... .......... .......... .......... 98% 26.3M 0s
498500K .......... .......... .......... .......... .......... 98%  129M 0s
498550K .......... .......... .......... .......... .......... 98% 26.3M 0s
498600K .......... .......... .......... .......... .......... 98% 35.0M 0s
498650K .......... .......... .......... .......... .......... 98% 23.4M 0s
498700K .......... .......... .......... .......... .......... 98% 37.0M 0s
498750K .......... .......... .......... .......... .......... 98% 32.5M 0s
498800K .......... .......... .......... .......... .......... 98% 28.8M 0s
498850K .......... .......... .......... .......... .......... 98% 35.1M 0s
498900K .......... .......... .......... .......... .......... 98% 30.0M 0s
498950K .......... .......... .......... .......... .......... 98% 31.7M 0s
499000K .......... .......... .......... .......... .......... 98% 28.4M 0s
499050K .......... .......... .......... .......... .......... 98% 33.2M 0s
499100K .......... .......... .......... .......... .......... 98% 24.1M 0s
499150K .......... .......... .......... .......... .......... 98% 30.0M 0s
499200K .......... .......... .......... .......... .......... 98% 33.4M 0s
499250K .......... .......... .......... .......... .......... 98% 22.4M 0s
499300K .......... .......... .......... .......... .......... 98% 31.8M 0s
499350K .......... .......... .......... .......... .......... 98% 21.4M 0s
499400K .......... .......... .......... .......... .......... 98% 36.9M 0s
499450K .......... .......... .......... .......... .......... 98% 27.7M 0s
499500K .......... .......... .......... .......... .......... 98% 26.7M 0s
499550K .......... .......... .......... .......... .......... 98% 18.1M 0s
499600K .......... .......... .......... .......... .......... 98% 19.4M 0s
499650K .......... .......... .......... .......... .......... 98% 18.5M 0s
499700K .......... .......... .......... .......... .......... 98% 21.8M 0s
499750K .......... .......... .......... .......... .......... 98% 19.5M 0s
499800K .......... .......... .......... .......... .......... 98% 96.1M 0s
499850K .......... .......... .......... .......... .......... 99% 17.6M 0s
499900K .......... .......... .......... .......... .......... 99% 26.8M 0s
499950K .......... .......... .......... .......... .......... 99% 22.3M 0s
500000K .......... .......... .......... .......... .......... 99% 25.4M 0s
500050K .......... .......... .......... .......... .......... 99% 23.6M 0s
500100K .......... .......... .......... .......... .......... 99% 20.0M 0s
500150K .......... .......... .......... .......... .......... 99% 33.3M 0s
500200K .......... .......... .......... .......... .......... 99% 24.8M 0s
500250K .......... .......... .......... .......... .......... 99% 19.9M 0s
500300K .......... .......... .......... .......... .......... 99% 11.4M 0s
500350K .......... .......... .......... .......... .......... 99% 19.4M 0s
500400K .......... .......... .......... .......... .......... 99% 32.1M 0s
500450K .......... .......... .......... .......... .......... 99% 23.1M 0s
500500K .......... .......... .......... .......... .......... 99% 28.9M 0s
500550K .......... .......... .......... .......... .......... 99% 26.4M 0s
500600K .......... .......... .......... .......... .......... 99% 30.6M 0s
500650K .......... .......... .......... .......... .......... 99% 31.7M 0s
500700K .......... .......... .......... .......... .......... 99% 46.9M 0s
500750K .......... .......... .......... .......... .......... 99% 81.2M 0s
500800K .......... .......... .......... .......... .......... 99% 22.8M 0s
500850K .......... .......... .......... .......... .......... 99% 36.8M 0s
500900K .......... .......... .......... .......... .......... 99%  135M 0s
500950K .......... .......... .......... .......... .......... 99% 43.1M 0s
501000K .......... .......... .......... .......... .......... 99% 50.0M 0s
501050K .......... .......... .......... .......... .......... 99%  187M 0s
501100K .......... .......... .......... .......... .......... 99% 27.4M 0s
501150K .......... .......... .......... .......... .......... 99% 39.1M 0s
501200K .......... .......... .......... .......... .......... 99% 27.7M 0s
501250K .......... .......... .......... .......... .......... 99% 37.5M 0s
501300K .......... .......... .......... .......... .......... 99% 42.1M 0s
501350K .......... .......... .......... .......... .......... 99% 26.5M 0s
501400K .......... .......... .......... .......... .......... 99% 35.5M 0s
501450K .......... .......... .......... .......... .......... 99% 40.2M 0s
501500K .......... .......... .......... .......... .......... 99% 36.9M 0s
501550K .......... .......... .......... .......... .......... 99% 25.8M 0s
501600K .......... .......... .......... .......... .......... 99% 34.4M 0s
501650K .......... .......... .......... .......... .......... 99% 35.0M 0s
501700K .......... .......... .......... .......... .......... 99% 32.6M 0s
501750K .......... .......... .......... .......... .......... 99% 43.7M 0s
501800K .......... .......... .......... .......... .......... 99% 40.7M 0s
501850K .......... .......... .......... .......... .......... 99% 24.8M 0s
501900K .......... .......... .......... .......... .......... 99% 32.1M 0s
501950K .......... .......... .......... .......... .......... 99% 34.7M 0s
502000K .......... .......... .......... .......... .......... 99% 41.8M 0s
502050K .......... .......... .......... .......... .......... 99% 23.7M 0s
502100K .......... .......... .......... .......... .......... 99% 37.4M 0s
502150K .......... .......... .......... .......... .......... 99% 37.1M 0s
502200K .......... .......... .......... .......... .......... 99% 31.3M 0s
502250K .......... .......... .......... .......... .......... 99% 72.7M 0s
502300K .......... .......... .......... .......... .......... 99% 32.3M 0s
502350K .......... .......... .......... .......... .......... 99% 18.4M 0s
502400K .......... .......... .......... .......... .......... 99% 59.8M 0s
502450K .......... .......... .......... .......... .......... 99%  124M 0s
502500K .......... .......... .......... .......... .......... 99% 54.7M 0s
502550K .......... .......... .......... .......... .......... 99% 68.7M 0s
502600K .......... .......... .......... .......... .......... 99% 94.1M 0s
502650K .......... .......... .......... .......... .......... 99% 41.0M 0s
502700K .......... .......... .......... .......... .......... 99% 52.3M 0s
502750K .......... .......... .......... .......... .......... 99% 61.3M 0s
502800K .......... .......... .......... .......... .......... 99% 32.3M 0s
502850K .......... .......... .......... .......... .......... 99% 31.9M 0s
502900K .......... .......... .......... .......... .......... 99% 27.5M 0s
502950K .......... .......... .......... .......... .......... 99% 39.0M 0s
503000K .......... .......... .......... .......... .......... 99% 27.6M 0s
503050K .......... .......... .......... .......... .......... 99% 34.6M 0s
503100K .......... .......... .......... .......... .......... 99% 24.4M 0s
503150K .......... .......... .......... .......... .......... 99% 36.0M 0s
503200K .......... .......... .......... .......... .......... 99% 23.9M 0s
503250K .......... .......... .......... .......... .......... 99% 31.5M 0s
503300K .......... .......... .......... .......... .......... 99% 34.0M 0s
503350K .......... .......... .......... .......... .......... 99% 25.9M 0s
503400K .......... .......... .......... .......... .......... 99% 21.6M 0s
503450K .......... .......... .......... .......... .......... 99% 39.5M 0s
503500K .......... .......... .......... .......... .......... 99% 28.4M 0s
503550K .......... .......... .......... .......... .......... 99% 40.5M 0s
503600K .......... .......... .......... .......... .......... 99% 24.3M 0s
503650K .......... .......... .......... .......... .......... 99% 30.2M 0s
503700K .......... .......... .......... .......... .......... 99% 33.1M 0s
503750K .......... .......... .......... .......... .......... 99% 25.1M 0s
503800K .......... .......... .......... .......... .......... 99% 32.6M 0s
503850K .......... .......... .......... .......... .......... 99%  115M 0s
503900K .......... .......... .......... .......... .......... 99% 31.7M 0s
503950K .......... .......... .......... .......... .......... 99% 79.1M 0s
504000K .......... .......... .......... .......... .......... 99% 31.4M 0s
504050K .......... .......... .......... .......... .......... 99% 20.1M 0s
504100K .......... .......... .......... .......... .......... 99% 47.2M 0s
504150K .......... .......... .......... .......... .......... 99%  118M 0s
504200K .......... .......... .......... .......... .......... 99% 31.4M 0s
504250K .......... .......... .......... .......... .......... 99%  191M 0s
504300K .......... .......... .......... .......... .......... 99% 52.2M 0s
504350K .......... .......... .......... .......... .......... 99% 33.9M 0s
504400K .......... .......... .......... .......... .......... 99% 41.0M 0s
504450K .......... .......... .......... .......... .......... 99% 34.6M 0s
504500K .......... .......... .......... .......... .......... 99% 38.7M 0s
504550K .......... .......... .......... .......... .......... 99% 37.0M 0s
504600K .......... .......... .......... .......... .......... 99% 30.6M 0s
504650K .......... .......... .......... .......... .......... 99% 35.5M 0s
504700K .......... .......... .......... .......... .......... 99% 31.9M 0s
504750K .......... .......... .......... .......... .......... 99% 49.6M 0s
504800K .......... .......... .......... .......... .......... 99% 31.5M 0s
504850K .......... .......... .......... .......... .......... 99% 38.6M 0s
504900K                                                       100% 13.7K=37s

2024-04-28 13:00:10 (13.3 MB/s) - ‘ESPbeta-macos-x86_64.tgz’ saved [517018302/517018302]

+ tar -xf ESPbeta-macos-x86_64.tgz
+ cd ESPbeta
+ rm -rf /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Slugs
++ uname -a
+ [[ Darwin macys.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* ]]
+ ./setup.command
Custom icon assigned to '/Users/jenkins/Desktop/ESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Custom icon assigned to '/Users/jenkins/Desktop/runESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/idle3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pyftsubset'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_op4'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/ttx'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/wingproj'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_op2'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pip3'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/undill'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/run_om_test'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/f90nml'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/webview'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/fonttools'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/openmdao'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pyNastranGUI'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/f2py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pydoc3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/2to3-3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pip3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_pynastrangui'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/numba'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/normalizer'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/virtualenv'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/reset_notebook'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/abaqus_to_nastran'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/get_gprof'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/format_converter'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pyftmerge'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/python3.11-config'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/f06'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/get_objgraph'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/config-3.11-darwin/Makefile'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/config-3.11-darwin/python-config.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/pkgconfig/python-3.11-embed.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/pkgconfig/python-3.11.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/_sysconfigdata__darwin_darwin.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/site-packages/mpi4py/mpi.cfg'
Patching 'bin/ompi_info'
Patching 'bin/orte-info'
Patching 'lib/libmpi.40.dylib'
Patching 'lib/libopen-pal.40.dylib'
Patching 'lib/openmpi/mca_io_romio321.so'
Patching 'lib/openmpi/mca_pmix_pmix3x.so'
Patching 'lib/pkgconfig/ompi-c.pc'
Patching 'lib/pkgconfig/ompi-cxx.pc'
Patching 'lib/pkgconfig/ompi-fort.pc'
Patching 'lib/pkgconfig/ompi.pc'
Patching 'lib/pkgconfig/orte.pc'
Patching 'lib/pkgconfig/pmix.pc'
Patching 'share/openmpi/mpic++-wrapper-data.txt'
Patching 'share/openmpi/mpicc-wrapper-data.txt'
Patching 'share/openmpi/mpifort-wrapper-data.txt'
Patching 'share/openmpi/ortecc-wrapper-data.txt'
+ rm -rf '/Users/jenkins/Desktop/*ESPbeta.command'
+ source /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN64
++ ESP_ARCH=DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad
++ export CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/OpenCASCADE-7.8.0
++ CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/OpenCASCADE-7.8.0
++ export CARARCH=.
++ CARARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/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_bPreBuilt/ESPbeta/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/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/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/include/python3.11
++ PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/ESP-localhost7681.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/ESP-localhost7681.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/wvClient/wv.html'
+ which python
/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/python
+ python --version
Python 3.11.9
+ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin
++ uname -a
+ [[ Darwin macys.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_bPreBuilt/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:169]]
        ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,0,999)"
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000158 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:176]]
        ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,14,999)"
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000164 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:183]]
        iend must not be less than ibeg when evaluating "slice(e3,4,-1)"
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (illegal_pmtr_index) in Branch Brch_000317 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:384]]
        index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000332 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:402]]
        index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000346 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:418]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000360 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:434]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000367 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:442]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000374 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:450]]
        column index must be between 1 and 3
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000381 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:458]]
        column index must be between 1 and 3
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (UNKNOWN) in Branch Brch_001805 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1914]]
        signal 1 thrown by user
    --> catching signal 1 (UNKNOWN)
ERROR:: (illegal_value) in Branch Brch_001813 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1924]]
        vertex and base must be different
    --> catching signal -225 (illegal_value)
==> serveESP completed successfully with no verification data

real	0m4.758s
user	0m0.283s
sys	0m0.021s
+ set +x

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

+ expectSuccess 02 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.414s
user	0m0.452s
sys	0m0.036s
+ set +x

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

+ expectSuccess 03 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m1.910s
user	0m3.054s
sys	0m0.787s
+ set +x

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

+ expectSuccess 04 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.589s
user	0m0.644s
sys	0m0.054s
+ set +x

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

+ expectSuccess 05 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.548s
user	0m0.719s
sys	0m0.068s
+ set +x

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

+ expectSuccess 06 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.560s
user	0m0.713s
sys	0m0.038s
+ set +x

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

+ expectSuccess 07 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m2.806s
user	0m4.908s
sys	0m0.618s
+ set +x

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

+ expectSuccess 08 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data

real	0m17.719s
user	0m32.194s
sys	0m2.189s
+ set +x

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

+ expectSuccess 09 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.567s
user	0m0.666s
sys	0m0.030s
+ set +x

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

+ expectSuccess 10 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data

real	0m20.922s
user	1m21.556s
sys	0m27.180s
+ set +x

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

+ expectSuccess 11 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
==> serveESP completed successfully with 1 warnings and no verification data

real	0m0.727s
user	0m0.465s
sys	0m0.042s
+ set +x

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

+ expectSuccess 12 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.582s
user	0m0.766s
sys	0m0.017s
+ set +x

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

+ expectSuccess 13 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.337s
user	0m0.356s
sys	0m0.015s
+ set +x

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

+ expectSuccess 14 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data

real	0m0.738s
user	0m0.548s
sys	0m0.020s
+ set +x

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

+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
....................................................   PCurve Map: 48 (alloc 48)!
   Surface Map: 12 (alloc 24)!
   Curve Map: 28 (alloc 28)!
 Writing PCurves...
 Writing Curves...
 Writing Surfaces...
 Writing 16 Nodes...
 Writing 28 Edges...
 Writing 12 Loops...
 Writing 12 Faces...
 Writing 1 Shells...
 EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 71 tests in 1.738s

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

real	0m4.758s
user	0m6.544s
sys	0m0.180s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
..Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing1, index = 1
	Name = Wing2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 143
	Number of elements = 282
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 282
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 155
	Number of elements = 306
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 306
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 298
	Combined Number of elements = 588
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 588
	Combined Elemental Quad4 = 0

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

Getting FEA properties.......
	Number of properties - 2
	Property name - Wing1
	Property name - Wing2
	Done getting FEA properties
Updating mesh element types based on properties input
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library -  d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing1, index = 1
	Name = Wing2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 209
	Number of elements = 414
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 414
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 186
	Number of elements = 368
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 368
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 395
	Combined Number of elements = 782
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 782
	Combined Elemental Quad4 = 0

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

Getting FEA properties.......
	Number of properties - 2
	Property name - Wing1
	Property name - Wing2
	Done getting FEA properties
Updating mesh element types based on properties input
..........--> Opening DESPMTR file "unitGeom.param"
    updating CFGPMTR series                          [ 1, 1] =  8412.000000
    updating CFGPMTR series2                         [ 1, 1] =    20.000000
    updating CFGPMTR VIEW:CFD                        [ 1, 1] =     1.000000
    updating CFGPMTR nrow                            [ 1, 1] =     3.000000
    updating CFGPMTR ncol                            [ 1, 1] =     2.000000
    updating DESPMTR area                            [ 1, 1] =    40.000000
    updating DESPMTR aspect                          [ 1, 1] =     5.000000
    updating DESPMTR taper                           [ 1, 1] =     0.500000
    updating DESPMTR twist                           [ 1, 1] =    15.000000
    updating DESPMTR wing:lesweep                    [ 1, 1] =    30.000000
    updating DESPMTR wing:dihedral                   [ 1, 1] =     1.000000
    updating DESPMTR wing:chord:root                 [ 1, 1] =     1.560000
    updating DESPMTR htail                           [ 1, 1] =     1.000000
    updating DESPMTR htail:chord                     [ 1, 1] =     2.000000
    updating DESPMTR vtail:chord                     [ 1, 1] =     3.000000
    updating DESPMTR vtail                           [ 1, 1] =     4.000000
    updating DESPMTR sphereR                         [ 1, 1] =    80.000000
    updating DESPMTR v@1:d_name                      [ 1, 1] =     1.000000
    updating DESPMTR despMat                         [ 1, 1] =    11.000000
    updating DESPMTR despMat                         [ 1, 2] =    12.000000
    updating DESPMTR despMat                         [ 2, 1] =    13.000000
    updating DESPMTR despMat                         [ 2, 2] =    14.000000
    updating DESPMTR despMat                         [ 3, 1] =    15.000000
    updating DESPMTR despMat                         [ 3, 2] =    16.000000
    updating DESPMTR despCol                         [ 1, 1] =    11.000000
    updating DESPMTR despCol                         [ 2, 1] =    13.000000
    updating DESPMTR despCol                         [ 3, 1] =    15.000000
    updating DESPMTR despRow                         [ 1, 1] =    11.000000
    updating DESPMTR despRow                         [ 1, 2] =    12.000000
    updating DESPMTR despRow                         [ 1, 3] =    13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
 CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. CAPS Info: Hit last success -- going live!
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> Opening DESPMTR file "unitGeom.param"
    updating CFGPMTR series                          [ 1, 1] =  8412.000000
    updating CFGPMTR series2                         [ 1, 1] =    20.000000
    updating CFGPMTR VIEW:CFD                        [ 1, 1] =     1.000000
    updating CFGPMTR nrow                            [ 1, 1] =     3.000000
    updating CFGPMTR ncol                            [ 1, 1] =     2.000000
    updating DESPMTR area                            [ 1, 1] =    40.000000
    updating DESPMTR aspect                          [ 1, 1] =     5.000000
    updating DESPMTR taper                           [ 1, 1] =     0.500000
    updating DESPMTR twist                           [ 1, 1] =    15.000000
    updating DESPMTR wing:lesweep                    [ 1, 1] =    30.000000
    updating DESPMTR wing:dihedral                   [ 1, 1] =     1.000000
    updating DESPMTR wing:chord:root                 [ 1, 1] =     1.560000
    updating DESPMTR htail                           [ 1, 1] =     1.000000
    updating DESPMTR htail:chord                     [ 1, 1] =     2.000000
    updating DESPMTR vtail:chord                     [ 1, 1] =     3.000000
    updating DESPMTR vtail                           [ 1, 1] =     4.000000
    updating DESPMTR sphereR                         [ 1, 1] =    80.000000
    updating DESPMTR v@1:d_name                      [ 1, 1] =     1.000000
    updating DESPMTR despMat                         [ 1, 1] =    11.000000
    updating DESPMTR despMat                         [ 1, 2] =    12.000000
    updating DESPMTR despMat                         [ 2, 1] =    13.000000
    updating DESPMTR despMat                         [ 2, 2] =    14.000000
    updating DESPMTR despMat                         [ 3, 1] =    15.000000
    updating DESPMTR despMat                         [ 3, 2] =    16.000000
    updating DESPMTR despCol                         [ 1, 1] =    11.000000
    updating DESPMTR despCol                         [ 2, 1] =    13.000000
    updating DESPMTR despCol                         [ 3, 1] =    15.000000
    updating DESPMTR despRow                         [ 1, 1] =    11.000000
    updating DESPMTR despRow                         [ 1, 2] =    12.000000
    updating DESPMTR despRow                         [ 1, 3] =    13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
 CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

----------------------------------------------------------------------
Ran 100 tests in 23.513s

OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
python -u -m unittest discover --verbose
test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.023   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.058   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
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          =     0.005   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.022   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.051   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
 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          =     0.023   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4122      6020
AFLR2 GG : Nodes, Faces      =      5812      9400
AFLR2 GG : Nodes, Faces      =      7299     12374
AFLR2 GG : Nodes, Faces      =      8574     14924
AFLR2 GG : Nodes, Faces      =      9729     17234
AFLR2 GG : Nodes, Faces      =     10787     19350
AFLR2 GG : Nodes, Faces      =     11767     21310
AFLR2 GG : Nodes, Faces      =     12683     23142
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     14278     26332
AFLR2 GG : Nodes, Faces      =     14999     27774
AFLR2 GG : Nodes, Faces      =     15682     29140
AFLR2 GG : Nodes, Faces      =     16312     30400
AFLR2 GG : Nodes, Faces      =     16899     31574
AFLR2 GG : Nodes, Faces      =     17451     32678
AFLR2 GG : Nodes, Faces      =     17959     33694
AFLR2 GG : Nodes, Faces      =     18443     34662
AFLR2 GG : Nodes, Faces      =     18877     35530
AFLR2 GG : Nodes, Faces      =     19283     36342
AFLR2 GG : Nodes, Faces      =     19650     37076
AFLR2 GG : Nodes, Faces      =     19994     37764
AFLR2 GG : Nodes, Faces      =     20325     38426
AFLR2 GG : Nodes, Faces      =     20638     39052
AFLR2 GG : Nodes, Faces      =     20940     39656
AFLR2 GG : Nodes, Faces      =     21240     40256
AFLR2 GG : Nodes, Faces      =     21523     40822
AFLR2 GG : Nodes, Faces      =     21792     41360
AFLR2 GG : Nodes, Faces      =     22053     41882
AFLR2 GG : Nodes, Faces      =     22305     42386
AFLR2 GG : Nodes, Faces      =     22521     42818
AFLR2 GG : Nodes, Faces      =     22696     43168
AFLR2 GG : Nodes, Faces      =     22829     43434
AFLR2 GG : Nodes, Faces      =     22953     43682
AFLR2 GG : Nodes, Faces      =     23050     43876
AFLR2 GG : Nodes, Faces      =     23110     43996
AFLR2 GG : Nodes, Faces      =     23139     44054
AFLR2 GG : Nodes, Faces      =     23157     44090
AFLR2 GG : Nodes, Faces      =     23175     44126
AFLR2 GG : Nodes, Faces      =     23183     44142
AFLR2 GG : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.053   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.005   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
 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          =     0.022   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.051   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 Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.009   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.005   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690

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


Writing vtk file ....

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

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


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.008   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.005   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 7):
	Number of nodes          = 1189
	Number of elements       = 6249
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4917
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 7):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 7):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 7):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 7):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 7):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 7):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2589
	Number of elements       = 13809
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11051
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4694
	Number of elements       = 25935
	Number of triangles      = 3326
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22609
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5554
	Number of elements       = 30862
	Number of triangles      = 3756
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 27106
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2260
	Number of elements       = 12133
	Number of triangles      = 2222
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9911
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2392
	Number of elements       = 12577
	Number of triangles      = 2666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9911
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3341
	Number of elements       = 18069
	Number of triangles      = 3110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3606
	Number of elements       = 18961
	Number of triangles      = 4002
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4414
	Number of elements       = 23974
	Number of triangles      = 3998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19976
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4811
	Number of elements       = 25310
	Number of triangles      = 5334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19976
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 4):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 4):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 4):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 4):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5490
	Number of elements       = 29891
	Number of triangles      = 4886
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25005
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6019
	Number of elements       = 31671
	Number of triangles      = 6666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25005
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 5):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 5):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 5):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 5):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 5):
	Number of nodes          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6542
	Number of elements       = 35667
	Number of triangles      = 5774
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29893
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 7203
	Number of elements       = 37891
	Number of triangles      = 7998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29893
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 6):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 6):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 6):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 6):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 6):
	Number of nodes          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 6):
	Number of nodes          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 7601
	Number of elements       = 41489
	Number of triangles      = 6662
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8394
	Number of elements       = 44157
	Number of triangles      = 9330
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 7):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 7):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 7):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 7):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 7):
	Number of nodes          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 7):
	Number of nodes          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 7):
	Number of nodes          = 1191
	Number of elements       = 6266
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4934
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 19800
	Number of elements       = 109798
	Number of triangles      = 15540
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 8 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 9 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 10 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 11 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 12 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 13 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 14 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 15 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 16 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 17 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 18 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 19 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 22741
	Number of elements       = 119570
	Number of triangles      = 25312
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 19):
	Number of nodes          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 19):
	Number of nodes          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 19):
	Number of nodes          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 19):
	Number of nodes          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 19):
	Number of nodes          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 19):
	Number of nodes          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 19):
	Number of nodes          = 1191
	Number of elements       = 6266
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4934
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 8 (of 19):
	Number of nodes          = 1193
	Number of elements       = 6272
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4940
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 9 (of 19):
	Number of nodes          = 1176
	Number of elements       = 6165
	Number of triangles      = 1330
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4835
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 10 (of 19):
	Number of nodes          = 1203
	Number of elements       = 6314
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4982
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 11 (of 19):
	Number of nodes          = 1192
	Number of elements       = 6269
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4937
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 12 (of 19):
	Number of nodes          = 1192
	Number of elements       = 6269
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4937
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 13 (of 19):
	Number of nodes          = 1198
	Number of elements       = 6296
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4964
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 14 (of 19):
	Number of nodes          = 1223
	Number of elements       = 6443
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5111
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 15 (of 19):
	Number of nodes          = 1184
	Number of elements       = 6224
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4892
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 16 (of 19):
	Number of nodes          = 1195
	Number of elements       = 6287
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4955
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 17 (of 19):
	Number of nodes          = 1197
	Number of elements       = 6311
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4979
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 18 (of 19):
	Number of nodes          = 1203
	Number of elements       = 6310
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4978
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 19 (of 19):
	Number of nodes          = 1191
	Number of elements       = 6253
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4921
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8857
	Number of elements       = 49191
	Number of triangles      = 6284
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42907
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8989
	Number of elements       = 49635
	Number of triangles      = 6728
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42907
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 7796
	Number of elements       = 43368
	Number of triangles      = 5396
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 1193
	Number of elements       = 6267
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4935
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9944
	Number of elements       = 55193
	Number of triangles      = 7174
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 48019
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10218
	Number of elements       = 56081
	Number of triangles      = 8062
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 48019
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7818
	Number of elements       = 43469
	Number of triangles      = 5398
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 38071
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1202
	Number of elements       = 6320
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4988
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 1198
	Number of elements       = 6292
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4960
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9609
	Number of elements       = 53228
	Number of triangles      = 6994
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46234
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9829
	Number of elements       = 53956
	Number of triangles      = 7722
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46234
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7789
	Number of elements       = 43295
	Number of triangles      = 5394
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37901
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1186
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 854
	Number of elements       = 4431
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3435
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9348
	Number of elements       = 51734
	Number of triangles      = 6812
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44922
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9531
	Number of elements       = 52330
	Number of triangles      = 7408
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44922
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7804
	Number of elements       = 43358
	Number of triangles      = 5386
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1200
	Number of elements       = 6311
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4979
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 527
	Number of elements       = 2661
	Number of triangles      = 690
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9183
	Number of elements       = 50871
	Number of triangles      = 6632
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44239
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9322
	Number of elements       = 51307
	Number of triangles      = 7068
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44239
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7927
	Number of elements       = 44116
	Number of triangles      = 5382
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 38734
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 868
	Number of elements       = 4530
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3534
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 527
	Number of elements       = 2661
	Number of triangles      = 690
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10181
	Number of elements       = 56797
	Number of triangles      = 6782
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 50015
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10671
	Number of elements       = 58561
	Number of triangles      = 8546
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 50015
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7741
	Number of elements       = 43010
	Number of triangles      = 5362
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37648
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 2692
	Number of elements       = 14435
	Number of triangles      = 2800
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11635
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 238
	Number of elements       = 1116
	Number of triangles      = 384
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 732
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1500
	Number of elements       = 7757
	Number of triangles      = 1986
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5771
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1564
	Number of elements       = 7881
	Number of triangles      = 2110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5771
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 1160
	Number of elements       = 6087
	Number of triangles      = 1308
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4779
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 360
	Number of elements       = 1635
	Number of triangles      = 718
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 917
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 44
	Number of elements       = 159
	Number of triangles      = 84
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 75
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 339
	Number of elements       = 1523
	Number of triangles      = 584
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 939
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 5):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 5):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 5):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 5):
	Number of nodes          = 711
	Number of elements       = 3685
	Number of triangles      = 844
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 2841
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 5):
	Number of nodes          = 1257
	Number of elements       = 6590
	Number of triangles      = 1424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5166
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file

Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


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


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Rib_Root, index = 1
	Name = Skin, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 46
Number of elements = 44
Number of triangle elements      = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes    = 47
Total number of elements = 44
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Rib_Root, index = 1
	Name = Skin, index = 2
	Name = Wing, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Rib_Root, index = 1
	Name = Skin, index = 2
	Name = Wing, index = 3
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 46
	Number of elements = 44
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 44
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 47
	Combined Number of elements = 45
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 44
Getting vortex lattice surface data
	VLM surface name - Skin_Top
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 3
	Surface 2: Number of points found for aero-spline = 6
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 2
	Property name - Rib_Root
	No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
	Property name - Skin
	No "material" specified for Property tuple Skin, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA supports.......
	Number of supports - 1
	Support name - ribSupport
	Done getting FEA supports

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

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim1
	Done getting FEA analyses

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

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

Writing Astros instruction file....
	Writing aeros card
	Writing analysis cards
	Writing constraint cards--each subcase individually
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
ok
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - VTail1
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - VTail2
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
	Section 1 of 2 (ID = 0)
	Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 2)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 0)
	  Control surface 1 of 1 
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice control surface data
	VLM control surface name - Elevator
	VLM control surface name - LeftAileron
	VLM control surface name - RightAileron
	VLM control surface name - Rudder
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 2)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 0)
	  Control surface 1 of 1 
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 28.284271 -nDiv 9 -maxR 7  -mesh2d > autoInputs.out
 Executing: ./aero.csh > aero.out
ok
test_outputs (test_cart3d.TestCart3D.test_outputs) ... ok
test_reenter (test_cart3d.TestCart3D.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Getting CFD functional.......
	Number of design variables - 1
	Objective name - Drag
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 Executing: ./aero.csh > aero.out
 Executing: ./aero.csh > aero.out
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.307131  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 Executing: ./aero.csh > aero.out
ok
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Mach
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_A
	Objective name - C_N
	Objective name - C_Y
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:05:17) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:05:18) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:05:19) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:05:21) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:05:21) Linearizing cut-cells
   (13:05:21) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:05:22) Computing gradients
   (13:05:30) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:05:31) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:05:32) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_D
	Objective name - C_L
	Objective name - C_S
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:05:33) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:05:34) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:05:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:05:37) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:05:37) Linearizing cut-cells
   (13:05:37) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:05:37) Computing gradients
   (13:05:45) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:05:47) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:05:48) 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_l
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:05:49) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:05:50) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:05:51) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:05:53) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:05:53) Linearizing cut-cells
   (13:05:53) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:05:53) Computing gradients
   (13:05:57) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:05:58) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:05:59) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_m
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:00) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:01) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:03) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:06:04) Linearizing cut-cells
   (13:06:04) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:06:04) Computing gradients
   (13:06:08) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:09) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:10) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_n
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:11) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:12) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:13) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:14) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:06:14) Linearizing cut-cells
   (13:06:14) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:06:15) Computing gradients
   (13:06:19) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:20) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:21) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_x
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:22) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:23) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:24) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:25) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:06:25) Linearizing cut-cells
   (13:06:25) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:06:25) Computing gradients
   (13:06:29) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:30) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:31) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_y
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:32) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:33) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:34) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:36) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:06:36) Linearizing cut-cells
   (13:06:36) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:06:36) Computing gradients
   (13:06:40) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:41) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:42) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_z
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:43) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:44) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:45) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:46) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:06:46) Linearizing cut-cells
   (13:06:46) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:06:47) Computing gradients
   (13:06:51) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:52) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:53) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1

Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - Mach
	Design Variable name - area
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_A
	Objective name - C_N
	Objective name - C_Y
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:55) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:06:56) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:06:57) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:07:00) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (13:07:00) Linearizing cut-cells
   (13:07:02) ... done
   o Number of simultaneous xsensit jobs:  2
   (13:07:02) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (13:07:10) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:07:11) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:07:12) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Wing1, index = 1
	Name = trailingEdge, index = 2

Writing FAST file ....
Finished writing FAST file

Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 9
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = nodeBody, index = 8
	Name = farfield, index = 9
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 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!
 700007E92000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 700007E92000 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
 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!
 700007E92000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 700007E92000 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
 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!
 700007E92000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 700007E92000 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
 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!
 700007E92000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 700007E92000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
ok
test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = nodeBody, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ok
test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

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


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

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


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_setInput (test_egadsTess.TestEGADS.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_egadsTess.TestEGADS.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 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:  0.119946
Creating surface mesh ...
Surface mesh seconds:  0.018447
Recovering boundaries...
Boundary recovery seconds:  0.080927
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.030313
Recovering Delaunayness...
Delaunay recovery seconds:  0.043438
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:  1.45299
Smoothing vertices...
Mesh smoothing seconds:  1.49981
Improving mesh...
Mesh improvement seconds:  0.036337

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

Output seconds:  0.00892
Total running seconds:  3.29167

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:  0.117311
Creating surface mesh ...
Surface mesh seconds:  0.019237
Recovering boundaries...
Boundary recovery seconds:  0.079071
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.030889
Recovering Delaunayness...
Delaunay recovery seconds:  0.045746
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:  1.51816
Smoothing vertices...
Mesh smoothing seconds:  1.41241
Improving mesh...
Mesh improvement seconds:  0.032184

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

Output seconds:  0.007785
Total running seconds:  3.26318

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

Writing MAPBC file ....
Finished writing MAPBC file


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

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 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          =     0.000   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       225       396
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

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

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


Writing vtk file ....

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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


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


Writing vtk file ....

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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


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


Writing vtk file ....

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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2600
	Number of elements       = 13864
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11106
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

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


Writing vtk file ....

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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

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


Writing vtk file ....

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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 438
	Number of elements       = 2179
	Number of triangles      = 644
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1535
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 936
	Number of elements       = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 3 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 8 Faces
EGADS    : Body 0 has 15 Edges
EGADS    : Body 0 has 8 Loops
EGADS    : Body 0 has 9 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 8 Faces
EGADS    : Body 1 has 15 Edges
EGADS    : Body 1 has 8 Loops
EGADS    : Body 1 has 9 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 2 Faces
EGADS    : Body 2 has 6 Edges
EGADS    : Body 2 has 2 Loops
EGADS    : Body 2 has 2 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        1        1   1 3 4 6
EGADS    :      3     Yes     0     0     1        1        1   1 2 4 7
EGADS    :      4     Yes     0     0     1        1        1   1 2 3
EGADS    :      5     Yes     0     0     1        1        1   1 6 7 8
EGADS    :      6     Yes     0     0     1        1        1   2 5 7 8
EGADS    :      7     Yes     0     0     1        1        1   3 5 6 8
EGADS    :      8     Yes     0     0     1        1        1   5 6 7
EGADS    :      9     Yes     1     0     1        0       10   10 11 12 13
EGADS    :     10     Yes     1     0     1        0       10   9 11 12 14
EGADS    :     11     Yes     1     0     1        0       10   9 10 12 15
EGADS    :     12     Yes     1     0     1        0       10   9 10 11
EGADS    :     13     Yes     1     0     1        0       10   9 14 15 16
EGADS    :     14     Yes     1     0     1        0       10   10 13 15 16
EGADS    :     15     Yes     1     0     1        0       10   11 13 14 16
EGADS    :     16     Yes     1     0     1        0       10   13 14 15
EGADS    :     17     Yes     2     0     1       NA       NA   18
EGADS    :     18     Yes     2     0     1       NA       NA   17

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 4 -3 -2
EGADS    :      2   3 7 -6 -5
EGADS    :      3   6 9 -1 -8
EGADS    :      4   -4 -9 -7
EGADS    :      5   -10 2 11 -12
EGADS    :      6   -11 5 13 -14
EGADS    :      7   -13 8 10 -15
EGADS    :      8   12 14 15
EGADS    :      9   16 19 -18 -17
EGADS    :     10   18 22 -21 -20
EGADS    :     11   21 24 -16 -23
EGADS    :     12   -19 -24 -22
EGADS    :     13   -25 17 26 -27
EGADS    :     14   -26 20 28 -29
EGADS    :     15   -28 23 25 -30
EGADS    :     16   27 29 30
EGADS    :     17   -31 -32 33 34
EGADS    :     18   -35 -34 36 32

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16
EGADS    :     17   17
EGADS    :     18   18

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 4 -3 -2
EGADS    :      2     Yes   3 7 -6 -5
EGADS    :      3     Yes   6 9 -1 -8
EGADS    :      4     Yes   -4 -9 -7
EGADS    :      5     Yes   -10 2 11 -12
EGADS    :      6     Yes   -11 5 13 -14
EGADS    :      7     Yes   -13 8 10 -15
EGADS    :      8     Yes   12 14 15
EGADS    :      9     Yes   16 19 -18 -17
EGADS    :     10     Yes   18 22 -21 -20
EGADS    :     11     Yes   21 24 -16 -23
EGADS    :     12     Yes   -19 -24 -22
EGADS    :     13     Yes   -25 17 26 -27
EGADS    :     14     Yes   -26 20 28 -29
EGADS    :     15     Yes   -28 23 25 -30
EGADS    :     16     Yes   27 29 30
EGADS    :     17     Yes   -31 -32 33 34
EGADS    :     18     Yes   -35 -34 36 32

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 5
EGADS    :      3     0     Yes     3     4        1   1 2
EGADS    :      4     0     Yes     2     4        1   1 4
EGADS    :      5     0     Yes     3     5        1   2 6
EGADS    :      6     0     Yes     5     6        1   2 3
EGADS    :      7     0     Yes     4     6        1   2 4
EGADS    :      8     0     Yes     5     1        1   3 7
EGADS    :      9     0     Yes     6     2        1   3 4
EGADS    :     10     0     Yes     1     7        1   5 7
EGADS    :     11     0     Yes     3     8        1   5 6
EGADS    :     12     0     Yes     7     8        1   5 8
EGADS    :     13     0     Yes     5     9        1   6 7
EGADS    :     14     0     Yes     8     9        1   6 8
EGADS    :     15     0     Yes     9     7        1   7 8
EGADS    :     16     1     Yes    10    11        1   9 11
EGADS    :     17     1     Yes    10    12        1   9 13
EGADS    :     18     1     Yes    12    13        1   9 10
EGADS    :     19     1     Yes    11    13        1   9 12
EGADS    :     20     1     Yes    12    14        1   10 14
EGADS    :     21     1     Yes    14    15        1   10 11
EGADS    :     22     1     Yes    13    15        1   10 12
EGADS    :     23     1     Yes    14    10        1   11 15
EGADS    :     24     1     Yes    15    11        1   11 12
EGADS    :     25     1     Yes    10    16        1   13 15
EGADS    :     26     1     Yes    12    17        1   13 14
EGADS    :     27     1     Yes    16    17        1   13 16
EGADS    :     28     1     Yes    14    18        1   14 15
EGADS    :     29     1     Yes    17    18        1   14 16
EGADS    :     30     1     Yes    18    16        1   15 16
EGADS    :     31     2   DEGEN    19    19        -   17
EGADS    :     32     2     Yes    20    19       NA   17 18
EGADS    :     33     2   DEGEN    20    20        -   17
EGADS    :     34     2     Yes    20    19       NA   17 18
EGADS    :     35     2   DEGEN    19    19        -   18
EGADS    :     36     2   DEGEN    20    20        -   18

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       3.77246052                0    0.00459131419
EGADS    :      2     Yes       5.90487498       7.07106781                0
EGADS    :      3     Yes                0                0                0
EGADS    :      4     Yes        4.0824829       7.07106781      0.123425948
EGADS    :      5     Yes       3.77001182                0                0
EGADS    :      6     Yes       5.90282524       7.07106781                0
EGADS    :      7     Yes       5.90487498                0                0
EGADS    :      8     Yes        4.0824829                0      0.123425948
EGADS    :      9     Yes       5.90282524                0                0
EGADS    :     10     Yes       11.5089842                0    0.00183652568
EGADS    :     11     Yes         12.36195       2.82842712                0
EGADS    :     12     Yes               10                0                0
EGADS    :     13     Yes       11.6329932       2.82842712     0.0493703791
EGADS    :     14     Yes       11.5080047                0                0
EGADS    :     15     Yes       12.3611301       2.82842712                0
EGADS    :     16     Yes         12.36195                0                0
EGADS    :     17     Yes       11.6329932                0     0.0493703791
EGADS    :     18     Yes       12.3611301                0                0
EGADS    :     19     Yes                0                0               80
EGADS    :     20     Yes                0                0                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 160
AFLR4    : Min Bounding Box Length     = 160
AFLR4    : Max Ref Bounding Box Length = 14.1421
AFLR4    : Min Ref Bounding Box Length = 0.890888
AFLR4    : Reference Length            = 0.890888
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 15.6122
AFLR4    : Abs Min Surf Spacing        = 0.00222722
AFLR4    : Min Surf Spacing            = 0.00445444
AFLR4    : Max Surf Spacing            = 0.0890888
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0                 STD
AFLR4    :          2            CAD geometry           0                 STD
AFLR4    :          3            CAD geometry           0                 STD
AFLR4    :          4            CAD geometry           0                 STD
AFLR4    :          5            CAD geometry           0                 STD
AFLR4    :          6            CAD geometry           0                 STD
AFLR4    :          7            CAD geometry           0                 STD
AFLR4    :          8            CAD geometry           0                 STD
AFLR4    :          9            CAD geometry           0                 STD
AFLR4    :         10            CAD geometry           0                 STD
AFLR4    :         11            CAD geometry           0                 STD
AFLR4    :         12            CAD geometry           0                 STD
AFLR4    :         13            CAD geometry           0                 STD
AFLR4    :         14            CAD geometry           0                 STD
AFLR4    :         15            CAD geometry           0                 STD
AFLR4    :         16            CAD geometry           0                 STD
AFLR4    :         17            CAD geometry           0            FARFIELD
AFLR4    :         18            CAD geometry           0            FARFIELD

AFLR4    : Case has 2 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4    : Component 2 includes Definitions 9 10 11 12 13 14 15 16

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=     12428
AFLR43   : Nodes             =      6220
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 22.6.0 x86_64
AFLR3    : Compile Date   11/01/23 @ 12:19PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6220         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                         Solid
UG3      :         12                         Solid
UG3      :         13                         Solid
UG3      :         14                         Solid
UG3      :         15                         Solid
UG3      :         16                         Solid
UG3      :         17                      FarField
UG3      :         18                      FarField
 
AFLR3    : CPU Time          =     0.012   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          =     0.128   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          =     3.578   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          =     1.331   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          =     0.061   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          =     5.297   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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 15

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 8

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 30

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 16

EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 34

EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 18

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Getting surface mesh for body 1 (of 7)
Getting surface mesh for body 2 (of 7)
Getting surface mesh for body 3 (of 7)
Getting surface mesh for body 4 (of 7)
Getting surface mesh for body 5 (of 7)
Getting surface mesh for body 6 (of 7)
 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!
 700007E92000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 700007E92000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes    = 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 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 Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1220
Number of elements = 2680
Number of triangle elements      = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1221
Total number of elements = 2680
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1220
	Number of elements = 2680
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 2680
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1221
	Combined Number of elements = 2681
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 2680
	Combined Elemental Quad4 = 0

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

Getting FEA properties.......
	Number of properties - 6
	Property name - Rib_Root
	Property name - Rib_Root_Point
	Property name - Ribs
	Property name - Skin
	Property name - Spar1
	Property name - Spar2
	Done getting FEA properties
Updating mesh element types based on properties input

'Smart_Restart' is ON
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh

Getting ZAERO UAIC Configurations.......
	Number of UAIC Configurations - 2

	UAIC Configuration: climb, id = 1
	- Mach Number : 0.200000
	- Reduced Freq: [0.020000, ... , 0.250000]

	UAIC Configuration: cruise, id = 2
	- Mach Number : 0.700000
	- Reduced Freq: [0.040000, ... , 0.350000]

Getting ZAERO Analysis Subcases.......
	Number of Analysis Subcases - 2

	Analysis Subcase: FlutterCruise, id = 1
	- Discipline : flutter
	- UAIC       : cruise

	Analysis Subcase: Trim, id = 2
	- Discipline : Trim
	- UAIC       : climb

Getting ZAERO Trim Variables.......
	Number of Trim Variables - 2

	Trim Variable: ANGLEA
	- Label : ALPHA
	- Value : free

	Trim Variable: URDD3
	- Label : NZ
	- Value : 1.0

	Updating StaticAeroelastic subcase: Trim
	- vectorToCG -> [0.345898, 1.652951, -0.041403]
	- weight -> 476456.149985
	- weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813290, 6179.981375, 19723.152207, 370546.335523]
ok

----------------------------------------------------------------------
Ran 143 tests in 602.973s

OK (skipped=10)
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest
+ ./execute_CTestRegression.sh
No options provided...defaulting to ALL
Running.... MINIMAL c-Tests
Running.... LINEARAERO c-Tests

=================================================
+ echo './avlTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./avlTest test;
+ ./avlTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: avlTest is hard coded to look for ../csmData/avlWingTail.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
	VLM control surface name - WingRightLE
	VLM control surface name - WingRightTE
	VLM control surface name - Tail
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Writing surface - Vertical_Tail (ID = 1)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 


Running AVL!


Value of Cltot = 0.619913

StripForces

Wing = {"Xle":[1.565221892029e+00,1.512117367810e+00,1.409527304938e+00,1.264443046659e+00,1.086751845411e+00,8.885630629098e-01,6.833829371601e-01,4.851941546545e-01,3.075029533974e-01,1.624186951053e-01,5.982863221714e-02,6.724107980270e-03,6.724107971058e-03,5.982863219013e-02,1.624186950623e-01,3.075029533414e-01,4.851941545893e-01,6.833829370902e-01,8.885630628399e-01,1.086751845346e+00,1.264443046603e+00,1.409527304895e+00,1.512117367783e+00,1.565221892020e+00],"Yle":[-3.856416046770e+00,-3.725576361740e+00,-3.472813499993e+00,-3.115352832843e+00,-2.677554714026e+00,-2.189254361841e+00,-1.683728638332e+00,-1.195428286135e+00,-7.576301672945e-01,-4.001695001132e-01,-1.474066383261e-01,-1.656695325269e-02,1.656695322999e-02,1.474066382596e-01,4.001695000074e-01,7.576301671565e-01,1.195428285974e+00,1.683728638159e+00,2.189254361668e+00,2.677554713865e+00,3.115352832706e+00,3.472813499887e+00,3.725576361674e+00,3.856416046747e+00],"Zle":[2.486597711706e-01,2.402232939480e-01,2.239252714835e-01,2.008763870743e-01,1.726473841027e-01,1.411620224705e-01,1.085659775407e-01,7.708061590764e-02,4.885161293456e-02,2.580272852328e-02,9.504706056265e-03,1.068228830823e-03,1.068228829360e-03,9.504706051974e-03,2.580272851645e-02,4.885161292566e-02,7.708061589728e-02,1.085659775295e-01,1.411620224593e-01,1.726473840924e-01,2.008763870654e-01,2.239252714767e-01,2.402232939437e-01,2.486597711692e-01],"Chord":[9.710071581587e-01,9.928137666999e-01,1.034940899447e+00,1.094517661923e+00,1.167483996219e+00,1.248867367237e+00,1.333121632734e+00,1.414505003754e+00,1.487471338054e+00,1.547048100535e+00,1.589175233289e+00,1.610981841837e+00,1.610981841841e+00,1.589175233300e+00,1.547048100553e+00,1.487471338077e+00,1.414505003781e+00,1.333121632763e+00,1.248867367266e+00,1.167483996246e+00,1.094517661946e+00,1.034940899465e+00,9.928137667110e-01,9.710071581625e-01],"Area":[6.420432739224e-02,1.924649501823e-01,3.191588402418e-01,4.398794051499e-01,5.463997379092e-01,6.272332670617e-01,6.695492724342e-01,6.620092145623e-01,5.978048871833e-01,4.770843222898e-01,3.080744268775e-01,1.065203328294e-01,1.065203327570e-01,3.080744268129e-01,4.770843222394e-01,5.978048871514e-01,6.620092145502e-01,6.695492724407e-01,6.272332670835e-01,5.463997379421e-01,4.398794051895e-01,3.191588402846e-01,1.924649502262e-01,6.420432743628e-02],"c_cl":[1.751976980131e-01,4.816388142980e-01,7.134545983425e-01,8.955798774854e-01,1.045275116632e+00,1.165642609066e+00,1.251488483106e+00,1.294909342036e+00,1.290147495293e+00,1.237589733955e+00,1.147354354590e+00,1.069716379938e+00,1.027204841580e+00,9.123069911140e-01,8.271224835189e-01,7.465072383829e-01,6.622506856527e-01,5.718077594720e-01,4.773770050905e-01,3.839108464455e-01,2.965810831880e-01,2.166269422082e-01,1.372747954618e-01,4.847522879861e-02],"ai":[2.423376448062e-01,1.891573605670e-01,1.387726073610e-01,1.136377561111e-01,1.056109957988e-01,1.077519869781e-01,1.163918473304e-01,1.297918603655e-01,1.465983278745e-01,1.624995174599e-01,1.707158095744e-01,1.656351191924e-01,-7.833998870069e-02,-4.190817556549e-02,-1.699095118252e-02,-7.589503463268e-04,7.958849673323e-03,1.019416065192e-02,8.688915578663e-03,6.053380335362e-03,5.120395027030e-03,9.296755297868e-03,2.004804046071e-02,3.330492577589e-02],"cl_norm":[2.044051829732e-01,5.494672225944e-01,7.808579037671e-01,9.268407130709e-01,1.014078158136e+00,1.057019341176e+00,1.062951411332e+00,1.036333388588e+00,9.816462634657e-01,9.051794884122e-01,8.167547094734e-01,7.499676468301e-01,7.211772113982e-01,6.503467495440e-01,6.057660560789e-01,5.686988847409e-01,5.305932247986e-01,4.861412346272e-01,4.332732553839e-01,3.727603475171e-01,3.071901673660e-01,2.373206031159e-01,1.568074209169e-01,5.666485024198e-02],"cl":[1.803741931756e-01,4.848688546459e-01,6.890559834545e-01,8.178762563197e-01,8.948575908405e-01,9.327503738523e-01,9.379850374388e-01,9.144963748400e-01,8.662385668551e-01,7.987616435483e-01,7.207325646090e-01,6.617973538495e-01,6.363916792640e-01,5.738884333905e-01,5.345488897546e-01,5.018395375447e-01,4.682137871232e-01,4.289878157188e-01,3.823352848870e-01,3.289366049983e-01,2.710752133784e-01,2.094198967381e-01,1.383722840117e-01,5.000302093687e-02],"cd":[4.708816796028e-03,1.893013552462e-02,2.388458719217e-02,2.809788812561e-02,3.450496926232e-02,4.310977683936e-02,5.296690620751e-02,6.273588035908e-02,7.092746653695e-02,7.623132904850e-02,7.793919402374e-02,1.330641046361e-01,7.642533954139e-02,1.575280561795e-02,1.020926164300e-02,5.734996040044e-03,2.453990236882e-03,7.034156944394e-05,-1.681061755697e-03,-2.904871637687e-03,-3.696799546922e-03,-4.291551637882e-03,-4.755989795807e-03,-4.178738547375e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-6.175122770636e-02,-1.541367450249e-01,-1.990020049078e-01,-2.179523703798e-01,-2.259241556000e-01,-2.291785023832e-01,-2.301045091168e-01,-2.293937884749e-01,-2.266765134794e-01,-2.205756980543e-01,-2.089282623641e-01,-1.947906406100e-01,-1.847119741766e-01,-1.559354818193e-01,-1.355315131375e-01,-1.232795365876e-01,-1.170486694971e-01,-1.141869860843e-01,-1.128288355904e-01,-1.117855412669e-01,-1.094863434133e-01,-1.016126232940e-01,-7.889656776610e-02,-3.215621313961e-02],"cm_LE":[-9.907391078332e-02,-2.553625521061e-01,-3.443180862961e-01,-3.917771248735e-01,-4.170475207536e-01,-4.288879437378e-01,-4.309998082914e-01,-4.249313258859e-01,-4.112512348868e-01,-3.899661415022e-01,-3.610798550199e-01,-3.345295675168e-01,-3.190696575594e-01,-2.776668920570e-01,-2.496150543393e-01,-2.306580335187e-01,-2.170714278267e-01,-2.053105443164e-01,-1.932221818518e-01,-1.798625218874e-01,-1.643057066258e-01,-1.427050164900e-01,-1.051753523064e-01,-4.137433282282e-02],"C.P.x/c":[5.923506801011e-01,5.678936810397e-01,5.388038268097e-01,5.164857534324e-01,5.024693961503e-01,4.957018606561e-01,4.953178888067e-01,5.008416597223e-01,5.116790825907e-01,5.261470832205e-01,5.398832002650e-01,5.443357803971e-01,5.402488831882e-01,5.217174153486e-01,5.035437183300e-01,4.956552889212e-01,4.999897967897e-01,5.161776906017e-01,5.451044281036e-01,5.898391652626e-01,6.538965497759e-01,7.352099770687e-01,8.201760893058e-01,8.930854083838e-01]}

Vertical_Tail = {"Xle":[5.481142821257e+00,5.457739875756e+00,5.413224828118e+00,5.351955121359e+00,5.279928261269e+00,5.204194738752e+00,5.132167878660e+00,5.070898171897e+00,5.026383124254e+00,5.002980178746e+00],"Yle":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"Zle":[1.462285642514e+00,1.415479751513e+00,1.326449656236e+00,1.203910242719e+00,1.059856522538e+00,9.083894775049e-01,7.643357573198e-01,6.417963437947e-01,5.527662485071e-01,5.059603574925e-01],"Chord":[7.291641787429e-01,7.525671242437e-01,7.970821718820e-01,8.583518786405e-01,9.303787387310e-01,1.006112261248e+00,1.078139121340e+00,1.139408828103e+00,1.183923875746e+00,1.207326821254e+00],"Area":[1.727730179136e-02,5.174997687051e-02,8.537019049526e-02,1.158415604078e-01,1.391867381176e-01,1.505166423044e-01,1.455036346588e-01,1.220345306258e-01,8.141205112924e-02,2.860720599220e-02],"c_cl":[4.143502484418e-02,1.146121890397e-01,1.669674480704e-01,2.000258625574e-01,2.165069436647e-01,2.173612378313e-01,2.020982864238e-01,1.687203348324e-01,1.143884794128e-01,4.073751989356e-02],"ai":[2.065296924524e-01,1.849180223915e-01,1.591285664757e-01,1.456224964407e-01,1.435231644006e-01,1.506386553619e-01,1.666466052405e-01,1.914179167692e-01,2.193221173426e-01,2.365321328628e-01],"cl_norm":[6.579957348175e-02,1.763463053600e-01,2.425545992661e-01,2.698370559984e-01,2.694590983036e-01,2.501591871286e-01,2.170544160378e-01,1.714623014102e-01,1.118766125248e-01,3.907064104103e-02],"cl":[5.682537081788e-02,1.522949719002e-01,2.094733190132e-01,2.330348048801e-01,2.327083956798e-01,2.160407403860e-01,1.874510278160e-01,1.480770823176e-01,9.661810337317e-02,3.374191575671e-02],"cd":[4.670566079259e-03,1.374698956983e-02,1.845844898550e-02,2.032218684722e-02,2.072187092669e-02,2.023884851594e-02,1.896705322928e-02,1.657142171116e-02,1.222733795464e-02,5.106244760906e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-3.303465544546e-02,-8.761746958841e-02,-1.194746602282e-01,-1.341488123562e-01,-1.380350789961e-01,-1.339349413679e-01,-1.218867053323e-01,-1.002593790934e-01,-6.716156843018e-02,-2.373448304332e-02],"cm_LE":[-4.232877133358e-02,-1.126299441676e-01,-1.539951982649e-01,-1.724118490115e-01,-1.757829360722e-01,-1.683239687782e-01,-1.510824211715e-01,-1.228726806386e-01,-8.171902803714e-02,-2.878672165371e-02],"C.P.x/c":[8.313363814436e-01,8.253142634666e-01,8.203574125382e-01,8.256599853196e-01,8.431675932571e-01,8.699522420103e-01,9.002322593393e-01,9.270755982235e-01,9.451240614896e-01,9.534124326092e-01]}


real	0m0.826s
user	0m0.477s
sys	0m0.140s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./avlTest passed (as expected)
=============================================


=================================================
+ echo './msesTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./msesTest test;
+ ./msesTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm

Value of CL = 0.276892 

real	0m1.534s
user	0m1.340s
sys	0m0.095s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./msesTest passed (as expected)
=============================================


=================================================
+ echo './frictionTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./frictionTest test;
+ ./frictionTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: frictionTest is hard coded to look for ../csmData/frictionWingTailFuselage.csm
To not make system calls to the friction executable the second command line option may be supplied - 0 = no analysis , >0 run analysis (default).

Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2


Running FRICTION!


Value of CDfric = 0.009900

Value of CDfric = 0.009190

real	0m0.705s
user	0m0.339s
sys	0m0.048s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./frictionTest passed (as expected)
=============================================

Running.... MESH c-Tests
Running.... CFD c-Tests

=================================================
+ echo './fun3dAFLR2Test test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dAFLR2Test test;
+ ./fun3dAFLR2Test 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: fun3dAFLR2Test is hard coded to look for ../csmData/cfd2D.csm
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mquad                       = 1         
UG PARAM : mpp                         = 3         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       841         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       841       841
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       168       338
AFLR2 IG : Nodes, Faces      =       336       674
AFLR2 IG : Nodes, Faces      =       504      1010
AFLR2 IG : Nodes, Faces      =       617      1236
AFLR2 IG : Nodes, Faces      =       672      1346
AFLR2 IG : Nodes, Faces      =       741      1484
AFLR2 IG : Nodes, Faces      =       803      1608
AFLR2 IG : Nodes, Faces      =       840      1682
AFLR2 IG : Nodes, Faces      =       841      1684
AFLR2 IG : Nodes, Faces      =       845      1684
AFLR2 IG : Nodes, Faces      =       841       841
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       841       841
AFLR2 GGp: Nodes, Faces      =      1648      2455
AFLR2 GGp: Nodes, Faces      =      2446      4051
AFLR2 GGp: Nodes, Faces      =      3257      5673
AFLR2 GGp: Nodes, Faces      =      4054      7267
AFLR2 GGp: Nodes, Faces      =      4821      8801
AFLR2 GGp: Nodes, Faces      =      5577     10313
AFLR2 GGp: Nodes, Faces      =      6325     11809
AFLR2 GGp: Nodes, Faces      =      7053     13265
AFLR2 GGp: Nodes, Faces      =      7732     14623
AFLR2 GGp: Nodes, Faces      =      8394     15947
AFLR2 GGp: Nodes, Faces      =      9022     17203
AFLR2 GGp: Nodes, Faces      =      9620     18399
AFLR2 GGp: Nodes, Faces      =     10176     19511
AFLR2 GGp: Nodes, Faces      =     10689     20537
AFLR2 GGp: Nodes, Faces      =     11181     21521
AFLR2 GGp: Nodes, Faces      =     11646     22451
AFLR2 GGp: Nodes, Faces      =     12098     23355
AFLR2 GGp: Nodes, Faces      =     12529     24217
AFLR2 GGp: Nodes, Faces      =     12943     25045
AFLR2 GGp: Nodes, Faces      =     13331     25821
AFLR2 GGp: Nodes, Faces      =     13710     26579
AFLR2 GGp: Nodes, Faces      =     14061     27281
AFLR2 GGp: Nodes, Faces      =     14424     28007
AFLR2 GGp: Nodes, Faces      =     14774     28707
AFLR2 GGp: Nodes, Faces      =     15107     29373
AFLR2 GGp: Nodes, Faces      =     15422     30003
AFLR2 GGp: Nodes, Faces      =     15707     30573
AFLR2 GGp: Nodes, Faces      =     15982     31123
AFLR2 GGp: Nodes, Faces      =     16233     31625
AFLR2 GGp: Nodes, Faces      =     16473     32105
AFLR2 GGp: Nodes, Faces      =     16685     32529
AFLR2 GGp: Nodes, Faces      =     16898     32955
AFLR2 GGp: Nodes, Faces      =     17104     33367
AFLR2 GGp: Nodes, Faces      =     17291     33741
AFLR2 GGp: Nodes, Faces      =     17468     34095
AFLR2 GGp: Nodes, Faces      =     17627     34413
AFLR2 GGp: Nodes, Faces      =     17781     34721
AFLR2 GGp: Nodes, Faces      =     17929     35017
AFLR2 GGp: Nodes, Faces      =     18060     35279
AFLR2 GGp: Nodes, Faces      =     18186     35531
AFLR2 GGp: Nodes, Faces      =     18292     35743
AFLR2 GGp: Nodes, Faces      =     18403     35965
AFLR2 GGp: Nodes, Faces      =     18499     36157
AFLR2 GGp: Nodes, Faces      =     18568     36295
AFLR2 GGp: Nodes, Faces      =     18603     36365
AFLR2 GGp: Nodes, Faces      =     18615     36389
 
AFLR2    : CPU Time          =     0.048   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     18615     36389
AFLR2 QI : Nodes, Faces      =     18608      1893
AFLR2 QI : Nodes, Faces      =     18608     17241
AFLR2 QI : Nodes, Faces      =     18608     36375
AFLR2 QI : Nodes, Faces      =     18606      1789
AFLR2 QI : Nodes, Faces      =     18606     17291
AFLR2 QI : Nodes, Faces      =     18606     36371
AFLR2 QI : Nodes, Faces      =     18604      1971
AFLR2 QI : Nodes, Faces      =     18604     17198
AFLR2 QI : Nodes, Faces      =     18604     36367
AFLR2 QI : Nodes, Faces      =     18604      2161
AFLR2 QI : Nodes, Faces      =     18604     17103
AFLR2 QI : Nodes, Faces      =     18604     36367
AFLR2 QI : Nodes, Faces      =     18604      2149
AFLR2 QI : Nodes, Faces      =     18604     17109
AFLR2 QI : Nodes, Faces      =     18604      2149
AFLR2 QI : Nodes, Faces      =     18604     17109
 
AFLR2    : CPU Time          =     0.023   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 18604
Number of elements = 20099
Number of tris = 2149
Number of quad = 17109

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

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - TunnelWall
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Creating a 3D volume mesh from a 2D surface
	Number of Nodes =  37208
	Number of Prisms =  2149
	Number of Hexahedral =  17109

Writing AFLR3 file ....
Finished writing AFLR3 file


Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
 NOT Running fun3d!

real	0m1.407s
user	0m1.128s
sys	0m0.478s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./fun3dAFLR2Test passed (as expected)
=============================================


=================================================
+ echo './fun3dTetgenTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dTetgenTest test;
+ ./fun3dTetgenTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: fun3dTetgenTest is hard coded to look for ../csmData/cfdMultiBody.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 9610
Number of elements = 19216
Number of triangle elements      = 19216
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 6142
Number of elements = 12280
Number of triangle elements      = 12280
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 265
Number of elements = 526
Number of triangle elements      = 526
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 16017
Total number of elements = 32022
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 - 16017, elements - 32022
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.13387
Creating surface mesh ...
Surface mesh seconds:  0.02889
Recovering boundaries...
Boundary recovery seconds:  0.101225
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.036189
Recovering Delaunayness...
Delaunay recovery seconds:  0.052004
Refining mesh...
  21350 insertions, added 16804 points, 756241 tetrahedra in queue.
  7109 insertions, added 2842 points, 312650 tetrahedra in queue.
Refinement seconds:  1.25302
Smoothing vertices...
Mesh smoothing seconds:  1.82155
Improving mesh...
Mesh improvement seconds:  0.039938

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

Output seconds:  0.008779
Total running seconds:  3.47646

Statistics:

  Input points: 16017
  Input facets: 32022
  Input segments: 48033
  Input holes: 2
  Input regions: 0

  Mesh points: 37140
  Mesh tetrahedra: 179120
  Mesh faces: 374251
  Mesh faces on exterior boundary: 32022
  Mesh faces on input facets: 32022
  Mesh edges on input segments: 48033
  Steiner points inside domain: 21123

Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Boundary condition name - Farfield
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
 NOT Running fun3d!

real	0m6.081s
user	0m6.439s
sys	0m0.310s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./fun3dTetgenTest passed (as expected)
=============================================

Running.... STRUCTURE c-Tests

=================================================
+ echo './interferenceTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./interferenceTest test;
+ ./interferenceTest
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Note: interferenceTest uses ../csmData/interference.csm
 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
  1:  1.000000e+00  Box
  2:  5.849745e-01  Sphere
  3:  7.191810e-01  Cylinder
  4:  4.000000e+01  OuterBox

  0.000000e+00  -2.741045e-02   0.000000e+00   0.000000e+00 
 -2.741045e-02   0.000000e+00   0.000000e+00  -2.592150e-02 
  0.000000e+00   0.000000e+00   0.000000e+00   0.000000e+00 
  0.000000e+00  -2.592150e-02   0.000000e+00   1.000000e+00 

 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
  1:  1.000000e+00  Box
  2:  5.886895e-01  Sphere
  3:  7.235323e-01  Cylinder

  0.000000e+00  -2.061201e-02   0.000000e+00 
 -2.061201e-02   0.000000e+00   0.000000e+00 
  0.000000e+00   0.000000e+00   0.000000e+00 


real	0m2.487s
user	0m3.962s
sys	0m0.091s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./interferenceTest passed (as expected)
=============================================


=================================================
+ echo './hsmCantileverPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmCantileverPlateTest test;
+ ./hsmCantileverPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: hsmCantileverPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 40
	Number of elements = 51
	Elemental Tria3 = 0
	Elemental Quad4 = 27

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	No "material" specified for Property tuple plate, defaulting to an index of 1
	Done getting FEA properties

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

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

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

Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
 Matrix Non-zero Entries = 1313

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   1*   0.326E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   1*   0.438E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2    0.274E+01  0.521E+01  0.106E-07    0.096  ddx @ (   1.00   0.07   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   2*   0.777E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   3    0.202E+01  0.439E+01  0.928E-07    0.114  ddz @ (   1.00   0.03   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.623E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.163E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.167E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4    0.192E+01  0.476E+01  0.126E-07    0.105  ddz @ (   1.00   0.03   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.451E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.394E+01  0.254E-07    0.127  ddz @ (   1.00   0.07   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.638E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6    0.156E+01  0.300E+01  0.112E-06    0.166  ddx @ (   1.00   0.03   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   6*   0.193E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   6*   0.272E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7    0.103E+01  0.323E+01  0.345E-07    0.155  ddx @ (   1.00   0.07   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.435E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8    0.756E+00  0.259E+01  0.139E-07    0.193  ddx @ (   1.00   0.03   0.00)
   8*   0.295E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.350E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.587E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9    0.678E+00  0.179E+01  0.639E-07    0.279  ddx @ (   0.89   0.10   0.00)
   9*   0.330E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.457E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.167E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   9*   0.264E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10    0.452E+00  0.171E+01  0.499E-07    0.292  ddz @ (   1.00   0.10   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.393E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.257E+00  0.120E+01  0.614E-08    0.417  ddz @ (   1.00   0.10   0.00)
  11*   0.206E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.283E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  11*   0.488E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  12    0.131E+00  0.647E+00  0.288E-08    0.772  ddz @ (   0.89   0.10   0.00)
  12*   0.238E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.357E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.849E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13    0.393E-01  0.238E+00  0.325E-07    1.000  ddx @ (   1.00   0.03   0.00)
  13*   0.335E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  13*   0.936E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
  14    0.475E-03  0.514E-02  0.635E-07    1.000  ddx @ (   1.00   0.00   0.00)
  15    0.893E-06  0.651E-06  0.135E-08    1.000  drx @ (   1.00   0.00   0.00)
  16    0.573E-10  0.216E-09  0.140E-11    1.000  ddx @ (   0.44   0.10   0.00)
  17    0.179E-15  0.693E-15  0.745E-15    1.000  dps @ (   0.78   0.00   0.00)

 Converging n vectors ...
 it =  1    dn =  0.193E+01   rlx = 1.000  (   9 )
 it =  2    dn =  0.516E-15   rlx = 1.000  (  13 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.285E+01   rlx = 0.351  (  24 )
 it =  2    de =  0.269E+01   rlx = 0.372  (  37 )
 it =  3    de =  0.249E+01   rlx = 0.402  (  21 )
 it =  4    de =  0.179E+01   rlx = 0.559  (  21 )
 it =  5    de =  0.954E+00   rlx = 1.000  (  21 )
 it =  6    de =  0.152E+00   rlx = 1.000  (  21 )
 it =  7    de =  0.887E-03   rlx = 1.000  (  21 )
 it =  8    de =  0.177E-09   rlx = 1.000  (  21 )
 it =  9    de =  0.876E-16   rlx = 1.000  (  28 )

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

real	0m0.925s
user	0m0.496s
sys	0m0.055s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmSimplePlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmSimplePlateTest test;
+ ./hsmSimplePlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: hsmTest2 is hard coded to look for ../csmData/feaSimplePlate.csm
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Number of nodal coordinates = 100
	Number of elements = 198
	Elemental Tria3 = 162
	Elemental Quad4 = 0

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	No "material" specified for Property tuple plate, defaulting to an index of 1
	Done getting FEA properties

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

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

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

Max Adjacency set to = 7
MaxDim = 36, numBCEdge = 0, numBCNode = 36, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 36
->HSMSOL
 Matrix Non-zero Entries = 8026

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.609E+00  0.519E+01  0.260E+01    0.096  ddy @ (   0.28   0.25   0.00)
   1*   0.571E-01  0.000E+00  0.000E+00    1.000  drz @ (   0.17   0.11   0.00)
   1*   0.159E-01  0.000E+00  0.000E+00    1.000  drz @ (   0.17   0.11   0.00)
   1*   0.254E-02  0.000E+00  0.000E+00    1.000  drz @ (   0.11   0.14   0.00)
   1*   0.838E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.06   0.14   0.00)
   2    0.768E-02  0.754E+00  0.102E+01    0.492  dps @ (   0.00   0.00   0.00)
   2*   0.336E-03  0.000E+00  0.000E+00    1.000  drx @ (   0.06   0.06   0.00)
   2*   0.690E-06  0.000E+00  0.000E+00    1.000  drz @ (   0.06   0.08   0.00)
   3    0.252E-02  0.204E+00  0.299E+00    1.000  dps @ (   0.50   0.03   0.00)
   3*   0.181E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.39   0.11   0.00)
   3*   0.675E-06  0.000E+00  0.000E+00    1.000  drx @ (   0.44   0.03   0.00)
   4    0.108E-03  0.157E-01  0.567E-01    1.000  dps @ (   0.39   0.14   0.00)
   4*   0.249E-05  0.000E+00  0.000E+00    1.000  drx @ (   0.44   0.22   0.00)
   5    0.103E-05  0.374E-03  0.159E-02    1.000  dps @ (   0.06   0.06   0.00)
   6    0.139E-08  0.994E-07  0.421E-06    1.000  dps @ (   0.50   0.00   0.00)
   7    0.106E-15  0.467E-13  0.133E-12    1.000  dps @ (   0.50   0.00   0.00)

 Converging n vectors ...
 it =  1    dn =  0.117E+01   rlx = 1.000  (  66 )
 it =  2    dn =  0.327E-15   rlx = 1.000  (  81 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.357E+00   rlx = 1.000  (  94 )
 it =  2    de =  0.167E+00   rlx = 1.000  (  67 )
 it =  3    de =  0.245E-01   rlx = 1.000  (  76 )
 it =  4    de =  0.567E-02   rlx = 1.000  (  59 )
 it =  5    de =  0.192E-02   rlx = 1.000  (  59 )
 it =  6    de =  0.648E-03   rlx = 1.000  (  59 )
 it =  7    de =  0.219E-03   rlx = 1.000  (  59 )
 it =  8    de =  0.740E-04   rlx = 1.000  (  59 )
 it =  9    de =  0.250E-04   rlx = 1.000  (  59 )
 it = 10    de =  0.845E-05   rlx = 1.000  (  59 )
 it = 11    de =  0.286E-05   rlx = 1.000  (  59 )
 it = 12    de =  0.965E-06   rlx = 1.000  (  59 )
 it = 13    de =  0.326E-06   rlx = 1.000  (  59 )
 it = 14    de =  0.110E-06   rlx = 1.000  (  59 )
 it = 15    de =  0.372E-07   rlx = 1.000  (  59 )
 it = 16    de =  0.126E-07   rlx = 1.000  (  59 )
 it = 17    de =  0.425E-08   rlx = 1.000  (  59 )
 it = 18    de =  0.144E-08   rlx = 1.000  (  59 )
 it = 19    de =  0.485E-09   rlx = 1.000  (  59 )
 it = 20    de =  0.164E-09   rlx = 1.000  (  59 )

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

real	0m0.968s
user	0m0.833s
sys	0m0.053s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmJoinedPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmJoinedPlateTest test;
+ ./hsmJoinedPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: hsmJoinedPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 40
	Number of elements = 56
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	No "material" specified for Property tuple plate, defaulting to an index of 1
	Done getting FEA properties

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

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

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

Max Adjacency set to = 16
MaxDim = 13, numBCEdge = 2, numBCNode = 4, numJoint = 13
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
 Matrix Non-zero Entries = 1242

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   1*   0.325E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.05   0.00)
   1*   0.434E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2    0.274E+01  0.521E+01  0.118E-07    0.096  ddx @ (   1.00   0.05   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   2*   0.772E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3    0.202E+01  0.439E+01  0.107E-06    0.114  ddz @ (   1.00   0.05   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3*   0.622E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3*   0.162E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3*   0.163E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4    0.192E+01  0.476E+01  0.147E-07    0.105  ddz @ (   1.00   0.05   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.448E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.395E+01  0.296E-07    0.127  ddz @ (   1.00   0.05   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5*   0.636E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   6    0.156E+01  0.301E+01  0.131E-06    0.166  ddx @ (   1.00   0.05   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.191E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.265E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7    0.103E+01  0.323E+01  0.408E-07    0.155  ddx @ (   1.00   0.05   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.432E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8    0.757E+00  0.260E+01  0.162E-07    0.192  ddx @ (   1.00   0.05   0.00)
   8*   0.296E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.351E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.586E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9    0.680E+00  0.181E+01  0.753E-07    0.276  ddx @ (   0.88   0.00   0.00)
   9*   0.329E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.452E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9*   0.159E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   9*   0.238E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10    0.457E+00  0.172E+01  0.586E-07    0.290  ddz @ (   1.00   0.10   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.392E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.258E+00  0.122E+01  0.666E-08    0.411  ddz @ (   1.00   0.10   0.00)
  11*   0.207E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.284E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.486E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12    0.135E+00  0.660E+00  0.377E-08    0.758  ddz @ (   0.88   0.00   0.00)
  12*   0.242E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.368E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.869E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13    0.430E-01  0.257E+00  0.505E-07    1.000  ddx @ (   1.00   0.05   0.00)
  13*   0.395E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  13*   0.128E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13*   0.196E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
  14    0.656E-03  0.680E-02  0.885E-07    1.000  ddx @ (   1.00   0.00   0.00)
  15    0.156E-05  0.177E-05  0.268E-10    1.000  ddx @ (   1.00   0.10   0.00)
  16    0.273E-09  0.106E-08  0.893E-11    1.000  ddx @ (   0.50   0.05   0.00)
  17    0.138E-15  0.353E-15  0.907E-15    1.000  dps @ (   0.38   0.10   0.00)

 Converging n vectors ...
 it =  1    dn =  0.197E+01   rlx = 1.000  (  17 )
 it =  2    dn =  0.866E-15   rlx = 1.000  (  18 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.753E+01   rlx = 0.133  (   1 )
 it =  2    de =  0.309E+01   rlx = 0.324  (  20 )
 it =  3    de =  0.324E+01   rlx = 0.309  (   2 )
 it =  4    de =  0.226E+01   rlx = 0.443  (   2 )
 it =  5    de =  0.140E+01   rlx = 0.716  (   4 )
 it =  6    de =  0.660E+00   rlx = 1.000  (   2 )
 it =  7    de =  0.860E-01   rlx = 1.000  (   4 )
 it =  8    de =  0.228E-03   rlx = 1.000  (   2 )
 it =  9    de =  0.428E-11   rlx = 1.000  (   4 )

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

real	0m0.630s
user	0m0.466s
sys	0m0.057s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmJoinedPlateTest passed (as expected)
=============================================

Running.... AEROELASTIC c-Tests
=================================================
Did not run examples for:

awave
pointwise
Mystran
=================================================

All tests pass!


=================================================
=================================================
+ ./execute_PyTestRegression.sh

=================================================
Using python : /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/python
=================================================

No options provided...defaulting to ALL
Running.... LINEARAERO PyTests

avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/avl

=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
CXtot   0.0006119078685747781
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	0m0.987s
user	0m0.670s
sys	0m0.442s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_AutoSpan_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_AutoSpan_PyTest.py test;
+ python -u avl_AutoSpan_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wing3, index = 3
Getting vortex lattice surface data
	VLM surface name - Wing1
	VLM surface name - Wing2
	VLM surface name - Wing3
	Done getting vortex lattice surface data
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Writing surface - Wing1 (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Wing2 (ID = 1)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 1)
	Section 3 of 7 (ID = 2)
	Section 4 of 7 (ID = 3)
	Section 5 of 7 (ID = 4)
	Section 6 of 7 (ID = 5)
	Section 7 of 7 (ID = 6)
Writing surface - Wing3 (ID = 2)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 3)
	  Control surface 1 of 1 
	Section 3 of 7 (ID = 4)
	  Control surface 1 of 1 
	Section 4 of 7 (ID = 1)
	Section 5 of 7 (ID = 5)
	  Control surface 1 of 1 
	Section 6 of 7 (ID = 6)
	  Control surface 1 of 1 
	Section 7 of 7 (ID = 2)
CXtot   -0.04120015370847253
CYtot   -2.245651489758113e-10
CZtot   -1.125018809209588
Cltot   -1.249805144528618e-09
Cmtot   -1.95474126745608
Cntot   1.91472801895405e-10
Cl'tot  -1.246273131991175e-09
Cn'tot  2.132557470099783e-10
CLtot   1.124128421567995
CDtot   0.06082816423341975
CDvis   0.0
CLff    1.12310544319429
CYff    -2.724509541923909e-10
CDind   0.06082816423341975
CDff    -0.2032091360666646
e       -0.3293037505986863

real	0m10.508s
user	0m13.394s
sys	0m8.013s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_AutoSpan_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_DesignSweep_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_DesignSweep_PyTest.py test;
+ python -u avl_DesignSweep_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002572533601556648
Cl = 0.2009337808875902
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002586364230247704
Cl = 0.2015191856817234
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002609799718822109
Cl = 0.2025075296435714
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002643444008430636
Cl = 0.2039185811661179
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002688200921004308
Cl = 0.2057816377793011
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002745342060022159
Cl = 0.2081373840562402
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002816610334305117
Cl = 0.2110406736708043
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002904376657741239
Cl = 0.2145646488018515
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003011879793049474
Cl = 0.2188068842337504
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.0031436020345932
Cl = 0.2238987294818338
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003305877285459626
Cl = 0.2300199286489827
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003507917885480169
Cl = 0.2374223860299378
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.00376364367726804
Cl = 0.246470714274774
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004095167898235838
Cl = 0.2577158067750639
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004540047408144653
Cl = 0.2720394012166652
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.005168237926862111
Cl = 0.2909701507466489
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.006128930715340598
Cl = 0.3174875485939033
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.007818359051284723
Cl = 0.358607891992251
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.01186220444375436
Cl = 0.4382638635248143
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002572533601556648
Cl = 0.2009337808875902
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002586364230247704
Cl = 0.2015191856817234
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002609799718822109
Cl = 0.2025075296435714
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002643444008430636
Cl = 0.2039185811661179
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002688200921004308
Cl = 0.2057816377793011
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002745342060022159
Cl = 0.2081373840562402
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002816610334305117
Cl = 0.2110406736708043
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002904376657741239
Cl = 0.2145646488018515
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003011879793049474
Cl = 0.2188068842337504
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.0031436020345932
Cl = 0.2238987294818338
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003305877285459626
Cl = 0.2300199286489827
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003507917885480169
Cl = 0.2374223860299378
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.00376364367726804
Cl = 0.246470714274774
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004095167898235838
Cl = 0.2577158067750639
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004540047408144653
Cl = 0.2720394012166652
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.005168237926862111
Cl = 0.2909701507466489
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.006128930715340598
Cl = 0.3174875485939033
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.007818359051284723
Cl = 0.358607891992251
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.01186220444375436
Cl = 0.4382638635248143
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002572533601556648
Cl = 0.2009337808875902
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002586364230247704
Cl = 0.2015191856817234
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002609799718822109
Cl = 0.2025075296435714
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002643444008430636
Cl = 0.2039185811661179
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002688200921004308
Cl = 0.2057816377793011
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002745342060022159
Cl = 0.2081373840562402
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002816610334305117
Cl = 0.2110406736708043
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002904376657741239
Cl = 0.2145646488018515
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003011879793049474
Cl = 0.2188068842337504
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.0031436020345932
Cl = 0.2238987294818338
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003305877285459626
Cl = 0.2300199286489827
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003507917885480169
Cl = 0.2374223860299378
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.00376364367726804
Cl = 0.246470714274774
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004095167898235838
Cl = 0.2577158067750639
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004540047408144653
Cl = 0.2720394012166652
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.005168237926862111
Cl = 0.2909701507466489
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.006128930715340598
Cl = 0.3174875485939033
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.007818359051284723
Cl = 0.358607891992251
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.01186220444375436
Cl = 0.4382638635248143
Cl[0] =  0.2009337808875902
Cd[0] =  0.002572533601556648

real	0m33.743s
user	0m14.500s
sys	0m18.371s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_ControlSurf_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_ControlSurf_PyTest.py test;
+ python -u avl_ControlSurf_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting design parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
	VLM control surface name - Tail
	VLM control surface name - WingRightLE
	VLM control surface name - WingRightTE
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Alpha  1.0
Beta   0.0
Mach   0.5
pb/2V  -0.0
qc/2V  0.0
rb/2V  -0.0
p'b/2V -0.0
r'b/2V -0.0
CXtot  -0.01911479917643672
CYtot  0.03828770401119253
CZtot  -0.6203123021542171
Cltot  0.05803020542928868
Cmtot  -0.364941579157723
Cntot  -0.02051317548235196
Cl'tot 0.05766336287208886
Cn'tot -0.0215228179571592
CLtot  0.6198842263418547
CDtot  0.02993783031517995
CDvis  0.0
CLff   0.6192452092597082
CYff   0.0328707962584744
CDind  0.02993783031517995
CDff   0.02861019822661107
e      0.7130586920544696

real	0m1.093s
user	0m0.760s
sys	0m0.456s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_EigenValue_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_EigenValue_PyTest.py test;
+ python -u avl_EigenValue_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
EigenValues  {'case 1': [[0.48252996, 1.0092579], [0.48252996, -1.0092579], [-6.42569, 0.0], [-1.2733929, 0.0], [-0.0011487329, 0.0], [-1.2380479, 0.49321593], [-1.2380479, -0.49321593], [0.77888703, 0.0]]}

real	0m0.929s
user	0m0.643s
sys	0m0.410s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_EigenValue_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_OpenMDAO_3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_OpenMDAO_3_PyTest.py test;
+ python -u avl_OpenMDAO_3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Alpha [2.] Beta [3.] Cmtot2 [0.04166298]
Alpha [2.] Beta [3.] Cmtot2 [0.04166298]
Cmtot2_Alpha [[0.68007176]]
Cmtot2_Beta [[0.0008466]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            2     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  4.16630D-02    |proj g|=  6.80072D-01
Alpha [1.31992824] Beta [2.9991534] Cmtot2 [0.03401795]
Cmtot2_Alpha [[0.60837327]]
Cmtot2_Beta [[0.0015253]]

At iterate    1    f=  3.40180D-02    |proj g|=  6.08373D-01
Alpha [-4.45133036] Beta [2.92288326] Cmtot2 [0.00071304]
Cmtot2_Alpha [[0.07860089]]
Cmtot2_Beta [[0.00107544]]

At iterate    2    f=  7.13044D-04    |proj g|=  7.86009D-02
Alpha [-5.30773219] Beta [2.90057802] Cmtot2 [2.43104345e-05]
Cmtot2_Alpha [[0.01420175]]
Cmtot2_Beta [[0.00021881]]

At iterate    3    f=  2.43104D-05    |proj g|=  1.42017D-02
Alpha [-5.49659696] Beta [2.89526135] Cmtot2 [3.72334447e-08]
Cmtot2_Alpha [[0.00055304]]
Cmtot2_Beta [[8.7325759e-06]]

At iterate    4    f=  3.72334D-08    |proj g|=  5.53036D-04
Alpha [-5.50424967] Beta [2.89504288] Cmtot2 [2.19764581e-12]
Cmtot2_Alpha [[4.24793146e-06]]
Cmtot2_Beta [[6.71418677e-08]]

At iterate    5    f=  2.19765D-12    |proj g|=  4.24793D-06

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    2      5      6      5     0     0   4.248D-06   2.198D-12
  F =   2.1976458136963880E-012

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-5.50424967] [2.89504288]

real	0m33.103s
user	0m4.323s
sys	0m1.540s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

friction: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/friction

=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]

real	0m0.647s
user	0m0.571s
sys	0m0.195s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================

tsfoil2: /Users/jenkins/util/tsfoil/tsfoil2

=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go.  Other input will terminate the job.
Cl =  0.933417
Cd =  0.000284
Cd Wave =  0.0
Cm =  -0.203436
Cp _Critcal =  -1.303869

real	0m0.736s
user	0m0.602s
sys	0m0.173s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================

mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/mses

=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.3783793240300122
Cd =  0.007775858044231098
Cm =  0.005262576090314894

real	0m2.435s
user	0m2.304s
sys	0m0.256s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'mses_OpenMDAO_3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_OpenMDAO_3_PyTest.py test;
+ python -u mses_OpenMDAO_3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - camber
	Done getting CFD design variables
camber [0.1] CD [0.01326534]
camber [0.1] CD [0.01326534]
CD_camber [[0.17647556]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         1 variables are exactly at the bounds

At iterate    0    f=  1.32653D-02    |proj g|=  1.76476D-01
camber [-0.07647556] CD [0.01022329]
CD_camber [[-0.08760106]]

At iterate    1    f=  1.02233D-02    |proj g|=  8.76011D-02
camber [-0.01793405] CD [0.00770371]
CD_camber [[-0.01328824]]

At iterate    2    f=  7.70371D-03    |proj g|=  1.32882D-02
camber [-0.00746595] CD [0.0076024]
CD_camber [[-0.0054235]]

At iterate    3    f=  7.60240D-03    |proj g|=  5.42350D-03
camber [-0.00024719] CD [0.00758207]
CD_camber [[-0.00011803]]

At iterate    4    f=  7.58207D-03    |proj g|=  1.18033D-04
camber [-8.65897362e-05] CD [0.00758208]
CD_camber [[-3.7300459e-06]]
camber [-0.0002103] CD [0.00758207]
CD_camber [[-9.42615953e-05]]

At iterate    5    f=  7.58207D-03    |proj g|=  9.42616D-05

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      5      7      5     0     0   9.426D-05   7.582D-03
  F =   7.5820708300072251E-003

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.0002103]

real	0m16.563s
user	0m15.812s
sys	0m0.915s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

xfoil: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/xfoil

=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  [1.05475230552582, 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	0m2.926s
user	0m2.844s
sys	0m0.200s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================

Running.... MESH PyTests


=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

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

Writing Tecplot file ....
Finished writing Tecplot file


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


Writing ugrid file ....
Finished writing ugrid file


real	0m5.824s
user	0m17.772s
sys	0m6.068s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'egadsTess_Box_Quad_Pytest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Box_Quad_Pytest.py test;
+ python -u egadsTess_Box_Quad_Pytest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = box1, index = 1
	Name = box2, index = 2
	Name = box3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 3 TFI quading disabled with attribute .qParams
	Face 4 TFI quading disabled with attribute .qParams
	TFI quading on all faces disabled with .qParams attribute on the body
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 602
Number of elements = 600
Number of triangle elements      = 0
Number of quadrilateral elements = 600
Body 2 (of 3)
Number of nodes    = 537
Number of elements = 535
Number of triangle elements      = 0
Number of quadrilateral elements = 535
Body 3 (of 3)
Number of nodes    = 1356
Number of elements = 1354
Number of triangle elements      = 0
Number of quadrilateral elements = 1354
----------------------------
Total number of nodes    = 2495
Total number of elements = 2489

Writing Tecplot file ....
Finished writing Tecplot file


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


Writing ugrid file ....
Finished writing ugrid file


real	0m3.998s
user	0m4.481s
sys	0m0.194s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_Box_Quad_Pytest.py passed (as expected)
=================================================


=================================================
+ echo 'egadsTess_Spheres_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Spheres_Quad_PyTest.py test;
+ python -u egadsTess_Spheres_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Spheres, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 4 has a degenerate edge - no TFI quading
	Face 5 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 6792
Number of elements = 6790
Number of triangle elements      = 0
Number of quadrilateral elements = 6790
----------------------------
Total number of nodes    = 6792
Total number of elements = 6790

Writing Tecplot file ....
Finished writing Tecplot file


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


Writing ugrid file ....
Finished writing ugrid file


real	0m6.344s
user	0m8.623s
sys	0m0.273s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_Spheres_Quad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'egadsTess_Nose_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Nose_Quad_PyTest.py test;
+ python -u egadsTess_Nose_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = nose, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 2 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
 EG_getSidepoint: LineSearch Failed (0.000000 0.973785)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.013232 0.966690)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.046939 0.962477)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.035376 0.957497)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.015407 0.966058)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (0.856445 0.971910)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (0.813517 0.972994)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
Body 1 (of 1)
Number of nodes    = 1498
Number of elements = 1496
Number of triangle elements      = 0
Number of quadrilateral elements = 1496
----------------------------
Total number of nodes    = 1498
Total number of elements = 1496

Writing Tecplot file ....
Finished writing Tecplot file


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


Writing ugrid file ....
Finished writing ugrid file


real	0m2.652s
user	0m2.920s
sys	0m0.207s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_Nose_Quad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.014   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          =     0.007   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

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

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


real	0m0.884s
user	0m0.978s
sys	0m0.503s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_PyTest.py test;
+ python -u aflr4_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Writing Tecplot file ....
Finished writing Tecplot file


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


Writing ugrid file ....
Finished writing ugrid file


real	0m1.257s
user	0m1.102s
sys	0m0.261s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_Symmetry_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_Symmetry_PyTest.py test;
+ python -u aflr4_Symmetry_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Symmetry
	Done getting mesh sizing parameters
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m2.111s
user	0m2.079s
sys	0m0.541s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_Symmetry_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_Generic_Missile.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_Generic_Missile.py test;
+ python -u aflr4_Generic_Missile.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = MissileOML, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m5.133s
user	0m9.158s
sys	0m0.677s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_Generic_Missile.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_TipTreat_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_TipTreat_PyTest.py test;
+ python -u aflr4_TipTreat_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m6.767s
user	0m6.394s
sys	0m0.427s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_TipTreat_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file


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


Writing ugrid file ....
Finished writing ugrid file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 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	0m10.337s
user	0m9.782s
sys	0m0.532s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_aflr3_Symmetry_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_Symmetry_PyTest.py test;
+ python -u aflr4_and_aflr3_Symmetry_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Symmetry
	Done getting mesh sizing parameters
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 333411
	Number of elements       = 1070785
	Number of triangles      = 44340
	Number of quadrilatarals = 1613
	Number of tetrahedrals   = 575437
	Number of pyramids       = 327
	Number of prisms         = 449068
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m22.984s
user	0m22.339s
sys	0m1.039s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_Symmetry_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_QuadMesh_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_QuadMesh_PyTest.py test;
+ python -u aflr4_QuadMesh_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m5.826s
user	0m17.793s
sys	0m6.949s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_QuadMesh_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_Tetgen_PyTest.py test;
+ python -u aflr4_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 30048, elements - 60084
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


real	0m10.166s
user	0m9.623s
sys	0m0.621s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_Tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_tetgen_Regions_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_tetgen_Regions_PyTest.py test;
+ python -u aflr4_tetgen_Regions_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SheetBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 11 Faces
EGADS    : Body 0 has 20 Edges
EGADS    : Body 0 has 11 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 6 8 10 11
EGADS    :      2     Yes     0     0     1        0        1   1 3 7 9 11
EGADS    :      3     Yes     0     0     1        0        1   2 4 6 9 11
EGADS    :      4     Yes     0     0     1        0        1   3 5 7 9 11
EGADS    :      5     Yes     0     0     1        0        1   4 6 8 10 11
EGADS    :      6     Yes     0     0     1        0        1   1 3 5 10 11
EGADS    :      7     Yes     0     0     1        0        1   2 4 8 9 11
EGADS    :      8     Yes     0     0     1        0        1   1 5 7 10 11
EGADS    :      9     Yes     0     0     1        0        1   2 3 4 7
EGADS    :     10     Yes     0     0     1        0        1   1 5 6 8
EGADS    :     11     Yes     0     0     1        0        1   1 2 3 4 5 6 7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 6 7 -2
EGADS    :      3   8 5 9 -10
EGADS    :      4   10 11 -12 -13
EGADS    :      5   14 15 -16 -11
EGADS    :      6   1 -17 -14 -9
EGADS    :      7   -18 12 -19 -7
EGADS    :      8   16 20 -3 19
EGADS    :      9   13 18 -6 -8
EGADS    :     10   -15 17 4 -20
EGADS    :     11   11 -19 -2 9

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 6 7 -2
EGADS    :      3     Yes   8 5 9 -10
EGADS    :      4     Yes   10 11 -12 -13
EGADS    :      5     Yes   14 15 -16 -11
EGADS    :      6     Yes   1 -17 -14 -9
EGADS    :      7     Yes   -18 12 -19 -7
EGADS    :      8     Yes   16 20 -3 19
EGADS    :      9     Yes   13 18 -6 -8
EGADS    :     10     Yes   -15 17 4 -20
EGADS    :     11     Yes   11 -19 -2 9

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 6
EGADS    :      2     0     Yes     1     3        1   1 2 11
EGADS    :      3     0     Yes     3     4        1   1 8
EGADS    :      4     0     Yes     2     4        1   1 10
EGADS    :      5     0     Yes     5     1        1   2 3
EGADS    :      6     0     Yes     5     6        1   2 9
EGADS    :      7     0     Yes     6     3        1   2 7
EGADS    :      8     0     Yes     7     5        1   3 9
EGADS    :      9     0     Yes     1     8        1   3 6 11
EGADS    :     10     0     Yes     7     8        1   3 4
EGADS    :     11     0     Yes     8     9        1   4 5 11
EGADS    :     12     0     Yes    10     9        1   4 7
EGADS    :     13     0     Yes     7    10        1   4 9
EGADS    :     14     0     Yes     8    11        1   5 6
EGADS    :     15     0     Yes    11    12        1   5 10
EGADS    :     16     0     Yes     9    12        1   5 8
EGADS    :     17     0     Yes    11     2        1   6 10
EGADS    :     18     0     Yes    10     6        1   7 9
EGADS    :     19     0     Yes     3     9        1   7 8 11
EGADS    :     20     0     Yes    12     4        1   8 10

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                1                0                0
EGADS    :      2     Yes                1                0                2
EGADS    :      3     Yes                1                1                1
EGADS    :      4     Yes                1                1                2
EGADS    :      5     Yes                1                0                0
EGADS    :      6     Yes                1                1                0
EGADS    :      7     Yes                0                0                0
EGADS    :      8     Yes                0                0                0
EGADS    :      9     Yes                0                1                1
EGADS    :     10     Yes                0                1                0
EGADS    :     11     Yes                0                0                2
EGADS    :     12     Yes                0                1                2

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 4
AFLR4    : Min Bounding Box Length     = 2
AFLR4    : Max Ref Bounding Box Length = 4
AFLR4    : Min Ref Bounding Box Length = 2
AFLR4    : Reference Length            = 1
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.0025
AFLR4    : Min Surf Spacing            = 0.01
AFLR4    : Max Surf Spacing            = 0.2
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0              TRANSP

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       137       228         0
AFLR4    : Nodes, Trias,Quads=       131       216         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       137       228         0
AFLR4    : Nodes, Trias,Quads=       132       218         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       137       228         0
AFLR4    : Nodes, Trias,Quads=       132       218         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       137       228         0
AFLR4    : Nodes, Trias,Quads=       131       216         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       196       340         0
AFLR4    : Nodes, Trias,Quads=       192       332         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       196       340         0
AFLR4    : Nodes, Trias,Quads=       192       332         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       134       226         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       135       228         0
AFLR4    : Nodes, Trias,Quads=       131       220         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       184       318         0
AFLR4    : Nodes, Trias,Quads=       178       306         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      1231      2504       464

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      1231      2504

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       140       234         0
AFLR4    : Nodes, Trias,Quads=       134       222         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       140       234         0
AFLR4    : Nodes, Trias,Quads=       133       220         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       140       234         0
AFLR4    : Nodes, Trias,Quads=       133       220         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       141       236         0
AFLR4    : Nodes, Trias,Quads=       133       220         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       207       362         0
AFLR4    : Nodes, Trias,Quads=       193       334         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       203       354         0
AFLR4    : Nodes, Trias,Quads=       193       334         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       136       230         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       137       232         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       193       336         0
AFLR4    : Nodes, Trias,Quads=       183       316         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      1246      2534       464

OVERALL  : CPU Time          =     0.078   seconds
Body 1 (of 1)
Number of nodes    = 1246
Number of elements = 2534
Number of triangle elements      = 2534
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1246
Total number of elements = 2534
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Number of surface: nodes - 1246, elements - 2534
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.008926
Creating surface mesh ...
Surface mesh seconds:  0.001931
Recovering boundaries...
Boundary recovery seconds:  0.004555
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000787
Recovering Delaunayness...
Delaunay recovery seconds:  0.001787
Refining mesh...
Refinement seconds:  0.009396
Smoothing vertices...
Mesh smoothing seconds:  0.012394
Improving mesh...
Mesh improvement seconds:  0.001104

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

Output seconds:  0.000445
Total running seconds:  0.04139

Statistics:

  Input points: 1246
  Input facets: 2534
  Input segments: 3777
  Input holes: 0
  Input regions: 2

  Mesh points: 1455
  Mesh tetrahedra: 5105
  Mesh faces: 11319
  Mesh faces on exterior boundary: 2218
  Mesh faces on input facets: 2534
  Mesh edges on input segments: 3777
  Steiner points inside domain: 209

Done meshing using TetGen!

Writing vtk file ....

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


Writing Tecplot file ....
Finished writing Tecplot file


real	0m0.855s
user	0m0.723s
sys	0m0.239s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_tetgen_Regions_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 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:  0.019183
Creating surface mesh ...
Surface mesh seconds:  0.004633
Recovering boundaries...
Boundary recovery seconds:  0.039408
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.005356
Suppressing Steiner points ...
Steiner suppression seconds:  8e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.007877
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:  0.518615
Smoothing vertices...
Mesh smoothing seconds:  0.33244
Improving mesh...
Mesh improvement seconds:  0.008231
Jettisoning redundant points.

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

Output seconds:  0.001639
Total running seconds:  0.93751

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	0m2.242s
user	0m2.165s
sys	0m0.329s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_Holes_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_Holes_PyTest.py test;
+ python -u tetgen_Holes_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 8995
Number of elements = 18112
Number of triangle elements      = 18112
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 8995
Total number of elements = 18112
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Number of surface: nodes - 8995, elements - 18112
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.163055
Creating surface mesh ...
Surface mesh seconds:  0.011913
Recovering boundaries...
Boundary recovery seconds:  0.072279
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.010062
Recovering Delaunayness...
Delaunay recovery seconds:  0.039189
Refining mesh...
Refinement seconds:  0.187873
Smoothing vertices...
Mesh smoothing seconds:  0.238112
Improving mesh...
Mesh improvement seconds:  0.007602
Jettisoning redundant points.

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

Output seconds:  0.002823
Total running seconds:  0.733261

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 1
  Input regions: 0

  Mesh points: 7140
  Mesh tetrahedra: 27881
  Mesh faces: 60802
  Mesh faces on exterior boundary: 10080
  Mesh faces on input facets: 10080
  Mesh edges on input segments: 15120
  Steiner points inside domain: 2098

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing Tecplot file ....
Finished writing Tecplot file


Writing FAST file ....
Finished writing FAST file


real	0m1.875s
user	0m1.754s
sys	0m0.247s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_Holes_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_Regions_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_Regions_PyTest.py test;
+ python -u tetgen_Regions_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 8995
Number of elements = 18112
Number of triangle elements      = 18112
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 8995
Total number of elements = 18112
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Number of surface: nodes - 8995, elements - 18112
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.156178
Creating surface mesh ...
Surface mesh seconds:  0.012841
Recovering boundaries...
Boundary recovery seconds:  0.069352
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.007803
Recovering Delaunayness...
Delaunay recovery seconds:  0.078075
Refining mesh...
Refinement seconds:  0.358122
Smoothing vertices...
Mesh smoothing seconds:  0.440125
Improving mesh...
Mesh improvement seconds:  0.013445

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

Output seconds:  0.00397
Total running seconds:  1.14033

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 0
  Input regions: 2

  Mesh points: 13181
  Mesh tetrahedra: 55765
  Mesh faces: 119562
  Mesh faces on exterior boundary: 16064
  Mesh faces on input facets: 18112
  Mesh edges on input segments: 27104
  Steiner points inside domain: 4186

Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


real	0m2.287s
user	0m2.158s
sys	0m0.254s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_Regions_PyTest.py passed (as expected)
=================================================

delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo

=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6

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

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


Writing ugrid file ....
Finished writing ugrid file


real	0m0.940s
user	0m0.882s
sys	0m0.496s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================

Running.... CFD PyTests


=================================================
+ echo 'su2_and_AFLR2_NodeDist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_NodeDist_PyTest.py test;
+ python -u su2_and_AFLR2_NodeDist_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       224       224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        46        94
AFLR2 IG : Nodes, Faces      =        92       186
AFLR2 IG : Nodes, Faces      =       138       278
AFLR2 IG : Nodes, Faces      =       184       370
AFLR2 IG : Nodes, Faces      =       196       394
AFLR2 IG : Nodes, Faces      =       224       450
AFLR2 IG : Nodes, Faces      =       228       450
AFLR2 IG : Nodes, Faces      =       224       224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =       224       224
AFLR2 GG : Nodes, Faces      =       440       656
AFLR2 GG : Nodes, Faces      =       649      1074
AFLR2 GG : Nodes, Faces      =       853      1482
AFLR2 GG : Nodes, Faces      =      1050      1876
AFLR2 GG : Nodes, Faces      =      1238      2252
AFLR2 GG : Nodes, Faces      =      1421      2618
AFLR2 GG : Nodes, Faces      =      1594      2964
AFLR2 GG : Nodes, Faces      =      1760      3296
AFLR2 GG : Nodes, Faces      =      1915      3606
AFLR2 GG : Nodes, Faces      =      2063      3902
AFLR2 GG : Nodes, Faces      =      2202      4180
AFLR2 GG : Nodes, Faces      =      2314      4404
AFLR2 GG : Nodes, Faces      =      2423      4622
AFLR2 GG : Nodes, Faces      =      2528      4832
AFLR2 GG : Nodes, Faces      =      2634      5044
AFLR2 GG : Nodes, Faces      =      2732      5240
AFLR2 GG : Nodes, Faces      =      2831      5438
AFLR2 GG : Nodes, Faces      =      2927      5630
AFLR2 GG : Nodes, Faces      =      3018      5812
AFLR2 GG : Nodes, Faces      =      3109      5994
AFLR2 GG : Nodes, Faces      =      3202      6180
AFLR2 GG : Nodes, Faces      =      3295      6366
AFLR2 GG : Nodes, Faces      =      3386      6548
AFLR2 GG : Nodes, Faces      =      3464      6704
AFLR2 GG : Nodes, Faces      =      3535      6846
AFLR2 GG : Nodes, Faces      =      3594      6964
AFLR2 GG : Nodes, Faces      =      3639      7054
AFLR2 GG : Nodes, Faces      =      3671      7118
AFLR2 GG : Nodes, Faces      =      3691      7158
AFLR2 GG : Nodes, Faces      =      3705      7186
AFLR2 GG : Nodes, Faces      =      3712      7200
AFLR2 GG : Nodes, Faces      =      3715      7206
 
AFLR2    : CPU Time          =     0.006   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      3715      7206
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 3715
Number of elements = 7430
Number of tris = 7206
Number of quad = 0

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

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


Running SU2......

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

Parsing config file for zone 0

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

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

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

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

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

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_SU2_aflr2.
Volume file name: flow_pyCAPS_SU2_aflr2.
Restart file name: restart_flow_pyCAPS_SU2_aflr2.dat.

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

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
3715 grid points.
7206 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
78 boundary elements in index 3 (Marker = BC_5).
7206 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 7206 TRIANGLE volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 177.06. Mean K: 1.97231. Standard deviation K: 13.0434.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        63.4343|             90|
|     CV Face Area Aspect Ratio|              1|        5.23543|
|           CV Sub-Volume Ratio|              1|        3.11804|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      3715|    1/1.00|        10|
|         1|      1048|    1/3.54|   7.96696|
|         2|       298|    1/3.52|   6.37252|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06136 m.
Area projection in the x-plane = 0.178383 m, y-plane = 0.994925 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138389 m.
Min. coordinate in the x-direction = -0.000250564 m, y-direction = -0.0151999 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.

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

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

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.8483e-02|   -0.385358|    2.453598|    1.625650|    5.369499|    0.360138|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.7411e-02|   -0.512634|    2.087781|    1.374671|    4.973554|    1.183036|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.7251e-02|   -0.792582|    1.733529|    1.142729|    4.657622|    3.896320|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.7804e-02|   -0.880738|    1.486539|    1.023158|    4.334759|   14.592265|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.7852e-02|   -0.987528|    1.351478|    0.932491|    4.191092|  111.166022|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  2.7982e-02|   -1.104038|    1.188715|    0.874764|    3.951825| -483.924340|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  2.8210e-02|   -1.178622|    1.124587|    0.844310|    3.820426|  127.331200|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  2.8116e-02|   -1.243517|    1.097463|    0.824869|    3.768858|   40.162273|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  2.8244e-02|   -1.287932|    1.075843|    0.810639|    3.733440|   25.154653|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  2.8107e-02|   -1.300689|    1.046363|    0.775886|    3.684245|   21.097801|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.30069|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_aflr2.dat  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_SU2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_SU2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 352 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.650457 Cd =  0.030831
Cmz =  0.373226
Cx =  0.030831 Cy =  0.650457
Pressure Contribution
Cl_p =  0.650457 Cd_p =  0.030831
Cmz_p =  0.373226
Cx_p =  0.030831 Cy_p =  0.650457
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m1.609s
user	0m1.334s
sys	0m0.744s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_NodeDist_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       545         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       545       545
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       110       222
AFLR2 IG : Nodes, Faces      =       220       442
AFLR2 IG : Nodes, Faces      =       330       662
AFLR2 IG : Nodes, Faces      =       440       882
AFLR2 IG : Nodes, Faces      =       517      1036
AFLR2 IG : Nodes, Faces      =       545      1092
AFLR2 IG : Nodes, Faces      =       549      1092
AFLR2 IG : Nodes, Faces      =       545       545
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       545       545
AFLR2 GGp: Nodes, Faces      =      1083      1621
AFLR2 GGp: Nodes, Faces      =      1616      2687
AFLR2 GGp: Nodes, Faces      =      2144      3743
AFLR2 GGp: Nodes, Faces      =      2661      4777
AFLR2 GGp: Nodes, Faces      =      3171      5797
AFLR2 GGp: Nodes, Faces      =      3672      6799
AFLR2 GGp: Nodes, Faces      =      4158      7771
AFLR2 GGp: Nodes, Faces      =      4653      8761
AFLR2 GGp: Nodes, Faces      =      5142      9739
AFLR2 GGp: Nodes, Faces      =      5608     10671
AFLR2 GGp: Nodes, Faces      =      6055     11565
AFLR2 GGp: Nodes, Faces      =      6482     12419
AFLR2 GGp: Nodes, Faces      =      6880     13215
AFLR2 GGp: Nodes, Faces      =      7257     13969
AFLR2 GGp: Nodes, Faces      =      7614     14683
AFLR2 GGp: Nodes, Faces      =      7947     15349
AFLR2 GGp: Nodes, Faces      =      8276     16007
AFLR2 GGp: Nodes, Faces      =      8575     16605
AFLR2 GGp: Nodes, Faces      =      8869     17193
AFLR2 GGp: Nodes, Faces      =      9140     17735
AFLR2 GGp: Nodes, Faces      =      9401     18257
AFLR2 GGp: Nodes, Faces      =      9654     18763
AFLR2 GGp: Nodes, Faces      =      9887     19229
AFLR2 GGp: Nodes, Faces      =     10110     19675
AFLR2 GGp: Nodes, Faces      =     10315     20085
AFLR2 GGp: Nodes, Faces      =     10497     20449
AFLR2 GGp: Nodes, Faces      =     10656     20767
AFLR2 GGp: Nodes, Faces      =     10791     21037
AFLR2 GGp: Nodes, Faces      =     10919     21293
AFLR2 GGp: Nodes, Faces      =     11022     21499
AFLR2 GGp: Nodes, Faces      =     11092     21639
AFLR2 GGp: Nodes, Faces      =     11145     21745
AFLR2 GGp: Nodes, Faces      =     11156     21767
 
AFLR2    : CPU Time          =     0.032   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          =     0.011   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

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

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


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

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


Running SU2......

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

Parsing config file for zone 0

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  7.7834e-02|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  7.6732e-02|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  7.4744e-02|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  7.3789e-02|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  7.2029e-02|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  7.1257e-02|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  7.1650e-02|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  7.1701e-02|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  7.2098e-02|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  7.2294e-02|   -1.221243|    1.499646|    1.130319|    4.189559|   -6.277653|

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

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

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

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

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

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

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

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

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

real	0m2.588s
user	0m2.202s
sys	0m1.033s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR4_AFLR3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR4_AFLR3_PyTest.py test;
+ python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 39312
	Number of elements       = 226864
	Number of triangles      = 12446
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 214418
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wake
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_4|
+-----------------------------------------------------------------------+
|                  Internal boundary|                               BC_3|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
39312 grid points.
214418 volume elements.
4 surface markers.
6594 boundary elements in index 0 (Marker = BC_1).
5358 boundary elements in index 1 (Marker = BC_2).
74 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
214418 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 4873.1. Mean K: 61.8682. Standard deviation K: 266.942.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        17.1608|         84.739|
|     CV Face Area Aspect Ratio|        1.11815|        37015.5|
|           CV Sub-Volume Ratio|        1.04044|         455686|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     39312|    1/1.00|        10|
|         1|      6485|    1/6.06|   8.22658|
|         2|      1015|    1/6.39|   6.65012|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.038 m^2.
Area projection in the x-plane = 11.1419 m^2, y-plane = 4.96714 m^2, z-plane = 55.4182 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.582636 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  9.5595e-01|   -0.064586|    2.297676|    2.033300|    5.426310|    1.967108|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.3271e-01|   -0.028142|    2.443813|    2.177084|    5.469820|    2.669025|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.2465e-01|    0.006388|    2.521945|    2.416533|    5.497519|    4.072698|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  9.2009e-01|   -0.032771|    2.543134|    2.541766|    5.444377|    5.959388|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  9.2528e-01|   -0.059484|    2.561671|    2.593774|    5.414288|    7.593451|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  9.2979e-01|   -0.076814|    2.565225|    2.615896|    5.407625|    8.782803|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  9.2464e-01|   -0.111978|    2.544207|    2.636258|    5.381265|    9.653546|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  9.1698e-01|   -0.156369|    2.495539|    2.651467|    5.333878|   10.185394|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  9.1301e-01|   -0.203072|    2.428150|    2.650114|    5.275471|   10.322264|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  9.0701e-01|   -0.251896|    2.375012|    2.624886|    5.221589|   10.161308|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.251896|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.796713 Cd =  0.078407
Cmx =  0.000211 Cmy =  -0.204659 Cmz =  0.000288
Cx =  0.06449 Cy =  0.000454 Cz =  0.79796
Pressure Contribution
Cl_p =  0.796713 Cd_p =  0.078407
Cmx_p =  0.000211 Cmy_p =  -0.204659 Cmz_p =  0.000288
Cx_p =  0.06449 Cy_p =  0.000454 Cz_p =  0.79796
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmx_v =  0.0 Cmy_v =  0.0 Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0 Cz_v =  0.0

real	0m32.025s
user	0m30.976s
sys	0m1.012s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_Morph_PyTest.py test;
+ python -u su2_Morph_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 56062
	Number of elements       = 324627
	Number of triangles      = 15872
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 308755
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wake
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing SU2 surface file
Writing SU2 Motion File - su2AFLRTest_motion.dat
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 15
 - bcProps.surfaceProp[2].surfaceType = 1
 - bcProps.surfaceProp[3].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Surface(s) affected by the design variables: BC_1, BC_2.
Input mesh file name: ../volumeMesh/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_4|
+-----------------------------------------------------------------------+
|                  Internal boundary|                               BC_3|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
56062 grid points.
308755 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
308755 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 5523.74. Mean K: 58.8177. Standard deviation K: 282.533.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        25.8353|        86.1799|
|     CV Face Area Aspect Ratio|        1.02126|        47603.8|
|           CV Sub-Volume Ratio|        1.04989|         165826|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     56062|    1/1.00|        10|
|         1|      9228|    1/6.08|   8.22061|
|         2|      1406|    1/6.56|     6.586|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 96.2324 m^2.
Area projection in the x-plane = 7.65774 m^2, y-plane = 4.21853 m^2, z-plane = 45.5887 m^2.
Max. coordinate in the x-direction = 12.3872 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.0650201 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.2644e+00|   -0.457870|    1.873279|    1.656710|    5.033025|    0.755651|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.2518e+00|   -0.472284|    2.010746|    1.748231|    5.024932|    1.425370|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.2501e+00|   -0.414217|    2.107665|    1.963200|    5.074925|    3.245288|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.2418e+00|   -0.400337|    2.167522|    2.099318|    5.078948|    7.034217|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.2387e+00|   -0.401529|    2.203755|    2.175567|    5.071313|   12.883621|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.2380e+00|   -0.407291|    2.221380|    2.217144|    5.067540|   20.159074|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.2381e+00|   -0.411436|    2.211548|    2.246056|    5.067163|   27.796880|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.2374e+00|   -0.418757|    2.160924|    2.267618|    5.055632|   32.034412|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.2344e+00|   -0.438528|    2.092229|    2.272883|    5.027335|   30.335774|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.2342e+00|   -0.487870|    2.016953|    2.255847|    4.971131|   25.705102|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -0.48787|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.52174 Cd =  0.020297
Projecting tessellation 1 (of 4) on to new body
Projecting tessellation 2 (of 4) on to new body
Projecting tessellation 3 (of 4) on to new body
Projecting tessellation 4 (of 4) on to new body
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wake
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing SU2 surface file
Writing SU2 Motion File - su2AFLRTest_motion.dat
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 15
 - bcProps.surfaceProp[2].surfaceType = 1
 - bcProps.surfaceProp[3].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Mesh Morphing......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_4|
+-----------------------------------------------------------------------+
|                  Internal boundary|                               BC_3|
+-----------------------------------------------------------------------+
Three dimensional problem.
56062 grid points.
308755 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
308755 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 2.08667e+06.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Ignoring Convergence Field(s): RMS_DENSITY 
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 11.505432 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |aflr3_CAPS.su2                     |
|CSV file                           |surface_deformed.csv               |
|Paraview                           |volume_deformed.vtu                |
|Paraview surface                   |surface_deformed.vtu               |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------



Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Surface(s) affected by the design variables: BC_1, BC_2.
Input mesh file name: aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_4|
+-----------------------------------------------------------------------+
|                  Internal boundary|                               BC_3|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
56062 grid points.
308755 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
308755 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 5523.56. Mean K: 58.7619. Standard deviation K: 282.437.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        17.0659|        85.7425|
|     CV Face Area Aspect Ratio|        1.02723|        55937.4|
|           CV Sub-Volume Ratio|        1.05439|         215979|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     56062|    1/1.00|        10|
|         1|      9228|    1/6.08|   8.22061|
|         2|      1406|    1/6.56|     6.586|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 95.6308 m^2.
Area projection in the x-plane = 9.17945 m^2, y-plane = 4.04295 m^2, z-plane = 44.962 m^2.
Max. coordinate in the x-direction = 12.3585 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.400127 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.2854e+00|   -0.397349|    1.978876|    1.645486|    5.093547|    1.917484|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.2894e+00|   -0.252045|    2.234760|    1.970250|    5.252026|    2.558863|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.2811e+00|   -0.196042|    2.339633|    2.224120|    5.301659|    3.948869|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.2841e+00|   -0.220076|    2.386540|    2.365409|    5.264943|    5.948479|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.2830e+00|   -0.253573|    2.408600|    2.430554|    5.223815|    7.864579|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.2782e+00|   -0.270783|    2.418936|    2.458803|    5.218653|    9.389224|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.2745e+00|   -0.286712|    2.403031|    2.476999|    5.213229|   10.603736|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.2767e+00|   -0.315381|    2.351751|    2.489815|    5.182543|   11.481006|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.2774e+00|   -0.352500|    2.274582|    2.487389|    5.133384|   11.951691|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.2805e+00|   -0.405104|    2.187417|    2.462671|    5.069866|   12.022914|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.405104|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.883374 Cd =  0.073474

real	0m59.577s
user	0m54.896s
sys	0m3.362s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_Morph_PyTest.py passed (as expected)
=================================================

delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo

=================================================
+ echo 'su2_and_Delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_Delaundo_PyTest.py test;
+ python -u su2_and_Delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5

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

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


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

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Warning: No boundary condition specified for capsGroup 2DSlice!
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

Parsing config file for zone 0

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

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

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

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

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

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2_CAPS.dat.
Surface file name: surface_flow_su2_CAPS.
Volume file name: flow_su2_CAPS.
Restart file name: restart_flow_su2_CAPS.dat.

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

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
6320 grid points.
12346 volume elements.
5 surface markers.
24 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_2).
24 boundary elements in index 3 (Marker = BC_4).
198 boundary elements in index 4 (Marker = BC_5).
12346 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
There has been a re-orientation of 294 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        45.3524|        89.3051|
|     CV Face Area Aspect Ratio|         1.0235|        15.7138|
|           CV Sub-Volume Ratio|              1|        7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      6320|    1/1.00|        10|
|         1|      1790|    1/3.53|   7.98287|
|         2|       504|    1/3.55|   6.35388|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
Computing wall distances.

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

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

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  5.1470e-02|   -1.163171|    1.073770|    1.341444|    4.312165|    0.062120|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  4.8621e-02|   -1.561828|    0.808636|    0.967487|    3.922716|    0.139775|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  4.7387e-02|   -1.601698|    0.943793|    1.009036|    3.876382|    0.373708|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  4.7801e-02|   -1.659374|    1.008221|    1.015635|    3.799753|    0.952935|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  4.7274e-02|   -1.663585|    1.011627|    0.956487|    3.788246|    2.344781|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  4.7149e-02|   -1.633451|    0.991734|    0.872954|    3.829708|    6.259549|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  4.7137e-02|   -1.626398|    0.990123|    0.847075|    3.843511|   26.349556|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  4.7308e-02|   -1.643439|    1.009125|    0.895796|    3.825758|  -56.104876|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  4.7428e-02|   -1.659565|    1.020774|    0.939260|    3.804303|  -24.431167|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  4.7578e-02|   -1.676757|    1.012633|    0.938320|    3.783310|  -21.456835|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.67676|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2_CAPS.dat          |

Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
|CSV file                           |surface_flow_su2_CAPS.csv          |

Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
|Tecplot binary                     |flow_su2_CAPS.szplt                |

Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
|Tecplot binary surface             |surface_flow_su2_CAPS.szplt        |
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 492 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.805231 Cd =  -0.037528
Cmz =  0.414714
Cx =  -0.037528 Cy =  0.805231
Pressure Contribution
Cl_p =  0.805231 Cd_p =  -0.037528
Cmz_p =  0.414714
Cx_p =  -0.037528 Cy_p =  0.805231
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m2.429s
user	0m1.615s
sys	0m0.785s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ python -u su2_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 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:  0.021372
Creating surface mesh ...
Surface mesh seconds:  0.005984
Recovering boundaries...
Boundary recovery seconds:  0.066986
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.005811
Suppressing Steiner points ...
Steiner suppression seconds:  1e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.009996
Refining mesh...
  4186 insertions, added 2132 points, 130189 tetrahedra in queue.
  1393 insertions, added 396 points, 133609 tetrahedra in queue.
  1857 insertions, added 413 points, 131356 tetrahedra in queue.
  2476 insertions, added 454 points, 112928 tetrahedra in queue.
  3300 insertions, added 466 points, 67068 tetrahedra in queue.
  4399 insertions, added 435 points, 292 tetrahedra in queue.
  5864 insertions, added 590 points, 479 tetrahedra in queue.
Refinement seconds:  0.690311
Smoothing vertices...
Mesh smoothing seconds:  0.411137
Improving mesh...
Mesh improvement seconds:  0.012911
Jettisoning redundant points.

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

Output seconds:  0.001692
Total running seconds:  1.22666

Statistics:

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

  Mesh points: 8091
  Mesh tetrahedra: 39789
  Mesh faces: 82710
  Mesh faces on exterior boundary: 6264
  Mesh faces on input facets: 6264
  Mesh edges on input segments: 9394
  Steiner points on input segments:  1
  Steiner points inside domain: 4953

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../myMesh/tetgen_CAPS.su2

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

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

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

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_Tetgen.dat.
Surface file name: surface_flow_pyCAPS_SU2_Tetgen.
Volume file name: flow_pyCAPS_SU2_Tetgen.
Restart file name: restart_flow_pyCAPS_SU2_Tetgen.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_3|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
8091 grid points.
39789 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
526 boundary elements in index 2 (Marker = BC_3).
39789 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08926e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 414.134. Mean K: 30.5804. Standard deviation K: 37.5377.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.66644|        84.3027|
|     CV Face Area Aspect Ratio|        1.51408|         6441.7|
|           CV Sub-Volume Ratio|        1.03202|        58553.9|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      8091|    1/1.00|        10|
|         1|      1351|    1/5.99|   8.25992|
|         2|       223|    1/6.06|   6.79647|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 120.046 m^2.
Area projection in the x-plane = 10.7914 m^2, y-plane = 4.58502 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.9412e-01|    0.617984|    3.049944|    2.093190|    6.108879|    1.810742|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.0090e-01|    0.748911|    3.251769|    2.987153|    6.248586|    2.155825|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.0029e-01|    0.688623|    3.311837|    3.249508|    6.186781|    3.173369|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.0015e-01|    0.587426|    3.265724|    3.310895|    6.060983|    4.532123|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.9682e-01|    0.563655|    3.196458|    3.256149|    6.028232|    5.638253|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      0.563655|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_Tetgen.dat |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_Tetgen.csv |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview                           |flow_pyCAPS_SU2_Tetgen.vtu         |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview surface                   |surface_flow_pyCAPS_SU2_Tetgen.vtu |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.751804 Cd =  0.13334
Cmx =  -0.004647 Cmy =  -0.210652 Cmz =  0.001238
Cx =  0.120199 Cy =  0.000192 Cz =  0.754017

real	0m14.001s
user	0m13.299s
sys	0m0.703s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_X43a_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = x43A, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 3808
Number of elements = 7616
Number of triangle elements      = 7616
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 5654
Number of elements = 11304
Number of triangle elements      = 11304
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9462
Total number of elements = 18920

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = x43A, index = 1
	Name = Farfield, index = 2
Number of surface: nodes - 9462, elements - 18920
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.049759
Creating surface mesh ...
Surface mesh seconds:  0.015201
Recovering boundaries...
Warning:  6 segments are not recovered.
Boundary recovery seconds:  0.156669
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.011693
Suppressing Steiner points ...
Steiner suppression seconds:  1.6e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.020192
Refining mesh...
  12618 insertions, added 5274 points, 8959 tetrahedra in queue.
Refinement seconds:  0.497978
Smoothing vertices...
Mesh smoothing seconds:  0.419854
Improving mesh...
Mesh improvement seconds:  0.014577
Jettisoning redundant points.

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

Output seconds:  0.005894
Total running seconds:  1.19607

Statistics:

  Input points: 9462
  Input facets: 18920
  Input segments: 28380
  Input holes: 1
  Input regions: 0

  Mesh points: 14879
  Mesh tetrahedra: 61475
  Mesh faces: 132413
  Mesh faces on exterior boundary: 18926
  Mesh faces on input facets: 18926
  Mesh edges on input segments: 28383
  Steiner points on input segments:  3
  Steiner points inside domain: 5414

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - x43A
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 3.5.
Angle of attack (AoA): 3 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.

Surface(s) plotted in the output file: BC_1.
Input mesh file name: ../myMesh/tetgen_CAPS.su2

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

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

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

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_x43a_Test.dat.
Surface file name: surface_flow_x43a_Test.
Volume file name: flow_x43a_Test.
Restart file name: restart_flow_x43a_Test.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
14879 grid points.
61475 volume elements.
2 surface markers.
7622 boundary elements in index 0 (Marker = BC_1).
11304 boundary elements in index 1 (Marker = BC_2).
61475 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.67744e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 95.6599. Mean K: 0.525129. Standard deviation K: 2.57985.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.97178|        85.1584|
|     CV Face Area Aspect Ratio|        1.89387|        2232.84|
|           CV Sub-Volume Ratio|              1|         662807|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14879|    1/1.00|        10|
|         1|      2664|    1/5.59|   8.45431|
|         2|       482|    1/5.53|   7.17255|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13596.7 m^2.
Area projection in the x-plane = 761.676 m^2, y-plane = 2062.48 m^2, z-plane = 5463.61 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        916077|             1|   m^2/s^2|        916077|
|            Velocity-X|       1189.41|             1|       m/s|       1189.41|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       62.3342|             1|       m/s|       62.3342|
|    Velocity Magnitude|       1191.04|             1|       m/s|       1191.04|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  3.0033e-01|    2.730957|    5.664998|    4.728682|    8.730433|   -0.398804|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.9099e-01|    3.137446|    6.177776|    5.665282|    9.126833|   -0.137986|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.8714e-01|    3.221739|    6.293564|    5.717532|    9.173826|   -0.037061|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.8523e-01|    3.189146|    6.230574|    5.640455|    9.149183|   -0.012053|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.8642e-01|    3.223156|    6.256981|    5.536034|    9.185450|   -0.028725|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       3.22316|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_x43a_Test.dat         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|CSV file                           |surface_flow_x43a_Test.csv         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview                           |flow_x43a_Test.vtu                 |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview surface                   |surface_flow_x43a_Test.vtu         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
+-----------------------------------------------------------------------+
Warning: there are 124 non-physical points in the solution.
Warning: 85 reconstructed states for upwinding are non-physical.

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

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

Total Force - Pressure + Viscous
Cl =  -3.497481 Cd =  121.75903
Cmx =  -17.512377 Cmy =  9356.955958 Cmz =  278.947628
Cx =  121.775208 Cy =  2.435697 Cz =  2.879687

real	0m8.151s
user	0m10.202s
sys	0m1.445s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================

./execute_PyTestRegression.sh: line 413: ulimit: stack size: cannot modify limit: Operation not permitted
flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC//flowCart

=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 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	0m14.001s
user	0m24.402s
sys	0m0.771s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_OpenMDAO_3_alpha_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> alpha [2.]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

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 - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 3.625615
 Tessellating body 1 with  MaxEdge = 0.090640  Sag = 0.003626  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7  -mesh2d > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:10) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (13:18:13) aero.csh done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.01631562]  CL 0.12773309
----------------------------------------
----------------------------------------
>>> alpha [2.]
>>> CL2 [0.01631562]  CL 0.12773309
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:14) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (13:18:16) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:18:17) Linearizing cut-cells
   (13:18:17) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:18:17) Computing gradients
   (13:18:21) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.01572627]]
========================================
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  1.63156D-02    |proj g|=  1.57263D-02
----------------------------------------
>>> alpha [1.98427373]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:22) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (13:18:25) aero.csh done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.01606724]  CL 0.12675617
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:26) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (13:18:28) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:18:28) Linearizing cut-cells
   (13:18:28) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:18:28) Computing gradients
   (13:18:32) ... done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.01560329]]
========================================

At iterate    1    f=  1.60672D-02    |proj g|=  1.56033D-02
----------------------------------------
>>> alpha [-0.01099175]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:33) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1
   (13:18:35) aero.csh done
 o case M0.5901A-0.0109918B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [6.05653687e-06]  CL 0.00246101
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:37) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1
   (13:18:40) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:18:40) Linearizing cut-cells
   (13:18:40) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:18:40) Computing gradients
   (13:18:44) ... done
 o case M0.5901A-0.0109918B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.00031042]]
========================================

At iterate    2    f=  6.05654D-06    |proj g|=  3.10424D-04
----------------------------------------
>>> alpha [-0.05149286]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:45) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (13:18:47) aero.csh done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [2.59817201e-10]  CL 1.612e-05
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:48) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (13:18:51) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:18:51) Linearizing cut-cells
   (13:18:51) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:18:51) Computing gradients
   (13:18:55) ... done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[2.03612486e-06]]
========================================

At iterate    3    f=  2.59817D-10    |proj g|=  2.03612D-06
----------------------------------------
>>> alpha [-0.05176027]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:56) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (13:18:58) aero.csh done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [9.26120217e-15]  CL 1e-07
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:18:59) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (13:19:02) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:19:02) Linearizing cut-cells
   (13:19:02) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:19:02) Computing gradients
   (13:19:06) ... done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[1.21394333e-08]]
========================================

At iterate    4    f=  9.26120D-15    |proj g|=  1.21394D-08

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      4      5      4     0     0   1.214D-08   9.261D-15
  F =   9.2612021713000013E-015

CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL            
Optimization Complete
-----------------------------------
Optimized value: [-0.05176027]

real	1m3.173s
user	0m42.320s
sys	0m9.341s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_alpha_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_OpenMDAO_3_twist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> twist [4.]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 3.630958
 Tessellating body 1 with  MaxEdge = 0.018155  Sag = 0.000908  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:19:10) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:19:21) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00411365]  CL 0.0641354
----------------------------------------
----------------------------------------
>>> twist [4.]
>>> CL2 [0.00411365]  CL 0.0641354
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:19:23) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:19:41) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37528
              Estimated cutter memory:  0.003753 GB / DV
              Estimated xsensit memory: 0.071303 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:19:41) Linearizing cut-cells
   (13:19:43) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:19:43) Computing gradients
   (13:19:47) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[0.00210056]]
========================================
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  4.11365D-03    |proj g|=  2.10056D-03
----------------------------------------
>>> twist [3.99789944]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.630955
 Tessellating body 1 with  MaxEdge = 0.018155  Sag = 0.000908  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:19:49) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:20:01) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.0041123]  CL 0.0641197
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:20:03) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:20:20) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37527
              Estimated cutter memory:  0.003753 GB / DV
              Estimated xsensit memory: 0.071301 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:20:20) Linearizing cut-cells
   (13:20:22) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:20:22) Computing gradients
   (13:20:26) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[0.00210014]]
========================================

At iterate    1    f=  4.11230D-03    |proj g|=  2.10014D-03
----------------------------------------
>>> twist [-6.47168788]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.635635
 Tessellating body 1 with  MaxEdge = 0.018178  Sag = 0.000909  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:20:29) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:20:40) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00980712]  CL -0.0990178
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:20:42) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:21:00) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37091
              Estimated cutter memory:  0.003709 GB / DV
              Estimated xsensit memory: 0.070473 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:21:01) Linearizing cut-cells
   (13:21:03) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:21:03) Computing gradients
   (13:21:07) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-0.00318447]]
========================================
----------------------------------------
>>> twist [-0.15773834]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.625777
 Tessellating body 1 with  MaxEdge = 0.018129  Sag = 0.000906  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:21:09) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:21:20) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [2.57285916e-07]  CL -0.00057627
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:21:21) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:21:39) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37755
              Estimated cutter memory:  0.003776 GB / DV
              Estimated xsensit memory: 0.071735 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:21:39) Linearizing cut-cells
   (13:21:41) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:21:41) Computing gradients
   (13:21:45) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-1.67855757e-05]]
========================================

At iterate    2    f=  2.57286D-07    |proj g|=  1.67856D-05
----------------------------------------
>>> twist [-0.12478736]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.625742
 Tessellating body 1 with  MaxEdge = 0.018129  Sag = 0.000906  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:21:47) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:21:59) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [1.79305245e-08]  CL 0.00016606
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:22:00) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:22:18) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37755
              Estimated cutter memory:  0.003776 GB / DV
              Estimated xsensit memory: 0.071735 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (13:22:18) Linearizing cut-cells
   (13:22:20) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:22:20) Computing gradients
   (13:22:24) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[4.43473201e-06]]
========================================

At iterate    3    f=  1.79305D-08    |proj g|=  4.43473D-06

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      3      5      3     0     0   4.435D-06   1.793D-08
  F =   1.7930524486000000E-008

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.12478736]

real	3m17.624s
user	4m53.260s
sys	0m10.492s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'fun3d_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
fun3d_Morph_PyTest.py test;
+ python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 79623
	Number of elements       = 464233
	Number of triangles      = 15680
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 448553
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - Alpha
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Cd2
	Objective name - Const
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data 
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 

real	0m8.985s
user	0m8.092s
sys	0m0.861s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case fun3d_Morph_PyTest.py passed (as expected)
=================================================

Running.... STRUCTURE PyTests


=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

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

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

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

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input
Area      3.428666259747
Mass      5383.006027803
Centroid  [1.222256036874, 0.1634981473778, -4.234377369776e-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	0m5.221s
user	0m11.665s
sys	0m10.127s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'masstran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_AGARD445_PyTest.py test;
+ python -u masstran_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 36
	Number of elements = 25
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 25

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

Getting FEA properties.......
	Number of properties - 1
	Property name - yatesPlate
	Done getting FEA properties
Updating mesh element types based on properties input
Area      547.7004
Mass      0.01605224431138
Centroid  [20.03586282449, 14.01686746988, 0.0]
CG        [20.03586282449, 14.01686746988, 0.0]
Ixx       1.140246300554
Iyy       0.919317482675
Izz       2.059563783229
Ixy       0.7352134614013
Ixz       0.0
Iyz       0.0
I         [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0]
II        [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]]

real	0m0.617s
user	0m0.518s
sys	0m0.198s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

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

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

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

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

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

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

real	0m0.920s
user	0m0.826s
sys	0m0.156s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_CantileverPlate_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 40
	Number of elements = 51
	Elemental Tria3 = 0
	Elemental Quad4 = 27

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

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

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

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

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

Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
->HSMSOL
 Matrix Non-zero Entries = 1313

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   1*   0.326E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.03   0.00)
   1*   0.438E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2    0.274E+01  0.521E+01  0.106E-07    0.096  ddx @ (   1.00   0.03   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   2*   0.777E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3    0.202E+01  0.439E+01  0.928E-07    0.114  ddz @ (   1.00   0.03   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.623E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.163E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.167E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4    0.192E+01  0.476E+01  0.126E-07    0.105  ddz @ (   1.00   0.03   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.451E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.394E+01  0.254E-07    0.127  ddz @ (   1.00   0.07   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.638E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6    0.156E+01  0.300E+01  0.112E-06    0.166  ddx @ (   1.00   0.03   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   6*   0.193E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.272E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7    0.103E+01  0.323E+01  0.345E-07    0.155  ddx @ (   1.00   0.03   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.435E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8    0.756E+00  0.259E+01  0.139E-07    0.193  ddx @ (   1.00   0.07   0.00)
   8*   0.295E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   8*   0.350E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   8*   0.587E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9    0.678E+00  0.179E+01  0.639E-07    0.279  ddx @ (   0.89   0.10   0.00)
   9*   0.330E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.457E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.167E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   9*   0.264E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10    0.452E+00  0.171E+01  0.499E-07    0.292  ddz @ (   1.00   0.00   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.393E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.257E+00  0.120E+01  0.614E-08    0.417  ddz @ (   1.00   0.10   0.00)
  11*   0.206E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.283E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.488E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12    0.131E+00  0.647E+00  0.288E-08    0.772  ddz @ (   0.89   0.10   0.00)
  12*   0.238E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.357E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.849E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13    0.393E-01  0.238E+00  0.325E-07    1.000  ddx @ (   1.00   0.03   0.00)
  13*   0.336E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  13*   0.936E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  14    0.475E-03  0.514E-02  0.635E-07    1.000  ddx @ (   1.00   0.00   0.00)
  15    0.893E-06  0.651E-06  0.135E-08    1.000  drx @ (   1.00   0.10   0.00)
  16    0.574E-10  0.216E-09  0.140E-11    1.000  ddx @ (   0.44   0.10   0.00)
  17    0.558E-15  0.304E-14  0.603E-15    1.000  ddx @ (   1.00   0.00   0.00)

 Converging n vectors ...
 it =  1    dn =  0.193E+01   rlx = 1.000  (  12 )
 it =  2    dn =  0.435E-15   rlx = 1.000  (  28 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.285E+01   rlx = 0.351  (  24 )
 it =  2    de =  0.292E+01   rlx = 0.342  (  34 )
 it =  3    de =  0.226E+01   rlx = 0.442  (  34 )
 it =  4    de =  0.151E+01   rlx = 0.660  (  34 )
 it =  5    de =  0.665E+00   rlx = 1.000  (  34 )
 it =  6    de =  0.609E-01   rlx = 1.000  (  34 )
 it =  7    de =  0.573E-04   rlx = 1.000  (  34 )
 it =  8    de =  0.478E-13   rlx = 1.000  (  34 )

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

real	0m0.752s
user	0m0.719s
sys	0m0.157s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected)
=================================================

ASTROS_ROOT: /Users/jenkins/util/astros/Astros/Darwin-64bit

=================================================
+ echo 'astros_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 366
	Number of elements = 523
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 190
	Elemental Quad4 = 333
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 367
	Combined Number of elements = 524
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 190
	Combined Elemental Quad4 = 333
Getting vortex lattice surface data
	VLM surface name - Skin_Top
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 48
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !

Getting Aero Reference Parameters.......

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

Getting FEA properties.......
	Number of properties - 5
	Property name - Rib_Root
	No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
	Property name - Ribs
	No "material" specified for Property tuple Ribs, defaulting to an index of 1
	Property name - Skin
	No "material" specified for Property tuple Skin, defaulting to an index of 1
	Property name - Spar1
	No "material" specified for Property tuple Spar1, defaulting to an index of 1
	Property name - Spar2
	No "material" specified for Property tuple Spar2, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA supports.......
	Number of supports - 1
	Support name - ribSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Rib_Root
	No "groupName" specified for Connection tuple Rib_Root!
	Looking for automatic connections from the use of capsConnectLink for Rib_Root
	42 automatic connections were made for capsConnect Rib_Root (node id 367)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim1
	Done getting FEA analyses

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

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

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

real	0m9.265s
user	0m20.686s
sys	0m7.349s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_AGARD445_PyTest.py test;
+ python -u astros_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 36
	Number of elements = 25
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 25
Aero_Reference value is NULL - No aero reference parameters set

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 2
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
Natural freq (Mode 1) = 5.78 (Hz)
Natural freq (Mode 2) = 30.66 (Hz)

real	0m0.777s
user	0m0.616s
sys	0m0.258s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Composite_PyTest.py test;
+ python -u astros_Composite_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 15
	Number of elements = 8
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 8
Aero_Reference value is NULL - No aero reference parameters set

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - cantilever
	No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards

real	0m1.039s
user	0m0.706s
sys	0m0.293s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Composite_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = wing, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - wing
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = wing, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = wing, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 429
	Number of elements = 817
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 817
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - root
	No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
Natural freq (Mode 1) = 5.91949 (Hz)
Natural freq (Mode 2) = 29.79990 (Hz)
Natural freq (Mode 3) = 39.10550 (Hz)
Natural freq (Mode 4) = 77.71580 (Hz)
Natural freq (Mode 5) = 99.79550 (Hz)
Natural freq (Mode 6) = 146.97500 (Hz)
Natural freq (Mode 7) = 176.90300 (Hz)
Natural freq (Mode 8) = 235.53300 (Hz)
Natural freq (Mode 9) = 274.42600 (Hz)
Natural freq (Mode 10) = 311.35900 (Hz)
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10

real	0m29.889s
user	0m28.776s
sys	0m0.786s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_CompositeWingFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

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

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

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

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

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

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

real	0m1.228s
user	0m0.893s
sys	0m0.392s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'astros_MultipleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 16
	Number of elements = 9
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 9
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

Getting FEA loads.......
	Number of loads - 5
	Load name - load_0
	Load name - load_1
	Load name - load_2
	Load name - load_3
	Load name - load_4
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 5
	Analysis name - load_0
	Analysis name - load_1
	Analysis name - load_2
	Analysis name - load_3
	Analysis name - load_4
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

real	0m0.947s
user	0m0.787s
sys	0m0.295s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_MultipleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 293
Number of elements = 217
Number of triangle elements      = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes    = 293
Total number of elements = 217
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 293
	Number of elements = 217
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 217
Aero_Reference value is NULL - No aero reference parameters set

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02335 (Hz)
Natural freq (Mode 2) = 0.02335 (Hz)
Natural freq (Mode 3) = 0.11619 (Hz)
Natural freq (Mode 4) = 0.11619 (Hz)
Natural freq (Mode 5) = 0.14468 (Hz)
Natural freq (Mode 6) = 0.14468 (Hz)
Natural freq (Mode 7) = 0.23352 (Hz)
Natural freq (Mode 8) = 0.23352 (Hz)
Natural freq (Mode 9) = 0.30497 (Hz)
Natural freq (Mode 10) = 0.30497 (Hz)

real	0m12.051s
user	0m18.216s
sys	0m10.344s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 6
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 6
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

real	0m0.858s
user	0m0.688s
sys	0m0.278s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ python -u astros_ThreeBarFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 2
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
Natural freq (Mode 1) = 86.13400 (Hz)
Natural freq (Mode 2) = 168.53300 (Hz)

real	0m0.855s
user	0m0.684s
sys	0m0.279s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarLinkDesign_PyTest.py test;
+ python -u astros_ThreeBarLinkDesign_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

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

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

Getting FEA optimization control.......
Done getting FEA Optimization Control

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - Bar1A
	Design_Variable name - Bar2A
	Design_Variable name - Bar3A
	Design_Variable_Relation name - Bar1A
	Design_Variable_Relation name - Bar2A
	Design_Variable_Relation name - Bar3A
	Number of design variable relations - 3
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 3
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
Done getting FEA design constraints

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

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing design constraint cards
	Writing load cards
	Writing material cards
	Writing property cards
	Writing design variable cards


Running Astros......
Done running Astros!

real	0m0.946s
user	0m0.787s
sys	0m0.288s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarLinkDesign_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ python -u astros_ThreeBarMultiLoad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 2
	Constraint name - conOne
	No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
	Constraint name - conTwo
	No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - loadOne
	Load name - loadTwo
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 2
	Analysis name - analysisOne
	Analysis name - analysisTwo
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m0.865s
user	0m0.712s
sys	0m0.287s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m0.849s
user	0m0.685s
sys	0m0.287s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ python -u astros_Trim_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

Getting FEA properties.......
	Number of properties - 3
	Property name - Body
	Property name - Edge
	Property name - Root
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA supports.......
	Number of supports - 1
	Support name - PointSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	8 automatic connections were made for capsConnect Root (node id 97)
	Done getting FEA connections

Getting FEA loads.......
	Number of loads - 2
	Load name - GravityLoad
	No "groupName" specified for Load tuple GravityLoad, going to use load name
	Load name - PointLoad
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

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

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

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

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

real	0m1.140s
user	0m0.890s
sys	0m0.362s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================

Running.... AEROELASTIC PyTests


=================================================
+ echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Pressure_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Pressure_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1293      2452         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1298      2462         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3418      6687         0
AFLR4    : Nodes, Trias,Quads=      3008      5867         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1315      2496         0
AFLR4    : Nodes, Trias,Quads=      1297      2460         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1298      2462         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1319      2504         0
AFLR4    : Nodes, Trias,Quads=      1294      2454         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       200       344         0
AFLR4    : Nodes, Trias,Quads=       160       264         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       193       330         0
AFLR4    : Nodes, Trias,Quads=       155       254         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        17        21         0
AFLR4    : Nodes, Trias,Quads=        11         9         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9344     18684       928

AFLR4    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.121   seconds
Body 1 (of 1)
Number of nodes    = 9344
Number of elements = 18684
Number of triangle elements      = 18684
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9344
Total number of elements = 18684
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 57182
	Number of elements       = 328851
	Number of triangles      = 18684
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 310167
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
57182 grid points.
310167 volume elements.
3 surface markers.
12290 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
310167 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 102.753. Mean K: 0.746817. Standard deviation K: 4.38935.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        48.3512|        85.9255|
|     CV Face Area Aspect Ratio|        1.09173|        21.9812|
|           CV Sub-Volume Ratio|              1|        19.0295|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     57182|    1/1.00|        10|
|         1|      9725|    1/5.88|   8.31064|
|         2|      1709|    1/5.69|   6.98249|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.04169 m^2.
Area projection in the x-plane = 0.644461 m^2, y-plane = 0.295795 m^2, z-plane = 4.29819 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.379751 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86125e-18 m, z-direction = -0.0467278 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.3975e+00|   -1.298444|    0.998175|    0.628773|    4.170662|   -1.025477|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.3842e+00|   -1.701949|    0.831442|    0.450794|    3.754061|   -0.652898|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.3765e+00|   -1.702925|    0.646421|    0.285522|    3.754270|    1.070356|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.70293|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Pressure_SA.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Pressure_SA.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Pressure_SA.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Pressure_SA.szplt|

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

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

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


Running PostAnalysis ...... su2

Running ...... astros
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 180
	Number of elements = 194
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 32
	Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

Getting FEA loads.......
	Number of loads - 1
	Load name - pressureAero
	No "groupName" specified for Load tuple pressureAero, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 273
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.103657e+09, tgt = 3.103657e+09, diff = 1.802185e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 273
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.018170e+09, tgt = 3.018170e+09, diff = 1.966771e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 273
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.340170e+07, tgt = 4.340170e+07, diff = 5.609043e-03
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

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

Writing subElement types (if any) - appending mesh file

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

real	0m14.380s
user	0m13.520s
sys	0m1.813s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Displacement_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... astros
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 180
	Number of elements = 194
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 32
	Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

Running PostAnalysis ...... astros

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1293      2452         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1298      2462         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3418      6687         0
AFLR4    : Nodes, Trias,Quads=      3008      5867         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1315      2496         0
AFLR4    : Nodes, Trias,Quads=      1297      2460         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1298      2462         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1319      2504         0
AFLR4    : Nodes, Trias,Quads=      1294      2454         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       200       344         0
AFLR4    : Nodes, Trias,Quads=       160       264         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       193       330         0
AFLR4    : Nodes, Trias,Quads=       155       254         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        17        21         0
AFLR4    : Nodes, Trias,Quads=        11         9         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9344     18684       928

AFLR4    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.121   seconds
Body 1 (of 1)
Number of nodes    = 9344
Number of elements = 18684
Number of triangle elements      = 18684
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9344
Total number of elements = 18684
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 57182
	Number of elements       = 328851
	Number of triangles      = 18684
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 310167
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Displacement_SA_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
57182 grid points.
310167 volume elements.
3 surface markers.
12290 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
310167 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 12.991525 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
57182 grid points.
310167 volume elements.
3 surface markers.
12290 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
310167 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63997.8.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 84.836. Mean K: 0.750398. Standard deviation K: 3.83276.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        48.2553|        85.9829|
|     CV Face Area Aspect Ratio|        1.03546|        23.8558|
|           CV Sub-Volume Ratio|              1|        328.121|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     57182|    1/1.00|        10|
|         1|      9725|    1/5.88|   8.31064|
|         2|      1709|    1/5.69|   6.98249|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89964 m.
Wetted area = 11.4382 m^2.
Area projection in the x-plane = 2.82758 m^2, y-plane = 1.25436 m^2, z-plane = 4.17954 m^2.
Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89964 m, z-direction = 0.526515 m.
Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86125e-18 m, z-direction = -0.705261 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.3652e+00|   -0.620749|    1.814328|    1.306826|    4.848357|    0.056579|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.3442e+00|   -1.097282|    1.519547|    1.164533|    4.374272|    0.038462|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.3374e+00|   -1.096031|    1.280932|    0.955386|    4.371094|    0.095320|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.09603|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Displacement_SA.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Displacement_SA.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Displacement_SA.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Displacement_SA.szplt|

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

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

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


Running PostAnalysis ...... su2

real	0m32.608s
user	0m29.114s
sys	0m3.558s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Displacement_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Iterative_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 2

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       374       678         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       927      1777         0
AFLR4    : Nodes, Trias,Quads=       821      1565         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       374       678         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        63        96         0
AFLR4    : Nodes, Trias,Quads=        55        80         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        64        96         0
AFLR4    : Nodes, Trias,Quads=        57        82         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        11        13         0
AFLR4    : Nodes, Trias,Quads=         7         5         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2592      5180       482

AFLR4    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.059   seconds
Body 1 (of 1)
Number of nodes    = 2592
Number of elements = 5180
Number of triangle elements      = 5180
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2592
Total number of elements = 5180
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10612
	Number of elements       = 60053
	Number of triangles      = 5180
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 54873
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 51.6883. Mean K: 0.709649. Standard deviation K: 3.22583.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        47.3226|        86.6106|
|     CV Face Area Aspect Ratio|        1.16069|        20.6612|
|           CV Sub-Volume Ratio|              1|        41.1673|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10612|    1/1.00|        10|
|         1|      1892|    1/5.61|    8.4424|
|         2|       394|     1/4.8|   7.50612|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 7.82006 m^2.
Area projection in the x-plane = 0.576038 m^2, y-plane = 0.250011 m^2, z-plane = 3.65657 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.37624 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.47212e-18 m, z-direction = -0.0403729 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.2136e-01|   -0.752613|    1.603074|    1.223267|    4.716493|   -1.311926|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.2240e-01|   -1.082205|    1.490442|    1.104154|    4.374404|   -1.114824|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.2040e-01|   -1.179368|    1.358096|    0.964605|    4.275251|   -0.533556|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.17937|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Iterative.szplt|

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

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

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


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 180
	Number of elements = 194
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 32
	Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

Getting FEA loads.......
	Number of loads - 1
	Load name - pressureAero
	No "groupName" specified for Load tuple pressureAero, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.097227e+09, tgt = 3.097226e+09, diff = 1.089483e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.012978e+09, tgt = 3.012977e+09, diff = 2.112743e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 3.927686e+07, tgt = 3.927686e+07, diff = 1.330411e-02
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 0.814580 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 1002 TETRAHEDRON volume elements.
There has been a re-orientation of 23 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 64538.3.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 24.8316. Mean K: 0.529483. Standard deviation K: 1.74855.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        6.73178|        85.1515|
|     CV Face Area Aspect Ratio|        1.16566|        193.442|
|           CV Sub-Volume Ratio|              1|        34954.9|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10612|    1/1.00|        10|
|         1|      1892|    1/5.61|    8.4424|
|         2|       394|     1/4.8|   7.50612|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 4.3593 m.
Wetted area = 166.1 m^2.
Area projection in the x-plane = 64.6678 m^2, y-plane = 36.8864 m^2, z-plane = 5.36952 m^2.
Max. coordinate in the x-direction = 2.77567 m, y-direction = 4.3593 m, z-direction = 17.7259 m.
Min. coordinate in the x-direction = -0.670758 m, y-direction = -0.0550182 m, z-direction = -19.2264 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.3982e-01|    1.850145|    4.803488|    4.927158|    7.319250|   -0.010446|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.4435e-01|    2.131732|    4.741224|    4.926819|    7.571356|   -0.035666|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.4582e-01|    2.210547|    4.837044|    4.848737|    7.715818|   -0.049133|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       2.21055|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 45 non-physical points in the solution.
Warning: 2 reconstructed states for upwinding are non-physical.

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

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


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.687756e+09, tgt = 1.687756e+09, diff = 7.186773e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.233025e+09, tgt = 1.233025e+09, diff = 6.614255e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 1.590171e+07, tgt = 1.590171e+07, diff = 1.389396e-02
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 1002 TETRAHEDRON volume elements.
There has been a re-orientation of 23 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 64538.3.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 2.349139 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 28050 TETRAHEDRON volume elements.
There has been a re-orientation of 1548 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 3.65804e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 39.6075. Mean K: 0.844735. Standard deviation K: 3.00893.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.479317|        81.3858|
|     CV Face Area Aspect Ratio|        1.53919|        2639.46|
|           CV Sub-Volume Ratio|              1|         180990|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10612|    1/1.00|        10|
|         1|      1874|    1/5.66|   8.41554|
|         2|       388|    1/4.83|   7.46782|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 41.5668 m.
Wetted area = 9666.02 m^2.
Area projection in the x-plane = 3150.89 m^2, y-plane = 3288.39 m^2, z-plane = 148.571 m^2.
Max. coordinate in the x-direction = 12.6348 m, y-direction = 41.5668 m, z-direction = 4.01911 m.
Min. coordinate in the x-direction = -0.892365 m, y-direction = -2.47212e-18 m, z-direction = -557.504 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.3024e-01|    4.427863|    7.391414|    7.171071|    9.896969|   -0.048645|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.3905e-01|    4.500985|    7.273408|    7.111650|    9.918170|   -0.069453|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.4146e-01|    4.616846|    7.247613|    7.127463|    9.958173|   -0.064079|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       4.61685|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 153 non-physical points in the solution.
Warning: 23 reconstructed states for upwinding are non-physical.

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

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


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.813277e+09, tgt = 1.813277e+09, diff = 1.999578e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.342755e+09, tgt = 1.342754e+09, diff = 6.730101e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 9.181107e+06, tgt = 9.181107e+06, diff = 1.363268e-03
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 28050 TETRAHEDRON volume elements.
There has been a re-orientation of 1548 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 3.65804e+06.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 28.563708 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 30940 TETRAHEDRON volume elements.
There has been a re-orientation of 1270 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 1.35468e+11.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 35.222. Mean K: 0.469176. Standard deviation K: 1.88589.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.790352|        86.6011|
|     CV Face Area Aspect Ratio|        1.51912|        44521.5|
|           CV Sub-Volume Ratio|              1|    5.44297e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10612|    1/1.00|        10|
|         1|      1877|    1/5.65|   8.42003|
|         2|       385|    1/4.88|   7.44853|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 1.62199 m.
Wetted area = 1672.23 m^2.
Area projection in the x-plane = 242.328 m^2, y-plane = 485.511 m^2, z-plane = 66.762 m^2.
Max. coordinate in the x-direction = 9.23512 m, y-direction = 1.62199 m, z-direction = 252.05 m.
Min. coordinate in the x-direction = 0.036096 m, y-direction = -17.7692 m, z-direction = -0.520959 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.2429e-01|    7.060281|   10.027137|    9.994175|   12.529387|   -0.052400|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.3721e-01|    7.556625|   10.163626|   10.009975|   12.932925|   -0.051576|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.4399e-01|    7.624057|   10.221020|   10.005047|   13.052262|   -0.051325|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       7.62406|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 954 non-physical points in the solution.
Warning: 52 reconstructed states for upwinding are non-physical.

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

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


Running PostAnalysis ...... su2
Cl =  -436.704139
Cd =  8508.552832

real	0m45.950s
user	0m42.760s
sys	0m3.522s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Iterative_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelastic_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelastic_Iterative_SU2_and_Astros.py test;
+ python -u aeroelastic_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 2

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       374       678         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       927      1777         0
AFLR4    : Nodes, Trias,Quads=       821      1565         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       374       678         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        63        96         0
AFLR4    : Nodes, Trias,Quads=        55        80         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        64        96         0
AFLR4    : Nodes, Trias,Quads=        57        82         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        11        13         0
AFLR4    : Nodes, Trias,Quads=         7         5         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2592      5180       482

AFLR4    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.061   seconds
Body 1 (of 1)
Number of nodes    = 2592
Number of elements = 5180
Number of triangle elements      = 5180
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2592
Total number of elements = 5180
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10612
	Number of elements       = 60053
	Number of triangles      = 5180
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 54873
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 51.6883. Mean K: 0.709649. Standard deviation K: 3.22583.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        47.3226|        86.6106|
|     CV Face Area Aspect Ratio|        1.16069|        20.6612|
|           CV Sub-Volume Ratio|              1|        41.1673|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10612|    1/1.00|        10|
|         1|      1892|    1/5.61|    8.4424|
|         2|       394|     1/4.8|   7.50612|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 7.82006 m^2.
Area projection in the x-plane = 0.576038 m^2, y-plane = 0.250011 m^2, z-plane = 3.65657 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.37624 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.47212e-18 m, z-direction = -0.0403729 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.2097e-01|   -0.752613|    1.603074|    1.223267|    4.716493|   -1.311926|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.2174e-01|   -1.082205|    1.490442|    1.104154|    4.374404|   -1.114824|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.2061e-01|   -1.179368|    1.358096|    0.964605|    4.275251|   -0.533556|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.17937|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelastic_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file                           |surface_flow_aeroelastic_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary                     |flow_aeroelastic_Iterative.szplt   |

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelastic_Iterative.szplt|

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

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

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


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Ribs_and_Spars, index = 1
	Name = Skin, index = 2
	Name = Rib_Root, index = 3
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 746
	Number of elements = 898
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 120
	Elemental Quad4 = 778
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - Rib_Root
	Property name - Ribs_and_Spars
	Property name - Skin
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - pressureAero
	No "groupName" specified for Load tuple pressureAero, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.097227e+09, tgt = 3.097227e+09, diff = 8.756132e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.012978e+09, tgt = 3.012978e+09, diff = 9.489151e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 3.927686e+07, tgt = 3.927686e+07, diff = 2.115920e-01
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 30 (total = 690)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 0.835260 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 13404 TETRAHEDRON volume elements.
There has been a re-orientation of 650 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 111190.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 245.791. Mean K: 2.36718. Standard deviation K: 11.9897.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.39637|        84.6329|
|     CV Face Area Aspect Ratio|        1.34045|        386.205|
|           CV Sub-Volume Ratio|              1|         180510|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10612|    1/1.00|        10|
|         1|      1882|    1/5.64|    8.4275|
|         2|       387|    1/4.86|    7.4614|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 12.5855 m.
Wetted area = 1346.09 m^2.
Area projection in the x-plane = 397.31 m^2, y-plane = 387.785 m^2, z-plane = 54.8726 m^2.
Max. coordinate in the x-direction = 3.34756 m, y-direction = 12.5855 m, z-direction = 30.1696 m.
Min. coordinate in the x-direction = -12.504 m, y-direction = -0.438272 m, z-direction = -85.3561 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.4237e-01|    2.878121|    5.830029|    6.291368|    8.347227|    0.331982|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.4780e-01|    3.320027|    5.828884|    6.170839|    8.765605|   -0.263310|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.4718e-01|    3.475259|    5.900326|    6.169734|    8.845550|    0.150985|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       3.47526|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelastic_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file                           |surface_flow_aeroelastic_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary                     |flow_aeroelastic_Iterative.szplt   |

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelastic_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 106 non-physical points in the solution.
Warning: 7 reconstructed states for upwinding are non-physical.

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

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


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.572339e+09, tgt = 1.572338e+09, diff = 2.144719e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.376972e+09, tgt = 1.376971e+09, diff = 8.282179e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 6.481441e+06, tgt = 6.481456e+06, diff = 1.544752e+01
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 30 (total = 690)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 13404 TETRAHEDRON volume elements.
There has been a re-orientation of 650 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 111190.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 28.721496 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 24594 TETRAHEDRON volume elements.
There has been a re-orientation of 1056 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 3.8774e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 118.236. Mean K: 1.06215. Standard deviation K: 4.15513.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        0.56777|        81.7169|
|     CV Face Area Aspect Ratio|        1.41926|        2972.63|
|           CV Sub-Volume Ratio|              1|         426925|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10612|    1/1.00|        10|
|         1|      1874|    1/5.66|   8.41554|
|         2|       389|    1/4.82|   7.47423|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 11.3508 m.
Wetted area = 9647.04 m^2.
Area projection in the x-plane = 4960.46 m^2, y-plane = 3530.78 m^2, z-plane = 581.313 m^2.
Max. coordinate in the x-direction = 27.7225 m, y-direction = 11.3508 m, z-direction = 253.509 m.
Min. coordinate in the x-direction = -1.60666 m, y-direction = -19.7475 m, z-direction = -85.223 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.3503e-01|    4.070526|    7.024857|    7.285496|    9.539632|    0.080019|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.4664e-01|    4.500756|    7.017601|    7.167392|    9.890627|    0.101047|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.4967e-01|    4.653905|    7.108917|    7.239351|   10.072423|    0.101567|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       4.65391|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelastic_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file                           |surface_flow_aeroelastic_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary                     |flow_aeroelastic_Iterative.szplt   |

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelastic_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 288 non-physical points in the solution.
Warning: 24 reconstructed states for upwinding are non-physical.

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

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


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.674330e+09, tgt = 1.674330e+09, diff = 1.629931e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.455089e+09, tgt = 1.455089e+09, diff = 1.510583e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 8.579855e+06, tgt = 8.579841e+06, diff = 1.432880e+01
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 30 (total = 690)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 24594 TETRAHEDRON volume elements.
There has been a re-orientation of 1056 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 3.8774e+06.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 28.595424 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
10612 grid points.
54873 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54873 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 29325 TETRAHEDRON volume elements.
There has been a re-orientation of 1610 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 4.15276e+11.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 7.11348. Mean K: 0.279879. Standard deviation K: 0.83558.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.613169|        75.5879|
|     CV Face Area Aspect Ratio|        1.53901|        17227.9|
|           CV Sub-Volume Ratio|              1|     1.4608e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10612|    1/1.00|        10|
|         1|      1870|    1/5.67|   8.40955|
|         2|       386|    1/4.84|   7.45497|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.15717 m.
Wetted area = 255968 m^2.
Area projection in the x-plane = 53302.2 m^2, y-plane = 1395.02 m^2, z-plane = 1267.64 m^2.
Max. coordinate in the x-direction = 2.15196 m, y-direction = 7.15717 m, z-direction = 2395.67 m.
Min. coordinate in the x-direction = -54.829 m, y-direction = -147.937 m, z-direction = -2.06064 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.3899e-01|    7.447666|   10.414518|   10.335403|   12.916772|    0.024748|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.4916e-01|    7.872151|   10.374304|   10.394736|   13.266411|    0.025398|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.5059e-01|    7.981035|   10.542010|   10.438858|   13.319519|    0.025159|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       7.98103|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelastic_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file                           |surface_flow_aeroelastic_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary                     |flow_aeroelastic_Iterative.szplt   |

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelastic_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 837 non-physical points in the solution.
Warning: 61 reconstructed states for upwinding are non-physical.

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

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


Running PostAnalysis ...... su2

real	1m35.517s
user	1m43.829s
sys	0m10.526s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelastic_Iterative_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Temperature_SU2_and_TACS.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Temperature_SU2_and_TACS.py test;
+ python -u aeroelasticSimple_Temperature_SU2_and_TACS.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1293      2452         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1298      2462         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3418      6687         0
AFLR4    : Nodes, Trias,Quads=      3008      5867         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1315      2496         0
AFLR4    : Nodes, Trias,Quads=      1297      2460         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1298      2462         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1319      2504         0
AFLR4    : Nodes, Trias,Quads=      1294      2454         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       200       344         0
AFLR4    : Nodes, Trias,Quads=       160       264         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       193       330         0
AFLR4    : Nodes, Trias,Quads=       155       254         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        17        21         0
AFLR4    : Nodes, Trias,Quads=        11         9         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9344     18684       928

AFLR4    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.116   seconds
Body 1 (of 1)
Number of nodes    = 9344
Number of elements = 18684
Number of triangle elements      = 18684
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9344
Total number of elements = 18684
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 57182
	Number of elements       = 328851
	Number of triangles      = 18684
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 310167
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

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

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

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

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

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
57182 grid points.
310167 volume elements.
3 surface markers.
12290 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
310167 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 102.753. Mean K: 0.746817. Standard deviation K: 4.38935.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        48.3512|        85.9255|
|     CV Face Area Aspect Ratio|        1.09173|        21.9812|
|           CV Sub-Volume Ratio|              1|        19.0295|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     57182|    1/1.00|        10|
|         1|      9725|    1/5.88|   8.31064|
|         2|      1709|    1/5.69|   6.98249|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.04169 m^2.
Area projection in the x-plane = 0.644461 m^2, y-plane = 0.295795 m^2, z-plane = 4.29819 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.379751 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86125e-18 m, z-direction = -0.0467278 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.3512e+00|   -1.298444|    0.998175|    0.628773|    4.170662|   -1.025477|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.3508e+00|   -1.701949|    0.831442|    0.450794|    3.754061|   -0.652898|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.3542e+00|   -1.702925|    0.646421|    0.285522|    3.754270|    1.070356|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.70293|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Temperature_SM.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Temperature_SM.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Temperature_SM.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Temperature_SM.szplt|

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

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

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


Running PostAnalysis ...... su2

Running PreAnalysis ...... tacs
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 12
Number of elements = 12
Number of triangle elements      = 4
Number of quadrilateral elements = 8
----------------------------
Total number of nodes    = 12
Total number of elements = 12
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8

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

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

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

Getting FEA loads.......
	Number of loads - 1
	Load name - Skin
	No "groupName" specified for Load tuple Skin, going to use load name
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
	Number of variables = 16
	Number of data points = 273
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature'
            Rank 0: src = 1.497709e+03, tgt = 1.497709e+03, diff = 8.633884e-06
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
	Number of variables = 16
	Number of data points = 273
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature'
            Rank 0: src = 1.453904e+03, tgt = 1.453904e+03, diff = 6.575376e-06
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
	Number of variables = 16
	Number of data points = 273
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature'
            Rank 0: src = 2.084131e+01, tgt = 2.084131e+01, diff = 0.000000e+00
Extracting external thermal loads from data transfer....
	TransferName = Skin_Top
	Number of Nodes = 9 (total = 9)
Extracting external thermal loads from data transfer....
	TransferName = Skin_Bottom
	Number of Nodes = 9 (total = 18)
Extracting external thermal loads from data transfer....
	TransferName = Skin_Tip
	Number of Nodes = 4 (total = 16)

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards

Running PostAnalysis ...... tacs

real	0m14.113s
user	0m13.411s
sys	0m1.723s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Temperature_SU2_and_TACS.py passed (as expected)
=================================================

Running.... CORSAIRLITE PyTests


=================================================
+ echo 'gp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
gp.py test;
+ python -u gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.00713 dimensionless

Variables
---------
   x  :   3.00000   [-]   The X variable
   y  :  81.00008   [-]   The Y variable
   z  :   0.19245   [-]   The Z variable

Sensitivities
-------------
   No Constants in the Formulation

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


real	0m10.744s
user	0m1.283s
sys	0m0.284s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case gp.py passed (as expected)
=================================================


=================================================
+ echo 'qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
qp.py test;
+ python -u qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

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

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

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

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

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


real	0m1.362s
user	0m1.357s
sys	0m0.166s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case qp.py passed (as expected)
=================================================


=================================================
+ echo 'sp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
sp.py test;
+ python -u sp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.45721 dimensionless

Variables
---------
   x  :  2.56155   [-]   The X variable
   y  :  6.56155   [-]   The Y variable
   z  :  1.17116   [-]   The Z variable

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

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Signomial Program--Standard 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  3 
   Termination Status     :  Converged, relative error (3.15e-04) is less than specified tolerance (1.00e-03) 


real	0m1.269s
user	0m1.324s
sys	0m0.168s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case sp.py passed (as expected)
=================================================


=================================================
+ echo 'boydBox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
boydBox.py test;
+ python -u boydBox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.00520 1 / meter ** 3

Variables
---------
   d  :  11.26658   meter   The Z variable
   h  :   2.92246   meter   The Y variable
   w  :   5.84486   meter   The X variable

Constants
---------
   Aflr   :  1000         meter ** 2   Area of floor          
   Awall  :   100         meter ** 2   Area of wall           
   alpha  :     0.50000      [-]       Aspect Ratio Constraint
   beta   :     2            [-]       Aspect Ratio Constraint
   delta  :     2            [-]       Aspect Ratio Constraint
   gamma  :     0.50000      [-]       Aspect Ratio Constraint

Sensitivities
-------------
   Sensitivities not computed

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


real	0m1.115s
user	0m1.150s
sys	0m0.161s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case boydBox.py passed (as expected)
=================================================


=================================================
+ echo 'hoburg_gp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_gp.py test;
+ python -u hoburg_gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   5905.58568 newton

Variables
---------
   AR          :       20.36983        [-]         aspect ratio                                                            
   C_D_0       :        0.01271        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.01273        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.00778        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.00180        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.00180        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.00180        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.00542        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.00542        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.00023        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.00549        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.00551        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.00575        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.57420        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.57421        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.11881        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.00002        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    36139.20785       newton       Root Bending unit per unit chord                                        
   P_max       :  1185884.98442        watt        Maximum Engine Power                                                    
   R           :     4999.98983     kilometer      Single Segment range                                                    
   Re_0        :  4232645.50367        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4051247.93913        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9305153.26607        [-]         Reynolds Number, segment 2                                              
   S           :       27.73109     meter ** 2     total wing area                                                         
   T_0         :      746.21338       newton       Thrust, segment 0                                                       
   T_1         :      684.51827       newton       Thrust, segment 1                                                       
   T_2         :     2208.51611       newton       Thrust, segment 2                                                       
   V_0         :       68.23357   meter / second   Velocity, segment 0                                                     
   V_1         :       65.30930   meter / second   Velocity, segment 1                                                     
   V_2         :      150.00638   meter / second   Velocity, segment 2                                                     
   V_stall     :       37.99896   meter / second   stall speed                                                             
   W_0         :    33698.97702       newton       Weight, segment 0                                                       
   W_1         :    30873.13301       newton       Weight, segment 1                                                       
   W_2         :    33698.96566       newton       Weight, segment 2                                                       
   W_MTO       :    36788.13387       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4091.65066       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2806.10727       newton       Engine Weight                                                           
   W_fuel_out  :     3079.86524       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     2825.71897       newton       Weight of fuel, return                                                  
   W_pay       :     4905.15902       newton       Payload Weight                                                          
   W_tilde     :    22409.98513       newton       Dry Weight, no wing                                                     
   W_web       :      139.91823       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8462.91404       newton       wing weight                                                             
   W_zfw       :    30872.92436       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.26999        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.26996        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.27945        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.90752        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.90742        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.93932        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.77139        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.77131        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.79842        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.78603        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.90003        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.45002        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.00456        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.00069        [-]         Spar web thickness per unit chord                                       
   tau         :        0.15000        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.08745        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.08758        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.78500           meter ** 2          Disk area of propeller                             
   CDA0             :         0.05000           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.50000              [-]              max CL with flaps down                             
   N_lift           :         6                    [-]              Ultimate Load Factor                               
   W_fixed          :     14700                   newton            fixed weight                                       
   e                :         0.95000              [-]              Oswald efficiency factor                           
   eta_eng          :         0.35000              [-]              Engine Efficiency                                  
   eta_v            :         0.85000              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                    [-]              Added Weight Fraction                              
   g                :         9.81000      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000              joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.03720     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.00002   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.75000              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.90912     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.22500     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700           kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700           kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       310                 megapascal          Allowable tensile stress of aluminum               
   sigma_max_shear  :       167                 megapascal          Allowable shear stress of aluminum                 
   w_bar            :         0.50000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not computed

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


real	0m9.109s
user	0m9.027s
sys	0m0.235s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hoburg_gp.py passed (as expected)
=================================================


=================================================
+ echo 'hoburg_blackbox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_blackbox.py test;
+ python -u hoburg_blackbox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   5905.2294 newton

Variables
---------
   AR          :       20.3737        [-]         aspect ratio                                                            
   C_D_0       :        0.0127        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.0127        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.0078        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.0018        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.0018        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.0018        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.0054        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.0054        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.0002        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.0055        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.0055        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.0057        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.5743        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.5743        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.1189        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.0000        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    36141.5015       newton       Root Bending unit per unit chord                                        
   P_max       :  1184357.7688        watt        Maximum Engine Power                                                    
   R           :     5000.0000     kilometer      Single Segment range                                                    
   Re_0        :  4231748.4656        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4050340.4364        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9301869.2065        [-]         Reynolds Number, segment 2                                              
   S           :       27.7189     meter ** 2     total wing area                                                         
   T_0         :      746.1648       newton       Thrust, segment 0                                                       
   T_1         :      684.5072       newton       Thrust, segment 1                                                       
   T_2         :     2206.5587       newton       Thrust, segment 2                                                       
   V_0         :       68.2403   meter / second   Velocity, segment 0                                                     
   V_1         :       65.3149   meter / second   Velocity, segment 1                                                     
   V_2         :      150.0000   meter / second   Velocity, segment 2                                                     
   V_stall     :       38.0000   meter / second   stall speed                                                             
   W_0         :    33694.3546       newton       Weight, segment 0                                                       
   W_1         :    30868.7209       newton       Weight, segment 1                                                       
   W_2         :    33694.3546       newton       Weight, segment 2                                                       
   W_MTO       :    36773.9503       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4091.0280       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2802.5264       newton       Engine Weight                                                           
   W_fuel_out  :     3079.5957       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     2825.6337       newton       Weight of fuel, return                                                  
   W_pay       :     4905.0000       newton       Payload Weight                                                          
   W_tilde     :    22407.5264       newton       Dry Weight, no wing                                                     
   W_web       :      139.5692       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8461.1945       newton       wing weight                                                             
   W_zfw       :    30868.7209       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.2700        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.2700        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.2795        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.9075        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.9074        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.9394        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.7714        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.7713        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.7985        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.7860        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.9000        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.4500        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.0046        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.0007        [-]         Spar web thickness per unit chord                                       
   tau         :        0.1500        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.0875        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.0876        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.7850           meter ** 2          Disk area of propeller                             
   CDA0             :         0.0500           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.5000              [-]              max CL with flaps down                             
   N_lift           :         6                   [-]              Ultimate Load Factor                               
   W_fixed          :     14700                  newton            fixed weight                                       
   e                :         0.9500              [-]              Oswald efficiency factor                           
   eta_eng          :         0.3500              [-]              Engine Efficiency                                  
   eta_v            :         0.8500              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                   [-]              Added Weight Fraction                              
   g                :         9.8100      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000             joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.0372     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.0000   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.7500              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.9091     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.2250     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700          kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700          kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       310                megapascal          Ultimate tensile stress of aluminum                
   sigma_max_shear  :       167                megapascal          Ultimate shear stress of aluminum                  
   w_bar            :         0.5000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not currently implemented for optimization type Logspace Sequential Quadratic Program 

Solve Report
------------
   Solve Method           :  Logspace Sequential Quadratic Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  7 
   Termination Status     :  Converged, gradient of Lagrangian (9.638917e-07) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 5 (Step 5).  Watchdog counter is 1
   2. Wolfe Condition 1 failed at iteration 6 (Step 6).  Watchdog counter is 2


real	0m34.887s
user	0m34.681s
sys	0m0.263s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hoburg_blackbox.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/sizeWing.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/sizeWing.py test;
+ python -u pyCAPS/sizeWing.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2

Objective
---------
   0.075 dimensionless

Variables
---------
   AR     :  10.000        [-]         Wing aspect ratio
   CD     :   0.075        [-]         Drag Coefficient 
   CL     :   0.999        [-]         Lift Coefficient 
   S      :   2.642     meter ** 2     Wing area        
   V      :   2.722   meter / second   Airspeed         
   W      :  11.979       newton       Aircraft weight  
   Wwing  :   1.598       newton       Wing weight      

Constants
---------
   ARmax     :  10                [-]            Max AR                                         
   CD0       :   0.040            [-]            Profile drag                                   
   CLmax     :   1                [-]            Max CL                                         
   E0        :  10               joule           Maximum elastic potential energy in rubber band
   Wfixed    :   0.100           newton          Weight of fixed components                     
   Wrock     :   2               newton          Weight of each rock                            
   e         :   0.900            [-]            Oswawld efficiency factor                      
   g         :   9.810    meter / second ** 2    Gravitational constant                         
   nrock     :   2                [-]            Number of rocks to carry                       
   rho       :   1.225   kilogram / meter ** 3   Density of air                                 
   rho_wing  :   1       kilogram / meter ** 3   Weight density of wing                         
   tau       :   0.120            [-]            Airfoil thickness as t/c                       

Sensitivities
-------------
   Sensitivities not computed

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

Optimized L/D: 13.267784561972134
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m1.724s
user	0m1.633s
sys	0m0.224s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/sizeWing.py passed (as expected)
=================================================

avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/avl

=================================================
+ echo 'pyCAPS/optTaperAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optTaperAvl.py test;
+ python -u pyCAPS/optTaperAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)

Objective
---------
   1.00805 dimensionless

Variables
---------
   e    :  0.99202   [-]   Oswald efficiency factor
   lam  :  0.39881   [-]   Wing taper ratio        

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  6 
   Termination Status     :  Converged, gradient of Lagrangian (5.888882e-08) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 5 (Step 5).  Watchdog counter is 1


real	0m6.348s
user	0m3.906s
sys	0m2.319s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/optTaperAvl.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/optWingAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optWingAvl.py test;
+ python -u pyCAPS/optWingAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2
Starting iteration 0 at 0.2998 seconds
AR : 9.0 dimensionless
CD : 0.1 dimensionless
CL : 1.0 dimensionless
S : 1.0 meter ** 2
V : 1.0 meter / second
W : 10.0 newton
Wwing : 0.1 newton
e : 1.0 dimensionless
lam : 0.3 dimensionless
AVL run case - lam, AR: 0.3 9.0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9905504143712885 dimensionless
dydx: [<Quantity(0.06083473495512859, 'dimensionless')>, <Quantity(-0.0014769756676574763, 'dimensionless')>]
Calling cvxopt.solvers.cp at 1.3793 seconds
Got sol from cvxopt at 1.3931 seconds
status optimal
x [ 1.05e-01]
[-3.26e-01]
[-1.49e-11]
[-4.10e-01]
[ 1.28e+00]
[-6.40e-01]
[ 7.00e-01]
[-1.08e-02]
[ 5.73e-03]
[-3.20e-16]
[ 3.50e-16]
[ 1.56e-16]
[ 5.20e-16]
[ 2.70e-16]
[ 4.16e-27]
[ 3.37e-16]
[ 2.07e-23]

y [-6.40e-01]
[ 7.00e-01]
[ 3.11e-01]

znl [ 6.74e-01]
[ 4.14e-08]

zl [ 1.04e+00]
[ 5.41e-01]
[ 8.31e-12]

snl [ 8.55e-11]
[ 2.03e-01]

sl [ 1.49e-11]
[ 4.30e-10]
[ 8.74e-01]

gap 8.743959706208345e-09
relative gap 7.194197617465325e-09
primal objective -1.2154183372695615
dual objective -1.215418341683548
primal slack 1.3843122277352784e-11
dual slack 8.310943825862027e-12
primal infeasibility 1.1390345696246042e-09
dual infeasibility 2.382358051743254e-11
AVL run case - lam, AR: 0.3017253411785187 9.999999995701312
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9892210301572447 dimensionless
dydx: [<Quantity(0.06359341837318677, 'dimensionless')>, <Quantity(-0.0014812479871501028, 'dimensionless')>]
logspace stuff at 2.4857 seconds
Starting iteration 1 at 2.5149 seconds
AR : 9.999999995701312 dimensionless
CD : 0.07217671497330198 dimensionless
CL : 0.9999999999851361 dimensionless
S : 0.6639217992634344 meter ** 2
V : 3.600068783658013 meter / second
W : 5.270412635736404 newton
Wwing : 0.20138431695627712 newton
e : 0.9892553874048063 dimensionless
lam : 0.3017253411785187 dimensionless
Calling cvxopt.solvers.cp at 2.5231 seconds
Got sol from cvxopt at 2.5352 seconds
status optimal
x [ 3.90e-10]
[-5.94e-05]
[-1.96e-07]
[ 1.14e-08]
[ 7.38e-08]
[-3.68e-08]
[ 1.70e-08]
[ 1.33e-04]
[ 8.64e-03]
[ 6.35e-21]
[-6.95e-21]
[ 2.23e-16]
[ 5.42e-17]
[ 2.20e-16]
[ 1.27e-26]
[ 5.00e-16]
[ 6.63e-26]

y [ 1.27e-05]
[-1.39e-05]
[ 4.46e-01]

znl [ 1.00e+00]
[ 1.33e-10]

zl [ 1.08e-01]
[ 4.39e-01]
[ 2.53e-11]

snl [ 2.06e-11]
[ 2.03e-01]

sl [ 1.96e-07]
[ 4.02e-11]
[ 8.74e-01]

gap 2.1363031594437688e-08
relative gap 8.126967446453998e-09
primal objective -2.62865967351191
dual objective -2.628659684337801
primal slack 2.057784648174032e-11
dual slack 2.5305040679144164e-11
primal infeasibility 3.0858033491332136e-09
dual infeasibility 3.1339130723066173e-09
AVL run case - lam, AR: 0.30434464835757047 9.99999999959832
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9893844569299911 dimensionless
dydx: [<Quantity(0.06135879009172007, 'dimensionless')>, <Quantity(-0.0014697917150108264, 'dimensionless')>]
logspace stuff at 3.6184 seconds
Starting iteration 2 at 3.6517 seconds
AR : 9.99999999959832 dimensionless
CD : 0.07217242517886913 dimensionless
CL : 0.9999998041107226 dimensionless
S : 0.6639218068635588 meter ** 2
V : 3.6000690493939635 meter / second
W : 5.270412441791245 newton
Wwing : 0.20138432037500312 newton
e : 0.9893868959018433 dimensionless
lam : 0.30434464835757047 dimensionless
Calling cvxopt.solvers.cp at 3.6595 seconds
Got sol from cvxopt at 3.6716 seconds
status optimal
x [ 7.75e-13]
[-3.52e-04]
[ 4.29e-09]
[-2.11e-10]
[-1.42e-09]
[ 1.25e-09]
[-3.17e-10]
[ 7.91e-04]
[ 4.20e-02]
[ 7.26e-21]
[-7.89e-21]
[ 2.23e-16]
[ 5.45e-17]
[ 2.20e-16]
[ 1.24e-26]
[ 5.00e-16]
[ 6.65e-26]

y [ 1.45e-05]
[-1.58e-05]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.33e-10]

zl [ 1.09e-01]
[ 4.39e-01]
[ 2.49e-11]

snl [ 2.02e-11]
[ 2.03e-01]

sl [ 1.92e-07]
[ 3.94e-11]
[ 8.74e-01]

gap 2.0979541929276537e-08
relative gap 7.980432611479698e-09
primal objective -2.628872763000075
dual objective -2.628872773631924
primal slack 2.022619551948966e-11
dual slack 2.4870270233858892e-11
primal infeasibility 3.030673275142993e-09
dual infeasibility 3.076932689522998e-09
AVL run case - lam, AR: 0.31740935131467607 9.999999999606068
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9901147289476424 dimensionless
dydx: [<Quantity(0.0507308561720321, 'dimensionless')>, <Quantity(-0.0014191909882388387, 'dimensionless')>]
logspace stuff at 4.7714 seconds
Starting iteration 3 at 4.8046 seconds
AR : 9.999999999606068 dimensionless
CD : 0.07214699157333947 dimensionless
CL : 0.9999998084033913 dimensionless
S : 0.6639218067235316 meter ** 2
V : 3.6000690442960215 meter / second
W : 5.270412448377283 newton
Wwing : 0.20138432031121437 newton
e : 0.9901696737886146 dimensionless
lam : 0.31740935131467607 dimensionless
Calling cvxopt.solvers.cp at 4.8129 seconds
Got sol from cvxopt at 4.8244 seconds
status optimal
x [ 2.14e-12]
[-1.28e-03]
[ 1.17e-08]
[-5.10e-10]
[-3.51e-09]
[ 4.16e-09]
[-7.67e-10]
[ 2.88e-03]
[ 1.81e-01]
[-4.10e-21]
[ 4.49e-21]
[ 2.23e-16]
[ 5.51e-17]
[ 2.20e-16]
[ 1.18e-26]
[ 5.00e-16]
[ 6.61e-26]

y [-8.19e-06]
[ 8.98e-06]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.32e-10]

zl [ 1.10e-01]
[ 4.40e-01]
[ 2.37e-11]

snl [ 1.92e-11]
[ 2.03e-01]

sl [ 1.80e-07]
[ 3.73e-11]
[ 8.74e-01]

gap 1.9913348951306756e-08
relative gap 7.572537674951306e-09
primal objective -2.629679746219923
dual objective -2.6296797563122976
primal slack 1.9233234442651708e-11
dual slack 2.3654666053878418e-11
primal infeasibility 2.8765759272243296e-09
dual infeasibility 2.9202708384568647e-09
AVL run case - lam, AR: 0.3802990571829513 9.999999999627487
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9919295458295698 dimensionless
dydx: [<Quantity(0.009583432731846697, 'dimensionless')>, <Quantity(-0.0013533445524949173, 'dimensionless')>]
logspace stuff at 5.9199 seconds
Starting iteration 4 at 5.9533 seconds
AR : 9.999999999627487 dimensionless
CD : 0.07205440311146945 dimensionless
CL : 0.9999998201037487 dimensionless
S : 0.6639218063847039 meter ** 2
V : 3.600069031643115 meter / second
W : 5.270412470306197 newton
Wwing : 0.20138432015683608 newton
e : 0.9930297814909534 dimensionless
lam : 0.3802990571829513 dimensionless
Calling cvxopt.solvers.cp at 5.9613 seconds
Got sol from cvxopt at 5.9726 seconds
status optimal
x [-1.57e-12]
[ 4.08e-04]
[-8.59e-09]
[ 5.53e-10]
[ 3.53e-09]
[-9.72e-10]
[ 8.30e-10]
[-9.18e-04]
[ 5.19e-02]
[-2.12e-20]
[ 2.32e-20]
[ 2.24e-16]
[ 5.46e-17]
[ 2.20e-16]
[ 1.23e-26]
[ 5.00e-16]
[ 6.59e-26]

y [-4.25e-05]
[ 4.64e-05]
[ 4.47e-01]

znl [ 1.00e+00]
[ 1.32e-10]

zl [ 1.09e-01]
[ 4.39e-01]
[ 2.45e-11]

snl [ 1.99e-11]
[ 2.03e-01]

sl [ 1.88e-07]
[ 3.88e-11]
[ 8.74e-01]

gap 2.068840347932985e-08
relative gap 7.866667127620657e-09
primal objective -2.6298816441197554
dual objective -2.629881654604457
primal slack 1.9944303018506357e-11
dual slack 2.4539201182233166e-11
primal infeasibility 2.98538234782961e-09
dual infeasibility 3.036429124305033e-09
AVL run case - lam, AR: 0.40055731598206795 9.999999999611775
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9920150584836795 dimensionless
dydx: [<Quantity(-0.0008541793291738653, 'dimensionless')>, <Quantity(-0.0013850816280497336, 'dimensionless')>]
logspace stuff at 7.0592 seconds
Starting iteration 5 at 7.0927 seconds
AR : 9.999999999611775 dimensionless
CD : 0.07208383829260467 dimensionless
CL : 0.9999998115160276 dimensionless
S : 0.6639218067517706 meter ** 2
V : 3.600069044356993 meter / second
W : 5.270412465184854 newton
Wwing : 0.20138432032400533 newton
e : 0.9921187131763987 dimensionless
lam : 0.40055731598206795 dimensionless
Calling cvxopt.solvers.cp at 7.1011 seconds
Got sol from cvxopt at 7.1124 seconds
status optimal
x [ 8.00e-13]
[ 4.58e-05]
[ 4.24e-09]
[-2.43e-10]
[-1.58e-09]
[ 8.36e-10]
[-3.65e-10]
[-1.03e-04]
[-4.33e-03]
[-2.09e-21]
[ 2.29e-21]
[ 2.23e-16]
[ 5.49e-17]
[ 2.19e-16]
[ 1.20e-26]
[ 5.00e-16]
[ 6.74e-26]

y [-4.18e-06]
[ 4.57e-06]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.35e-10]

zl [ 1.10e-01]
[ 4.39e-01]
[ 2.41e-11]

snl [ 1.96e-11]
[ 2.03e-01]

sl [ 1.84e-07]
[ 3.80e-11]
[ 8.74e-01]

gap 2.03195584299249e-08
relative gap 7.726423169451732e-09
primal objective -2.629879050666439
dual objective -2.6298790609642584
primal slack 1.96170271739492e-11
dual slack 2.4096853737054615e-11
primal infeasibility 2.932364427218199e-09
dual infeasibility 2.9672633872176456e-09
AVL run case - lam, AR: 0.3988264545569237 9.999999999619773
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9920158805953644 dimensionless
dydx: [<Quantity(-6.436455185498957e-06, 'dimensionless')>, <Quantity(-0.0013814190269140214, 'dimensionless')>]
logspace stuff at 8.3541 seconds
Starting iteration 6 at 8.3886 seconds
AR : 9.999999999619773 dimensionless
CD : 0.07208714305299323 dimensionless
CL : 0.9999998157581855 dimensionless
S : 0.663921806590554 meter ** 2
V : 3.6000690386621303 meter / second
W : 5.270412469588717 newton
Wwing : 0.20138432025057312 newton
e : 0.9920165401543825 dimensionless
lam : 0.3988264545569237 dimensionless
Calling cvxopt.solvers.cp at 8.3971 seconds
Got sol from cvxopt at 8.4090 seconds
status optimal
x [ 2.35e-13]
[ 2.97e-07]
[ 1.09e-09]
[-5.55e-11]
[-3.69e-10]
[ 2.96e-10]
[-8.34e-11]
[-6.65e-07]
[-3.26e-05]
[ 1.22e-24]
[-1.28e-24]
[ 2.23e-16]
[ 5.49e-17]
[ 2.19e-16]
[ 1.20e-26]
[ 5.00e-16]
[ 6.76e-26]

y [ 2.45e-09]
[-2.57e-09]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.35e-10]

zl [ 1.10e-01]
[ 4.39e-01]
[ 2.40e-11]

snl [ 1.95e-11]
[ 2.03e-01]

sl [ 1.83e-07]
[ 3.78e-11]
[ 8.74e-01]

gap 2.0211071384152197e-08
relative gap 7.685171306919208e-09
primal objective -2.629879097939628
dual objective -2.629879108182283
primal slack 1.9527381358880008e-11
dual slack 2.3958347059782203e-11
primal infeasibility 2.915631182161227e-09
dual infeasibility 2.933788345710238e-09
AVL run case - lam, AR: 0.39881343720167217 9.999999999622123
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9920158812322761 dimensionless
dydx: [<Quantity(-5.709554107280468e-07, 'dimensionless')>, <Quantity(-0.0013813957757918827, 'dimensionless')>]
logspace stuff at 9.4963 seconds

Objective
---------
   0.072 dimensionless

Variables
---------
   AR     :  10.000        [-]         Wing aspect ratio       
   CD     :   0.072        [-]         Drag Coefficient        
   CL     :   1.000        [-]         Lift Coefficient        
   S      :   0.664     meter ** 2     Wing area               
   V      :   3.600   meter / second   Airspeed                
   W      :   5.270       newton       Aircraft weight         
   Wwing  :   0.201       newton       Wing weight             
   e      :   0.992        [-]         Oswald efficiency factor
   lam    :   0.399        [-]         Wing taper ratio        

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  7 
   Termination Status     :  Converged, gradient of Lagrangian (1.043841e-07) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 3 (Step 3).  Watchdog counter is 1

13.872092548132615

real	0m11.135s
user	0m6.951s
sys	0m4.075s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/optWingAvl.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/GPSize.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/GPSize.py test;
+ python -u pyCAPS/GPSize.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   6339.9402476213 newton

Variables
---------
   AR          :       18.0583068591        [-]         aspect ratio                                                            
   C_D_0       :        0.0127966186        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.0128135534        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.0077622395        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.0017626506        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.0017626506        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.0017626510        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.0056016002        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.0056028716        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.0002594009        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.0054327043        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.0054483614        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.0057382717        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.5494535783        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.5495159270        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.1182390122        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.0000193397        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    32106.9717613474       newton       Root Bending unit per unit chord                                        
   P_max       :  1211155.7559680410        watt        Maximum Engine Power                                                    
   R           :     4999.9816129528     kilometer      Single Segment range                                                    
   Re_0        :  4636790.3991634697        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4427330.4209076529        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9995446.9239517339        [-]         Reynolds Number, segment 2                                              
   S           :       28.3664420021     meter ** 2     total wing area                                                         
   T_0         :      799.0178645705       newton       Thrust, segment 0                                                       
   T_1         :      729.4239244544       newton       Thrust, segment 1                                                       
   T_2         :     2252.7493855701       newton       Thrust, segment 2                                                       
   V_0         :       69.5874592840   meter / second   Velocity, segment 0                                                     
   V_1         :       66.4439512429   meter / second   Velocity, segment 1                                                     
   V_2         :      150.0084591036   meter / second   Velocity, segment 2                                                     
   V_stall     :       37.9986643205   meter / second   stall speed                                                             
   W_0         :    34307.5807516552       newton       Weight, segment 0                                                       
   W_1         :    31281.5531631161       newton       Weight, segment 1                                                       
   W_2         :    34307.5610637156       newton       Weight, segment 2                                                       
   W_MTO       :    37630.4011124297       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4278.1047592241       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2854.2361754189       newton       Engine Weight                                                           
   W_fuel_out  :     3314.0247993997       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     3025.9122892774       newton       Weight of fuel, return                                                  
   W_pay       :     4905.2326701420       newton       Payload Weight                                                          
   W_tilde     :    22457.8594632444       newton       Dry Weight, no wing                                                     
   W_web       :      133.6940460361       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8823.3040844200       newton       wing weight                                                             
   W_zfw       :    31281.2018350684       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.2693167459        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.2692858916        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.2791280518        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.9052651192        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.9051614203        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.9382448822        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.7694756986        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.7693875506        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.7975082496        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.7860410805        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.9000448519        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.4500404597        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.0043345438        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.0006000270        [-]         Spar web thickness per unit chord                                       
   tau         :        0.1499996279        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.0922115805        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.0923337617        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.7850000000           meter ** 2          Disk area of propeller                             
   CDA0             :         0.0500000000           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.5000000000              [-]              max CL with flaps down                             
   N_lift           :         6                         [-]              Ultimate Load Factor                               
   W_fixed          :     14700                        newton            fixed weight                                       
   e                :         0.9500000000              [-]              Oswald efficiency factor                           
   eta_eng          :         0.3500000000              [-]              Engine Efficiency                                  
   eta_v            :         0.8500000000              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                         [-]              Added Weight Fraction                              
   g                :         9.8100000000      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000                   joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.0372000000     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.0000171000   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.7500000000              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.9091220000     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.2250000000     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700                kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700                kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       250                      megapascal          Allowable tensile stress of aluminum               
   sigma_max_shear  :       167                      megapascal          Allowable shear stress of aluminum                 
   w_bar            :         0.5000000000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not computed

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

 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m9.684s
user	0m9.386s
sys	0m0.395s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/GPSize.py passed (as expected)
=================================================

mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/mses

=================================================
+ echo 'pyCAPS/MSES.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/MSES.py test;
+ python -u pyCAPS/MSES.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   6434.8686749750 newton

Variables
---------
   AR                :        17.8761256208        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :        22.6429660188       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :        22.6292970435       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :        18.8664135056       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :         0.0127145406        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :         0.0126772467        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :         0.0074768775        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :         0.0017735677        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :         0.0017735677        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :         0.0017735677        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :         0.0053218277        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :         0.0052849468        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :         0.0002611265        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :         0.0056191456        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :         0.0056187325        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :         0.0054421793        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :         0.5327871651        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :         0.5309281670        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :         0.1180315549        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :         0.5327871651        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :         0.5309281670        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :         0.1180315549        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :         0.0000189749        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :     31633.5137385074       newton       Root Bending unit per unit chord                                        
   P_max             :   1155617.0255680946        watt        Maximum Engine Power                                                    
   R                 :      5000.0000033336     kilometer      Single Segment range                                                    
   Re_0              :   4714256.8311429033        [-]         Reynolds Number, segment 0                                              
   Re_1              :   4504811.2195102284        [-]         Reynolds Number, segment 1                                              
   Re_2              :  10014801.7689142171        [-]         Reynolds Number, segment 2                                              
   S                 :        28.1917813790     meter ** 2     total wing area                                                         
   T_0               :       812.1924689899       newton       Thrust, segment 0                                                       
   T_1               :       739.4274750426       newton       Thrust, segment 1                                                       
   T_2               :      2155.8460657551       newton       Thrust, segment 2                                                       
   V_0               :        70.6090282177   meter / second   Velocity, segment 0                                                     
   V_1               :        67.4719865369   meter / second   Velocity, segment 1                                                     
   V_2               :       150.0000229949   meter / second   Velocity, segment 2                                                     
   V_stall           :        37.9999993888   meter / second   stall speed                                                             
   W_0               :     34032.6295170036       newton       Weight, segment 0                                                       
   W_1               :     30966.4603184510       newton       Weight, segment 1                                                       
   W_2               :     34032.6295170036       newton       Weight, segment 2                                                       
   W_MTO             :     37401.3303577012       newton       Maximum Takeoff Weight                                                  
   W_cap             :      4175.0307826594       newton       Weight of Wing Spar Cap                                                 
   W_eng             :      2747.7840319609       newton       Engine Weight                                                           
   W_fuel_out        :      3368.6997598764       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :      3066.1689150985       newton       Weight of fuel, return                                                  
   W_pay             :      4905.0001650177       newton       Payload Weight                                                          
   W_tilde           :     22352.7841009881       newton       Dry Weight, no wing                                                     
   W_web             :       131.8074022566       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :      8613.6764251259       newton       wing weight                                                             
   W_zfw             :     30966.4602788176       newton       Zero Fuel Weight                                                        
   eta_0_0           :         0.2696090441        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :         0.2696770159        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :         0.2798306963        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :         0.9062488877        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :         0.9064773642        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :         0.9406073826        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :         0.7703115546        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :         0.7705057596        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :         0.7995162752        [-]         Propeller Efficiency, segment 2                                         
   nu                :         0.7859964418        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :         1.9000000050        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :         1.4500000078        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :         0.0042483467        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :         0.0005949059        [-]         Spar web thickness per unit chord                                       
   tau               :         0.1499765271        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :         0.0943866350        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :         0.0944151528        [-]         Breguet Range Factor, segment 1                                         

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  23 
   Termination Status     :  Converged, relative change in the objective function (5.56e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Attempted step of size 1.00e+00 at iteration 2 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    2. Attempted step of size 9.00e-01 at iteration 2 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    3. Wolfe Condition 1 failed at iteration 4 (Step 4).  Watchdog counter is 1
    4. Wolfe Condition 1 failed at iteration 7 (Step 7).  Watchdog counter is 1
    5. Wolfe Condition 1 failed at iteration 10 (Step 10).  Watchdog counter is 1
    6. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 2
    7. Attempted step of size 1.00e+00 at iteration 12 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    8. Wolfe Condition 1 failed at iteration 12 (Step 12).  Watchdog counter is 3
    9. Attempted step of size 1.00e+00 at iteration 13 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   10. Wolfe Condition 1 failed at iteration 13 (Step 13).  Watchdog counter is 4
   11. Attempted step of size 1.00e+00 at iteration 15 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   12. Wolfe Condition 1 failed at iteration 17 (Step 17).  Watchdog counter is 1
   13. Wolfe Condition 1 failed at iteration 18 (Step 18).  Watchdog counter is 2
   14. Attempted step of size 3.81e-01 at iteration 19 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   15. Wolfe Condition 1 failed at iteration 19 (Step 19).  Watchdog counter is 3
   16. Wolfe Condition 1 failed at iteration 22 (Step 22).  Watchdog counter is 1


real	3m50.554s
user	3m41.031s
sys	0m8.398s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/MSES.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/Camber.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/Camber.py test;
+ python -u pyCAPS/Camber.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   5426.1151483814 newton

Variables
---------
   AR                :       19.2162640327        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :       17.8914424476       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :       17.7697968272       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :       14.0762024635       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :        0.0110624638        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :        0.0107985659        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :        0.0066444504        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :        0.0017867958        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :        0.0017867958        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :        0.0017867958        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :        0.0052915770        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :        0.0049110860        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :        0.0002509872        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :        0.0039840922        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :        0.0041006848        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :        0.0046066672        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :        0.5506832646        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :        0.5306373281        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :        0.1199145032        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :        0.5506832646        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :        0.5306373281        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :        0.1199145032        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :        0.0000216301        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :    33586.4310550239       newton       Root Bending unit per unit chord                                        
   P_max             :  1012883.7806372986        watt        Maximum Engine Power                                                    
   R                 :     5000.0000034463     kilometer      Single Segment range                                                    
   Re_0              :  4495822.2263598200        [-]         Reynolds Number, segment 0                                              
   Re_1              :  4401584.9845399503        [-]         Reynolds Number, segment 1                                              
   Re_2              :  9626916.1443104651        [-]         Reynolds Number, segment 2                                              
   S                 :       27.9909833450     meter ** 2     total wing area                                                         
   T_0               :      689.8159590696       newton       Thrust, segment 0                                                       
   T_1               :      645.4379395215       newton       Thrust, segment 1                                                       
   T_2               :     1902.1543451014       newton       Thrust, segment 2                                                       
   V_0               :       70.0425369997   meter / second   Velocity, segment 0                                                     
   V_1               :       68.5713261573   meter / second   Velocity, segment 1                                                     
   V_2               :      150.0000046309   meter / second   Velocity, segment 2                                                     
   V_stall           :       37.9999468104   meter / second   stall speed                                                             
   W_0               :    34329.1239584747       newton       Weight, segment 0                                                       
   W_1               :    31708.3658558579       newton       Weight, segment 1                                                       
   W_2               :    34329.1239584747       newton       Weight, segment 2                                                       
   W_MTO             :    37134.8408818262       newton       Maximum Takeoff Weight                                                  
   W_cap             :     4681.6117001178       newton       Weight of Wing Spar Cap                                                 
   W_eng             :     2471.6469879882       newton       Engine Weight                                                           
   W_fuel_out        :     2805.3570136383       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :     2620.7581347431       newton       Weight of fuel, return                                                  
   W_pay             :     4905.0000233408       newton       Payload Weight                                                          
   W_tilde           :    22076.6469868519       newton       Dry Weight, no wing                                                     
   W_web             :      134.2483282176       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :     9631.7196947430       newton       wing weight                                                             
   W_zfw             :    31708.3658072022       newton       Zero Fuel Weight                                                        
   camberLocation    :        0.7949613224        [-]         location of maximum airfoil camber scaled by chord                      
   eta_0_0           :        0.2728257920        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :        0.2733261445        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :        0.2817016557        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :        0.9170614858        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :        0.9187433430        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :        0.9468963218        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :        0.7795022629        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :        0.7809318415        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :        0.8048618736        [-]         Propeller Efficiency, segment 2                                         
   maxCamber         :        0.0404380681        [-]         maximum airfoil camber scaled by chord                                  
   nu                :        0.7859963901        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :        1.9000000025        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :        1.4500000039        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :        0.0049899222        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :        0.0006416725        [-]         Spar web thickness per unit chord                                       
   tau               :        0.1486735000        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :        0.0785522626        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :        0.0794369045        [-]         Breguet Range Factor, segment 1                                         

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  76 
   Termination Status     :  Converged, relative change in the objective function (1.16e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Attempted step of size 1.00e+00 at iteration 2 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    2. Attempted step of size 1.00e+00 at iteration 3 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    3. Attempted step of size 3.00e-01 at iteration 3 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    4. Attempted step of size 9.00e-02 at iteration 3 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    5. Wolfe Condition 1 failed at iteration 4 (Step 4).  Watchdog counter is 1
    6. Attempted step of size 1.00e+00 at iteration 5 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    7. Wolfe Condition 1 failed at iteration 7 (Step 7).  Watchdog counter is 1
    8. Wolfe Condition 1 failed at iteration 8 (Step 8).  Watchdog counter is 2
    9. Wolfe Condition 1 failed at iteration 9 (Step 9).  Watchdog counter is 3
   10. Attempted step of size 1.00e+00 at iteration 10 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   11. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 1
   12. Wolfe Condition 1 failed at iteration 13 (Step 13).  Watchdog counter is 1
   13. Attempted step of size 1.00e+00 at iteration 14 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   14. Wolfe Condition 1 failed at iteration 16 (Step 16).  Watchdog counter is 1
   15. Attempted step of size 2.68e-01 at iteration 23 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   16. Attempted step of size 2.25e-01 at iteration 26 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   17. Attempted step of size 1.49e-01 at iteration 38 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   18. Wolfe Condition 1 failed at iteration 40 (Step 40).  Watchdog counter is 1
   19. Attempted step of size 1.27e-01 at iteration 45 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   20. Attempted step of size 1.21e-01 at iteration 48 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   21. Attempted step of size 9.93e-02 at iteration 61 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   22. Wolfe Condition 1 failed at iteration 75 (Step 75).  Watchdog counter is 1


real	11m11.854s
user	10m42.834s
sys	0m25.372s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/Camber.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/CMConstraint.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/CMConstraint.py test;
+ python -u pyCAPS/CMConstraint.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   6382.6426006034 newton

Variables
---------
   AR                :        17.7333703368        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :        22.5429905278       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :        22.4111491959       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :        18.7501009583       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :         0.0127173739        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :         0.0124235499        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :         0.0076171667        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :         0.0017790524        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :         0.0017790524        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :         0.0017790524        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :         0.0054317603        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :         0.0051614721        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :         0.0002635564        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :         0.0055065615        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :         0.0054830267        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :         0.0055745543        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :         0.5360678775        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :         0.5221785656        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :         0.1180981774        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :         0.5360678775        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :         0.5221785656        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :         0.1180981774        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :         0.0000187470        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :     31432.1630184581       newton       Root Bending unit per unit chord                                        
   P_max             :   1174722.0623270900        watt        Maximum Engine Power                                                    
   R                 :      5000.0000379642     kilometer      Single Segment range                                                    
   Re_0              :   4714269.7355839955        [-]         Reynolds Number, segment 0                                              
   Re_1              :   4560828.3991480591        [-]         Reynolds Number, segment 1                                              
   Re_2              :  10039944.6132115945        [-]         Reynolds Number, segment 2                                              
   S                 :        28.1055377816     meter ** 2     total wing area                                                         
   T_0               :       805.4977326683       newton       Thrust, segment 0                                                       
   T_1               :       735.5874132058       newton       Thrust, segment 1                                                       
   T_2               :      2189.5656770467       newton       Thrust, segment 2                                                       
   V_0               :        70.4293805792   meter / second   Velocity, segment 0                                                     
   V_1               :        68.1346248085   meter / second   Velocity, segment 1                                                     
   V_2               :       150.0000188498   meter / second   Velocity, segment 2                                                     
   V_stall           :        37.9999983650   meter / second   stall speed                                                             
   W_0               :     33947.7281781365       newton       Weight, segment 0                                                       
   W_1               :     30904.2652518139       newton       Weight, segment 1                                                       
   W_2               :     33947.7281781365       newton       Weight, segment 2                                                       
   W_MTO             :     37286.9111353013       newton       Maximum Takeoff Weight                                                  
   W_cap             :      4126.5009765832       newton       Weight of Wing Spar Cap                                                 
   W_eng             :      2784.1970728166       newton       Engine Weight                                                           
   W_fuel_out        :      3339.1797308950       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :      3043.4628697084       newton       Weight of fuel, return                                                  
   W_pay             :      4905.0004716166       newton       Payload Weight                                                          
   W_tilde           :     22389.1976028674       newton       Dry Weight, no wing                                                     
   W_web             :       131.0323168331       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :      8515.0668638773       newton       wing weight                                                             
   W_zfw             :     30904.2646428063       newton       Zero Fuel Weight                                                        
   camberLocation    :         0.3680356411        [-]         location of maximum airfoil camber scaled by chord                      
   eta_0_0           :         0.2696744327        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :         0.2702130567        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :         0.2795857752        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :         0.9064686815        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :         0.9082791822        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :         0.9397841182        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :         0.7704983793        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :         0.7720373049        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :         0.7988165005        [-]         Propeller Efficiency, segment 2                                         
   maxCamber         :         0.0216847844        [-]         maximum airfoil camber scaled by chord                                  
   negCMp1_0         :         1.0526444661        [-]         Negative CM about 0.25c + 1, segment 0                                  
   negCMp1_1         :         1.0529199185        [-]         Negative CM about 0.25c + 1, segment 1                                  
   negCMp1_2         :         1.0545680466        [-]         Negative CM about 0.25c + 1, segment 2                                  
   nu                :         0.7859965065        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :         1.9000000307        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :         1.4500000425        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :         0.0042012338        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :         0.0005933949        [-]         Spar web thickness per unit chord                                       
   tau               :         0.1498553099        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :         0.0938224326        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :         0.0939302493        [-]         Breguet Range Factor, segment 1                                         

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  21 
   Termination Status     :  Converged, relative change in the objective function (8.56e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Wolfe Condition 1 failed at iteration 2 (Step 2).  Watchdog counter is 1
    2. Attempted step of size 1.00e+00 at iteration 3 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    3. Wolfe Condition 1 failed at iteration 4 (Step 4).  Watchdog counter is 1
    4. Wolfe Condition 1 failed at iteration 5 (Step 5).  Watchdog counter is 2
    5. Wolfe Condition 1 failed at iteration 7 (Step 7).  Watchdog counter is 1
    6. Wolfe Condition 1 failed at iteration 9 (Step 9).  Watchdog counter is 1
    7. Wolfe Condition 1 failed at iteration 10 (Step 10).  Watchdog counter is 2
    8. Attempted step of size 1.00e+00 at iteration 11 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    9. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 3
   10. Wolfe Condition 1 failed at iteration 14 (Step 14).  Watchdog counter is 1
   11. Attempted step of size 1.00e+00 at iteration 15 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   12. Attempted step of size 3.00e-01 at iteration 15 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   13. Wolfe Condition 1 failed at iteration 15 (Step 15).  Watchdog counter is 2
   14. Wolfe Condition 1 failed at iteration 20 (Step 20).  Watchdog counter is 1


real	3m14.244s
user	3m6.660s
sys	0m7.092s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/CMConstraint.py passed (as expected)
=================================================

Traceback (most recent call last):
  File "<string>", line 1, in <module>
ModuleNotFoundError: No module named 'torch'

*************************************************
*************************************************

=================================================
Did not run examples for:

awave
autoLink
Pointwise
Fun3D
abaqus
Nastran
Mystran
Plato
Mystran
=================================================

All tests pass!


=================================================
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt
+ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ find /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
data/Plugs/plugs0a.csm
data/Plugs/plugs0b.csm
data/Plugs/plugs0c.csm
data/Plugs/plugs0d.csm
total 50752
-rw-r--r--  1 jenkins  staff   1.2M Apr 27 18:01 ASTRO.D01
-rw-r--r--  1 jenkins  staff   277K Apr 27 18:01 ASTRO.IDX
-rwxr-xr-x  1 jenkins  staff   129K Apr 27 18:03 ESPxddm
-rwxr-xr-x  1 jenkins  staff   210K Apr 27 18:03 Slugs
-rwxr-xr-x  1 jenkins  staff    85K Apr 27 18:03 TestFit
-rwxr-xr-x  1 jenkins  staff   1.8M Apr 27 18:01 avl
-rwxr-xr-x  1 jenkins  staff    34K Apr 28 10:41 cart3dTest
-rwxr-xr-x  1 jenkins  staff    34K Apr 28 10:41 egads2cart
-rwxr-xr-x  1 jenkins  staff    70K Apr 27 18:03 egads2cgt
-rwxr-xr-x  1 jenkins  staff   416K Apr 27 18:02 friction
-rwxr-xr-x  1 jenkins  staff   8.9M Apr 27 18:01 mastros.exe
-rwxr-xr-x  1 jenkins  staff   2.2M Apr 27 18:01 mses
-rwxr-xr-x  1 jenkins  staff   2.5M Apr 27 18:01 mset
-rwxr-xr-x  1 jenkins  staff    34K Apr 28 10:41 phaseUtil
-rw-r--r--  1 jenkins  staff   1.6K Apr 28 13:01 pod.egads
-rw-r--r--  1 jenkins  staff     0B Apr 28 13:01 port7681.jrnl
-rwxr-xr-x  1 jenkins  staff   1.2M Apr 27 18:01 pplot
-rwxr-xr-x  1 jenkins  staff   1.2M Apr 27 18:01 pxplot
-rwxr-xr-x  1 jenkins  staff    68K Apr 28 10:41 sensCSM
-rwxr-xr-x  1 jenkins  staff   206K Apr 27 18:03 serveCSM
-rwxr-xr-x  1 jenkins  staff   174K Apr 27 18:03 serveESP
-rwxr-xr-x  1 jenkins  staff    51K Apr 27 18:03 vCurvature
-rwxr-xr-x  1 jenkins  staff    35K Apr 27 18:03 vGeom
-rwxr-xr-x  1 jenkins  staff    52K Apr 27 18:03 vTess
-rwxr-xr-x  1 jenkins  staff   1.9M Apr 27 18:03 vTesstatic
-rw-r--r--  1 jenkins  staff   195K Apr 28 13:01 wingMultiModel.bdf
-rwxr-xr-x  1 jenkins  staff   1.8M Apr 27 18:01 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0a.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 converged, dmax= 5.416e-07,     rmsbest= 6.132e-04, reclass= 4562, unclass=    0
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 5.366e-07,     rmsbest= 7.097e-04, reclass=    2, unclass=    0
Starting pass 3 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m6.851s
user	0m6.686s
sys	0m0.393s
++ set +x
data/Plugs/plugs0a                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0b.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 converged, dmax= 3.039e-07,     rmsbest= 4.036e-02, reclass= 4562, unclass=    0
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 2.814e-07,     rmsbest= 1.924e-03, reclass= 1033, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 4.494e-07,     rmsbest= 5.920e-04, reclass=  473, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 5.366e-07,     rmsbest= 7.097e-04, reclass=   17, unclass=    0
Starting pass 5 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m6.164s
user	0m7.517s
sys	0m0.055s
++ set +x
data/Plugs/plugs0b                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0c.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 ran out of iterations,          rmsbest= 1.677e-01, reclass= 4562, unclass=  554
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 4.016e-07,     rmsbest= 6.330e-02, reclass= 1676, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 1.881e-07,     rmsbest= 8.736e-03, reclass=  791, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 3.081e-07,     rmsbest= 1.037e-03, reclass=  428, unclass=    0
Starting pass 5 (of 25) of phase2
    Pass  5 converged, dmax= 5.816e-07,     rmsbest= 7.097e-04, reclass=  109, unclass=    0
Starting pass 6 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m16.168s
user	0m24.116s
sys	0m0.112s
++ set +x
data/Plugs/plugs0c                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0d.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 ran out of iterations,          rmsbest= 1.677e-01, reclass= 4562, unclass=  554
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 4.016e-07,     rmsbest= 6.330e-02, reclass= 1676, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 1.881e-07,     rmsbest= 8.736e-03, reclass=  791, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 3.081e-07,     rmsbest= 1.037e-03, reclass=  428, unclass=    0
Starting pass 5 (of 25) of phase2
    Pass  5 converged, dmax= 5.816e-07,     rmsbest= 7.097e-04, reclass=  109, unclass=    0
Starting pass 6 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m16.114s
user	0m24.012s
sys	0m0.109s
++ 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_bPreBuilt')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_bPreBuilt/ESPVersion=beta,buildnode=macys #69'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS